Friction,
Lubrication and Wear
Edited by Mohammad Asaduzzaman Chowdhury
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Meet the editor
Mohammad Asaduzzaman Chowdhury is a professor of Mechanical Engineering at Dhaka University of Engineering and Technology (DUET), Gazipur, Bangladesh. His research interests include
engineering tribology, surface engineering, coating technology,
polymer and composite materials, metals and alloys, erosive wear
of different materials, material fabrication, characterization of
materials, self-energy-generating materials, and atomic transfer
mechanism, among others. He serves as an editorial board member for many international journals of repute and is an editor and reviewer for many indexed journals and
books. He has also published many research and review papers in refereed international journals and conference proceedings. He works as a consultant, advisor and
expert member of many government and autonomous organizations. He has 20 years’
experience as a teacher and researcher. He is involved with different cultural and
social activities, such as writing articles, stories, lyrics, and poems.
Contents
Preface
Section 1
Friction and Wear
XIII
1
Chapter 1
Abrasive Wear Performance of Fe2B Layers Applied on Steel Substrates
by Armando Irvin Martínez Pérez, Edgar Ernesto Vera Cárdenas,
Manuel Vite Torres, José Luis Bernal Ponce, Karina Alemán Ayala
and Marisa Moreno Rios
3
Chapter 2
Experimental Results of the Tribology of Aluminum in the Presence of
Polytron Additive
by Syed Mohammad Hassan Ahmer, Nusratullah Khan, S. Inayat Ali Shah
and Lal Said Jan
17
Chapter 3
Structural-Energy Interpretation of the Friction
by Sergey Fedorov
35
Chapter 4
Thin Films: Study of the Influence of the Micro-Abrasive Wear Modes on
the Volume of Wear and Coefficient of Friction
by Ronaldo Câmara Cozza
63
Chapter 5
Novel Predictors for Friction and Wear in Drivetrain Applications
by Walter Holweger
75
Chapter 6
Tribological and Wear Behavior of Metal Alloys Produced by Laser Powder
Bed Fusion (LPBF)
by Massimo Lorusso
93
Chapter 7
Tribological Characteristics of Smart Materials (Magneto-Rheological Fluids
and Elastomers) and Their Applications
by Peng Zhang, Chenglong Lian, Kwang-Hee Lee and Chul-Hee Lee
105
Section 2
Lubrication
119
Chapter 8
A Review of Surface Treatments for Sliding Bearings Used at Different
Temperature
by Jun Cao, Liang Qin, Aibing Yu, Haibo Huang, Guoping Li, Zhongwei Yin
and Huiyu Zhou
121
Chapter 9
Tribology: The Tool to Design Materials for Energy-Efficient and Durable
Products and Process
by Amaya Igartua, Raquel Bayon, Ana Aranzabe and Javier Laucirica
147
Chapter 10
High-Temperature Self-Lubricating Metal Nitride-Based Nanostructure
Composite Films
by Hongbo Ju
179
Chapter 11
Testing of the Resistance to Scuffing of Spiral Bevel Gears: Test Rig, Method,
and Results of Verification Testing
by Waldemar Tuszynski, Marek Kalbarczyk, Bartosz Kiser, Michal Michalak,
Remigiusz Michalczewski, Jerzy Mydlarz, Witold Piekoszewski, Marian Szczerek
and Jan Wulczynski
189
XII
Preface
The function of numerous electrical, electrochemical, mechanical, and biological
systems or components depends on suitable friction and wear as well as tribological
values. In this context, the study of friction, wear and lubrication is of tremendous
pragmatic importance. In recent years, the study of tribological behavior of a
component has received great attention, as the wastage of resources resulting from
friction and wear has become clearer.
This book provides the motivation for research aimed at developing a fundamental
understanding of the nature and consequences of the interaction between materials
or components on friction, lubrication and wear perspectives. This book guides the
rational design of material for technological application.
Chapter 1 “Abrasive Wear Performance of Fe2B Layers Applied on Steel Substrates’’
evaluates the resistance of dry abrasive wear in the Fe2B layer deposited on AISI D2
and 1040 steel substrates, using the powder-pack boriding process.
Chapter 2 “Experimental Results of the Tribology of Aluminum in the Presence of
Polytron Additive” discusses experimental studies on a brand-new additive called
Polytron to assess its role in the minimization of friction and wear.
Chapter 3 “Structural-Energy Interpretation of the Friction” studies the structuralenergy model of elastic-plastic deformation as the main mechanism of transformation and dissipation of energy under friction. It proposes equations of friction
energy balance, the energy interpretation of the coefficient of friction, and a
structural-energy diagram of the friction surfaces.
Chapter 4 “Thin Films: Study of the Influence of the Micro-abrasive Wear Modes
on the Volume of Wear and Coefficient of Friction” studies the influence of microabrasive wear modes on the behaviors of the volume of wear (V) and of the coefficient of friction (µ) of thin films submitted to micro-abrasive wear.
Chapter 5 “Novel Predictors for Friction and Wear in Drive Train Applications”
derives a molecular model that shows how the release and the approach of additives toward a surface is essential and related to the reaction processes that occur
during loading.
Chapter 6 “Tribological and Wear Behavior of Metal Alloys Produced by Laser
Powder Bed Fusion (LPBF)” investigates the different behavior of principal metallic
alloys by LPBF. Since LPBF is an additive manufacturing technique for the production of parts with complex geometry it is especially appropriate for structural
applications in aircraft and automotive industries.
Chapter 7 “Tribological Characteristics of Smart Materials (Magneto-Rheological
Fluids and Elastomers) and their Applications” shows the tribological characteristics of magneto-rheological fluids (MRFs) and magneto-rheological elastomers
(MREs), as smart materials have been widely studied in various engineering fields
to address vibration issues because the mechanical properties are controllable under
the strength of a magnetic field.
Chapter 8 “A Review of Surface Treatments for Sliding Bearings Used at Different
Temperature” reviews different treatment technologies to improve tribological properties and select the best treatment for different bearings used at different temperature.
This is helpful considering that boundary lubrication and dry friction of plain bearings
at different work are unable to be avoided under the start and stop conditions.
Chapter 9 “Tribology: The Tool to Design Materials for Energy-Efficient and
Durable Products and Process” describes a summary of the main tribological
achievements carried out at TEKNIKER technology centre during the last 37 years.
It covers the description of commercial and newly developed tribological test
benches and case studies for a wide variety of applications.
Chapter 10 “High-Temperature Self-lubricating Metal Nitride-Based Nanostructure
Composite Films” reviews the formation mechanism of Magnéli phases and the influence of Magnéli phases on the high-temperature tribological properties of hard transition metal nitride films synthesized using magnetron sputtering. Film technology is
one of the most efficient methods of modifying the surface properties of materials.
Chapter 11 “Testing of the Resistance to Scuffing of Spiral Bevel Gears - Test Rig,
Method and Results of Verification Testing” studies the development of a new bevel
gear test rig and scuffing test method at ITeE-PIB research institute. It investigates
the effect of various gear oils and the deposition of a low-friction coating on the
resistance to scuffing.
I am very much grateful to Dhaka University of Engineering & Technology
(DUET), Gazipur, for creating the opportunities to do this work.
I wish to give my heartfelt and sincere thanks to Md. Bengir Ahmed Shuvho,
Lecturer, National Institute of Textile Engineering and Research (NITER), Savar,
Dhaka, for his continuous technical and valuable support. I appreciate and
acknowledge his contributions in reviewing all the chapters. I immensely benefited from the help of Author Service Manager Ms. Ivana Barac and my publisher
IntechOpen. I am also grateful to the authors for their worthy contributions. I
learned a lot of ideas for editing this book from Professor Dr. Mohammed Alauddin,
Honorable Vice Chancellor of DUET, Gazipur. Hopefully this book will be used for
fundamental and applied research by students and researchers alike.
Special thanks go to my wife Anisa Akhtar, my son Ayan and my daughter Afsheen,
who were forbearing during the year I spent long days and night in conducting
research and keeping up with the literature as I prepared this book.
Mohammad Asaduzzaman Chowdhury
Dhaka University of Engineering and Technology,
Gazipur,
Bangladesh
XIV
Section 1
Friction and Wear
1
Chapter 1
Abrasive Wear Performance of
Fe2B Layers Applied on Steel
Substrates
Armando Irvin Martínez Pérez, Edgar Ernesto Vera Cárdenas,
Manuel Vite Torres, José Luis Bernal Ponce,
Karina Alemán Ayala and Marisa Moreno Rios
Abstract
The resistance of dry abrasive wear in Fe2B layer deposited on AISI D2 and
1040 steel substrates, using the powder-pack boriding process, was evaluated. The
boriding process was carried out at temperatures of 1220 and 1320 K for a time of
8 h. A Rockwell hardness tester was used to assess the Daimler-Benz adhesion test.
The abrasive wear tests were carried out in dry conditions according to the ASTM
G65 test standard. The test parameters used were a sand flow of 400 g/min, a
nominal rubber wheel constant rotation of 200 rpm, a load of 122 N, and a sliding
distance of 716.28 m. The type of abrasive used was steel round grit with a grain
size of 260 μm and a hardness of 1100 HV. The total time for each test was 30 min,
removing the specimens every 5 min to determine the amount of mass loss using an
analytical balance (sensitivity of 0.0001 g). The average value of volume loss and
wear rates is reported. Optical microscopy and SEM were carried out in order to
identify the wear mechanisms. The wear mechanisms presented in this study were
two-body abrasive wear, pitting action, and plastic deformation.
Keywords: dry abrasive wear, Fe2B layer, steel substrates, boriding, wear mechanisms
1. Introduction
Abrasive wear occurs when a hard particle slides on a surface, causing loss of
material. This type of wear depends on factors such as hardness, roughness, and
particle geometry [1–4].
Different coatings are used as anti-abrasive wear materials. Some of them are as
follows: ceramics coatings, such as, Al2O3/TiO2, SiO2/TiO2/Cr2O3, SiC, B4C, ZrO2,
CaO, CrN/AlCrN, CrN/BCN, SiO2, WC, and TiC [5, 6]; polymer coatings [7, 8]; and
DLC coatings [9, 10].
On the other hand, some works have been developed using boron coatings as
anti-wear material. Boronizing is a thermo-diffusion process in which boron atoms,
due to their small diameter and high mobility at elevated temperatures, diffuse into
a metal surface and form intermetallic compounds with atoms of base metal [11].
Abrasive wear tests were carried out using boronizing on SAE 1010, 1040, D2,
and 304 steels [12]. It was seen that boronizing improved the wear strengths
3
Friction, Lubrication and Wear
considerably. The best abrasive wear strengths were obtained in boronizing for 8 h
at 900°C for SAE 1010 and SAE 1040 steels, 4 h at 900°C for D2 steel, and 6 h at
900°C for 304 steel. In another work [13], abrasive wear resistance of boride layers
on Fe-15Cr alloy was studied. It was found that the dry abrasive wear resistance of
borided alloy samples was around 45 times greater than that of non-borided ones.
In another study [14], the micro-abrasive wear of boride layers on AISI D2 tool steel
was investigated. Some results indicated that wear resistance of the borided samples
was superior to the hardened, uncoated AISI D2 steel. According to literature [15],
wear resistance of boronized steels in abrasive wear conditions depends on the
phase composition and hardness of the layer and its stress state, but the hardness of
abrasive particles also has a significant importance on the wear speed.
The objective of this work was to evaluate the resistance of dry abrasive wear
in Fe2B layer deposited on AISI D2 and 1040 steel substrates without a previous
heat treatment (hardened and tempered) using the powder-pack boriding process. The substrate materials were selected in order to compare the wear abrasion
behavior of a plain carbon (1040) versus a high-carbon, high-chromium steel
(D2). AISI 1040 steel is frequently cold drawn to specified physical properties
for use without heat treatment for some practical applications such as cylinder
head studs. AISI D2 tool steel has desirable properties such as abrasion resistance,
high hardness, and no deforming characteristics, and is used in lamination and
stamping dies, shear blades, master tools, etc. The wear resistance of D2 tool steel
is approximately eight times that of plain carbon steels, so also was of interest
to know if this great difference in wear behavior could increase or decrease in
borided conditions.
2. Experimental work
2.1 Test specimens
The specimens had a rectangular shape with dimensions of 50 × 25 mm and
10 mm in thickness. The chemical composition of the AISI D2 and 1040 steels is
shown in Table 1 [16, 17].
The boriding process used in the specimens of AISI D2 and 1040 steel substrates
was the same as reported in a previous work [18]. The only difference is that for this
work, two boriding temperatures were employed (1220 and 1320 K).
It is important to mention that, based on the Fe-B phase diagram and the high
iron content of the AISI D2 and 1040 steels [19], in addition to the diffusion of
boron at high temperatures (1220 and 1320 K) and the treatment time of 8 h, the
formation of a Fe2B monolayer is ensured under the conditions of the boriding
process proposed in this work. Because the Fe-B phase is formed on the surface of
the sample, which generates the Fe-B/Fe interface between the Fe-B phase and the
steel, this allows the gradual formation of the Fe2B phase that grows when the thickness of the boride is increased and at the same time the Fe-B phase decreases. At the
Steel
Composition
C
Mn
Si
Cr
Mo
V
S
P
Fe
AISI D2
1.55
0.35
0.35
11.8
0.85
0.85
0.03
0.03
84.22
AISI 1040
0.38
0.6
0.1
0
0
0
0.02
0.02
98.87
Table 1.
Chemical composition of specimens (wt.%).
4
Abrasive Wear Performance of Fe2B Layers Applied on Steel Substrates
DOI: http://dx.doi.org/10.5772/intechopen.83814
Figure 1.
(a) Experimental setup and (b) schematic diagram of the apparatus.
end of the 8 h, corresponding to the treatment time, the Fe-B phase was consumed
completely, and so the only phase present (Fe2B) stops growing [20].
2.2 Test procedure
The tests were performed according to the ASTM G65 test standard [21]. Figure 1
shows the experimental rig and a simplified schematic diagram of the dry/sand rubber
wheel apparatus used in this research work [22].
The test parameters used were a sand flow of 400 g/min, a nominal rubber
wheel constant rotation of 200 rpm, a load of 122 N, and a total sliding distance
of 716.28 m, using a 228.6 mm diameter wheel rotating. The wheel consists of
a steel disk with an outer layer of neoprene rubber tire molded to its periphery
with hardness A60. As the rubber wheel reduces in diameter, the number of
wheel revolutions was adjusted to equal the sliding distance of the new wheel.
The type of abrasive used was steel round grit with a grain size of 260 μm and
a hardness of 1100 HV. The total time for each test was 30 min, removing the
specimens every 5 min to determine the amount of mass loss using an analytical balance (sensitivity of 0.0001 g). Before the overall tests were performed,
the specimens were cleaned by washing in ethanol in an ultrasonic bath
(Fisherbrand 11020).
The average value of volume loss (V), wear rates (Q ), and wear coefficients
(k) are reported. Optical microscopy and SEM were carried out on the damaged
surfaces in order to identify the wear mechanisms. Additionally, the profiles of the
wear scars are presented using a Mitutoyo Surftest Profilometer.
3. Results and discussion
3.1 Fe2B layer hardness
A load of 100 g was used to evaluate the hardness of Fe2B layers with a Vickers
indenter. The variation of the hardness, depending on the depth of layers, is shown
in Figure 2. Also, the roughness of specimens was obtained with a Mitutoyo
Surftest Profilometer, see Table 2.
5
Friction, Lubrication and Wear
Figure 2.
Variation of hardness.
Boriding temperature (K)
1220
1320
Borided steel
Vickers hardness (HV)
Roughness (Ra)
(μm)
AISI D2
1270.7
0.86
AISI 1040
964.4
1.14
AISI D2
1354.5
0.22
AISI 1040
1179.5
0.35
Table 2.
Properties of the specimens.
3.2 SEM, X-ray diffraction, and EDS
Figure 3 shows the cross-sectional view of SEM micrographs. A zigzag teeth
shape is observed in both steels. This columnar shape comes from the direction
in which diffusion is preferred, and the boride is of stronger (002) texture [23].
The presence of this typical morphology for good adhesion between coating and
substrate is necessary.
The boriding is a diffusive process highly anisotropic [24]. In Figure 3, it was
observed that the boride on the surface of AISI D2 steel presents a columnar morphology; in the case of boride formed on the surface of AISI 1040 mold steel is observed a
dense structure due to alloying elements it has. Depending on the conditions of processing time, temperature, and chemical composition of substrates, the depth obtained
of the boride layer was an interval of 10–60 μm (Figure 2). It was observed that the
depth of borides formed on AISI D2 is more homogeneous than that of AISI 1040.
The results of X-ray diffraction studies are presented in Figure 4. The XRD
analysis shows well-defined peaks at 42.67 and 45.11° confirming Fe2B phase. Also,
the presence of chromium boride (CrB) phase in the borided AISI D2 steel was
determined. This is due to the significant presence of chromium in AISI D2 steel as
an alloying element [25, 26]; apparently, during powder-pack boriding, it reacted
with boron atoms and formed a little intermediate phase of CrB.
6
Abrasive Wear Performance of Fe2B Layers Applied on Steel Substrates
DOI: http://dx.doi.org/10.5772/intechopen.83814
Figure 3.
SEM cross-sectional micrograph, and XRD of borided samples: (a) AISI D2 at 1220 K, (b) AISI 1040 at
1220 K, (c) AISI D2 at 1320 K and (d) AISI 1040 at 1320 K.
The EDS analysis obtained by SEM, for the borided steels, is shown in
Figure 5a–d. The presence of borides formed on the surfaces of the steels was
confirmed considering the presence of boron and iron.
Figure 4.
Diffraction patterns of borided specimens: (a) AISI 1040 at 1220 K, (b) AISI 1040 at 1320 K, (c) AISI D2 at
1220 K, and (d) AISI D2 at 1320 K.
7
Friction, Lubrication and Wear
Figure 5.
EDS spectrum of borided samples. (a) AISI D2 at 1220 K, (b) AISI 1040 at 1220 K, (c) AISI D2 at 1320 K, and
(d) AISI 1040 at 1320 K.
3.3 Fe2B layer adhesion test
A Cientec Rockwell hardness tester model 200HR-150 was used to assess the
Daimler-Benz adhesion tests [27]. Figure 6 shows the indentations on the surfaces.
For the AISI D2 steel, some small cracks and no visible delamination are observed
(Figure 6a and c), and the adhesion strength quality is related to HF1 map [28]. In
the case of AISI 1040 steel (Figure 6b and d), microcracks and small delamination
are observed, and the adhesion category belongs to the HF4 level.
3.4 Wear profile
The abrasion tests carried out caused wear damage on surfaces. The wear profiles
were measured using a Mitutoyo Surftest profilometer and are shown in Figure 7. The
results are compatible with the volume loss (Figure 8), where 1040 steel borided at
1220 K has the greatest wear volume and the D2 steels at 1320 K had the minor wear.
3.5 Volume loss
The volume loss was obtained for all the borided and unborided steel substrates.
These data were calculated using Eq. (1). The mass loss was obtained weighing the
specimens before and after the test. The graph of the Figure 8 shows that the AISI
D2 steel borided at 1320 K exhibited a higher wear resistance compared to the other
specimens. The results also show the great difference in volume loss between borided
and unborided steels. The reason that the D2 steel had a greater wear resistance is
due most likely to the mechanical properties conferred by a high content of C and
Cr, which is higher than in the 1040 steel (see Table 1). According to Figure 8, the
abrasion wear resistance of borided D2 tool steel is approximately 16 times greater
than borided 1040 plain carbon steel. This could justify the use of this tool steel for
abrasion wear applications when it is borided to the conditions used in this work,
8
Abrasive Wear Performance of Fe2B Layers Applied on Steel Substrates
DOI: http://dx.doi.org/10.5772/intechopen.83814
Figure 6.
Indentations on surfaces. (a) AISI D2 borided at 1220 K, (b) AISI 1040 borided at 1220 K, (c) AISI D2
borided at 1320 K, and (d) AISI 1040 borided at 1320 K.
without a previous heat treatment, as usual. These results also indicate that its
core strength was not affected due to high temperatures of powder-pack boriding
treatment.
Volume loss (mm3) = (Mass loss (g) / density (g / cm3)) × 1000
(1)
3.6 Wear rates (Q ) and wear coefficients (k)
The wear rates were obtained from Eq. (2).
Q = V / d.
(2)
where Q = wear rate (mm3/m), V = volume loss (mm3), and d = sliding
distance (m).
Figure 9 shows the wear rates obtained every 716 m of the borided and
unborided D2 and 1040 steels. AISI D2 borided steels at 1320 and 1220 K had the
best performance against the dry abrasive wear conditions. It was due to its good
mechanical properties and chemical composition. Additionally, the adhesion tests
on this steel showed an excellent performance. On the other hand, the 1040 steel
borided at 1320 K had a good behavior, almost similar to the D2 steel. For the AISI
1040 steels borided at 1220 K, an abnormal value was observed at a sliding distance
of 716 m, where the wear rate had a great increase. This performance was mainly
due to the running in period of the test.
9
Friction, Lubrication and Wear
Figure 7.
Roughness profiles of wear scars.
Figure 8.
Volume loss of borided and unborided steels.
3.7 Wear mechanisms
Figure 10a–f shows the wear on the surface of the unborided and borided
specimens. In both steels, as expected, the wear damage was more severe on the
unborided specimens (Figure 10a and b). In the case of the borided steels, AISI
1040 at 1220 K (Figure 10c) showed the greater damage and the AISI D2 borided
at 1320 K (Figure 10d) showed the lower damage. This was in accordance to the
results of the wear profiles showed in Figure 7 and wear rates showed in Figure 9.
In the case of borided steels, the main wear mechanism observed in the wear scars
was the two-body abrasive wear due to the presence of parallel lines to the sliding
direction. These parallel lines were produced by wear debris acting as indenters
causing, in some cases, depth grooves.
Figure 11a–d shows the SEM micrographs of the wear damage of the borided
steels. In the case of AISI 1040 steel borided at 1220 K (Figure 11a), wear debris was
observed, which was derived from the three-body abrasion situation, where hard
particles were trapped between the two sliding surfaces. Also, severe pitting action
was observed, caused by the particles of material and abrasive particles. Finally,
10
Abrasive Wear Performance of Fe2B Layers Applied on Steel Substrates
DOI: http://dx.doi.org/10.5772/intechopen.83814
Figure 9.
Wear rate of borided and unborided steels.
Figure 10.
(a) 1040 steel substrate, (b) D2 steel substrate (c) 1040 borided—1220 K, (d) D2 borided—1220 K, (e) 1040
borided—1320 K, and ( f) D2 borided—1320 K.
Figure 11.
SEM micrographs of wear scars. (a) AISI 1040 at 1220 K, (b) AISI D2 at 1220 K, (c) AISI 1040 at 1320 K, and
(d) AISI D2 at 1320 K.
11
Friction, Lubrication and Wear
plastic deformation occurred due mainly to the sliding action. Figure 11b (AISI
D2 steel at 1220 K) shows a typical effect of abrasive wear, where sharp asperities
plowed the surface, causing permanent deformation. This plowing action produced
a groove in the softer material. Also, parallel lines were observed caused by wear
debris probably inlaid in the rubber wheel. In the case of AISI 1040 steel borided
at 1320 K (Figure 11c), severe micropitting action and plastic deformation were
observed. Finally, in the case of the AISI D2 steel at 1320 K, wear debris and pitting
action were observed, but to a lesser degree. This matches with the results of wear
rates obtained and indicated in Figure 9.
4. Conclusions
1. The formation of a Fe2B monolayer is ensured under the conditions of the
process of boron powder-pack proposed in this work. The Fe-B phase is formed
on the surface of the sample, which generated the Fe-B/Fe interface between
the Fe-B phase and the steel, which allowed the gradual formation of the Fe2B
phase that grows when the thickness of the boride is increased and at the same
time the Fe-B phase decreases.
2. The Rockwell-C adhesion tests showed that for the AISI D2 steel, the adhesion
strength quality, of Fe2B layers, is related to HF1 map, showing some small
microcraks and the AISI 1040 steel fits to HF4 category, where microcracks
and some delamination was observed.
3. AISI D2 steel specimens borided at 1320 K showed a higher wear resistance, in
accordance to the wear rates and wear coefficients results. It was due to its good
mechanical properties and chemical composition. Additionally, the adhesion
tests on this steel showed an excellent performance.
4. The wear mechanisms presented in this study were as follows: two-body
abrasive wear, which was due to the presence of parallel lines to the sliding
direction; pitting action, which was caused by the particles of the material and
abrasive particles; and plastic deformation, which occurred due mainly to the
sliding action.
12
Abrasive Wear Performance of Fe2B Layers Applied on Steel Substrates
DOI: http://dx.doi.org/10.5772/intechopen.83814
Author details
Armando Irvin Martínez Pérez1, Edgar Ernesto Vera Cárdenas2*,
Manuel Vite Torres3, José Luis Bernal Ponce4, Karina Alemán Ayala5
and Marisa Moreno Rios2
1 Polytechnic University of Pachuca, Zempoala, Hidalgo, Mexico
2 National Technology of Mexico/Technological Institute of Pachuca,
Pachuca, Hidalgo, Mexico
3 National Polytechnic Institute, ESIME Zacatenco, Mexico City, Mexico
4 National Technology of Mexico/Technological Institute of Orizaba,
Orizaba, Veracruz, Mexico
5 Autonomous University of the State of Hidalgo, Mineral de la Reforma, Hidalgo,
Mexico
*Address all correspondence to:
[email protected]
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
13
Friction, Lubrication and Wear
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[19] Repovský P, Homolová V, Čiripová
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Experimental study and
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[20] Yu LG, Chen XJ, Khor KA,
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15
[28] Verein Deutscher Ingenieure
Normen VDI 3198. Düsseldorf: VDIVerlag (Coating (CVD, PVD) of cold
forging tools); 1991. pp. 1-8
Chapter 2
Experimental Results of the
Tribology of Aluminum in the
Presence of Polytron Additive
Syed Mohammad Hassan Ahmer, Nusratullah Khan,
S. Inayat Ali Shah and Lal Said Jan
Abstract
Friction is an ever-present obstacle that causes energy loss in mechanical parts.
To alleviate this nuisance, we carried out experimental studies on a brand new
additive called Polytron to assess its role in the minimization of friction and wear.
The wear, the volume wear rate, the wear coefficient, and the coefficient of friction
of the aluminum surface were measured at room temperature with pin-on-disk
tribometer without and with 10% Polytron in Helix oil. In the base oil Helix, their
values were found to be 70 μm, 1.28 × 10 −3 mm3 / min, 1.27 × 10 −10 m2 / N, and 0.012,
respectively, which with the incorporation of Polytron additive in the
Helix oil
2
m , and 0.004. The
correspondingly reduced to 20μm, 6.08 × 10 −5 mm3 / min, 4.22 × 10 −11 ___
N
experimental verdict points to an ionic character of the additive in that it impregnates the crystal structure of the metal, thereby prompting a hard surface layer
which subsequently curtails wear and friction.
Keywords: friction, wear rate, polytron additive, aluminum metal,
lubrication, helix oil
1. Introduction
Whenever and wherever two surfaces and/or two parts move against each other
in the form of translation, rotation, or oscillation, an opposition is encountered. This
opposing or resistive force to motion is described as friction. In fact, friction is an
ever-present irritant and is the real source of energy and power losses in every industry and every activity whatsoever. This can be realized in our everyday life and the
different industries like automotive, aerospace, agriculture, marine, electronics, and
telecommunication, and even the so-called cosmetics industry, and the movements
of the human joints are not exempt from this scourge one way or another. The word
friction derives from the Latin verb fricare, which means to rub. It is of interest to
know that the word tribology, introduced in 1966 by the Jost Report, derives from the
Greek word τριβοσ (tribos), which also means rubbing. As indicated by this report,
tribology was defined as the science and technology of interacting surfaces in relative
motion. Nevertheless, a better definition of tribology might be the science and technology of lubrication, friction, and wear of moving or stationary parts [1, 2]. Even
if the term tribology is difficult for the general public to comprehend, the dawn of
computer disk drives, micro-devices, and nanotechnology has driven friction science
17
Friction, Lubrication and Wear
and tribology to the front position. Now, the designers have to deal with the challenge
of controlling friction of interacting surfaces in relative motion at sizes far too small
for the naked eye to see. This is the nano-mechanical device and nano-tribological
regime where the ultimate source of friction is perceived to be van der Waals force
and Coulomb force [3–7]. In addition to friction, an associated observable fact with
the protracted mechanical motion or rubbing of the mating surfaces is the wreckage
of the surfaces and generation of heat and pressure in the surrounding area which will
definitely curtail the useful life of the mechanical parts. This scoring of the coupling
surfaces is termed as wear. The critical issue is to minimize the amount of wear and
friction being produced in any mechanical operation so as to avoid any possible
mechanical malfunction. It is hard to stop wear of the surfaces and generation of heat
and pressure; but there are different ways to minimize the effects, and one of them is
lubrication [7]. A lubricant is any substance that is interposed between two surfaces
in relative motion for the purpose of reducing the friction and wear between them.
By and large, lubricants can be solids, liquids, or gases; but in any case, they reduce
the negative influence in the moving parts. Other than friction reduction, lubricants
carry away heat and wear particles as well and can serve as the means to distribute
corrosion inhibitors and biocides. Lubricating films should support the pressure
between opposing surfaces, separate them, and reduce the sliding or rolling resistance
in the interface. To reduce friction, the liquid lubricants are formulated in such a way
that chemical species within it react with the surface of the bodies to form lubricative
films. This chemical species is named as additive. The function of the additive is to
provide a smooth surface plus reduce the amount of wear; that is, they are expected
to have antifriction and antiwear properties. For example, calcium sulfonate causes
the formation of protective layers on highly loaded surfaces. Phosphorus can react
with frictional hot spots on ferrous surfaces and thus can reduce wear and friction.
Friction modifiers and antiwear additives to oils are the focus of extensive research in
oil companies. The amount of the above-mentioned components and their nano-sized
counterparts can vary, depending upon the application, in the range of 1–20 wt%
[7–15]. By the same token, it has been noticed that the variation of friction and wear
rate depends on various interfacial conditions. There are a number of studies in the
literature which report that wear and friction primarily change with load, speed,
and/or temperature [16–22], surface roughness [23, 24], type of material or mating
component, and other environmental dynamics [25–30]. Yet, a group of researchers
argue that friction and wear rate vary with geometry, relative surface motion, surface
roughness of the rubbing surfaces, type of the material, system rigidity, stick-slip,
lubrication, and vibration and/or type of additive, which means that wear and friction
are functions of the specific tribosystem [31–52]. Even then, in many applications,
the wear reduction mechanism and quantitative analysis of the additives are not well
known and a thorough exploration is still inevitable. A literature survey reveals that
there is a peculiar and unexplored additive with the brand name of Polytron which
has not been thoroughly investigated by the tribological community. Accordingly, this
chapter has been devoted to an academic research on the Polytron additive. Polytron
is an oily fluid mixture of petroleum-based chemicals mixed with oxidation inhibitors
and detergent chemicals and behaves exactly like a stable grease at ambient pressure
and temperature in stark contrast to the conventional lubricants. Polytron additive is
petroleum based and thus contains no solid particles; hence, it is compatible with all
the lubricants available in the market whether mineral, synthetic, vegetable, or animal. Polytron comprises 80% para and 20% meta polytron. In this chapter, we will focus
on the metal treatment concentrate (MTC) trademark of polytron having an inherent
ionic/polar nature due to which it is attracted to metallic surfaces and develops a
durable polished-like microscopic layer through metallurgical process that can resist
wear, extreme pressure, and excessive temperature.
18
Experimental Results of the Tribology of Aluminum in the Presence of Polytron Additive
DOI: http://dx.doi.org/10.5772/intechopen.84620
2. Experimental details
2.1 Tribometer machine
Wear tests were conducted on pin-on-disk tribotester (Ducom TR-20LE) wear
testing machine. Figure 1 gives a schematic sketch of the pin and disk while Figure 2
displays the actual tribometer device.
In Figure 1, F N stands for the normal force that is the load on the aluminum
pin whereas F R represents the resistive force called friction that arises from the
sliding contact of the aluminum pin on the steel disk. In Figure 2, the pin is firmly
attached to the pin support and then linked to the rotating plain disk with the
desired load which is usually applied through a pulley system. Lubricant is pumped
continuously from the machine. To simplify the contact geometry, a hemispherical
pin is used which directly touches the disk surface at the beginning of the experiment. A hygrometer measures the relative humidity of the air in the chamber
whereas the rpm of the rotating shaft that supports the disk is measured with
the help of tachometer. The variation of friction coefficient with friction time is
recorded automatically. Necessary information regarding stainless steel disk and
aluminum pin is presented in Tables 1–3. The aluminum pin is in fact an alloy of
aluminum and silicon. In addition, the data sheets for the Helix oil and Polytron
additive are given in Tables 4 and 5. The data and basic information with reference
Figure 1.
Sketch of the pin-on-disk. The dimensions of the pin were 32 mm (l) × 10 mm(dia) and dimensions of the disk
were 8 mm (l) × 163 mm (dia).
Figure 2.
Pin-on-disk tribotester machine.
19
Friction, Lubrication and Wear
Component
Specification/weight percent
165 nm (diameter) × 8 mm (height)
Disk dimensions
Counter bore
M5 holes from bottom × 4 nos.
Counter bore
M5 holes from top × 4 nos.
Holes
M4 tapped holes × 2 nos.
Chemical composition (weight percent)
Carbon (C)
≤ 0.08%
Silicon (Si)
≤ 1.00%
Manganese (Mn)
≤ 2%
Phosphorous (P)
≤ 0.045%
Sulfur (S)
≤ 0.30%
Nickel (Ni)
≤ 8 –10.5%
Chromium (Cr)
≤ 18.00–20.00%
Table 1.
Specification and composition of stainless steel disk (SUS304) [53–55].
Composition
Min (weight percent)
Max (weight percent)
0.4%
0.8%
—
0.7%
0.15%
0.15%
Manganese
—
0.15%
Magnesium
0.8%
1.2%
Chromium
0.04%
0.35%
Zinc
—
0.25%
Titanium
—
0.15%
95.85%
98.56%
Silicon
Iron
Copper
Aluminum
Table 2.
Chemical composition of aluminum pin (A390) [53–55].
Property
Alloy
Aluminum pin A390
3
8000 kg/m3
Density
2.72 g/cm
Hardness
112.65 VHN
88 HB
250.00
520 MPa
Yield strength
—
240 MPa
Young’s modulus
—
190 GPa
Poisson ratio
—
0.27–0.30
Tensile strength
Table 3.
Mechanical properties of the aluminum pin and steel disc [53–55].
20
Steel disk SUS304
Experimental Results of the Tribology of Aluminum in the Presence of Polytron Additive
DOI: http://dx.doi.org/10.5772/intechopen.84620
Property
Method
SAE viscosity grade
Shell Helix Ultra
5W–40
Kinematic viscosity
°
@40 C cSt
°
@100 C cSt
Viscosity index
IP 71
81.1
IP 71
14.5
IP 226
187
IP 365
0.856
Flash point PMCC ( C )
IP 34
206
Pour point ( C)
IP 15
–39
°
Density @15 C (kg/L)
°
°
HTHS viscosity @ 150°C (mPa s)
3.68
Table 4.
Typical physical properties of Shell Helix Ultra oil (5W–40) [53–55].
Physical/chemical property
Remarks
State
Liquid
Color
Yellowish clear
Smell
Odorless
Specific gravity
60/60 ≈ 1.00
Boiling point range
>300°C
Flash point
>200°C
°
Viscosity @100 F
SUS 391
°
Viscosity @210 F
SUS 61
Water solubility (T = 20 C)
Low
Evaporation point
Higher than ether (>34.6°C)
°
Table 5.
Data sheet of Polytron [53–55].
to aluminum metal, steel disk, Helix oil, and polytron are taken from the research
work of Ahmer et al. [53], John [54], and Ahmer et al. [55]. One can guess from
Table 5 that Polytron is marketed in a liquid state and is yellowish in color and,
unlike other solid additives, it is odorless. Its flash point is beyond 200 ° C whereas its
boiling point is further than 300 ° C and it is scarcely soluble in water.
2.2 Materials and chemicals
The experimental work was performed in the Tribology Laboratory of
Universiti Kebangsaan Malaysia, UKM,at ambient temperature (300 K) and pressure (760 mmHG) and approximately 70% relative humidity. Helix oil was chosen
as representative base oil for the experiment and its brand 5W–40 was supplied by
Shell Oils. The additive was Polytron MTC which was supplied by the Malaysian
Association of Productivity. We used soft aluminum-silicon alloy A390 and stainless steel SUS304 as pin and disk material, respectively. Separate test runs were
taken for the base oil stock and the 10% polytron additive plus the base oil stock.
The runs were executed for 240 min in each case and the wear rates of the pin were
then calculated from the measured weight loss. The mass and volume of the pin
21
Friction, Lubrication and Wear
Test variable
Assessed value
Before the wear run
Material of the wear disk
Diameter of the wear disk
Mass of the pin
Length of the pin
Stainless steel S304
80 mm
6.4480 g
32.00 mm
During the wear run
Speed of the wear disk
Time allocated
Sliding speed
Sliding distance
500 rpm
240 min≈ 14,400 s
2.09 m/s
30.163 km ≈ 30,163.2 m
After the wear run
Mass of the pin
Length of the Pin
6.4470 g
31.981 mm
Table 6.
Recorded data of the wear test for helix base oil (5W–40).
Test variable
Assessed value
Before the wear run
Quantity of Helix plus Polytron
Load
Material of the pin
2000 mL
196.2 N
Al▬Si alloy A390
Pin diameter
10.00 mm
Length of the pin
32.00 mm
Material of the wear disk
Stainless steel SUS 304
Diameter of the wear disk
80 mm
During the wear run
Speed of the wear disk
Time allocated
Sliding speed
Sliding distance
500 rpm
240 min≈ 14,400 s
2.09 m/s
30.163 km ≈ 30163.2 m
After the wear run
Mass of the pin
Length of the pin
6.4472 g
31.996 mm
Table 7.
Recorded data of the wear test for the Helix oil plus 10% polytron.
were measured both before and after running the experiment and the data set are
presented in Tables 6 and 7.
2.3 Procedure and calculations
In the experiment, an aluminum pin having a diameter of 10 mm was slid
against the steel disk. The applied load was 20.0 kg. In the first instance, 100%
22
Experimental Results of the Tribology of Aluminum in the Presence of Polytron Additive
DOI: http://dx.doi.org/10.5772/intechopen.84620
Helix oil was used and its volume in the graduated cylinder was 2000 mL. In the
second instance, 90% Helix oil having a volume of 1800 mL was mixed with 10%
polytron additive which amounted to 200 mL volume of polytron. Before running
the test, the disk was completely covered with the lubricant by keeping a steady
flow rate of the lubricant at nearly 0.5 mL/min. The wear volume was calculated
from the diameter of the wear scar generated by the pin. Typical wear versus time
curves were obtained with the help of MatLab software and were polynomially
fitted in order to decide the data trend.
Wear process is in general quantified by the wear rate. Wear rate is defined as
the volume or mass of material removed per unit time or per unit sliding distance.
In order to determine the extraordinary contribution of the polytron additive in
the helix lubricant, we calculated three key tribological parameters, namely, mass
wear rate, volume wear rate, and wear coefficient. The defining equations for these
parameters are specified by Eqs. (1–3) as written down below [56].
Mass wear rate = m / t
(1)
Volume wear rate = V / t
(2)
Wear coefficient (k) = (V × H) / (N × S)
(3)
Eq. (3) is the famous Archard equation of tribology.
The coefficient of friction μ is obtainable from the experimentally obtained data.
The popular defining expression for the coefficient of friction is like that described
by Eq. (4).
μ = FR/N
(4)
In the above equations, the variable m stands for the worn out mass of the aluminum pin, t represents the time span of the experimental run, V refers to the worn
out volume of the pin called the wear volume, H points to the hardness of the sliding
pin, F R is the tangential resistive force between the pin and the disk and is termed as
friction force, N is the normal load, and S is the sliding distance on the disk. It is to
be noted that the friction coefficient μ is a convenient way to characterize the resistance to relative motion between the surfaces, but it is not a material property nor
is it a physical constant. The effect of the polytron additive on different tribological
parameters in the experiment and the computed values from the above-mentioned
equations are recorded in Table 8.
Parameter
Wear
Mass wear rate
Volume wear rate
Coefficient of friction
Wear coefficient (k)
Total mass loss
Total volume loss
Helix base oil (100%)
Helix oil (90%) plus Polytron (10%)
70 μm
20 μm
−3
3.33 × 10 mg/min
8.33 × 10 −4 mg/min
−3
1.28 × 10 mm /min
6.08 × 10 −5 mm3/min
0.012
0.004
—
4.22 × 10 −11 m2/N
3
0.7992 mg
0.1992 mg
0.3079 mm3
0.01459 mm3
Table 8.
Computed tribological parameters for the aluminum pin.
23
Friction, Lubrication and Wear
3. Results and discussion
The experimentally obtained data and their polynomial fits for the wear behavior of the aluminum metallic pin are displayed in Figures 3 and 4 for two different
configurations in which the experiment was carried out. The adopted test configurations in the experiment were: aluminum pin versus Helix oil-on-steel disk, tagged
as AHS configuration, and aluminum pin versus 10% polytron plus 90% Helix
oil-on-steel disk, which will be referred to as the APS configuration in the forthcoming discussion.
Figures 3 and 4 show the plot of the wear pattern of the aluminum pin with the
passage of time and then the sliding distance on the steel disk of the experiment
under consideration. The red line represents wear in the AHS configuration whereas
the blue line symbolizes the wear in the APS configuration. It is very much clear
from this plot that the polytron additive provides excellent let-up the wear of the
tribosystem consisting of an aluminum pin on a steel disk interposed by an oil film
of 10% Polytron and 90% Helix. It shows that that the wear in the AHS configuration
starts from 70 micron and then stabilizes at approximately 65 micron, but in the APS
Figure 3.
Graph of the wear of aluminum pin against time in the AHS and APS configurations. The time for the
experiment was 240 min.
Figure 4.
Graph of the wear of aluminum vs. sliding distance in the AHS and APS configuration. The sliding distance for
the experiment was 30.163 km.
24
Experimental Results of the Tribology of Aluminum in the Presence of Polytron Additive
DOI: http://dx.doi.org/10.5772/intechopen.84620
Figure 5.
Evolution of the COF with time in AHS and APS configuration. The experimental time was 240 min.
Figure 6.
Evolution of COF with sliding distance in the AHS and APS configuration. The sliding distance for the
experiment was 30.161 km.
configuration wear stays at nearly 20 micron. Then, for the same two configurations
and under the same experimental conditions, the evolution of the coefficient of
friction μ with reference to time span and sliding distance has been plotted as shown
in Figures 5 and 6.
It is perceivable from the graph of Figures 5 and 6 that in the AHS format, the
initial value of the friction coefficient is almost zero and increases almost linearly
to a value of 0.012 in a time span of 100 min of rubbing after which COF stands
stable at this very value. The low value of μ in the initial stage of rubbing is probably due to the presence of a layer of foreign material on the disk surface which
may be due to some moisture or oxide of the aluminum metal because it readily
oxidizes in air. Conversely, in the APS setup, the coefficient of friction starts from
a value of 0.005 and then further declines to virtually 0.004. It is recognizable that
polytron reduces the wear of the aluminum pin significantly and one can predict
that the ratio in the
APS configuration is effectively more than 30% in comparison with AHS configuration. Despite the fact that in our experiment the normal force and sliding distance had very large values in difference with other experimenters, nevertheless
the evolved coefficient of friction had negligibly small value when meager 10%
polytron was added to 90% helix which in turn endorsed the positive contribution of the polytron in friction minimization. These findings in our tribological
25
Friction, Lubrication and Wear
Figure 7.
Graph of the mass loss of aluminum pin vs. time for the AHS and APS configuration. The time of the
experiment was 240 min.
Figure 8.
Experimental graph of the mass loss of aluminum pin vs. sliding distance in the AHS and APS configuration.
Sliding distance for the experiment was 30.161 km.
Figure 9.
Graph of the volume loss of aluminum pin vs. time in the AHS and APS configuration. Time for the experiment
was 240 min.
experiment with polytron additive in Helix oil are significantly superior in comparison with the findings of other researchers like Nuruzzaman and Chowdhury
[57], Bhushan and Kulkarni [58], and Le and Lin [59].
To further clarify the effect of polytron additive, we examined the mass and
volume losses of the aluminum pin with regard to time as well as sliding distance
and separate graphs were drawn for both the AHS and APS configurations. The
comparison plots for the mass losses are shown in Figures 7 and 8 while the comparison graphs for the volume losses are illustrated in Figures 9 and 10. A deep
examination of all the figures reveals that the mass as well as volume loss cannot
be controlled with Helix oil alone; rather, it will damage the contact surfaces in a
26
Experimental Results of the Tribology of Aluminum in the Presence of Polytron Additive
DOI: http://dx.doi.org/10.5772/intechopen.84620
Figure 10.
Graph of the volume loss of aluminum vs. time in the AHS and APS configuration. The sliding distance for the
experiment was 30.161 km.
short while, whereas only a scanty addition of 10% of Polytron reduces the mass
as well as the volume losses to almost zero level. This is a tremendous change
and is visible to the naked eye and directly identifies the supreme antifriction
and antiwear capability of the polytron additive. This observation with the
addition of polytron additive is fairly divergent with the high wear rate results
of researchers like Suarez et al. [60] who studied the popular ZDDP additive in
mineral oil stock.
In the same vein, the tribological parameters in our research work are much
better than those of Anand et al. [61] who used phosphonium ionic liquid additives in diesel engine lubricants. More to the point, the experimental predictions in
our research effort on wear and friction minimization are even far superior to the
findings of Chen et al. [62] and Su et al. [63] who used nano-additives in different
lubricating media. With an advantage, the calculated values of mass and volume
losses of the aluminum pin show that polytron additive attenuates the mass wear
rate by an order of magnitude while the volume wear rate of aluminum is alleviated
by two orders of magnitude and these outcomes in sequence yield just a nominal
value for the wear coefficient as can be noticed from Table 8. This outstanding performance identifies that polytron had the capability of permeation into the metal
crystal structure of aluminum and subsequent adherence to the metallic surface
as an unbreakable surface film that diminished the wear of aluminum surface and
consequently curtailed friction between the rubbing surfaces of aluminum and
steel.
4. Conclusions
1. The wear of the aluminum metal surface in the Helix base oil was circa 70 μm.
The addition of 10% of Polytron additive declined the wear to 20 μm, representing an excess of 2/3 decrement in the wear of the metal.
2. The mass wear rate of the aluminum pin in the Helix base oil was 3.3×10−3 mg/min
which decreased by an order of magnitude in the Helix plus Polytron mixture,
attaining a value of 8.33×10−4 mg/min.
3. The mass wear rate of the aluminum pin in the Helix base oil was
1.28 × 10−3 mm3/min and it decreased by two orders of magnitude in the Helix
plus Polytron mixture by assuming a value 6.08 × 10−5 mm3/min.
27
Friction, Lubrication and Wear
4. The value of the coefficient of friction in the Helix oil was estimated at 0.012
which trimmed down to an extremely low value of 0.004 in the combination
of 10% polytron additive and 90% Helix oil.
5. Polytron, due to its polar nature, proves to be an effective antiwear additive
in the Helix base oil and hence can intrinsically reduce friction by orders of
magnitude in mechanical processes and consequently prolong the life span of
mechanical parts and, in turn, contribute to considerable fuel and oil economy.
Acknowledgements
The authors are obliged to the management of Universiti Kebangsaan Malaysia for
providing laboratory facilities and are especially thankful to the cooperative technical staff of the tribology laboratory. S. M. H. Ahmer and L. S. Jan pay special thanks
to Dr. Mohamed Ahmed Siddig of Al-Neelain University, Sudan, and Dr. Siti Fazlili
Abdullah of Universiti Tenaga Nasional, Malaysia, for their valuable suggestions.
Conflict of interest
The authors declare that there is no conflict of interest regarding the publication
of this paper.
Nomenclature
MTC
FN
FR
TCP
ZDDP
μ
28
metal treatment concentrate
normal force/(load)
resistive force/friction
tricresylphosphate
zinc dialkyl-diethylthiophosphate
coefficient of friction (COF)
Experimental Results of the Tribology of Aluminum in the Presence of Polytron Additive
DOI: http://dx.doi.org/10.5772/intechopen.84620
Author details
Syed Mohammad Hassan Ahmer1, Nusratullah Khan2, S. Inayat Ali Shah3
and Lal Said Jan4*
1 Department of Physics, Yanbu University College, Yanbu al Sinaiyah, KSA
2 Department of Computer Science, Yanbu University College, Yanbu al Sinaiyah,
KSA
3 Islamia College University, Peshawar, Khyber Pakhtunkhwa, Pakistan
4 Department of Physics, Government Postgraduate College, Timergara, Khyber
Pakhtunkhwa, Pakistan
*Address all correspondence to:
[email protected]
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
29
Friction, Lubrication and Wear
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34
Chapter 3
Structural-Energy Interpretation
of the Friction
Sergey Fedorov
Abstract
The structural-energy model of elastic-plastic deformation is considered as the
main mechanism of transformation and dissipation of energy under friction. The
equations of friction energy balance are proposed. The energy interpretation of the
coefficient of friction is given. A structural-energy diagram of the friction surfaces
is proposed. The energy regularities of evolution of tribological contact (elementary
tribosystem) are discussed. The idea of the smallest structural element of dissipative
friction structures (mechanical (nano) quantum) is discussed. Mechanical quantum
is dynamic oscillator of dissipative friction structure. The nano-quantum model of
the surfaces damping is proposed. Calculations for some Hertzian heavily loaded
contacts of real tribosystems are proposed.
Keywords: energy balance, contact evolution, adaptation, dissipation,
nanostructure, wear standard
1. Introduction
Modern tribology considers elastic-plastic deformation of friction surfaces as the
main mechanism of transformation and dissipation of energy during friction.
The modern view of plastic deformation offers ergodynamics of deformable
solids [1–3]. Ergodynamics of deformable solids is a synthesis to the problem of
deformation most general laws of thermodynamics for non-reversable processes,
molecular kinetics and dislocation theory in their mutual, dialectical tie on the
basis of a most general law of nature—the law of energy conservation at its
transformations.
The macroscopic phenomenon of plastic deformation, damage and destruction
of a solid element is considered as a set of a huge number of microscopic elementary
acts of atomic-molecular rearrangements, causing the generation (reproduction) by
sources, movement, interaction and destruction of various kinds of elementary
defects on the drains. Each defect is a carrier of excess potential energy and on its
formation is spent strictly defined work of external forces.
From the thermodynamic point of view, the whole variety of mechanisms and
structural levels of plastic flow can be divided into two most characteristic groups—
adaptive and dissipative types. The first group should include the mechanism of
nucleation and accumulation in the local volumes of various kinds of elementary
defects and damages of the structure. The second group includes elementary acts of
atomic-molecular rearrangements associated with the movement and destruction of
various defects on the drains, that is, controlling the dynamic return.
35
Friction, Lubrication and Wear
Such structural-energy interpretation of plastic deformation (friction of contact
volumes) determines kinetic and competitive regularities of the process [1–3].
If you apply the basic concepts of plastic deformation of solids this theory for the
analysis of the process of friction, it is possible to consider the method of triboergodynamics [4].
The major distinction of triboergodynamics from general ergodynamics of
deformed solids is “scale factor” which exhibits itself in existence of critical friction
volume. This volume determines the limit friction parameters and separate, in
essence, the surface deformation from the traditional volume deformation.
In the most general case the triboergodynamics should be seen as structuralenergy interpretation of the friction process. In the framework of triboergodynamics the process of friction is considered as an evolutionary phenomenon of
the contact friction (rubbing surfaces).
2. Short fundamentals of ergodynamic of deformed solids
2.1 Structural model of the material
The deformable body is considered as an open, multicomponent, essentially
inhomogeneous and nonequilibrium system, representing a hierarchy of statistically
uniformly distributed over the volume of metastable structural elements (defects
and damages) of various (from macro- to micro-) levels. Some of these structural
elements are virtual sources and sinks of elementary defects (vacancies, dislocations, etc.), others—obstacles to their movement.
The main parameters characterizing the structural state of the material are [2, 3]:
γ σ is the coefficient of overstress on interatomic bonds, characterizing the uneven
distribution of external stresses σ on interatomic bonds σ 0 ðγ σ ¼ σ 0 =σ ≥ 1Þ; ue is the
density of latent (free) energy of defects and damages; v is the coefficient of
unevenness of the distribution of latent energy in volume, representing the ratio
between the density of latent energy in the local volume u0e to the average value
ue ν ¼ u0e =ue . The complex structural parameter k ¼ γ σ =v0, 5 ¼ σ ∗ =S ∗ characterizes the relationship between the theoretical σ ∗ and real S ∗ strength of a solid.
2.2 Physical model and structural-energy interpretation of the process
Macroscopic phenomena of plastic deformation and scattered destruction of the
body element are a cooperation of a huge number of microscopic elementary acts of
atomic and molecular rearrangements in the field of external (thermal, mechanical,
electrical, etc.) forces activated by thermal energy fluctuations. The whole variety
of mechanisms and structural levels of the process from the thermodynamic point
of view is divided into two most characteristic groups—adaptive and dissipative
(relaxation) type, which differ in physical nature and kinetic laws. The first group
includes elementary acts that control the origin and accumulation of elementary
defects in the deformable body (damageability). The integral characteristic of
intensity of the specified processes is specific (referred to unit of volume) power of
pumping of excess (latent) energy u_ e
u_ e ¼
due
¼ A sinh ασ 2i � ν ue =2kT :
dt
The second group includes mechanisms and elementary acts that control
relaxation (dissipative) processes of plastic deformation. The integral
36
(1)
Structural-Energy Interpretation of the Friction
DOI: http://dx.doi.org/10.5772/intechopen.86123
characteristic of these processes is the specific power of the thermal effect q_ of
plastic deformation
q_ ¼
dq
¼ B sinh ασ 2i þ ν ue =2kT :
dt
(2)
here, A and B are the kinetic coefficient
2kT n 0
U 0 ðσ 0 ; T Þi
,
∑ U ðσ 0 ; T Þ exp �
A¼
hV 0 1 i
kT
2kT n ″
U ″ ðσ 0 ; T Þi
,
B¼
∑ U ðσ 0 ; T Þ exp �
kT
hV 0 1 i
U 0i ðσ 0 ; T Þ ¼ U 00i þ ΔU 0 ðT Þ � βσ 20 , U ″i ðσ 0 ; T Þ ¼ U ″0i þ ΔU ″ ðT Þ � βσ 20 ,
α¼
γ 2σ V 0
γ2 V 0
,β ¼ σ ,
6G
2K
(3)
(4)
(5)
(6)
where U0 0i, U″0i is the activation energy of the formation and diffusion of the ith
defect, respectively; σ 0 , σ i is the hydrostatic stress and stress intensity; V 0 is the
atomic volume; k is the Boltzmann constant; h is the Planck constant; T is the
absolute temperature; G, K is the shear and bulk elasticity modules.
2.3 Thermodynamic analysis of interrelation between deformation and
fracture
From the thermodynamic point of view, the process of plastic deformation and
destruction is characterized by the competition of two opposite, interrelated and
simultaneously occurring trends in the body element—the growth of the latent
energy density ue of various defects and damages arising and accumulating in the
material due to the work of external forces ωр , and its reduction (release) due to
relaxation processes occurring inside the deformable body element; in this case,
the first trend is associated with the deformation hardening and material damage,
the second-with the dynamic return and dissipation of strain energy, causing the
thermal effect q of plastic deformation.
A significant part of the dissipation energy q is not retained in the deformable
element of the body, passes through it as if in transit and dissipates in the environ!
ment due to heat exchange q . Only a small part of the dissipation energy q accumulates in the deformable element of the body in the form of a thermal component
!
of the internal energy ΔuT ¼ q� q increasing its temperature (self-heating effect).
In accordance with the law of conservation and transformation of energy
_
ωp ¼ Δue þ q and ω_ p ¼ u_ e þ q:
(7)
In the mechanics of a deformable solid, irreversible work ωp and the power ω_ p of
deformations are associated with the stress-strain state of the body element by the
relation
p
p
dωp ¼ σ i dεi , ω_ p ¼ σ i ε_ i :
p
(8)
where ε_ i is the rate of irreversible deformation.
Joint consideration Eqs. (7) and (8) allows to establish a unique relationship
between the stress-strain and thermodynamic states of the body element
37
Friction, Lubrication and Wear
p
ε_ i ¼
ω_ p
1
q
¼ ðu_ e þ q_ Þ ¼ ε_ ei þ ε_ i :
σt
σi
(9)
Therefore, from the thermodynamic point of view, the total values
of the work
�
p
p�
ωp and irreversible deformation εi and the rates of their change ω_ p ; ε_ i can be
represented as the sum �of two terms
� associated, respectively,
� q with the
� deformation
_ i controlling
hardening and damage ε_ ei ¼ u_ e =σ i and dynamic return ε_ i ¼ q=σ
quasi-viscous flow of the body element.
This important conclusion is of fundamental importance in the analysis of the
relationship between the processes of deformation and destruction of the body
element. For damage and destruction of the body element is responsible only part of
the plastic (irreversible) deformation εei controlled by microscopic processes associated with deformation hardening and accumulation of latent energy of defects and
q
damages. A significant part of the irreversible deformation εi controlled by relaxation (dissipative) processes does not affect the damage and destruction of the body
element, but only causes its quasi-viscous flow (stationary creep). The relationship
between the work and the degree of irreversible deformation and their components
varies within a very wide range and depends on the structure of the material and the
conditions of its deformation [1].
2.4 Thermodynamic condition of local fracture
The parameter of damage (scattered destruction) is taken as the density of the
internal energy u accumulated in the deformable volumes, determined by the sum
of two components: potential (latent) ue and kinetic (thermal) uT that is
Δu ¼ Δue þ ΔuT , u_ ¼ u_ e þ u_ T :
(10)
This energy is associated with the accumulation in the deformable element of the
body of static ðΔue Þ and dynamic ðΔuT Þ damages and distortions of the crystal lattice,
therefore, is dangerous, responsible for the scattered destruction (damage). The
element of the body is considered to be destroyed if at least one local micro-volume
responsible for the destruction, the density of internal energy reaches a critical (limit)
value u ∗ corresponding to the loss of crystal lattice stability “in a large.” This point
corresponds to the appearance in the local micro-volume of a crack of critical size
(according to Griffiths-Orovan-Irvin) and a sharp localization of the process at the
mouth (top) of the crack. The thermodynamic condition of local fracture is written as
uðr ∗ ; t ∗ Þ ¼ uðr ∗ ; 0Þ þ
tð∗
0
u_ ðr ∗ ; tÞdt ¼ u ∗ ¼ const:
(11)
here, u ðr ∗ ; 0Þ is the density of internal energy in the local micro-volume of the
material in the initial (before deformation t ¼ 0) state; u_ ðr ∗ ; tÞis the specific power
of internal energy sources in the local volume�responsible
� for the destruction; r ∗ is
the parameter characterizing the coordinates x ∗ ; y ∗ ; z ∗ of the local volume
responsible for the fracture.
2.5 Thermodynamic criterion of fracture
In accordance with the structural-energy analogy of the process of mechanical
destruction and melting of metals and alloys [5] and theoretical and experimental
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studies [1, 6], the critical value of the internal energy density u ∗ in the local
macro-volume of the material responsible for destruction coincides well with the
known thermodynamic characteristic of the material ΔHS is the enthalpy of
melting, that is.,
u ∗ ¼ ΔHs ¼
T
ðs
0
cp dT þ Ls :
(12)
here, T S is the melting temperature; cp is the heat capacity; LS is the latent heat
of melting.
3. Triboergodynamic’s method
3.1 Friction
3.1.1 Initial or zero axiom of friction
The present day analysis of sum total of modern friction investigations may be
presented in the form of three theses (others are also possible) of essential property
which are shared by many research workers as undoubt proof as to the most
characteristic properties of generalized friction model:
1. Friction is the phenomenon of resistance to the relative movement
(movement) of surfaces, localized at the points of contact tangent to them;
2. Friction is the process of converting (transforming) the energy of external
mechanical motion into other types of energy, and mainly into thermal
energy;
3. Friction is a process of elastic-plastic deformation and fracture localized in
thin surface layers of friction pair materials.
These three axioms may be regarded as initial friction axioms and called “zero”
friction axioms as the starting-point of whence it is possible to develop logical
analysis of generalized engineering property for friction process.
In the capacity of axiomatic method of friction investigation of initial friction
axioms [4] mentioned above the author thinks it expedient to use the method of
ergodynamics of deformable solids [1–3] which are at present may be taken as
axiomatic, that is, method which may be trusted owing to the theoretical, experimental and practical substantiation.
3.1.2 Balanced and unitary attributes of friction
Taking into consideration that basic attribute of any system is a balance attribute
then tribosystem framework should be determined by the framework of obeying,
for example, energy balance friction. Then it follows that basic equation for
tribosystem is an energy balance equation characterizing movement within friction
system in a generalized and quantitative way. Constituent parts of this balance must
determine basic quantitative regulations of energy transformations (and movement) within the system.
39
Friction, Lubrication and Wear
Thus, tribosystem in the most generalized sense is quantitatively characterized
by the energy balance equation. Most generalized quantitative regulatities of
tribosystem behavior (states) are determined by magnitudes relations among constituencies of friction energy balance. These conditions may also be taken as friction
axioms. In accordance with that it is possible to show justice of entropy balance
equation and so of information and etc.
Taking into consideration the fact that the most characteristic magnitude of the
most global balance principle is unit (whole), then, consequently, the basic parameters of tribosystem (friction), expressed as indexes of relations among balance
constituents must also have criterion (limit) magnitudes equal to unit.
3.1.3 Common energy analysis of friction process
In the most general case the work of friction process W F is summed up from the
plast
and plastic W F deformation and wear (failure) of contact
work of elastic W elast
F
volumes (Figure 2) and work for overcoming forces of viscous friction and failure
of lubricant material W lub :
plast
W F ¼ W elast
þ WF
F
þ W lubr ,
(13)
For particular case of friction without lubrication (W lub ffi 0) and in the conditions of stationary (developed) friction, when the work of elastic deformation may
be neglected due to their insignificance, friction work W F will be determined
mainly by the work of plastic deformation of surfaces (contact volumes) of shaft
plast
plast
W F1 and of bearing W F2 :
plast
WF ¼ WF
plast
plast
¼ W F1 þ W F2 :
(14)
3.2 Structural-energy interpretation of friction process
It is known friction is characterized a product of frictional forces F by friction
distance ℓ, that is., the work ωf , expended on overcoming frictional forces
ωf ¼ Fℓ,
(15)
ωf ¼ Δue þ q,
(16)
_
ω_ f ¼ u_ e þ q:
(17)
here, ω_ f ¼ dωf =dt is a power of friction dissipation of energy; u_ e ¼ due =dt is the
rate of storing latent energy in deformed (contact) volumes; q_ ¼ dq=dt the power of
thermal effect of plastic deformation (friction).
Since the contact volumes of both materials that make up the friction pair are
deformed by friction (see Figure 2), Eqs. (16) and (17) should be written as
ωf ¼ Δue1 þ Δue2 þ q1 þ q2 ,
(18)
ω_ f ¼ u_ e1 þ u_ e2 þ q_ 1 þ q_ 2 :
(19)
These equations show, that from thermodynamic point of view, the work ωf of
friction forces, (friction power ω_ f ) is related to plastic deformation of the contact
volumes. The work ωf may be divided conventionally into two specific parts.
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The first part of the friction work is related to the change in the deformable
(contact) volumes of materials of latent (potential) energy Δue1 and Δue2 . It is the
energy of various elementary defects and damages arising and accumulating in
deformable volumes. This energy is a unique and integral characteristic of submicroand microstructural changes that occur in plastically deformable volumes of materials
[1, 2, 7]. It is a measure of deformation hardening and damage of materials.
The second part of the friction work ωf is related to the processes of dynamic
return, accompanied by the release of latent energy and the thermal effect q1 , q2 of
friction. This energy is associated with the movement and destruction of various
elementary defects of opposite signs, their exit to the surface, healing reversible
submicroscopic discontinuities, etc.
The relations between the components of the energy balance of the friction
process Δue1 and Δue2 , as well as q1 and q2 vary widely and are determined by the
physical and chemical properties of the materials that make up the friction pair,
their structure and the conditions of the friction process.
In the most general case, Eqs. (18) and (19) should be presented (Figure 2)
taking into account the real (not unit) sizes of the tribocontacts.
W f ¼ ΔU e þ Q ¼ ΔU e1 þ ΔU e2 þ Q 1 þ Q 2 ,
(20)
_ f ¼ U_ e þ Q_ ¼ U_ e þ U_ e þ Q_ 1 þ Q_ 2 ,
W
1
2
(21)
where ΔU e ¼ V f Δue ; U_ e ¼ V f u_ e ; V f is contact (deformed) volume of the
materials of the friction pair.
Solving Eqs. (20) and (21) with respect to the friction force F, we obtain
generalized equations for the friction force
ΔU e1 þ ΔU e2 Q 1 þ Q 2
þ
:
l
l
U_ e þ U_ e2 Q_ 1 þ Q_ 2
þ
,
Fv ¼ 1
v
v
Fl ¼
(22)
(23)
where l and v are the friction path and the slip velocity.
Dividing both parts of the Eqs. (22) and (23) by the normal force N, we present
generalized equations for the coefficient of friction
ΔU e1 þ ΔU e2 Q 1 þ Q 2
þ
,
Nl
Nl
U_ e þ U_ e2 Q_ 1 þ Q_ 2
þ
:
μv ¼ 1
Nv
Nv
(24)
μl ¼
(25)
Thus, friction is generally described by the equation of energy balance and from
the thermodynamic point of view [1–4] it is a competitive process of two (mentioned above) opposite, interrelated and simultaneously occurring in the deformable contacts trends. According to the energy balance scheme (Figure 1) for plastic
deformation and fracture [1] presented above (relationships Δ u ¼ Δ ue þ Δ uT and
!
q ¼ Δ uT þ q ), equations [8] for friction work W f , frictional force F and friction
coefficient μ (without lubrication) has view
!
41
!
W f ¼ ΔU e þ Q ¼ ΔU e1 þ ΔU e2 þ ΔU T1 þ ΔU T 2 þ Q 1 þ Q 2 ,
(26)
!
!
_
_
_ f ¼ U_ e þ Q_ ¼ U_ e þ U_ e þ U_ T þ U_ T þ Q 1 þ Q 2 ,
W
1
2
1
2
(27)
Friction, Lubrication and Wear
ΔU e Q ΔU e1 þ ΔU e2 Q 1 þ Q 2
þ ¼
þ
,
l
l
l
l
U_ e þ U_ e2 Q_ 1 þ Q_ 2
þ
¼ Fmechanical þ Fmolecular ,
Fv ¼ 1
v
v
ΔU e1 þ ΔU e2 Q 1 þ Q 2
þ
¼ μadapt þ μdis ¼ μadapt þ μT ðdisÞ þ μ ! ,
μl ¼
Q ðdisÞ
Nl
Nl
U_ e þ U_ e2 Q_ 1 þ Q_ 2
þ
¼ μdeformation þ μadhesion ,
μv ¼ 1
Nv
Nv
Fl ¼
(28)
(29)
(30)
(31)
!
!
where ΔU e ¼ V f Δ ue ; Q ¼ V f q; Q ¼ V f q ; U_ e ¼ V f u_ e ; u_ e ¼ d ue =d t is the rate of
latent energy density change in the contact volumes; V f is a deformable volume of
friction; μ is the coefficient of friction; μadapt is the adaptive coefficient of friction;
μTðdisÞ and μQ! ðdisÞ are the static and dynamic components of dissipative coefficient of
friction; ΔU T is the thermal component of internal energy; N is the normal load; l is
the friction distance; v is the sliding velocity. The latent energy density Δue is an
integral parameter of tribostate and damageability (failure (Δue∗ )) of solids [1].
Thus, viewed thermodynamically, the work done by friction forces W f (the
_ f ), the friction force F and the friction coefficient μ may be
friction power W
Figure 1.
Scheme of the energy balance for the plastic deformation (friction) of a solid [1–3].
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classified conventionally into two specific components with different kinetic
behavior [3, 9]. The first component is associated with microscopic mechanisms of
adaptive type and relates to the change of latent (potential) energy (Δ ue1 , Δ ue2 ) of
various elementary defects and damages that are generated and accumulate in the
deformable volumes of materials friction pair (Figure 1). This energy is a unique
and integral characteristic of the submicro- and microstructural transformations
that occur in plastically strained materials [1–3, 9]. It is a measure of deformation
hardening and damage of materials. The second component is associated with
microscopic mechanisms of dissipative type and related to dynamic recovery processes in which latent energy is released and heat effect of friction (q1 , q2 ) take
place. This energy is associated with the movement and destruction of various
elementary defects of opposite signs, their exit to the surface, healing reversible
submicroscopic discontinuities, etc. The ratios of the components Δ ue1 and Δ ue2 as
well as q1 , q2 of the balance vary over a wide range, depending on the physical,
chemical, and structural properties of the materials that comprise the friction couple and the friction process conditions [8].
Thus, the thermodynamic analysis of the plastic deformation and fracture of the
solid volume at friction allows us to obtain generalized (two-term) dependences for
the friction force F and the friction coefficient μ, which corresponds to the modern
concepts of the dual nature of friction [10, 11]. It is a molecular mechanical Eq. (29)
and deformation-adhesion Eq. (31) theories of friction. But, more correctly it is
necessary to speak about adaptive-dissipative nature (model) of friction Eq. (30).
As follows from the equations of the energy balance of friction Eqs. (26) and
(27), the whole variety of manifestations of friction and wear can be conditionally
reduced to at least two fundamentally different states. The first condition determines all types of damageability and wear, the second-the so-called condition of
“wearlessness” [7].
The state of damageability and wear is characterized by the components of
energy balance Eqs. (26) and (27), which are responsible for accumulation of
internal energy Δ u ¼ Δ ue1 þ Δ ue2 þ Δ uT1 þ Δ uT2 in deformed volumes, that is,
the process is irreversible [4, 8]. The “wearlessness” state is characterized by the
components of the energy balance Eqs. (26) and (27), which are responsible for the
dynamic dissipation (reversibility) of strain energy into elastic and structural dissi!
!
!
pated energy q ¼ q 1 þ q 2 of friction contact [4, 8].
In its turn, the first state may be classified depending on the relation between
potential Δ ue and kinetic Δ uT components of internal energy. It is subdivided
conventionally into mechanical damage and wear (due to so-called structure activation) and thermal damage and wear (due to thermal activation). For instance, let
the thermal component of internal energy Δ uT be equal to zero (Δ uT ¼ 0) and the
internal energy variation at damage and wear be defined only by variation of the
potential Δ ue ðΔ u ¼ Δue Þ component. Then, the mechanical damage and wear
with brittle fracture of surfaces take place. On the contrary, if we have Δ ue ¼ 0
(Δ u ¼ Δ uT ), then the thermal damage and wear with ductile fracture of surfaces
take place. All the intermediate values of the components are associated with quasibrittle or quasi-ductile fracture of solids [4, 8].
In the most general case, taking into account a fundamental tribology’s notion of the
“third body” [10], the energy balance at dry friction Eq. (20) should be written as
W f ¼ ΔU e1 þ ΔU e2 þ ΔU e3 þ Q 1 þ Q 2 þ Q 3 :
(32)
In the special case, where the friction is localized into volume of the “third body”
(Figure 2) Eq. (32) develops into
43
Friction, Lubrication and Wear
!
W f ¼ ΔU e3 þ Q 3 :
(33)
here, ΔU e3 ¼ V 3 Δue3 .
3.3 Energy interpretation of the friction coefficient by Amonton
(Leonardo da Vinci)
According to the main conclusion of the thermodynamic theory of strength [1],
as a structural parameter should not take the entire value of the accumulated plastic
deformation, but only its part associated with the deformation hardening, which is
uniquely and integrally determined by the density of the potential component of the
internal energy (i.e., the density Δ ue of the so-called latent energy) of various
defects and damages accumulated in the plastically deformable volumes of the
material. With this in mind, if we neglect the heat effect Q of friction, one will infer
from the thermodynamic analysis of friction of Eqs. (24) and (25) that the Amonton
(Leonardo da Vinci) friction coefficient is
μ¼
ΔU e
F
ΔU e
¼ ;F ¼
; Q ffi 0, μ ∗ ¼ 1:
∗
μ Nl N
l
(34)
Consequently, the coefficient of friction has a very deep physical sense. On the
one hand, it is the parameter which generally characterizes the resistance of
relative displacement (movement) of surfaces, for it reflects the portion of energy,
which “is done by friction away” as accumulated latent energy ΔU e , by relation to
parameter of external forces work μ ∗ Nl (energy of external relative movement) [12].
On the other hand, it is the generalized characteristic of damage, for it is defined of
the latent energy density Δ ue as integral characteristic of the structure defectiveness
measure, because this energy is the generalized parameter of damage. Here too,
coefficient of friction generally reflects the structural order (disorder) of deforming
contact volume, since the parameter ΔU e ¼ Δue V f is defined of the energy of
defects and damages of different types, that are accumulated into contact volumes
V f solids [12].
Thus, the coefficient of friction is a true and generalized parameter of the state
of the tribosystem. It follows a very important conclusion that the analysis of the
regularities of the evolution of the states of tribosystems is, first of all, the analysis
Figure 2.
Conditional scheme of friction contact [4].
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of the laws of change of the accumulated latent energy of deformation by the
contacting volumes of the solid, that is, change of Amontons coefficient of friction [12].
3.4 Generalized experimental friction curves
The dependences obtained for the friction coefficient μ are in agreement with
experimental curves μ ¼ μðN; vÞ (Figures 3–5). Analyzing various experimental
friction curves using the Eqs. (20)–(31) of friction energy balance, it was concluded
Figure 3.
Experimental results of Conti [13].
Figure 4.
Generalized friction experiments in I.V. Kragelsky’s interpretation [10]: sliding velocity (load: 1—small; 2 and
3—medium; 4—considerable).
45
Friction, Lubrication and Wear
Figure 5.
Experimental results of Watanabe for a pair of friction—nylon 6—steel [14].
Figure 6.
Structural-energy diagram of the evolution of friction surfaces [4, 16–18].
[4] that the experimental friction curves (Figures 3–5) of the type a μ ¼ μðN; vÞ are
generalized experimental friction curves and reflect the general (for all materials
and friction pairs) laws of evolution (changes in the friction coefficient) of
tribosystems.
3.5 Structural-energy regularities of rubbing surfaces evolution
An analysis of modern experimental data using Eqs. (20)–(31) has shown that
the experimental friction curves of type μ ¼ μðN; vÞ are the generalized
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Structural-Energy Interpretation of the Friction
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experimental friction curves that reflect the evolution (the change in the friction
coefficient) of tribosystem.
We propose an energetic interpretation of the experimental friction curves
μ ¼ μðN; vÞ (Figure 6). According to our concept [4, 15, 16], the ascending portion
of the friction coefficient curve μ is mainly controlled by processes associated with
the accumulation of latent energy ΔU e in various structural defects and damages.
Here the increase in μ is due to the increasing density of latent (potential) energy
Δ ue and the increasing adaptive friction volume V f . The descending portion of the
friction curve is mainly controlled by processes associated with the release and
!
dissipation of energy Q ¼ ΔU T þ Q . Here the decrease in μ is due to the decrease in
latent energy density within the friction volume V f or (which is virtually the same)
to the decrease of the adaptive friction volume V adapt ue ¼ ue∗ ) and to the increase
∗
!
of the dissipative volume V dis q ¼ ue∗ .
The evolution of the tribosystem is presented in the form of a diagram
(Figure 6) and has an adaptive-dissipative character Eqs. (29)–(34) and reflects the
competitive (dialectical) nature of friction. The evolutionary curve has a number of
fundamental points (1–5) of transition states of the tribosystem, which are strictly
subject to the balance principle of friction. Between these points there are the most
characteristic areas of behavior of the tribosystem. These areas reflect the most
general properties of nonlinear dynamics of friction evolution.
So, in Figure 6 you can see the following conditionally marked points and areas:
0-1—the area of static friction and strain hardening; 1—the point of the limit strain
hardening; 1-2—excess energy pumping area; 2—point of adhesion (seizure) and
transition of external friction into internal (point of critical instability); area of
formation of dissipative structures (formation of temperature fluctuation in the
friction volume); 3—the point of minimum compatibility (maximum frictionness);
1-2-3—area of self-organization; 3-4—compatibility area; 4—point of wearlessness
(abnormally low friction); 5—thermal adhesion point.
The ideal evolution of the friction contact is symmetric. The friction process
begins and ends in areas of elastic behavior. Between them is the plastic maximum
(super activated state) as a condition of self-organization and adaptation. In the
most general case, the regularities of evolution (adaptation) of tribosystems can be
represented as two-stage (Figure 6). At the first stage (0–2) of the evolution of
the friction contact, it tends to form a critical volume V f∗ of friction (point 2).
This is the smallest volume of friction that has accumulated the maximum
potential energy of structure defects. This is an elementary tribosystem, that is., an
elementary and self-sufficient energy transformer. In the first stage, the latent
energy density Δue increases to a limit value Δue∗ within the critical friction
volume V f∗ .
The volume of friction V f∗ is constant in the second stage of evolution. At this
stage, contact is evolutionarily developed due to structural transformation. At this
stage, a wide spectrum of compatible friction structures (Figure 6) can be formed
depending on the nature of the environment. The second stage (2–4) can be considered as a structural transformation of the critical friction volume V f∗ (elementary
tribosystem) conditionally to the adaptive V adapt and dissipative V dis friction volumes (Figure 7). The end point (point 4) of this stage of evolution is characterized
∗
into
by the complete transformation of the critical adaptive friction volume V adapt
∗
the dissipative V dis one.
The above volumes mentioned characterize different regularities of energy
conversion of external mechanical motion at friction. Adaptive volume V adapt
47
Friction, Lubrication and Wear
Figure 7.
The model of the energy evolution of the contact friction volume at points 1–5 of the diagram (Figure 6) [4].
is associated with irreversible absorption of strain energy. In this volume, there is
an accumulation of latent deformation energy Δue and centers of destruction are
born. The dissipative volume V dis is able to reversibly transform (dissipate) the
energy of the outer movements. In this volume, there is no accumulation of latent
deformation energy due to the flow of reversible elastic-viscoplastic deformation.
Theoretical and calculated estimates [4, 16, 18] have shown that the dissipative
friction volume performs a reversible elastic transformation of the energy of external
!∗
mechanical motion with a density q equal to the critical density ue∗ of the latent energy.
The culmination of the evolution of the tribosystem is its final and limiting state of
point 4—the state of abnormally low friction and wearlessness (maximum efficient).
A schematic evolution of the contact volume of friction in diagram’s points 1–5 is
presented in Figure 7.
Calculations show [4] that with the ideal evolution of the tribosystem, the
adaptive (Amonton) coefficient of friction μadapt at point 2 of the diagram drops
sharply, reaching at point 4 the elastic coefficient of friction μelast . For point 4 of
compatibility area 3-4, an equation of energy balance Eq. (30) should be put in the
following way:
μadapt ¼ μ ∗ � μdis ¼ 1 � μdis ¼ μplast ¼ 0 ¼ μelast ; μ ∗ ¼ 1, 0:
(35)
Thus, we have at point 4 of the ideal evolution of the contact friction volume the
condition of perfectly elastic-viscous-plastic deformation. This actually shows the
Eq. (35), that is, the coefficient of friction of Amonton μadapt , being, in fact, a plastic
coefficient of friction μplast has a minimum value equal to zero. Consequently,
plastic friction becomes elastic with the coefficient μelast of friction. This means that
the plastic deformation of the contact friction volume is realized with the maximum
!
dynamic dissipation (Q ¼ max) of the accumulated latent energy. Therefore, the
amount of accumulated energy at point 4 is zero (ΔU e ¼ 0). This fact proves the
ideal state with the full evolution of the contact volume. From the physical point of
view, this state can be explained by the complete dissipating of the energy ΔU e∗
accumulated at point 2, along the newly formed structures of point 4 in the form of
!∗
elastic energy of interaction between them (energy Q of dynamic dissipation).
Here μdis ¼ 1, 0. The structural elements themselves are defectlessness—μadapt ¼ 0,
and friction is elastic—μ ¼ μelast .
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It is shown [4] that the value of the minimum adaptive friction volume V min
adapt
corresponding to the zero value of the plastic friction component μadapt is not zero,
but is equal to the size of a certain minimum structural element of the deformable
solid.
3.6 The idea of a mechanical (nano) quantum of dissipative friction structures
The result of ideal elementary tribosystem (contact) evolution is forming of
unique nanostructure—a mechanical (nano) quantum. Strict ideas about mechanical quantum obtained [4, 18] considering for point 4 of the friction evolution
diagram the equation of a quasi-ideal solid:
!∗
Q
!
!
∗
¼ S Q T ¼ μdis
Nlf ¼ V f∗ ue∗ ¼ V f∗ q ∗ :
(36)
This equation is a special case of the solution of the equations of energy balance
!
∗
. Here S Q is the inertial entropy
of friction Eq. (29), at μadapt ¼ 0 and μdis ¼ 1 ¼ μdis
of compatible friction volume; T is the characteristic temperature of compatible
contact friction volume; lf is the linear dimension of elementary contact.
Accordingly, under the conditions of maximum compatibility (point 4),
when the tribosystem implements a complete evolutionary cycle of adaptation
with the formation of the most perfect, dissipative structure, its (structure)
behavior is subject to the equation of state of a quasi-ideal solid, that is, it should
be assumed that the interactions between the elements of this structure are
minimized—the state of ideal elasticity in dynamics. Eq. (28), taking into
account the Planck-Boltzmann formula S ¼ k ln W and the real number of
atomic oscillators N f in the volume of the elementary tribosystem (contact) V f∗ ,
is given to the form explaining the regularities of friction in terms of the
evolution of systems:
μdiss ¼
!
kTN f ln W
SQ
¼
,
Nlf
Nlf
μadapt ¼ 1 � μdiss ¼ 1 �
(37)
!
kTN f ln W
SQ T SU T
¼1�
¼
,
Nlf
Nlf
Nlf
(38)
where k is the Boltzmann constant; W is the probability of state; SU is the
configuration entropy of friction (contact) volume.
The tribosystem always tends to some optimal state characterized, that is, to the
most probable state W 0 ¼ N f ln W for the given friction conditions.
The analysis and solution of these equations [4, 16–18] allows to show the
principle of the constancy of the magnitude of the probability (the state’s parameter
(order)) W of the tribological system) for the entire range of compatible friction,
namely ln W ¼ 3, and W ¼ e3 ¼ 20, 08553696….
The number of thermodynamic state probability W equal to 20, 08553696… was
interpreted [4, 12–15] as the smallest number of linear, atomic oscillators in one of
the three directions of the minimum adaptive friction volume V min
adapt corresponding
to the state of almost absolute elastic friction—abnormally low friction (safe deformation threshold). Accordingly, the number of atomic oscillators in this volume is
3
V Q ¼ ðe3 Þ ¼ ð20; 08553695…Þ3 ¼ 8103, 083969….
It is the universal size (volume) of mechanical quantum [4, 7, 16–18].
49
Friction, Lubrication and Wear
On the other hand, taking the meaning of Boltzmann entropy S, we obtain a
universal friction constant Rf ¼ kN f [4, 16–18], which in physical sense
characterizes the “energy size” of the elementary tribosystem (TS) containing
under ideal conditions the same number of atomic oscillators N f (mechanical
quanta N Q ):
Rf ¼ k � N f ¼ k � W 3 � N Q ¼ RMQ � N Q ,
RMQ ¼ k � W 3 ,
J
,
grade � MQ
J
,
grade � TS
(39)
(40)
where RMQ is the universal constant of deformation at friction.
As follows from the calculations [4], the size of the minimum adaptive friction
volume V min
adapt coincides in its magnitude with the size of the submicroscopic zone at
the mouth of the crack, which for metals is equal ð4:::9Þ � 10�6 mm, that is, with the
size of the critical volume responsible for the fracture. Thus, the size of the minimum adaptive friction volume V min
adapt ¼ V elast can be represented as the size of some
mechanical “quantum”.
This mechanical quantum is the minimum number of atoms capable of providing a configuration of their distribution (structure), which has the property of
reversibly absorb and dissipate (return) the energy of external mechanical motion
(action). It also represents the smallest structural formation under plastic deformation and is formed during the transition of the tribosystem (deformable volume)
through the extremely activated (critical) state (Figure 6) due to the development
of self-organizational processes of adaptation of the tribosystem. The mutual
rotational-oscillatory motion of these mechanical quanta relative to each other
inside the elementary tribosystem (contact) determines the state of the most perfect dissipative structure of friction. Actually, this state is described by the equation
of state of a quasi-ideal solid Eq. (36), the state when the interaction between the
elements of the structure (mechanical quanta) is minimized-the state of the ideal
elasticity of the quasi-viscous flow. The calculated coefficient of friction between
the quanta is approximately 10�8 [4, 16–18].
The conclusion that the mechanical quantum is the smallest structural formation
under plastic deformation (friction) is confirmed by the calculation. If we compare
the values of the elastic modules E to the atomic (true) elasticity Er , we obtain
values equal to 60, where the number 60 ¼ 3W can be interpreted as a characteristic of the volume elasticity of one mechanical quantum—the minimum adaptive
friction volume V min
adapt . Calculation of the parameter W ffi 20 ¼ E=3Er for different
metals and steels gives an average value of 20, 77 (Table 1); ΔHS ¼ 3Er is the
enthalpy of melting.
It is concluded [4, 16–18] that for all materials, under the conditions of the ideal
evolution of the tribosystem, the number of atoms N f (mechanical quanta (MQ)) in
the volume of one elementary tribosystem (TS) is constant. Thus, we can talk about
the amount of matter equal in mass to one elementary tribosystem and to one
mechanical quantum.
3.7 The synergy of the tribosystem and the optimality states
Mechanical quantum is a dynamic oscillator of dissipative friction
structures. The ideal, quasi-elastic state of contact at its full evolution is the effect
of the most complete energy dissipation of external mechanical motion on the
50
Structural-Energy Interpretation of the Friction
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Metals and steels
E � 10�3 , MPa
Cr
235.4
Mg
Ag
�
�
ue∗ ΔH S � 10�3 , MJ/m3
E=3Er
8.5
27.69
44.4
1.9
23.37
79.0
3.7
21.35
Au
78.7
4.0
19.67
Co
200.1
10.6
18.88
Fe
211.4
9.9
21.35
Ta
184.4
10.6
17.39
Ti
105.9
6.7
15.8
Nb
104.0
9.2
11.3
Zr
95.6
5.7
16.77
Mo
316.9
12.0
26.4
W
392.4
14.4
27.25
Ni
201.1
9.4
21.39
Iron
210.9
10.1
20.88
20
200.1
9.5
21.06
1Kh13
206.0
8.9
23.14
3Kh13
218.8
9.2
23.78
Kh18N9T
199.1
9.4
21.19
Kh18M9
199.1
9.6
20.74
30Kh
214.1
10.2
20.99
30N3
207.5
10.3
20.11
40
209.4
9.7
21.58
30G2
207.2
10.0
20.72
30KhGN3
208.0
10.2
20.4
G13
204.0
10.0
20.4
50S2G
196.2
10.3
19.05
U8
198.0
10.3
19.22
U12
198.0
10.4
19.04
ΔHS ¼ 3Er , E=3Er ¼ 20:77.
Table 1.
Parameter estimation for different metals and steels [4].
newly formed (on the mechanism of self-organization in the vicinity of the
critical state) structural elements-mechanical quanta (dynamic oscillators),
which implement the most complete rotational-oscillatory behavior relative to
each other in the volume of the elementary tribosystem. At the same time, the
resistance to their relative interaction is minimal-elastic and corresponds to the
elasticity of ideal atomic (thermodynamically equilibrium) interactions at the level
of electronic shells.
The universal constants of the mechanical quantum and the elementary
tribosystem (material point) determine both the quantum model of surface
damping:
51
Friction, Lubrication and Wear
μdis ¼
3RMQ Tni
U 1Q ni
ni
¼
¼
¼ 1 � μadapt ;
Nlf
U 1Q n∗ n∗
μadapt ¼ 1 �
ni
ndest
¼
,
n∗
n∗
(41)
taking into account the quanta of destruction ndest (irreversible component of the
process) and the quanta of damping ni (reversible, elastic component (fatigue
number)), and the probabilistic model of the evolution of the tribosystem to the
most ordered state:
μadapt ¼ 1 � μdis ¼ 1 �
Rf T ln W i
ln W i
¼1�
:
Nlf
ln W ∗
(42)
where 3RMQ T ¼ U 1Q is the energy of one mechanical quantum; W i and W ∗ is
the current and limit probabilities of states of compatible tribosystems.
According to the model of quantum damping of surfaces under friction in the
conditions of the most complete evolution (adaptation) of the elementary
tribosystem, all mechanical quanta except one, elastically and reversibly transform
the energy of external action (mechanical motion). One mechanical quantum of
radiation (ffi 8103 atoms)—there is a minimum loss (the essence of wearlessness
(the ideal damping properties) or the standard of wear).
The linear size of a mechanical quantum is equal to the diameter of a spherical
ideal crystal with atomic roughness [4, 7]:
DMQ ¼ 2 � W � da � ð3=4 � π Þ
1=3
¼ 7, 177nm:
(43)
here, da is the average atomic diameter, for metals; W ¼ e3 is the mechanical
quantum state parameter [4].
The mechanical quantum (Figure 8) itself should be considered as an elementary nanostructure of a metal solid.
Figure 8.
Model of an ideal crystal of elementary nanostructure of friction contact (8103 atomic cubical cells)
[4, 16–18].
52
Structural-Energy Interpretation of the Friction
DOI: http://dx.doi.org/10.5772/intechopen.86123
Calculations have shown [4, 8] the number N Q of such mechanical “quanta”
∗
to be
(subtribosystems) within the elementary tribosystem’s volume V f∗ ¼ V dis
0:63 � 108 which is close to the safe number n ∗ of fatigue cycles.
Therefore, the smaller the coefficient of friction μadapt (the greater the coefficient μdis ) of the tribosystem, the higher its fatigue endurance (durability), as a
greater number of mechanical quanta involved in the process of damping (elastic
return) of the energy of the external mechanical motion (impact), and consequently the smaller the number of quanta associated with the fracture (accumulation of latent energy of defects and damage of the limit value). In the limit, the
tribosystem is characterized by the effect of “wearlessness” (abnormally low friction), corresponding to the state of almost complete thermodynamic reversibility of
the friction (deformation) process. Here, all mechanical quanta, with the exception
of one, reversible elastic transform (damp out) the energy of external mechanical
movement. By analogy with classical quantum theory, we can say that in this case
the system (tribosystem) is in the ground state (here, as if all mechanical quanta are
directed against the field)—tribosystem cannot give energy to any other system
(environment) simply because it (tribosystem) and does not accumulate energy in
this state. In this case, the tribosystem is in almost perfect balance with the environment.
The principle of mechanical quantum determines nanoquantum levels of all
friction parameters of compatible (optimal) tribosystems and other.
4. The model for the evaluation of wear of compatible friction
The model [4] of the moving critical (equilibrium) friction volume (Figure 9) is
considered for the analysis of wear problems.
_ f is connected with the
Here, the instantaneous value of the friction work W
i
_
friction work W f per unit time, taking into account the uniform distribution of
contacts (micro-shocks) in the longitudinal nv and transverse nн directions of the
friction surface:
_ f ¼W
_ fn¼W
_ f nн nv ¼ W
_ f H � Lv :
W
i
i
i
lf lf
Figure 9.
Scheme to the calculation of wear parameters of friction [4].
53
(44)
Friction, Lubrication and Wear
Accordingly, we have a number of ratios for power, force and coefficient of
friction
_ ∗ � n ¼ V ∗ � Δu ∗ � n ¼ V ∗ � Δu ∗ � nv ,
_ ∗ ¼W
W
f
fi
f
e
fH
e
F∗ ¼
_ ∗
W
f
v
¼
V f∗ � Δue∗ � n
lf � nv
¼
V f∗H � Δue∗
lf
,
_ ∗
V f∗ � Δue∗ � n V f∗H � Δue∗
W
T
¼
¼
:
μ ¼ ∗
N∗ � v
N �v
N∗ � v
∗
(45)
(46)
(47)
Here V f∗H ¼ V f∗ � nH (Figure 9); W iT∗ is the instantaneous (contact) the value of
Vt
the friction work; n ¼ V ff ¼ nv � nH is the ratio of the volume of friction V tf deform-
able per unit time t to the instantaneous volume of friction V f ; nv , nH is the number
of micro-shocks in the sliding direction of the sample per unit time and in the
transverse direction.
h �Δu ∗
h �Δu ∗
Eq. (47), performed to the form of the μ ∗ ¼ rp �lf e ¼ ap �Be , represents the basic
equation of wear for compatible friction region:
r
a
τr ¼
hr
Δue∗ ¼ Ir Δue∗ ,
lf
(48)
τa ¼
ha
Δue∗ ¼ Ia Δue∗ :
B
(49)
here, Ir , Ia is the linear wear rate, related to the real and nominal areas of
contact; B, H is the sample sizes in the slide and the longitudinal directions.
5. Nano quantum models of the maximum capacity for work of the
tribosystem
5.1 The principle of calculating the wear of gears
All parameters of compatible (optimal) friction should be in nanoquant
levels, which are commensurate with the parameters of one mechanical quantum—
standard of wear.
Operation of all heavily loaded tribosystems should be considered from the
standpoint of the ideal evolution of tribosystems. This is a perfect condition
contact friction is the true indicator of the state of the tribosystem for practical
examples of tribology. This is the standard of maximum efficiency of the
tribosystem—abnormally low friction and wearlessness.
A typical example of wear (destruction) of real tribosystems on the model of
mechanical quantum is the work of gears (for example, reducers) and systems of
wheel-rail and other, in which the elementary particle of wear (pitting) is wear
equal to one mechanical quantum. Imagine the engagement of a pair of teeth
involute profile on the field of the length of the active line of engagement
(Figure 10) as the model of smooth surfaces with uniformly distributed equilibrium
roughnesses after run-in (elementary tribosystems, which are analogues of the
material point of mechanics). Engagement of a pair of teeth corresponds to the
theoretical principle of running two cylinders under the conditions of Hertz elasticplastic contact. The materials of the teeth work at the limit of the fatigue threshold,
which corresponds to the minimum loss (pitting) of the contact volume (elementary tribosystem) in the form of a single mechanical quantum.
54
Structural-Energy Interpretation of the Friction
DOI: http://dx.doi.org/10.5772/intechopen.86123
Figure 10.
Model of active tooth surface of a gear wheel with equilibrium roughness of spherical shape [4].
When working gear engagement, for each revolution of the wheel (gear), each
roughness (material point) of the active surface of the tooth is loaded once, with a
minimum loss (wear) in one mechanical (nano) quantum. Since the critical volume
of friction (elementary tribosystem) contains 0:63 � 108 mechanical quantum, the
number of loads (wheel revolutions), equal to the critical number of loading cycles
—63 millions, leads to fatigue wear (loss) of the material layer of unit thickness h ∗ .
Linear wear h ∗ of the gear wheel is equal to the diameter Q TS ¼ 2:85 � 10�6 m of the
equilibrium friction volume V f∗ (Figure 10) [19]. This is a physical criterion of
wear. Accordingly, it is clear that the constructive limit criterion of wear of the
tooth of the gear is equal to the limit of wear when the bending strength of the tooth
is violated. For example, this is approximately 0.3 modulus of the tooth of the gear.
Consequently, the elementary nanostructure of deformable solids should be
considered as the wear standard and used to optimize the operating time of real
highly loaded Hertzian friction systems.
5.2 Evaluation of the capacity for work of bearings of internal combustion
engines
Let’s take an engine with an average shaft rotation—n ¼ 1500 min‐1 . Take the
limit linear wear of the bearing which is equal to h ∗ ¼ 0:1 mm. We know the linear
size of the elementary tribosystem—DTS ¼ 2:85 mkm ¼ 2:85 � 10�6 m [19]. For each
revolution of the shaft one elementary tribosystem (equilibrium, run-in contact)
loses one mechanical quantum. The number of revolutions required for the wear of
one elementary tribosystem is equal to the number of mechanical quanta in this
tribosystem, that is, it is nMQ ¼ 0:63 � 108 revolutions.
Now we can determine the wear time of one elementary tribosystem:
nMQ 0:63 � 108
42, 000
700
¼
¼ 42, 000 min ¼
¼ 700 hour ¼
¼ 29, 166 day
n
1500
60
24
29, 166
¼ 0:0799 year:
¼
365
(50)
tTS ¼
55
Friction, Lubrication and Wear
Now let’s define the number of layers of elementary tribosystems into linear
wear—0:1 mm:
ah ∗ ¼
h∗
1 � 10�4
¼
¼ 0:35 � 102 ¼ 35:
DTS 2:85 � 10�6
(51)
Now, let’s define the time of wear of shaft-bearing system with the ultimate
linear given wear—h ∗ ¼ 0:1 mm, namely:
tmotor ¼ tTS � ah ∗ ¼ 0:0799 � 35 ¼ 2, 7968 year:
(52)
Finally, we have 2, 7968 years of continuous work at ultimate load.
For this result we have the wear rate—i ¼ 4 nm=h. For example, this fits
well with the data for the engine wear rate—i ¼ 5 nm=h specified by
Prof. F. Franek [20].
If we work 8 hours per day, then we will get the following result:
2, 7968 � 3 ¼ 8:39 year:
(53)
This is a real result for modern cars. If we work less than 8 hours a day, then the
duration will increase significantly.
5.3 The principle of critical wheel rolling speed
The limit of this speed is determined by the principle of filling the entire nominal friction area of the sliding system with elementary tribosystems damping the
process. Above this speed of movement of the vehicle there will be a complete
unloading of the tribosystem, the separation of the wheel from the rail surface,
since the principle of minimum resistance to movement (the principle of one
elementary tribosystem or the principle of irreversibility) will be violated. In this
case, all mechanical quanta in the elementary tribosystem will repel the wheel.
There will be no quantum activating the process of maintaining the system in an
excited state.
The calculation will be made in the following order [21]. The elementary nomi8
nal size of the contact area is known. By definition [4], nTS
∗ ¼ 0:63 � 10 elementary
tribosystems can be placed and operate on the elementary nominal contact area.
Each elementary tribosystem (for the model of spherical roughness) has a size
D1TS ¼ 2:85 � 10�6 m [19] and is capable of providing a rolling path of the wheel in
the elementary act of rolling on the length of this tribosystem.
Thus, if all elementary tribosystems work in a unit of time on the entire nominal
contact area, then the path traversed by the wheel in a unit of time is equal to
∗
¼ 2:85 � 10�6 � 0:63 � 108 ¼ 179:55 m:
LΣTS ¼ D1TS � nTS
(54)
Consequently, the critical speed of wheel rolling is equal
v ∗ ¼ LΣTS � 3600 ¼ 646, 38 km=h:
(55)
This result is close to modern speed of 574:8 km=h (TGV, France).
5.4 Self-organized nanoquantum solid lubricant
Information above allows us to consider new self-organized surface layer as
follows: (1) the layer that separates the two original surfaces (alloys) of friction
56
Structural-Energy Interpretation of the Friction
DOI: http://dx.doi.org/10.5772/intechopen.86123
Figure 11.
Notional scheme of hydrodynamic lubrication.
from each other; (2) layer, which has a low coefficient of internal friction; (3) layer,
which has a high capacity for work, that is, very small wear; and (4) layer, which
may be seen as a solid lubricant.
Now you need to determine a value for the coefficient of friction of this selforganized solid lubricant and compare it with the coefficient of friction, for example, the most effective, or hydrodynamic lubrication.
It is known that the hydrodynamic lubrication when the stationary condition
(Figure 11) has coefficients of friction μ down to 0:005÷0:001 values.
For nanoquantum self-organized solid lubricant friction coefficient will be
calculated in the following order:
1. It is known [4, 15] that between the nanoquanta coefficient of friction is
equal to μMQ ¼ 1:587 � 10�8 .
Figure 12.
Conditional scheme for equilibrium elementary tribosystem, structured mechanical quanta. At length of this
tribosystem there are 397 mechanical quantums.
57
Friction, Lubrication and Wear
2. It is known [19] that the size of the critical volume of frictional contact
(elementary tribosystem) is equal to DTS ¼ 2:85 � 10�6 m.
3. Let’s picture an elementary tribosystem in the plane as a circle with a
diameter of DTS ¼ 2:85 mkm (Figure 12).
4. Next, let’s define the number of mechanical (nano) quanta n0MQ on a length
DTS of elementary tribosystem (Figure 12):
n0MQ ¼
DTS
2:85 � 10�6
¼
¼ 397:
DMQ 7:177 � 10�9
(56)
Figure 13.
Notional scheme of friction on the wavelength, structured elementary tribosystems. At the surface friction
wavelength is 351 elementary tribosystems.
Figure 14.
Notional scheme of self-organized nanoquantum contact with unsteady hydrodynamic lubrication.
58
Structural-Energy Interpretation of the Friction
DOI: http://dx.doi.org/10.5772/intechopen.86123
5. Let’s define the coefficient of friction for a single equilibrium critical volume
of friction (elementary tribosystem), the length of which is 397 mechanical
quantums (Figure 12).
μTS ¼ μMQ � n0MQ ¼ 1:587 � 10�8 � 397 ¼ 0:63 � 10�5 :
(57)
6. Let’s take the average friction surface wavelength equal to LW ffi 1 � 10�3 m.
Now define a number of elementary tribosystems on this wave length (Figure 13)
nTS ¼
LW
1 � 10�3
¼
¼ 351:
DTS 2:85 � 10�6
(58)
7. Now define friction coefficient at a wavelength of friction surface
μW ¼ μTS � nTS ¼ 0:63 � 10�5 � 351 ¼ 0:0022
(59)
As a result, we have a full conformity (Figure 14) of friction coefficient values
for hydrodynamic lubrication—0:005÷0:001 and solid lubricant—0:0022.
Thus, it is fair to talk about nanoquantum self-organized solid lubrication.
6. Conclusions
1. Structural-energy analysis of the friction process allows us to consider the
friction process as an evolutionary process.
2. From the equations of the energy balance of friction it follows that the
evolution of the tribosystem (contact) has an adaptive-dissipative character.
3. The coefficient of friction has an energy interpretation that reveals its deep
physical sense.
4. Experimental friction curves of μ ¼ μðN; vÞ type may be examined as
generalized friction experimental curves.
5. Structural-energy diagram of the evolution of rubbing surfaces (friction
contact) interprets the general regularities of transformation and dissipation
of energy during friction.
6. In the process of evolution of the friction contact, an elementary tribosystem
is formed as a self-sufficient energy transformer under friction. This
elementary tribosystem (critical friction volume) can be considered as an
analogue of the material point of mechanics.
7. The most complete evolution of the tribosystem has a symmetrical form—the
friction process begins and ends in the elastic region.
8. With the most complete evolution of the friction contact (elementary
tribosystem), a unique nanostructure (tribosubsystem) is formed; the basis
of this nanostructure is a mechanical (nano) quantum and the friction contact
(material point of mechanics) consists of about 0:63 � 108 such nano quanta.
9. We can consider the mechanical quantum as the smallest structural form of a
material solid and as the structural standard of material solid.
59
Friction, Lubrication and Wear
10. The mechanical quantum is precisely an asymptotically stable attractor of the
limit cycle type for a deformable solid body (at friction).
11. All parameters of compatibility (optimal) friction have to be in quanta levels
—commensurable with the parameters of the one mechanical quantum.
12. Interaction between nanoquantums is nature the net elasticity. The value of the
coefficient of friction between mechanical quanta has order
μMQ ¼ 1:587 � 10�8 .
13. Exploitation of gear wheels and other heavy-loaded tribosystems (Hertzian
contact) are subjected to model of nano-quantum damping, when one
mechanical quantum is the standard of contact structure and wear.
Author details
Sergey Fedorov
Kaliningrad State Technical University, Kaliningrad, Russia
*Address all correspondence to:
[email protected]
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
60
Structural-Energy Interpretation of the Friction
DOI: http://dx.doi.org/10.5772/intechopen.86123
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friction and friction coefficient in
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62
Chapter 4
Thin Films: Study of the Influence
of the Micro-Abrasive Wear
Modes on the Volume of Wear and
Coefficient of Friction
Ronaldo Câmara Cozza
Abstract
The purpose of this work is to study the influence of the micro-abrasive wear
modes on the behaviors of the volume of wear (V) and of the coefficient of friction (μ)
of thin films submitted to micro-abrasive wear. Experiments were conducted with thin
films of TiN, TiAlN, TiN/TiAlN, TiHfC, ZrN, and TiZrN, using a ball of AISI 52100
steel and abrasive slurries prepared with black silicon carbide (SiC) particles and
glycerine. The results show that the abrasive slurry concentration affected the microabrasive wear modes (“grooving abrasion” or “rolling abrasion”) and, consequently,
the magnitude of the volume of wear and of the coefficient of friction, as described:
(i) a low value of abrasive slurry concentration generated “grooving abrasion,” which
was related to a relatively low volume of wear and high coefficient of friction, and (ii)
a high value of abrasive slurry concentration generated “rolling abrasion,” which was
related to a relatively high volume of wear and low coefficient of friction.
Keywords: micro-abrasive wear, grooving abrasion, rolling abrasion, thin films,
volume of wear, coefficient of friction
1. Introduction
The micro-abrasive wear test by rotating ball (“ball-cratering wear test”) is an
important method adopted to study the micro-abrasive wear behavior of metallic,
polymeric, and ceramic materials. Figure 1 presents a schematic diagram of the
principle of this micro-abrasive wear test, in which a rotating ball is forced against
the tested specimen in the presence of an abrasive slurry, generating, consequently,
the called “wear craters” on the surface of the tested material.
Initially, the development of the ball-cratering wear test aimed to measure
the thickness of thin films (Figure 2a and b) [1], which can be made using the
equations detailed in Ref. [2]. Because of the technical features, this type of microabrasive wear test has been applied to study the tribological behavior of different
materials [3–5], for example, in the analysis of the volume of wear (V), coefficient
of wear (k), and coefficient of friction (μ) of thin films [2, 6–10].
As a function of the abrasive slurry concentration, two micro-abrasive wear
modes can be usually observed on the surface of the worn crater: “grooving abrasion” is observed when the abrasive particles slide on the surface, whereas “rolling abrasion” results from abrasive particles rolling on the specimen’s surface.
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Friction, Lubrication and Wear
Figure 3a [11, 12] and Figure 3b presents, respectively, images of “grooving
abrasion” and “rolling abrasion.”
Many works on coefficient of friction (μ) during abrasive wear and other types
of tests are available in the literature [13–19], but only a few were dedicated to
the coefficient of friction in ball-cratering wear tests [2–4, 10, 11]. In particular,
Shipway [20] has studied the coefficient of friction in terms of the shape and
movement of the abrasive particles, Kusano and Hutchings [21] presented a
theoretical model for coefficient of friction in micro-abrasive wear tests with
“free-ball” equipment configuration, and Cozza et al. [2–4, 11, 22] measured the
tangential force developed during tests conducted in a “fixed ball” equipment
configuration, which allowed direct calculation of the friction coefficient by the
ratio between the tangential and normal forces. Besides, using a proper electronic
instrumentation, Cozza et al. [2, 23–25] have studied and measured the behavior
of the coefficient of friction in thin films in ball-cratering wear tests; however, in
those works [2, 23–25], the test sphere has reached the substrate.
Figure 1.
Micro-abrasive wear test by rotating ball: a representative figure showing the operating principle and the
abrasive particles between the ball and the specimen; “h” is the depth of the wear crater.
Figure 2.
Examples of wear craters generated on coated system: (a) multilayer and (b) thin film of TiN.
64
Thin Films: Study of the Influence of the Micro-Abrasive Wear Modes on the Volume of Wear…
DOI: http://dx.doi.org/10.5772/intechopen.86459
Figure 3.
Micro-abrasive wear modes: (a) “grooving abrasion” [11, 12] and (b) “rolling abrasion.”
Analyzing and studying important researches regarding to tribological behavior
of materials submitted to micro-abrasive wear test conditions [7–9, 26], the purpose
of this work is to report the influence of the micro-abrasive wear modes on the
behaviors of the volume of wear (V) and coefficient of friction (μ) of thin films
submitted to micro-abrasive wear tests by rotating ball.
2. Equipment, materials, and methods
2.1 Ball-cratering wear test equipment
A ball-cratering wear test equipment with free-ball mechanical configuration
(Figure 4 [27]) was used for the micro-abrasive wear tests, which has two load cells:
one load cell to control the “normal force” (N) and one load cell to measure the
“tangential force” (T) that is developed during the experiments. The values of “N”
and “T” are read by a readout system.
65
Friction, Lubrication and Wear
2.2 Materials
Experiments were conducted with thin films of:
• TiN
• TiAlN
• TiN/TiAlN
• TiHfC
• ZrN
• TiZrN
deposited on substrates of cemented carbide. For the counter-body, one ball of
AISI 52100 steel with diameter of D = 25.4 mm was used.
The abrasive material was black silicon carbide (SiC) with an average particle
size of 3 μm; Figure 5 [4] presents a micrograph of the abrasive particles (Figure 5a)
Figure 4.
Ball-cratering micro-abrasive wear test equipment used in this work: free-ball mechanical configuration, able
to acquire, simultaneously, the “normal force N” and the “tangential force T.”
Figure 5.
SiC abrasive [4]: (a) scanning electron micrograph and (b) particle size distribution.
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DOI: http://dx.doi.org/10.5772/intechopen.86459
Normal force [N]
Abrasive slurry concentration (in volume)
Ball rotational speed [rpm]
N
0.4
C1
5% SiC + 95% glycerine
C2
50% SiC + 50% glycerine
n
70
Table 1.
Test parameters selected for the ball-cratering wear experiments.
and the particle size distribution (Figure 5b). The abrasive slurries were prepared
with SiC and glycerine.
2.3 Methods
Table 1 presents the values of the test parameters defined for the micro-abrasive
wear experiments.
The normal force value defined for the wear experiments was N = 0.4 N, combined with two abrasive slurries concentrations (C), C1 = 5% SiC + 95% glycerine
and C2 = 50% SiC + 50% glycerine (volumetric values), with the purpose to produce, respectively, “grooving abrasion” and “rolling abrasion” on the surfaces of the
thin films. The ball rotational speed was set to n = 70 rpm.
All tests were non-perforating, e.g., only the thin films were worn. The normal
force (N) was constant during the tests; the tangential force (T) was monitored and
registered during all experiments.
The volume of wear (V) and the coefficient of friction (μ) were then calculated
using Eqs. (1) [1] and (2), respectively; “d” is the diameter of the wear crater, and
“R” is the radius of the ball:
4
πd , for d < < R
V ≈ ____
64R
T
μ = __
N
(1)
(2)
3. Results and discussion
Figures 6 and 7 show examples of worn surfaces obtained in the experiments;
in all wear craters, the maximum depth (h) observed was, approximately, h ≈ 8 μm.
Figure 6 displays the action of “grooving abrasion,” characteristic of C1 = 5%
67
Friction, Lubrication and Wear
Figure 6.
Occurrence of “grooving abrasion” on the surface of the thin film of TiN.
Figure 7.
Occurrence of “rolling abrasion” on the surface of the thin film of TiN.
SiC + 95% glycerine; Figure 7 displays a wear crater under the action of “rolling
abrasion,” reported for the abrasive slurry concentration C2 = 50% SiC + 50%
glycerine. These results qualitatively agree with the conclusions obtained by
Trezona et al. [28], in which low concentrations of abrasive slurries (<5% in volume
of abrasive material, approximately) favor the occurrence of “grooving abrasion”
and high concentrations of abrasive slurries (>20% in volume of abrasive material,
approximately) favor the action of “rolling abrasion.”
The actions of the micro-abrasive wear modes showed an important influence
on the volume of wear and on the coefficient of friction of the thin films studied in
this research. A significant increase in the volume of abrasive particles from C1 = 5%
SiC + 95% glycerine to C2 = 50% SiC + 50% glycerine (causing, consequently, the
micro-abrasive wear transition from “grooving abrasion” to “rolling abrasion”)
caused an increase in the volume of wear and a decrease in the coefficient of
friction.
Figures 8 and 9 show the behaviors of the volume of wear (V) and coefficient of
friction (μ) as a function of the micro-abrasive wear modes; the maximum errors
observed were V = 0.4 × 10−3 mm3 and μ = 0.1, for the volume of wear and coefficient of friction, respectively.
The values of the volume of wear reported under conditions of “rolling abrasion” (high-abrasive slurry concentration, C2 = 50% SiC + 50% glycerine) were
higher than the values of the volume of wear reported under conditions of “grooving
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Thin Films: Study of the Influence of the Micro-Abrasive Wear Modes on the Volume of Wear…
DOI: http://dx.doi.org/10.5772/intechopen.86459
Figure 8.
Volume of wear (V) as a function of the micro-abrasive wear modes’ “grooving abrasion” and “rolling
abrasion.”
Figure 9.
Coefficient of friction (μ) as a function of the micro-abrasive wear modes’ “grooving abrasion” and “rolling abrasion.”
abrasion” (low-abrasive slurry concentration, C1 = 5% SiC + 95% glycerine), as
reported by Mergler and Huis in ‘t Veld [5] and Trezona et al. [28].
The values of the coefficient of friction reported under “grooving abrasion”
(low-abrasive slurry concentration, C1 = 5% SiC + 95% glycerine) were higher than
the values of the coefficient of friction reported under “rolling abrasion” (highabrasive slurry concentration, C2 = 50% SiC + 50% glycerine), and this behavior
can be explained based on patterns of movements that act on “rolling abrasion” and
“grooving abrasion” micro-abrasive wear modes: in “rolling abrasion,” the abrasive
particles are free to roll between the ball and the specimen, facilitating the relative
movement between these elements and, consequently, decreasing the coefficient
of friction on the tribological system; however, in “grooving abrasion,” the abrasive
particles are fixed on the counter-body (in this case, on the ball), limiting their
movements and requiring higher tangential forces.
4. Conclusions
The results obtained indicated the conclusions:
69
Friction, Lubrication and Wear
1. The concentration of abrasive slurry affected the occurrence of “grooving
abrasion”—under low concentration—or “rolling abrasion,” under high
concentration.
2. The volume of wear increased with the increase of the abrasive slurry
concentration.
3. With the low concentration of abrasive slurry, “grooving abrasion” and,
consequently, high values of coefficient of friction were reported. In this situation, the abrasive particles were incrusted on the counter-body, hindering their
movements and generating high tangential forces.
4. On the other hand, when the high concentration of abrasive slurry was used,
“rolling abrasion” occurred. In this case, the abrasive particles were free to roll
along the surface of the thin film, causing a low coefficient of friction.
Appendix
A list of symbols used in this manuscript is given:
C
abrasive slurry concentration—in volume, [% SiC + % glycerine]
d
diameter of the wear crater, [mm]
D
diameter of the ball, [mm]
h
depth of the wear crater, [μm]
k
coefficient of wear, [mm3/N m]
n
ball rotational speed, [rpm]
N
normal force, [N]
R
radius of the ball, [mm]
T
tangential force, [N]
V
volume of wear, [mm3]
Greek letter
μ
coefficient of friction
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DOI: http://dx.doi.org/10.5772/intechopen.86459
Author details
Ronaldo Câmara Cozza1,2
1 Department of Mechanical Engineering, University Center FEI—Educational
Foundation of Ignatius “Padre Sabóia de Medeiros”, São Bernardo do Campo, SP,
Brazil
2 Department of Mechanical Manufacturing, CEETEPS—State Center of
Technological Education “Paula Souza”, Technology Faculty—FATEC, Mauá, SP,
Brazil
*Address all correspondence to:
[email protected]
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
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Friction, Lubrication and Wear
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Chapter 5
Novel Predictors for Friction and
Wear in Drivetrain Applications
Walter Holweger
Abstract
Reliability in a drivetrain is given by the life of its constituents, e.g., gears,
clutches, and bearings. Lubrication contributes to the life cycle, preventing wear,
friction, and environmental impacts. As lubricants and their additives are chemicals
with an expected reactivity in a tribological contact, it comes to the question how
surface fatigue phenomena due to loading may be influenced by the reactivity of
functional additives and how this might be embedded in construction guidelines. A
very basic study based on an elementary gear test rig presents the result that pitting
life of a gear is substantially influenced by the chemical structure of wearpreventing additives. Even under appropriate loading conditions, the lubricant
structure comes as a life-limiting factor. A molecular model shows how the release
and the approach of the additives toward a surface is essential and related to the
reaction processes that occur during the loading.
Keywords: drivetrain, gears, bearings, reliability, pitting, wear, gray staining,
life cycle, molecular modeling
1. Introduction
Wear is a central topic in tribology. As a system property, it is defined as a
continuous loss of material out of a solid surface, caused by mechanical impact, e.g.,
contact and relative motion of counterpart such as solids, liquids, or gases [1–6].
As such, wear is not a property of a single component. Drivetrain components
(e.g., bearings, gears, clutches, etc.) are constructed due to their life expectation in
order to come to a predictive reliability in the life cycle. However, in reality they are
exposed to wear processes as an incidental or continuous impact. Hence, it is
important to know how the entrance of wear in drivetrain components will
influence their life expectations and the reliability of the drivetrain as such.
Within a construction, the expected life is a function of the load capacity of the
materials, e.g., their fatigue strength with respect to load cycles and pressure.
As reliability is defined yet by the load capacity of the involved materials due to
cyclic stress, the question is about how wear relates to fatigue. In a classical view,
fatigue is a matter related to stress-strain properties due to the elastic plastic
behavior of the load carrying components. If a pressure with no tangential component acts on moving parts, the fatigue phenomena are given by slow changes of the
subsurface microstructure due to phase alterations, migration of interstitial atoms,
and dislocations. As tangential forces due to slip are coming up, the fatigue processes moves up toward the surface. However, fatigue phenomena near the surface
75
Friction, Lubrication and Wear
will bring up the question at which point fatigue crosses wear and vice versa. While
reliability up to now is defined by fatigue properties of the material, the crossing
between fatigue and wear, especially those, induced by lubricants is still not solved.
Within real applications it might be the case that, due to the operating conditions,
fatigue comes to lubricant-induced wear and does not fit with the standard construction guidelines.
We present here a basic study, how fatigue and lubricant-induced wear push
each other in a standard gear and bearing test. It comes up that this stimulation is
due to the basic behavior of lubricant components, e.g., the reactivity of additives
combined with the mechanical loading. As a main and future question of research, it
addresses the need of advanced understanding on a molecular scale (10–9 m),
molecular modeling, and in situ spectrometry to embed them in future construction
guidelines.
2. Gear and bearing life in terms of lubricants
Pitting and gray staining in gears and bearings appear as surface features. In a
worst case, they may promote a decay in life expectation, due to their progression
in time.
Within the traditional view, they are interpreted by the assumption that
loading exceeds the load capacity of the material. Consequently the mating parts
will get in touch and come to rupture. As such, lubricants as separating media are
only seen as a material to avoid this by separating the surfaces due to viscous
effects. However, it is well known that lubricants as a matter of their composition
will influence the surface load capacity as well (see Figure 1) [7, 8] as seen for
gears in FZG standard test conditions, using SAE 4320 case-hardened material
[7–9].
Figure 2 shows the wear rate by the use of different anti-wear and extreme
pressure additives base on the FZG test rig (16) as a function of the pitch line speed:
Same as for gears, bearings are impacted also by wear raising from the composition of a lubricant [10, 11] (see Figure 3), using the Schaeffler FE8 test rig as a
standard (2100 MPa contact pressure, 80 rpm, 80 h, cylindrical roller bearing, SAE
52100, Martensite):
Within the FZG gear test rig [9, 12–17] (DIN ISO 14635), different lubricants
(A, B) differ in wear as a fact of temperature. While oil A shows a decay by raising
the temperature, oil B is opposite (see Figure 4).
As a result of those studies, reaction layers with different thicknesses under
mechanical influence are created. While thick and uncontrolled layers cause early
fatigue and wear, thin oxide layers with a strong bonding to the interface cause no
wear, same as reported earlier [1, 11]. It is of interest to describe these effects with
respect to their chemical structures of the reactive components and how they
undergo a transformation of the tribological contact area by creating those layers.
Structure property relationship would lead to predictors for wear derived from the
chemical structure of a given lubricant.
As a standard the FZG test rig (DIN ISO 14635) as a back-to-back gear test is
used (Figure 5) [7, 18–20]. The gears, type FZG C-PT, are set in a gearbox, fully
lubricated. Cylindrical roller bearings (type NJ406, steel cage) are used for the
pinion shaft 1 and cylindrical roller bearings, type NJ308, for the motor shaft.
Investigations were made on the gears and the cylindrical roller bearings NJ 406.
The test conditions are given in Table 1. The oil temperature is set constant to
90°C and motor speed to 1500 rpm. A running-in period with 1025 N/mm2 is set for
2 h; the test run at 1700 N/mm2 till pitting is reached is recorded. The speed at the
76
Novel Predictors for Friction and Wear in Drivetrain Applications
DOI: http://dx.doi.org/10.5772/intechopen.85060
Figure 1.
The influence of different oils and additives on gear load cycles referring to the FZG test (DIN ISO 14635) [9].
Figure 2.
Wear rate of lubricants as a function of pitch line speed.
Figure 3.
Wear rate (roller) at a cylindrical roller bearing (CRB) from the Schaeffler test rig FE8 (DIN 51819) as a
function of lubricants. While oil 1 and oil 3 do not show any wear, oil 2 is high in wear.
77
Friction, Lubrication and Wear
Figure 4.
Influence on wear due to temperature.
Figure 5.
FZG test rig (DIN ISO 14635).
Table 1.
Conditions of the test.
pinion is set to 2250 rpm, the torque moment T1 to 372.6 Nm. The tangential speed
at the pinion is calculated to 2.42 m/s, at the wheel to 3.87 m/s, the sliding speed at
the pinion to 1.45 m/s (reflecting the negative slip), the sliding speed at the wheel
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Novel Predictors for Friction and Wear in Drivetrain Applications
DOI: http://dx.doi.org/10.5772/intechopen.85060
to 1.45 m/s, and the sum of speed to 6.29 m/s. As the slip percentage is given by the
ratio of sliding speed to the sum of the speed, the slip at the pinion is 23% and at
the wheel +23%.
The material of the gears applies for a case-hardener SAE 4320.
The test specific data of the CRB NJ206 are given in Table 2.
The material of the bearing accords to the SAE 52100, martensitic hardening,
tempered at 180°C, 2 hours, with 10–12% retained austenite.
Two lubricants were tested (Table 3). Lubricant 1 reflects a standard technology, using zincdithiophosphates (C4ZndtP) as a sulfur-phosphorus carrier.
As a representative of a new ashless additive technology, the lubricant formulation 2
(C4NdtP) is used. The Poly-α-olefine viscosity is 46 mm2/s at 40°C.
The organic chain length of the phosphorus-sulfur core is given by four C atoms,
meaning that during the synthesis of the additives, a C4 (butyl) alcohol component
was used.
The structure of the additives are shown in Figures 6 and 7, both looking rather
complex. In detail a core of sulfur, phosphorus, and zinc is attached to the carbon
sites, containing four C atoms (ZndtPC4) (Figure 6).
Figure 7 represents the C4NdtP; two structures are held together by an ionic
bonding: a sulfur-phosphorus component with two carbon sites, each containing
four C atoms and their attached hydrogen and nitrogen component with a positively charged nitrogen at the edge, attached to a carbon site with eight C atoms
(C4NdtP). The principal of this substance is similar to ionic liquids, where
opposite-charged atoms create an ionic binding, while the carbon sites are responsible for the liquid structure.
The test runs by the use of the different additives are given in Table 4 for both
gears and bearings (NJ406) as a function of the load cycles. Clearly the table shows
how the change in the chemical structure of the additive, despite the same chain
lengths on the carbon edge (C4), end up in different load cycles (Table 4):
Table 2.
Data from the CRB NJ206 bearing.
Table 3.
Lubricants used for the test.
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Friction, Lubrication and Wear
Figure 6.
Zincalkyldithiophosphate (C4ZndtP).
Figure 7.
Ammoniumdithiophosphate (C4NdtP) as an ionic liquid-like structure.
Table 4.
Test conditions set on the different additive structures.
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3. Results for the gear
While the C4-Zincalkyldithiophosphate (C4ZndtP) causes pitting and does not
meet the expected load cycles, the test carried out with the C4NdtP was out of
failure [7]. Secondary neutral mass spectrometry (SNMS) profiles [21–23] were
carried out at the pinion addendum (Position 1: see arrow in Figure 8) (area of
positive slip referring to the pinion), the pitch line (Position 2: see arrow in Figure 8)
(zero slip referring to the pinion), and tooth dedendum (Position 3: see arrow in
Figure 8) (area of negative slip) in order to evaluate how the reaction rate of
additives might depend on load cycles. The nature of the reaction was analyzed by
secondary neutral mass spectrometry (SNMS). While secondary ion mass spectrometry (SIMS) is sensitive due to the local elements, specifically oxygen, SNMS is
less sensitive and allows to track elements quantitatively as depth profiles from the
top of the surface down to a few microns. The spatial resolution is around 4 mm2,
thus averaging local deviations in elements making the results more accurate.
The relevant depth profiles were taken at the dedendum of the pinion tooth
flank for the additives C4-zincalkyldithiophosphate (C4ZndtP) and C4-aminealkyldithiophosphate (C4NdtP) with respect to load cycles are shown in Figure 9
(C4ZndtP: 9 106 load cycles); Figure 10 (C4ZndtP: 10 1010 load cycles);
Figure 11 (C4NdtP: 12 106 load cycles); and Figure 12 (C4ZndtP: 16 1010
load cycles).
Figure 8.
Gear tooth segment with addendum Position 1 (pitch line), Position 2, and Position 3 as dedendum.
Figure 9.
SNMS depth profile: C4ZndtP in FZG pitting test at 9 106 load cycles.
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Friction, Lubrication and Wear
Figure 10.
SNMS depth profile: C4ZndtP in FZG pitting test at 10 106 load cycles.
Figure 11.
SNMS depth profile: C4NdtP in FZG pitting test at 12 106 load cycles.
Figure 12.
SNMS depth profile: C4NdtP in FZG pitting test at 16 106 load cycles.
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As a result from A1–A2, C4ZndTP causes pitting and increases in layer thickness
formation, while B1–B2 C4NdtP does not at prolong load cycles however shows an
increase in surface reaction of the phosphorus component while the reaction layer
stays constant.
4. Results for the bearing (NJ406)
The calculation of the load distribution is shown in Table 5 and Figure 13.
The maximum force is acting on roller nr. 7 with a contact pressure of
1481 N/mm2 [7].
The results (see Figures 14 and 15) show an impact of zinc, assumed to be a
mixture of phosphates and zinc oxide in the case of the C4ZndtP at 19 106 load
cycles (Figure 14), while compared with the oxygen in the case of the C4NdtP stays
low (Figure 15).
The bearing thus gives a different reaction by embedding zinc oxide in the
near surface. The results for the C4NdtP are quite similar to the reactions seen in
the gear.
Table 5.
Conditions at the bearing NJ406.
Figure 13.
Load distribution for the NJ406 bearing.
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Friction, Lubrication and Wear
Figure 14.
SNMS depth profile: rollers, C4ZndtP in FE8 bearing test at 19 106 load cycles.
Figure 15.
SNMS depth profile: C4NdtP in the FE8 wear test, rollers at 29 106 load cycles.
5. Gear: reaction rates
For the gear (pinion, dedendum) the reaction turnover stays constant or slightly
decreases for the C4ZndtP (Figure 16) but increases in depth by the use of C4NdTP
(Figure 17).
The reaction film thickness shows a progression in the case for the C4ZndtP
(Figure 18), while the C4NdtP shows a regression in time (Figure 19).
6. Gear: nanohardness measurement at the pinion
Nanohardness measurements are shown in Figures 20–22: Figure 20 shows the
as-received hardness profile of the dedendum, pitch, and addendum for the asreceived pinion tooth flank material (case-hardener SAE 4320).
Figure 21 shows a steep decrease by the use of the C4ZndtP compared to the asreceived material at the surface.
Figure 22 shows a steep increase by the use of C4NdtP compared to the asreceived material at the surface.
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DOI: http://dx.doi.org/10.5772/intechopen.85060
Figure 16.
SNMS profiles: reaction rate (elements phosphorus and oxygen) in the FZG gear tests for C4ZndtP as a function
of load cycles.
Figure 17.
SNMS profiles: reaction rate (elements phosphorus and oxygen) in the FZG gear test for C4NdtP as a function
of load cycles.
Figure 18.
C4ZndtP: process of film thickness formation as a matter of load cycles.
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Friction, Lubrication and Wear
Figure 19.
C4NdtP: process of film thickness formation as a matter of load cycles.
Figure 20.
Nanohardness measurements for the as-received pinion (from dedendum via pitch to the addendum).
Figure 21.
C4ZndtP: pinion tooth nanohardness as a function of depth (nanometer) and location (dedendum, pitch, and
addendum).
7. Molecular description
As functional groups in additives determine the reliability of drivetrain components, it is of interest how those processes are to interpret. Coming from the
molecular perspective with a size of 10–9 m, it takes effort to interpret effects
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Novel Predictors for Friction and Wear in Drivetrain Applications
DOI: http://dx.doi.org/10.5772/intechopen.85060
Figure 22.
C4NdtP: pinion tooth nanohardness as a function of depth (nanometer) and location (dedendum, pitch, and
addendum).
on 10–9 till 10–3 m, e.g., magnitudes of 106 in length scale. However, considerable
progress in multi-scale modeling has become real in the last years; it is of interest
how to predict the observed effects reported here by the use of predictors. Basically
predicators are obtained by the properties of a molecule, e.g., coming from the
chemical bonding. Exploring molecules by quantitative structure property relationship (QSPR) [24] and the molecular properties by the use of density functional
theory (DFT) is a standard [25]. The interaction of molecules with themselves and
with surfaces is part of molecular dynamics and ab initio methods.
Figure 24A and B shows the surface of the additive C4ZndtP with one molecule
PAO (as a hydrogenated Di-Dec-1-ene, C20H42) (A) and the additive C4NdtP with
one molecule PAO (as a hydrogenated Di-Dec-1-ene, C20H42) (B) energy minimized by the use of molecular dynamics.
Figure 24A shows the surface of the additive C4ZndtP with one molecule PAO
(as a hydrogenated Di-Dec-1-ene, C20H42) and the additive C4NdtP with one molecule PAO (as a hydrogenated Di-Dec-1-ene, C20H42) (B) attached to an ideal bodycentered cubic (bcc) iron surface as C for the C4ZndtP and D for the C4NdtP,
energy minimized by the use of molecular dynamics.
Figure 23.
(A) C4ZndtP structure in PAO and (B) C4NdtP structure in PAO.
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Friction, Lubrication and Wear
Figure 24.
(A) Approaching a (A) C4ZndtP and (B) C4NdtP to an ideal bcc, iron surface. Labeled atoms are: red: iron;
dark red: oxygen; blue: carbon; gray: hydrogen; and yellow: sulfur.
Figure 23B shows the surface of the additive C4ZndtP with one molecule PAO
(as a hydrogenated Di-Dec-1-ene, C20H42), and the additive C4NdtP with one
molecule PAO (as a hydrogenated Di-Dec-1-ene, C20H42) (B) attached to an ideal
body-centered cubic (bcc) iron surface as C for the C4ZndtP and D for the C4NdtP,
energy minimized by the use of molecular dynamics. Approaching this system to an
ideal iron surface, it is obvious that the C4Zn is attached with the polar edge (Zn, P, S)
to the surface (see Figure 24A), while the C4NdtP is attached via the carbon shell
(see Figure 24B).
8. Discussion
The results shown here may give a reasoning about the elementary analyses
found by SNMS where the C4ZndtP progressively acts in time by increasing the
reaction layers toward 50 nm constituted by P, O, and Zn oxides, while the C4NdtP
shows an initial reaction in the beginning, but regressing the layer to a constant film
at 10 nm [26].
As for the C4ZndtP, the reactive core is near to the surface; the reaction may
proceed by continuous load cycling, which is found in the SNMS profiles. Due to the
continuous degression of the surface toward oxides, the C4ZndtP shows a decrease
in the nanohardness by the fact that the surface gets covered with material softer
than the base. Also the reaction rate goes down due to fact that the reaction layers
are chemically inert compared to iron. The remote position of the reactive group in
the C4NdtP exposes the sulfur-phosphorus core to the environment as oxygen.
Tribological impacting may then promote the oxidation of the reactive site, rather
than a reaction with the metal surface. This means that in the first step the C4NdtP
reacts with oxygen at the reactive site, coming to phosphoric acid specie. Those
would turn to the surface as they are not soluble in the base oil and naturally get
attracted by the oxide sites at the metal surface. The amine would be dissolved back
into the base oil. As a fact those phosphoric acid specie are found to be detached on
the surface of the pinion dedendum. The oxidation will continue; hence, it is
expected that the phosphorus-oxide layer will increase on top, but no material will
be leached out due to the fact that the phosphates and polyphosphates are uniquely
covering the surface, not being soluble in the matrix.
While the C4ZndtP obviously causes a successive exchange of near-surface
material (e.g., iron), the C4NdtP does not. The hardness profiles might be coherent
with the carbon profile (SNMS): while the C4ZndtP converts constantly the surface
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material by smooth oxides, the C4NdtP creates a thin phosphorus-oxide layer on
top on a size of 10 nm. The carbon site exposed to the metal might protect it against
oxidation, and as the reactive phosphorus-sulfur site is remote, the hardness at least
does not go down. The steep increase could be caused by a hardening process of the
surface due to carbide formation at the interface as a degradation process of the
carbon site. It is noteworthy to say that this interpretation is related to the positions
of negative slip and speculative.
Hence, the structure of an additive determines how it approaches and how the
subsequent reactions take place, either on the site of the functional head or on the
site of the carbon, ending up in the reliability of the application with respect to
pitting.
9. Conclusions
The reliability of drivetrain with respect to its expected life cycle is of key
interest in the value chain of an installation. Each component contributes to this by
the matter of load impacting the load capacity of the materials involved. As load
capacity is well defined for the construction materials, e.g., gears and bearings, this
definition becomes vague for lubricants. Even though a malfunction of a lubricant
could cause damage features, like wear, friction, and tribocorrosion, the understanding of the real function and how to judge it by robust predictors is still missing.
Lubricants may give malfunction even in the case of a proper application due to the
interaction of functional additives with the mating surfaces. Plenty of contributions
worldwide show that the “construction” of a lubricant by adding functional additives into a base oil may lead to premature failures given by the interaction of the
functional additives with the given surface. Normally additives are readily dissolved
in a base oil and as such transported to the points of interacting surfaces, there
getting released in order to uptake a function like wear prevention or friction
reduction. However, the energy offered by the contact due to sliding and contact
pressure makes additives reactive, causing chemical reactions. The chemical reactions with different additives are seen by the use of specific test conditions,
presented in the study as an FZG back-to-back gear test rig. The study brings out
that a traditional anti-wear additive such as a zincdithiophosphate (C4ZndtP)
reacts continuously at a given threshold with the surface, exchanging the nearsurface material. The softening causes continuously material loss over time, ending
up in pitting. In contrast, just by changing the chemical structure from a
zincdithiophosphate to an ionic liquid like amine-neutralized dithiophosphate
(C4NdtP); it is obvious that the application fulfills the complete life cycle without
pitting. Compared to the zincdithiophosphate (C4ZndtP), it comes out that the
amine-neutralized dithiophosphate (C4NdtP) hardens up at the area of negative
slip at the pinion dedendum. Technical data are not to explain this elementary topic.
Hence, it has to be seen in a deeper aspect. As additives are dissolved readily in the
base oil, the tribological process makes them approach the surface. This brings up
the question how the additive is released from the base oil toward the surface as the
initial step. In the given example, a simple molecular model shows that in the case of
the zincdithiophosphate, the additive approaches the surface with the reactive site
given by the sulfur and phosphorus core, continuously leaching iron out of the
surface with a subsequent weakening created by reaction layers with little binding
to the core of the material. In the case of ammonium-neutralized dithiophosphate,
the molecular model shows that this additive approaches the surface by the carbon
site, while the sulfur-phosphorus site is remote. This additive gives a hardness
increase during the tribological interaction, and as a speculation, the tribological
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energy may crack the molecule to carbon specie, subsequently hardening the surface up by carbides and preventing an excessive penetration of reaction products.
10. Summary
Additives are part of a drivetrain reliability. It comes clearly that within a
construction, the tribological energy offered by the kinematics, the surrounding
temperature and environment plus the material involved, has to be judged in terms
of the structure of lubricants in the molecular level and how those structures
compete with the offer of tribological energy.
Starting from a very basic and standard molecular model, it is essential to
understand how additives dissolve in a base oil and how they get released and
redissolved at a tribological contact area. Even though how additives act toward a
surface might be a minor question, it turns out to be very essential and at least the
limiting factor of an application reliability if the criticality of those processes are
unknown and might pop up in a given application as premature failure.
Abbreviations
C4ZndtP
C4NdtP
FZG
FE8
PAO
SNMS
CRB
bcc
MPa
isobutyl-zincdithiophosphate
isobutyl-dithiophosphoric acid reacted with an alkylamine
gear test rig (DIN ISO 14635)
bearing test rig (DIN 51819)
poly-α-olefine as a hydrogenated poly-dec-1-ene
secondary neutral mass spectrometry
cylindrical roller bearing
body-centered cubic
megapascal (106 Pa)
Author details
Walter Holweger1,2
1 Technological Consultant Agency, Epfendorf, Germany
2 Schaeffler Technologies AG & Co. KG, Herzogenaurach, Germany
*Address all correspondence to:
[email protected]
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
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DOI: http://dx.doi.org/10.5772/intechopen.85060
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Chapter 6
Tribological and Wear Behavior
of Metal Alloys Produced by Laser
Powder Bed Fusion (LPBF)
Massimo Lorusso
Abstract
Laser powder bed fusion (LPBF) is an additive manufacturing technique for
the production of parts with complex geometry, and it is especially appropriate
for structural applications in aircraft and automotive industries. Wear is the most
important cause of malfunction of mechanical systems. Abrasive wear accounts
for 50% of wear in industrial situations, and it is most common in components of
machines. LPBF is very attractive due to its extremely high melting and solidification rates that make possible to obtain materials with particular tribological and
wear behavior than those by traditional manufacturing routes. The aim of this
chapter is to investigate the different behaviors of principal metallic alloys by LPBF.
Keywords: additive manufacturing (AM), laser powder bed fusion (LPBF),
metallic alloys, wear
1. Introduction
According to ASTM F2792-10, additive manufacturing (AM) is defined as “The
process of joining materials to make objects from 3D model data, usually layer upon
layer, as opposed to subtractive manufacturing technologies.” The fundamental principle of AM is that a geometric representation, originally generated using 3D-CAD
system, can be manufactured directly without a need to process planning [1].
Today AM is receiving a very high attention from the mainstream media,
investment community, national governments, and scientific communities. Nearly
10 years ago (2008), only 231 articles were published with AM topic, 5 years ago
(2013) about 800 articles, and in 2018 about 4900 articles; in 10 years the number
of articles per year is increased more than 20 times (Figure 1).
AM technologies have a strong potential to change the characteristic of manufacturing process, away from mass production in large factories with dedicated tooling
and with high costs, to a world of mass customization and distributed manufacture.
Everyday new and innovative applications are emerging for the additive
manufacturing [2]:
• Prototyping
• Art and jewelry
• Tooling
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Friction, Lubrication and Wear
Figure 1.
Number of scientific articles per years with AM topic (source: Scopus).
• Medical and dental
• Automotive
• Aerospace
In many application of the AM, the wear resistance is important to guarantee
the efficacy and the safety. Wear is the most important cause of malfunction of
mechanical systems; for this reason, it is important to study the effect of wear and
generally, the tribological characteristic of material used and processed by AM [3].
The aim of this chapter is to investigate the different behaviors of principal
metallic alloys processed by laser powder bed fusion (one of the most diffused AM
technologies) in terms of tribological properties, with a particular focus on the
wear resistance and the coefficient of friction (COF). At the moment, few studies
are available about tribological properties of metallic alloys produced by LPBF; this
chapter searches to organize the works present.
2. Additive manufacturing
2.1 Introduction
Seven different technologies are classified for additive manufacturing agreed by
the AM SIG (special interest group) as can be seen in detail in Table 1 [4].
2.2 Laser powder bed fusion (LPBF)
The SLM process has been defined as the laser powder bed fusion process
(LPBF), according to ISO/ASTM 52900. It is also known by the trade names
LaserCUSING or DMLS (Direct Metal Laser Sintering), which directly produces
homogenous metal objects, layer by layer, from 3D CAD data, by selectively melting
very fine layers of metal powder (Figure 2) with a laser beam.
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DOI: http://dx.doi.org/10.5772/intechopen.85167
Classification
Description
Technology
Materials
Direct energy
deposition
Builds parts using focused
thermal energy and wire to
fuse materials and they are
deposited on a substrate
Laser deposition
Laser consolidation
Direct metal
deposition
Electron beam direct
melting
Metals
Binder jetting
Creates objects by deposition
of a binding agent to join
powdered material
3D printing
Ink-jetting
S-print
M-print
Metals,
polymers, and
ceramics
Material extrusion
Fused deposition modeling
Fused deposition
modeling
Polymers
Material jetting
Builds parts by depositing
small droplets of build
material, which are then
cured by exposure to light
Polyjet
Ink-jetting
Thermojet
Photopolymers,
wax
Powder bed fusion
Creates objects by using
thermal energy to fuse regions
of a powder bed
Selective laser melting
Laser powder bed
fusion
Selective laser
sintering
Electron beam melting
Metals,
polymers, and
ceramics
Sheet lamination
Builds parts by trimming
sheets of material and binding
them together in layers
Ultrasonic
consolidation
Laminated object
manufacturing
Metals,
ceramics, and
hybrids
VAT
photopolymerization
Builds parts by using a vat of
liquid photopolymer resin,
out of which the model is
constructed layer by layer. An
ultraviolet (UV) light is used
to cure or harden the resin
where required.
Stereolithography
Digital light
processing
Photopolymers
and ceramics
Table 1.
Classification of AM adapted from ASTM AM classification.
Figure 2.
Scanning electron magnification (SEM) observation of typical powder used in LPBF process (AlSi10Mg).
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Friction, Lubrication and Wear
Laser powder bed fusion (LPBF) is an additive manufacturing technique for
the fabrication of near net-shape parts directly from computer-aided design data
by melting together different layers with the help of a laser source. LPBF process
produces parts with good surface quality, high accuracy and detail resolution,
and excellent mechanical properties. The components are built layer by layer; it is
possible to project internal channel and features that are impossible to obtain by
casting or machining. LPBF does not require special tooling like casting, so it is
more convenient for not so big production. It is a good alternative to conventional
machining for complex metallic parts [5].
It has been demonstrated, in recent literature, that SLM can also be used to
fabricate metal matrix composites (MMCs). These could have applications in
automotive and aerospace industries, where it is necessary to improve mechanical
properties (stiffness and hardness) and specially the wear resistance [6].
3. Aluminum alloys
3.1 Introduction
The most used Al alloys are Al-Si alloys, which represent 80% of aluminum casting alloys, thanks to their high fluidity, high weldability, good corrosion resistance,
and low coefficient of thermal expansion. The binary Al-Si system is a eutectic alloy
when the amount of Si is 11–13 wt%, a hypoeutectic alloy when Si is less than 11 wt%,
and a hypereutectic alloy when Si is more than 13 wt%. The strengthening of these
alloys is generally possible, through the addition of other alloying elements such as
Cu and Mg that make the Al-Si alloys hardenable either by means of a heat treatment. There is a large demand for Al-Si-Mg alloys for different applications, such as
the aerospace industry, and for automotive and heat exchangers, due to their high
mechanical properties, like strength and hardness, in the heat-treated state [7–9].
The most popular Al-Si alloy processed by LPBF is AlSi10Mg alloy (similar to A360).
Other Al-Si alloys by LPBF are AlSi7Mg (called also A357) [10–11] and AlSi12Mg [12].
Despite this growing interest in the AM processability of Al-Mg-Zn-Cu alloys,
to date, few studies are available on the AM process of high mechanical properties’
(harness and strength) aluminum alloys. It is well-known that the alloys belonging
to the Al-Mg-Zn-Cu alloys are appropriate for different applications in aerospace as
they are characterized by toughness and high strength reached mainly through the
precipitation of the MgZn2 phase. These alloys are not well weldable because they
suffer strongly from liquation cracking [13–14].
3.2 AlSi10Mg
In the literature, it is demonstrated that AlSi10Mg alloy produced by casting has
a coefficient of friction (against a WC cemented with CO pin) lower than AlSi10Mg
alloy by LPBF since their microstructure and hardness are different. The typical
microstructure of metallic alloys by LPBF without heat treatments is characterized
of a small grain size. At higher magnification after hatching, it can be seen as a fine
cellular-dendritic structure made by agglomerates of grains with mean diameters of
a hundred of nanometers or less. It is generally observed that materials with large
grains have a COF lower than materials with a fine microstructure; this is one of the
most important reasons of higher COF of AlSi10Mg by LPBF [15].
The different sizes of microstructure influence the hardness very strong. The
hardness is higher for the finer grain size. As suggested by the theoretical considerations, the material with the highest hardness has the highest wear resistance. The
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difference between the wear resistance of the AlSi10Mg alloy produced by casting
and by LPBF is immediately evident. During pin on disc test, the volume per meter
loss of the AlSi10Mg produced by LPBF is 35% less than the volume per meter loss of
the AlSi10Mg produced by casting.
3.3 Other aluminum alloys
In general, for the conventional casted alloys, the Al-Si alloys with small primary
silicon phase present a higher wear resistance than that of the alloys with large silicon phase, due to their high surface-volume fraction. The aluminum alloys by LPBF
show the inverse results that could be attributed to their ultrafine microstructure.
During the wear process, the fine primary silicon particles form a full contacted
wear layer; the primary silicon is directly pressed into Al-matrix and then forms the
full contacted wear layer [7]. For this reason alloys with small primary silicon have a
relative poor wear resistance. The A357 aluminum alloy has less silicon (6.5–7.56%)
than AlSi10Mg (9–11%) but higher COF and wear [16].
For the Al-Zn-Mg alloys, the microstructure has a strong influence on the wear
behavior that is due to higher content and the higher amount of MgZn2 precipitate that
is harder than α-aluminum matrix and helps to protect the surface of material [13].
3.4 Aluminum matrix composites (AMCs)
Aluminum matrix composites (AMCs) have generally excellent mechanical
properties such as improved stiffness, strength, and hardness when compared with
the aluminum matrix. AMCs attract much attention because they are characterized by low density and high specific strength and good tribology properties. The
limits of this material are the high difficulty in the process of production and in the
post-processing phases. The principal problem when a ceramic is used as reinforcement is the clustering and agglomeration caused by the poor wettability and a large
surface-to-volume ratio that does not promote a homogenous dispersion.
The LPBF process seems to be particularly suitable for the production of AMCs
because near net-shape complex components can be made, which reduces the postprocessing phases. The most used ceramic reinforcements in AMCs produced by
LBPF are magnesium spinel (MgAl2O4) and titanium diboride (TiB2) [15].
The sufficiently high densification rate combined with the homogeneous incorporation of nanoscale TiC reinforcement throughout the matrix led to the considerably low coefficient of friction (COF) and resultant wear rate [17].
Figure 3.
Example of detached particles that have an effect of solid lubrication (third part).
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Friction, Lubrication and Wear
The presence of reinforcements causes a reduction of COF. If the reinforcements have a micro-size, the effect is bigger than with nano-sized reinforcement.
The reduction of COF is probably due to the detachment from the aluminum
matrix of micro- or nanoparticles of ceramic reinforcements that can act as a third
body (Figure 3).
4. Nickel alloys
4.1 Introduction
The most used nickel alloys produced through LPBF for their high weldability
are Inconel 718 and 625. Inconel 718 and 625 have been used in high-temperature
applications, such as nuclear reactors, pumps, molds, and gas-turbine engine
aircraft. These nickel alloys are endowed with high-temperature strength, high
creep, and oxidation resistance. These two alloys can be used depending on the
applications, but the production of objects with a complex shape is expensive with
conventional manufacturing technologies. Therefore, the ability to produce complex components without using molds makes LPBF process particularly interesting.
The microstructure created during LPBF process are out-of-equilibrium, and it is
necessary to perform some heat treatments in order to homogenize the microstructural features. Depending to application it would be necessary to carry out a simple
stress relieving to reduce residual stress induced by thermal gradients during LPBF
process. As for other applications, annealing or solution treatment to allow the
grain recrystallization and growth, thus improving the creep resistance, is typically
requested [18–21].
4.2 Inconel
Inconel 625 is a nickel-chromium alloy designed as solid-solution-strengthened.
The heat treatments favor the formation of metastable Ƴ” phase that further
improves the mechanical properties. Inconel 625 thanks to higher concentration of
Cr and Mo with respect to Inconel 718 has higher corrosion resistance.
Inconel 718 is an age-hardenable nickel-chromium alloy mainly due to the
presence of aluminum, titanium, and niobium that leads to precipitation of gamma
prime Ƴ’ Ni3(Al,Ti) phase and metastable gamma double prime Ƴ” Ni3Nb phase
[18]. Inconel by LPBF is more difficult to be machined than the same materials produced by extruding or rolling processes. During milling process of Inconel by LPBF,
the cutting speed and chip load are lower due the presence of hard precipitated
particles. In general, the Inconel produce by LPBF exhibited relatively good wear
performance. Such microstructures indicated that the presence of severe adhesive
wear in turn resulted a relatively higher wear rate. The clustered Ƴ dendrites gave
rise to the fluctuations of COF. The formed protective adherent tribolayer on worn
surfaces made considerable contributions to the further improved wear performance of LPBF-produced parts. The combined influence of elevated microhardness
and the formation of adherent tribolayer contributed to the improvement of wear
performance [20].
Different studies, in particular about Inconel 718, show that addition of tungsten carbide (WC) or titanium carbide (TiC) particles significantly increased the
hardness, friction resistance, and wear performance. The composite acquired a
considerably low COF. The existence of a gradient interface has a very important
role in improving the wear performance of LPBF-processed WC/Inconel 718 and
TiC/Inconel 718 composites [22].
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5. Titanium
5.1 Introduction
Titanium and its alloys have good mechanical properties, good corrosion resistance, and excellent biocompatibility. These alloys are the most interesting metallic
biomaterials for orthopedic and dental implants. Until few years ago, titanium processing via AM technologies was given little consideration by the medical industry
due to the high cost of production. However, in recent years, AM metal technologies
are becoming popular in biomedical field because of the ability to build metals with
customized porous architectures and shape. The titanium alloy Ti6Al4V (the most
popular titanium alloy) has been widely used in various industrial applications due
to its mechanical and physical properties. Beyond the biomedical field, Ti6Al4V
has been commonly employed in producing aircraft engine airframe parts owing
to its high strength to mass ratio and good performance at high temperature (up to
400–500°C) [23–24].
5.2 Ti6Al4V
Ti6Al4V has very good mechanical properties, but it has also been reported to
exhibit poor tribology properties, such as a high COF and low wear resistance. The
poor tribological property of Ti6Al4V is attributable to its low resistance to plastic
shearing, low work hardening, and the low protection afforded by surface oxidation. No significant differences are present between TI6Al4V produced by the different processing technologies. Generally on Ti6Al4V produced by LPBF, less oxidized
areas are found during the wear tests [25].
During the LPBF process, the high cooling rate of laser melting leads to higher
amount of α and α’ harder phases on Ti6Al4V alloy than the traditional process. The
presence of harder microstructural constituents on Ti6Al4V produced by LPBF leads
to a higher wear resistance. The heat-treatment Ti6Al4V generates a protective tribolayer containing oxygen without plastic deformation in the bulk material, which has
the lowest wear rate [26].
Investigation of reinforced Ti6Al4V with TiB2 shows that nano-sized TiB whiskers are formed by the in situ reaction between Ti and TiB2. The interface between
matrix and TiB is a very strong interface bonding. During the wear test, this avoids
the possibility of easy detachment of TiB whiskers. This reduces the wear rate
significantly but not the COF, because the detached particles are few and it is not
present enough third part that reduces significantly the friction [27].
6. Stainless steel (316L)
The 316L austenitic stainless steel has numerous application in different fields
for its high resistance at oxidation and corrosion. The most popular applications
are in marine, nuclear, oil and gas, and biomedical industry. 316L austenitic stainless steel which comprises iron alloyed with chromium of mass fraction up to 18%,
nickel up to 14%, molybdenum up to 3% , manganese down 2%, silicon down
0.75%, copper down 0.5% and carbon down 0.03% along with minor elements [28].
During wear test on 316L stainless steel produced by LPBF, the passive layer
made by chromium and nickel oxidation is removed and leaves iron exposed to the
air, which easily gets oxidized especially at high temperature. Regarding the wear
mechanisms, the worn surfaces of 316L stainless steel exhibited plastic deformation
due to adhesive wear as well as grooves aligned along the sliding direction due to the
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Friction, Lubrication and Wear
abrasive wear. The wear rate and the friction of 316L stainless steel by LPBF were
lower than the 316L traditionally processed; the LPBF-processed steel has a very
fine austenite grains, the size of which was much smaller than in the traditionalprocessed 316L stainless steel. These fine grains in the 316L stainless steel by LPBF
increase the wear resistance, and the surface is subjected to slight plastic deformation
[29–30].
Investigation of the wear resistance of reinforced 316L stainless steel (with
TiB2 or TiC) shows that the wear resistance increases with the increasing TiB2
content due to combined effects of grain refinement and grain-boundary
strengthening [31].
7. Lubrication condition and heat treatment
Metallic alloys by LPBF have generally pores and cracks that influence the wear
under lubricated condition. Few studies are available in literature under boundary
lubrication regime.
In those studies [26, 30], when a lubricating film is not yet formed, the metal
alloys by LPBF have better wear performance than metal alloys by traditional
processes.
Surface pores may positively influence the formation of the lubricating film.
The effect of lubricant is critical in reducing friction and wear. The choice of
oil needs to be carefully considered before applying LPBF process to hydraulic
components.
In general, heat treatment (used to reduce the stress in material after LPBF process) reduces the wear resistance of metallic alloys. The wear resistance is reduced
because the heat treatment changes the microstructure of metallic alloys by LPBF
and lost the very fine microstructure. The most sensibility materials at heat treatment are aluminum alloys [15, 32]. The only metallic alloy that increases the wear
resistance and reduces COF after heat treatments is Ti6Al4V because the oxidation
of surface (if the heat treatment is realized in the presence of oxygen) produces a
protective tribo-oxide layer [26].
8. Conclusions
In conclusion, metallic alloys by LPBF generally have higher wear resistance and
less COF than metallic alloys produced by traditional processes under dry condition
and boundary lubrication mainly due to the fine grains and high hardness.
The LPBF processing parameters are fundamental for wear rate since a fully
densified part usually has high wear resistance and COF.
The existence of pores reduces the bonding between molten pools, resulting in cracks. These cracks can further cause material shell off which greatly
increases wear.
In general, the metallic alloys produced by LPBF are more difficult to machine
than the same metallic alloys produced by traditional processes. For this, it is
important to reduce at the minimum the post-process machining.
The presence of ceramic particle reinforcements in MMCs causes generally a
reduction of COF; this effect is due to the detachment from the metallic matrix
of ceramic particles that can act as a third body. The interfacial bond between the
matrix and the reinforcements has a fundamental role in wear process; a strong
interfacial bond guaranties a low wear rate; a weak interfacial bond causes a low
COF and sometimes high wear rate.
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Tribological and Wear Behavior of Metal Alloys Produced by Laser Powder Bed Fusion (LPBF)
DOI: http://dx.doi.org/10.5772/intechopen.85167
The heat treatment in general reduces the wear resistance and increases the COF.
Acknowledgements
The author is grateful for the moral and scientific support of PhD Diego
Manfredi, PhD Flaviana Calignano, and Professor Matteo Pavese.
Author details
Massimo Lorusso
Istituto Italiano di Tecnologia (IIT), Torino, Italy
*Address all correspondence to:
[email protected]
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
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Friction, Lubrication and Wear
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Chapter 7
Tribological Characteristics
of Smart Materials (MagnetoRheological Fluids and
Elastomers) and Their
Applications
Peng Zhang, Chenglong Lian, Kwang-Hee Lee
and Chul-Hee Lee
Abstract
Magneto-rheological fluids (MRFs) and magneto-rheological elastomers
(MREs), as smart materials, have been widely studied in various engineering fields
to address vibration issues because the mechanical properties are controllable under
the strength of a magnetic field. Their tribological characteristics are also important
to be evaluated, as applications using MRFs and MREs contain various contact
interfaces under reciprocating and rotating working conditions. The performance
and durability of these materials are related to their tribological characteristics.
Therefore, various working conditions and environmental conditions are taken into
consideration, and their tribological characteristics are experimentally examined.
In addition, applications using MRFs and MREs are introduced, and the tribological
performances of these materials are evaluated.
Keywords: tribology, magneto-rheological fluid, magneto-rheological elastomer,
smart material, friction control
1. Introduction
Magneto-rheological fluids (MRFs) and magneto-rheological elastomers
(MREs) have been extensively studied to solve vibration problems in various engineering fields. They have one or more attributes that can be significantly changed
in a controlled way by external stimuli (magnetic fields). It is essential to evaluate
the tribological properties as they relate to the performance of smart material-based
applications.
MRF consists of base fluid with magnetic particles forming chain shape along
the magnetic field direction. Because of its fast response speed, it has the potential
to be applied to various industrial sectors such as automotive, aviation, construction, etc., [1]. Although research on MRF-based applications with control method is
being conducted, tribological characteristics of MRF remain in early stage.
For example, tribological properties of magnetic particles in MRF are examined
by Bullough [2]. It is noted that the parameters such as particle concentration,
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Friction, Lubrication and Wear
surface condition, sliding speed, and contact pressure should be considered to
understand sliding contact mechanism. Lubrication performance of MRF is evaluated using tribological tester [3].
The performance of MRF is based on the yield stress, which can be changed
by the strength of a magnetic field [4]. The applied magnetic field can change
the intensity of the particles arranged along the magnetic field direction. The
particles can affect the friction and wear at the contact surfaces. Furthermore, the
environmental conditions can affect the properties of fluid, and the changed liquid
properties can also affect friction and wear. Fridrich studied that the heated surface
leads to the high specific wear rate with lower friction coefficient [3]. Most research
focuses on the tribological characteristics of MRF without the magnetic field [2, 5].
Since there is a disadvantage that the environmental pollution problem due to
leakage can occur, it is essential to apply the technology to prevent leakage of the
fluid. Performance degradation due to particle deposition in the fluid is also a major
problem. To solve these drawbacks, MRE has been proposed. It consists of base
material (generally polymer) and magnetic particles. As with MRF, mechanical
properties can be varied depending on the presence or absence of a magnetic field
[6]. Studies on the friction and wear characteristics of ordinary rubber have been
actively conducted, but the research on MRE is still insufficient [7].
MREs, as smart elastomers, are also investigated for use in various types of
equipment [8]. Specifically, MREs are also used in various external environments at
different temperatures, relative humidity conditions [9], and vibration conditions
[10]. However, there is a paucity of studies examining the friction and wear properties of MREs. The friction coefficient of an MRE can be controlled using external
magnetic fields by changing the hardness of the MRE. Therefore, this property can
be applied in some hardness-controllable devices.
MRFs and MREs have been widely studied and applied in various mechanical
devices. Because of their controllable mechanical properties under the magnetic
field, their tribological characteristics are important for evaluation. However, in
this chapter, the tribological characteristics of MRFs and MREs will be explained,
including friction and wear properties of MRFs and MREs under different environmental conditions such as temperature, humidity, and vibration conditions.
2. Tribological characteristics of magneto-rheological fluids (MRFs)
and their applications
2.1 Friction and wear properties of MRF under different applied loads and speeds
The potential applications using MRF are operated under various loads and
speed conditions. It is necessary to estimate the performance of applications that
take into account friction and wear characteristics. As most contacts are occurred
in linear motion, friction and wear characteristics are examined under different
working conditions (oscillating frequency, load, and magnetic field). The detailed
mechanism of the tester is shown in Figure 1. The magnetic field is applied to the
MRF, and its direction is perpendicular to the moving direction. Cartridge heaters
under the specimen can provide the heat on the contact surface. The oscillating
frequency and the applied load are fixed to 0.5/1.0 Hz and 1/5 N, respectively. The
results in Figure 2 show the friction coefficient changes concerning the working
cycles. The lower values are observed under higher load condition with no magnetic field. The tendency of the results with different oscillating frequencies is
almost the same.
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Figure 1.
Schematic of reciprocating friction and wear tester (R&B 108-RF).
The microscopic images of the specimen before and after the tests are compared
as shown in Figure 3. The machining marks are only observed on the surface before
the tests, but some wear marks such as ridges are shown on the surface after the
tests. The distance between wear marks is very close, and a smoother surface is
observed when a magnetic field is applied. The particles in MRF form a chain shape
along the direction of a magnetic field. The formed structure works as resistance
resulting in small motion at contact interfaces. However, the main reason for
surface wear is free-moving particles.
2.2 Friction and wear properties of different types of MRFs
Since the mechanical properties of MRF are controllable, various types of MRF
(122EG, 132DG, 140CG) are studied to improve the MR effects. The weight percentage of particles in the fluid is one of the key factors. The particles in the fluid
affect friction and wear properties at contact interfaces. Therefore, various MRF
types are taken into consideration to estimate the tribological characteristics under
different working conditions such as the strength of the magnetic field, load, and
oscillating frequency. The magnetic field strength is changed to 9 mT from 3 mT
with a 3 mT step. Moreover, oscillating frequency and the applied load are fixed to
1 Hz and 10 N, respectively.
The results of the friction coefficient change with different magnetic field
strengths are shown in Figure 4. The friction coefficient tends to increase as the
magnetic field strength increases. The particles are constrained in the chain shape
along the direction of the applied magnetic field. Some may have an abrasive effect
on the surface during the friction process. Most of them show the resistance on the
surface due to the gathered particle under the presence of a magnetic field. The
particles are turned into the additional tribological pair and increase the friction
coefficient. Moreover, the interactions among the particles under the magnetic
field continuously occur during the movement, and it causes energy consumption,
resulting in friction coefficient increase. Such an interaction force tends to increase
under higher magnetic field strength.
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Friction, Lubrication and Wear
Figure 2.
Friction coefficient change of MRF under different loads and speed conditions (aluminum).
(a) 0.5 Hz/unapplied and applied magnetic field and (b) 1.0 Hz/unapplied and applied magnetic field.
2.3 Friction and wear properties of MRF with the coatings
Since the types of MR fluid have influence on the tribological properties, the demand for the improved friction and wear performance in contact
interfaces is increasing. The surface coating is the solution that can enhance
the friction and wear performance while maintaining the controllable properties of MR fluid in various industrial applications. Various coating materials
are taken into consideration to evaluate the friction and wear properties of
MRF. Most common coating materials widely used in industrial area are PTFE
and DLC. Therefore, two different coating materials and pairs are considered
with the fixed working conditions. The oscillating frequency, applied load, the
strength of a magnetic field, and temperature are 1 Hz, 5 N, 5 mT, and 25°C,
respectively.
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Figure 3.
Microscopic surface images before and after wear (5 N/1 Hz). (a) magnetic field on and (b) magnetic field off.
Figure 5 shows the friction coefficient changes with different coating materials
and pairs. The material of the specimen is aluminum (pin and plate), and they are
coated with DLC and PTFE. The friction coefficient tends to increase with no coatings. However, it shows the lower values with coatings. The stable results are shown
for the coating surface. PTFE-coated surfaces show improved friction performance
compared to DLC and no coating. The best friction performance is observed for
PTFE coating pairs.
DLC coating is widely used for industrial applications due to the better
mechanical properties than PTFE. Thus, it is suggested that the DLC coatings are
more appropriate to most of the applications. The temperature is another factor that affects friction performance as the properties of fluid change at higher
temperature conditions. The specimen with DLC coating under different temperature conditions is tested. The results of the friction coefficient change with
temperature up to 130°C are shown in Figure 6, and it tends to decrease as the
cycles increase. The degraded viscosity of MRF due to the temperature increase
gives more freedom to the particles in the fluid resulting in the improved friction
performance [9].
2.4 Friction and wear behavior of MRF applied to pin-bushing system
Bushings are widely used in many mechanical applications working as bearings.
Therefore, it is important to either maintain or enhance the tribological properties
of bushings. MRF can be applied as a lubricant to bushings to enhance the loadcarrying capacity. The friction performance of bushing is evaluated using specially
designed tester shown in Figure 7. This tester can adjust the oscillating frequency,
angle, and load. Friction performance of MRF is tested with a step load up to 5kN
from 1kN with and without a magnetic field. The results are compared to the one
with conventional grease. In Figure 8, the friction coefficient tends to decrease
when the load is 3kN and becomes stable. The highest friction coefficient is shown
when a magnetic field is activated during the test. It is assumed that the particles
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Friction, Lubrication and Wear
in the fluid work as a solid lubricant in the shape of the chain in the direction of a
magnetic field. The force among the particles leads to resistance during the operation. The friction performance at the contact interface can be controlled with a
magnetic field. The load-carrying capacity also can be changed with MRF.
Figure 4.
Friction coefficient changes with respect to types of MRF and strength of magnetic field. (a) MRF, 122 EG;
(b) MRF, 132 DG; and (c) MRF, 140 CG.
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Figure 5.
Friction coefficient changes of MRF with various coating surfaces (5 N/1 Hz).
Figure 6.
Friction coefficient changes of MRF with various temperature conditions on DLC-coated surface (5 N/1 Hz).
Figure 7.
Schematic diagram of pin-bushing friction and wear tester.
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Friction, Lubrication and Wear
Figure 8.
Friction coefficient chance under step-load condition.
3. Tribological characteristics of magneto-rheological elastomer (MRE)
and its applications
3.1 Friction and wear properties of MREs under different temperature conditions
MREs are new types of a smart material that can change mechanical properties under a magnetic field. Like other smart materials, MREs should maintain its
durability under severe environmental conditions. As MRF shows different friction
characteristics under different temperature conditions, MRE should be tested under
the same conditions. The friction and wear performance of MRE surfaces are evaluated on the temperature up to 100°C from room temperature. Figure 9 shows the
results of the friction coefficient and wear depth changes concerning the temperature increases. Friction coefficient tends to increase as the temperature increases,
and higher values are observed with no magnetic field. The presence of a magnetic
field increases the hardness. The difference in wear depth is larger than the friction
coefficient. The friction and wear performance of MRE is affected by the temperature condition. It seems that lower resistance is observed at high-temperature
conditions. In the case of fixed load and velocity conditions, the temperature is the
major factor of wear at contact interfaces.
3.2 Friction and wear properties of MRE under different humidity conditions
It is mentioned that temperature is the major factor related to the friction and
wear characteristics of MRE. It is considered that humidity is another factor. The
same tests are conducted with different humidity conditions to estimate friction and wear performance. The test conditions were implemented by adjusting
the relative humidity through the humidifier. The humidity conditions are 40,
60, and 80%. The result in Figure 10 shows the friction coefficient and wear
depth change according to the humidity variation. Additionally, the results
are compared with or without a magnetic field. Higher values of friction coefficient appear when a magnetic field is applied, and they tend to decrease as the
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Figure 9.
Results of (a) average friction coefficient and (b) wear depth for MRE under different temperature conditions.
humidity increases. The friction coefficient difference remains almost constant
under magnetic field conditions. The applied magnetic field changes the hardness. The reason for the lower friction coefficient under high humidity condition
is that the contact surface is affected by the local hydrodynamic effect resulting
in a lubricating effect. Also, the water is absorbed in MRE, and its shear strength
seems to be decreased.
The wear depth is also reduced as the humidity increases. It is assumed that the
shear strength of the contact surface can be reduced by the hydrodynamic effect.
This leads to lower energy consumption during frictional movement. The results
of wear depth show that severe wear does not appear when the humidity reaches to
80% regardless of a magnetic field. Furthermore, it does not show the significant
change of wear depth when the humidity is 60%, which is assumed to be a saturation point.
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Friction, Lubrication and Wear
Figure 10.
Results for average friction coefficient (a) and wear depth (b) of MRE at different relative humidity
conditions.
3.3 Friction and wear properties of MRE under different vibration conditions
Most industrial applications have vibration issues during the operation. Such
vibration is correlated to friction and wear. Previously, friction and wear properties are affected by various environmental conditions. Additionally, it is necessary
to estimate the tribological performance of MRE under vibration condition. The
tests are conducted under various frequencies and amplitude conditions. The
results are shown in Figure 11. The average friction coefficients are obtained,
which are compared each other, to analyze how the vibration frequency and
amplitude affect.
The friction coefficient tends to increase as the frequency increases except
at the resonant frequency. Elastomers show different tribological properties,
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Figure 11.
Average friction coefficient results of MRE under (a) different vibration frequencies and (b) vibration
amplitudes. A1, A3, and A5: 100, 200, and 2100 Hz without a magnetic field. A2, A4, and A6: 100, 200, and
2100 Hz with a magnetic field. B1, B3, B5: 1, 2, 4 μm without a magnetic field. B2, B4, and B6: 1, 2, and 4 μm
with a magnetic field.
unlike metal material in which friction coefficient reduces under vibration conditions [10]. The surfaces of elastomer have less resistance as temperature increases,
reducing the friction coefficient. When high-frequency oscillations occur, vibration energy is converted into heat energy. The temperature of MRE is increased
by 2°C when a vibration is applied. It is assumed that the generated heat on the
surface leaded higher friction coefficient under vibration conditions. Also, the
increased contact time under high frequency causes a higher friction coefficient.
The lower values are observed at the conditions of 100 and 200 Hz. After 200 Hz,
the vertical load at the contact surface is reduced by the resonance. The lower friction coefficient can be obtained due to the reduced load. The vibration amplitude
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Friction, Lubrication and Wear
is taken into consideration to evaluate the tribological properties of MRE. The
previous results show that the friction coefficient clearly decreases when a magnetic field is applied, which is related to the hardness change. The small deformation on the contact surface appeared when a magnetic field is applied, resulting in
small deformation; when a vibration amplitude increases, the friction coefficient
decreases. It is assumed that the separation of the contact pair appears when the
amplitude is high.
3.4 Rolling friction characteristics of MRE
Previously, the friction coefficient under reciprocating motion can be controlled
by the strength of a magnetic field. Rolling friction is another factor to be considered in engineering applications. As the motion is different, tribological characteristics of MRE under rolling motion should be taken into consideration. The tests are
carried out under a fixed velocity and load conditions.
The micro slip at the contact interfaces, adhesion, and plastic deformation are
the key factors of rolling friction of elastomer. The schematic of the rolling friction
of elastomer is shown in Figure 12. In the analytical model [11], the rolling friction
coefficient can be obtained as follows:
1
_
2
MR
2a = ___
4α _____
W
= α____
μR = ____
WR
3𝜋𝜋R 3π { 𝜋𝜋R E∗ }
(1)
According to Eq. (1), the rolling friction coefficient can be reduced by increasing
the modulus. It can be increased under a magnetic field. Thus, the theoretical values
of rolling friction coefficient can be obtained. The theoretical and experimental
values are compared in Figure 13. The results show that the values tend to decrease
as the magnetic field strength increases. The tendency of experimental results
is similar to the one in theory. The difference between experiment and theory is
caused by micro slip and adhesion at contact interfaces.
Figure 12.
Analytical model of rolling friction of an elastomer.
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Tribological Characteristics of Smart Materials (Magneto-Rheological Fluids and Elastomers)…
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Figure 13.
Comparison of rolling friction coefficient of MRE with respect to magnetic field strength from experiment and
theoretical analysis.
Author details
Peng Zhang1, Chenglong Lian2, Kwang-Hee Lee3 and Chul-Hee Lee3*
1 Nanjing Research Institute for Agricultural Mechanization Ministry of
Agriculture, Nanjing, PR China
2 College of Forestry, Shandong Agricultural University, Taian, PR China
3 Department of Mechanical Engineering, Inha University, Incheon, South Korea
*Address all correspondence to:
[email protected]
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
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Friction, Lubrication and Wear
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Systems and Structures. 2003;14:71-78.
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[9] Odfalk M, Vingsbo O. Influence
[2] Wong P, Bullough W, Feng C,
[10] Wen S, Huang P. Principles of
Lingard S. Tribological performance
of a magneto-rheological suspension.
Wear. 2001;247:33-40. DOI: 10.1016/
S0043-1648(00)00507-X
[3] Song W, Cai Q , Choi S, Lee C. A
study of finishing process of magnetorheological fluid on steel surface. Civil
Engineering and Building Materials.
2011;1:17-24
[4] Zhang P, Lee K, Lee C.
Reciprocating friction characteristics
of magneto-rheological fluid for
aluminium under magnetic field.
Transactions of Nonferrous Metals
Society of China. 2014;24:171-176. DOI:
10.1016/S1003-6326(14)63044-2
[5] Zhang P, Lee K, Lee C. Friction
behavior of magnetorheological
fluids with different material types
and magnetic field strength. Chinese
Journal of Mechanical Engineering.
2016;29:84-90. DOI: 10.3901/
CJME.2015.1126.139
[6] Carlson J, Jolly M. MR fluid, foam
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2000;10:555-569. DOI: 10.1016/
S0957-4158(99)00064-1
[7] Lancaster J. A review of the
influence of environmental
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10.1016/0301-679X(90)90053-R
[8] Persson B. Rubber friction and
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Tribology. Beijing: John Wiley & Sons;
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[11] Williams J. Engineering
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University Press; 2005. DOI: 10.1017/
CBO9780511805905
Section 2
Lubrication
119
Chapter 8
A Review of Surface Treatments
for Sliding Bearings Used at
Different Temperature
Jun Cao, Liang Qin, Aibing Yu, Haibo Huang, Guoping Li,
Zhongwei Yin and Huiyu Zhou
Abstract
The boundary lubrication and dry friction of plain bearings at different work
temperature are unable to be avoided under the start and stop condition. The poor
lubrication is one reason of bearing broken. In order to improve the tribological
properties and select the best treatment for different bearings used at different
temperature, the studies of different treatment technologies are reviewed in this
paper. The review shows that the shortages of bonding fiber woven materials, inlaying solid lubricating materials, electro plating and magnetron sputtering are poor
temperature resistance, low load capacity, environment pollution and low production efficiencies respectively. Based on the analyses and summaries, the liquid dope
spraying and thermal powder spraying are suggested to deposit coating on the
surface of bearing which working temperature is lower than 200 and above 800°C
respectively. However, the technology processes, the mechanisms of spraying and
self-lubrication materials should be studied further and deeply.
Keywords: plain bearing, surface treatment, wide range temperature,
lubrication materials, technology process
1. Introduction
1.1 Background of the research review
Sliding bearings are widely used as the basic components in marine power,
aerospace, water conservancy and hydropower industries. As shown in Figure 1, the
sliding bearings are divided into integral sliding bearings and split sliding bearings
according to their structures. They have some features, such as low noise, stable work
operation, compact structure and heavy load bearing capacity [1]. With the advancement of science and technology, the automotive, marine, electric power transportation and some other industries are developing into ‘serious conditions’ such as high
speed and high load, making the sliding bearing under a wide temperature environment. For example, the work temperature of engine rises from room temperature
to about 140°C during different operating conditions, such as starting, accelerating,
constant speed, deceleration and shutdown. From the research data, the temperature
even rises up to 200°C at the time of bearing broken [2]. The work temperature of
some bearings is high, for example, the working temperature of the socket bearing
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Friction, Lubrication and Wear
of missile launching mechanism exceeds 800°C. Under high temperature conditions,
grease and lubricating oil fail, and unlubricated bearings will quickly be broken
under the action of high friction coefficient and wear. Ordinary sliding bearings are
normally lubricated due to lubricating oil with the hydrodynamic lubricating oil
film. Under normal conditions, sliding bearings can generally satisfy the requirements of long-term service. However, the reasons of ablation and friction damage of
the bearings 12.5% are due to poor lubrication the investigation.
As shown in Figure 2, the sliding bearing damage quickly due to the lacking
of self-lubricating properties of bearing, and the mixed lubrication and even dry
contact friction at the start-stop stage of engine [3]. Therefore, researching and
improving the friction mechanical properties of the bearing under dry friction conditions is one of the key technologies for improving the bearing life of at start-stop
stage. In the case of large dust, high temperature and no lubricating oil or grease,
the life of the sliding bearing will be drastically reduced. For example, the working environment temperature of rolling steel rolling mill is about 200°C, and the
maximum service life of the bearing is no longer than 3 months. In order to avoid
the bearing damage and improve the service life of the sliding bearing at the dry
friction stage, it requires the sliding bearing should have self-lubricating property to
reduce the high torque requirement and tribology at the stages of start-stop under
different temperature conditions [4].
Figure 1.
The applications of plain bearings and their structures.
Figure 2.
Friction damage of sliding bearings.
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The self-lubricating treatment technology of sliding bearings in China is still
backward. Bearings with self-lubricating properties at different temperature conditions are still very rare. Compared with the advanced bearings of European and
North American, the sliding bearings of China have short life, low carrying capacity, poor self-lubricating performance and overcapacity. High-performance sliding
bearings such as, self-lubricating, high-load, and long-life are relied on import.
The lack of high-performance sliding bearings restricts the development of China’s
basic manufacturing industry, especially the military industry. Therefore, the selflubricating performance of the sliding bearing during in wide temperature range
should be improved, and the different lubricating methods for different bearings at
different temperature should be selected.
The development, manufacturing and processing capabilities of sliding bearing
materials of China should be improved. At present, the main production technologies sliding bearings are centrifugal casting and alloy powders metallurgical.
However, most bearings have no surface lubrication and will be quick broken. For
example, more than 90% of the bearing bushes prepared by powder metallurgy
in the automotive industry are not subjected to surface self-lubricating treatment
such as electroplating and magnetron sputtering. Powder metallurgy technology of
sliding bearing preparation has high production efficiency and low cost. The sliding
bearing prepared by metallurgical process has high porosity without centrifugal
force. In addition, the bearing alloys such as copper, aluminum and tin are easily
oxidized at high temperature during the metallurgy preparation of sliding bearing,
and metallographic organization is not uniform [5]. Centrifugal casting is another
common production process for sliding bearings. The integral and thick-walled
plain bearings are usually produced by centrifugal casting. However, most of the
sliding bearings produced by centrifugal casting process are not subjected to inert
gas protection or vacuum environmental protection, therefore, the bearing alloys
are oxidized and the alloy grains size are not uniform [6].
With high dry friction coefficient and low load bearing capacity of bearings,
the common methods are the surface treatments which improve the bearing life
effectively. The electroplating, magnetron sputtering, self-lubricating liner antifriction, and inlaying self-lubricating materials are the main surface treatments for
bearings. The lubrication and mechanical properties of the sliding bearing surface
are changed by one or several electro-plating alloy layers. However, the plating solution is highly polluted, and electroplating technology of sliding bearings is seeking
alternative process technology [7].
The magnetron sputtering is one of the most advanced technologies for the
preparation of sliding bearings. Compared with electroplated bearings, magnetron
sputtering bearings have better bonding strength and surface lubricity. However,
magnetron sputtering requires a process such as pumping, vacuuming, and sputtering to form a uniform film. The magnetron process needs long production time and
high production cost, and its target materials utilization rate are lower than 40%,
which cannot satisfy the requirements of large-scale production. What is more,
due to the constraints such as size and structure, just small bearings are able to be
prepared by magnetron sputtering [8]. At present, it is an urgent problem to find
a mass production of sliding bearing to satisfy the requirements of self-lubrication
at wide temperature range, and having good lubricity under special working
conditions such as start-stop, lean lubrication or even dry friction. The materials
of electroplated plain bearing are mainly babbitt alloy, ternary and quaternary
indium alloys which friction coefficient is large under dry friction conditions, and
it does not have wide temperature range self-lubricating performance. The Kevlar
aramid fiber modified with nano-solid lubricants, and pasted on the surface of the
sliding bearing that is the liner anti-friction technology. The liner and pasted glue
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Friction, Lubrication and Wear
cannot be used at high temperature conditions, and it does not have self-lubricating
properties at wide temperature. The sliding bearing inlaid solid self-lubricating
materials such as graphite, MoS2, WS2 and so on, and they are punched on the
working surface of the sliding bearing. With self-lubricating materials, the selflubricating materials are crushed to form a self-lubricating film to reduce the friction coefficient of the bearing. However, single-phase self-lubricating material such
as graphite and MoS2 cannot satisfy the requirements of wide temperature range
self-lubrication, and the inlaid holes will reduce the mechanical strength and load
capacity of the bearing. The temperature environment of the joint bearing, machine
tool and electric equipment sliding bearings is room temperature environment; the
working temperature of the sliding bearing for hot-burning furnace, gas pump and
rolling steel rolling roller is about 200°C; the working temperature of the bearing
socket for aviation is above 800°C, and they require self-lubricating materials at
different temperature environments. Studies have shown that the use of coating
lubrication technology improves the friction and wear, impact resistance, high
temperature and longevity of the sliding shaft without changing the bearing matrix
structure and composition [9]. Therefore, bearing surface coating technologies are
one of the most critical and feasible methods to improve the overall technology of
the domestic sliding bearing industry.
1.2 Significance of the research review
Due to the higher requirements of high-speed, high-load and high-temperature,
the lubrication of sliding bearings under different temperature conditions and different load conditions will directly determine the working state and service life of
the bearings and the whole machine. Many scholars have studied the self-lubricating methods of sliding bearings such as electroplating, magnetron sputtering, inlaying solid lubricants, and adhesive self-lubricating liner. However, these traditional
sliding bearing self-lubricating methods have some defects. With the improvement
of environmental protection requirements, the sliding bearings prepared under
large-scale and high-volume production conditions have excellent self-lubricating
properties under different temperature conditions, which are the keys of the current research. One of the current advanced treatment technologies for self-lubricating sliding bearings is liquid coating technology, but the theoretical calculation of
bearing spraying is litter. The phenomenon of bearing sag and leveling has not been
studied deeply. The optimum thickness of coating, the best surface roughness of
the substrate, and coating the optimum curing temperature and optimum cooling
temperature of the layer also lack of relevant details and theoretical analysis. The
studies of sliding bearings with wide temperature range self-lubricating coating
materials under different temperature conditions are lacking.
2. Reviews of self-lubricating sliding bearing
The traditional self-lubricating sliding bearing production and preparation processes are mainly electroplating, magnetron sputtering, inlaying solid lubricants,
and adhesive self-lubricating liner and so on. The self-lubricating bearing processes
and their performances are summarized as follows.
2.1 Review of self-lubricating sliding bearings at room temperature
In the severe conditions such as large dust, high pollution, high load bearing, lacking of lubricating oil and grease, sliding bearings only rely on their own
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lubrication to improve work performance. For example, in the automobile manufacturing, cement production and coal mining industries, the inlaying solid lubricants
and adhesive self-lubricating liner are the common methods of the joint bearings
and bushing sleeves.
2.1.1 Adhesive liner for self-lubricating bearing
The friction coefficient of the bearing is reduced, the wear resistance is improved
and the working life is prolonged through the modified liners for sliding bearings.
Braided liners are generally composed of Kevlar aramid fiber materials (KEVLAR),
polytetrafluoroethylene (PTFE), modified carbon fiber materials, and nano-additives [10]. The structure of sliding bearing with liner is shown in Figure 3. In order to
obtain a small shear force and a large bonding strength, the fabric liner is bonded on
the bearing surface through the adhesive glue. The frictional coefficient is decreased
by changing the metal to metal contact to metal to liner contact. Aderikha studied
the friction and wear properties of the liner based on PTFE and plasma treated
polymer fibers. The results showed that the friction coefficient was 0.15–0.2 under
different loads [11]. Li studied the friction and wear properties of nano-materials
SiC and WS2, and the friction coefficient of surface liner under dry friction was
about 0.05–0.06 [12]. Fabrics were treated with rare earths CeO2, LaCl3, La2O3 and
CeF3 by Shen, Zhan and some scholars, and their friction, wear properties and bonding properties of the joint bearings with the modified rare earths were studied. The
results shown that the bonding strength was higher under the action of rare earths,
the film formation is faster, and the coefficient of friction is generally less than 0.1
[13–16]. Liners and adhesive glue as the main component cannot be used at medium
and high temperatures, and the bonding liner method is generally applicable to small
thick-walled sliding bearings, which has certain limitations for medium and large
sliding bearings.
2.1.2 Bearings with inlaid solid self-lubricating materials
The self-lubricating materials are inlayed on the surface of bearing. As shown
in Figure 4, the solid lubrications will be expanded when sliding bearing subjected
to load, and the bulged out lubrications are ground to tiny wear debris. With
the sliding movement of bearing, the frictional coefficient is decreased with the
formation of lubricating film from the debris. The inlaid materials are generally the
solid lubricant materials such as graphite, molybdenum disulfide and PTFE. Wei
prepared a new self-lubricating material consisted of PTFE, graphite and glass
fiber. The results showed that the friction and wear properties of self-lubricating
materials prepared by 40% PTFE + 20% graphite + 20% lead powder + 20% glass
fiber were the best [17]. MoS2/Sb2O3 mixed powders were produced to form solid
Figure 3.
Join bearing with self-lubricating liner.
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Friction, Lubrication and Wear
Figure 4.
Plain bearing inlaying with solid lubrications.
lubricant by Zabinski with thermosetting bonding method. The results pointed
out that MoS2 and Sb2O3 have synergistic antifriction effect on friction work, and
Sb2O3 can prevent MoS2 from oxidizing [18]. Li prepared FeS/copper-tin alloys
as the inlaying materials by powder metallurgy. The research showed that the
increase of FeS content reduce the friction coefficient. When the FeS content is
10%, the friction coefficient is 0.15 [19]. The research studies of inlaid solid selflubricating materials showed that the working conditions of the prepared materials
were mostly room temperature environment, and the studies of medium and high
temperature self-lubricating materials were few. Therefore, the working conditions
of sliding bearings embedded with solid self-lubricating materials on the market
are mostly room temperature environments. In addition, the inlaid structure will
reduce the strength of the bearing, resulting in low bearing capacity.
Sliding bearings prepared by modified liner technology and inlaid solid selflubricating technology satisfy the self-lubricating requirements of room temperature conditions, but the fiber fabric materials cannot be used at high temperature.
However, there are few studies of solid self-lubricating materials that satisfy the
self-lubricating under the wide temperature range. Generally, bearings with inlaying solid materials are used at room temperature environment, and the structural
strength of the bearing will be reduced by this technology.
2.2 Review of self-lubricating sliding bearing at medium temperature condition
2.2.1 Electroplating
The working temperature of bearing bush, plain bearing of rolling mills near
to furnace and sleeves is from 100 to 200°C. At the start and stop stages, the
automobile bearing bush is under a boundary lubrication or even a dry friction
state because the lubricating oil film is not formed at start stage or broken at stop
stage. However, the sliding bearings of rolling steel and the bearings in the heating
furnace may cause the lubricating oil and grease to fail due to the high working
environment temperature. In order to improve the performance of the bearing and
prolong its service life, bearings need to be self-lubricated. The most common selflubricating treatment methods for plain bearings represented by bearing bushes
are electroplating and magnetron sputtering. As shown in Figure 5, one or more
layers can be prepared on the surface of the bearing to improve bearing lubrication
and improve bearing fatigue strength and service life. Wang studied Ni/SiC and Ni/
Al2O3 electroplating techniques, and ceramics such as SiC and Al2O3 were added
to the coating material, which improve the wear resistance of the bearing [20]. Li
studied the friction and wear behavior of nano-Ni-PTFE composite coating on
steel substrate. The results showed that the coating friction coefficient range was
0.05–0.15 under different loads [21]. Zhang prepared a MoS2 coating containing
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Figure 5.
Technology of electroplating of bearings.
nano-graphite particles by electroplating brush, and tested the friction coefficient
was from 0.05 to 0.15 [22]. However, the plating prepared by the electroplating
brush is not uniform, and the bonding strength is not as good as that of chemical
electrophoresis. Studies had shown that metals such as In, Ni, and W improve the
wear resistance of sliding bearing coatings [23, 24]. The addition of rare earth metals such as La, Ta, Nb significantly improved the frictional mechanical properties of
the sliding bearing coating [25–27]. The friction coefficient of electroplated coppertin alloy, aluminum-tin alloy and babbitt alloys under dry friction conditions is
generally 0.3–0.6, which needs to be combined with lubricating oil and grease to
satisfy the lubrication requirements [28]. Electroplated plain bearings are currently
the most widely used preparation methods, but the plating solution is highly polluting and does not satisfy environmental production requirements.
2.2.2 Magnetron sputtering
Unlike electroplating, magnetron sputtering does not cause environmental pollution. The magnetron sputtering process shown in Figure 6 has a dense film, and
the thin metallographic structure in a vacuum environment makes the performance
of the sliding bearing superior to that of the electroplated production. Li prepared
a Babbitt Cu-Sn-Sb film on a steel substrate by magnetron sputtering. The friction
coefficient was from 0.1 to 0.25 after dry friction experiment of 4000 rpm [29].
The Max- phase Ti3SiC2 material was sputtered during magnetron sputtering of Cu
film. It studied by Li, and results showed that the physical and mechanical properties of Cu film were significantly improved after adding new materials [30]. Guo
studied the metallographic properties and hardness of the magnetron sputtering
bearing of AlSn20 material, and the experimental results reached the international
advanced level like Miba bearings [31]. Song prepared AlSn20Cu thin films by
magnetron sputtering. The hardness of the tested films was 120 HV, and the friction
coefficient was less than 0.1 under oil lubrication [32]. Although the high hardness
film improves the bearing capacity of the bearing, it also reduces the adhesion of
the bearing. However, if the surface hardness of bearing is less than 50 HV will have
better embedding performance [33].
The different compound films can be synthesized and synthesized because
maximum as eight targets can be sputtered simultaneously from magnetron
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Friction, Lubrication and Wear
Figure 6.
Technology of magnetron sputtering.
sputtering. In the existing research, bearing alloy composite films such as Ti/Cu/N
CuxSny, TiN/Cu had been prepared, and adhesin strength of these films is excellent [34, 35]. However, the tribological properties of above materials are the same
as the bearing materials such as AlSn20 and AlSn20Cu. The friction coefficient
is higher under dry friction conditions and mixed lubrication conditions, which
cannot satisfy the self-lubricating performance requirements at wide temperature.
To improve the tribological and mechanical properties, the noble metal materials such as indium or rare earth materials are used during the electroplating plating
process. However, the plating solution is a strong acid or a strong alkali substance,
which is likely to cause serious environmental pollution. Magnetron sputtering
equipment is expensive to manufacture. Many magnetron sputtering equipment
only produce small test specimens in a laboratory environment, and cannot be
mass-produced or mass-produced for large-sized sliding bearings. The utilization
rate of magnetron sputtering target is generally less than 40%, and the working
time is long and the production efficiency is not high when vacuuming, injection
and depositing materials [36]. Therefore, it is necessary to find a new technology to
prepare a self-lubricating sliding bearing.
2.2.3 Liquid dope of spraying
The most advanced surface treatment method available today is the surface
spraying coating method. Compared with traditional surface treatment processes
such as electroplating and magnetron sputtering, it has the advantages of environmental friendliness, high production efficiency, coating processing, and good coating lubrication performance. Spraying sliding bearings are characterized by high
speed and high efficiency. It takes only several seconds to spray lubricating liquids,
and large-scale and large-scale production will be realized if solidification furnaces
and cooling furnaces are enough. For example, an automatic spraying production
line of Shanghai Federal-Mogul company produces more than 12 million bushings
with spraying coating (Figure 7 and Figure 9).
The north Americans first began to study the coating technology of sliding
bearing coatings and applied for related technology patents. For example, in the
1970s, Campbell used MoS2 and Sb2O3 as solid fillers and epoxy resin as a binder to
prepare self-lubricating coating, which was applied to sliding bearings [37]. The
bearing coating prepared from materials such as MoS2, Sb2O3 and epoxy resin has
the advantage of low friction coefficient, but the ordinary epoxy resin working
temperature generally does not exceed 140°C, which does not satisfy the long-term
use requirements of temperature conditions above 200°C.
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Figure 7.
Plain bearings with dope coating of overseas.
After several decades of development, the of plain bearings with self-lubricating
coating made from liquid spraying have been large scale produced by developed
companies such as Federal-Mogul Co., Austrian Miba Co., Japan TAIHO KOGYO
Co. However, there are few research materials on self-lubricating coatings in China.
In the year of 1983, the first MoS2 self-lubricating coatings prepared by liquid dope
was studied by Liu of the Institute of Coatings, however, the coatings were not
applied to sliding bearings [38]. The sliding bearing surface coating technology of
China started late, and it is still a new technology. In recent years, many bearing
research institutes and manufacturers in China have begun to study the coating
technology of sliding bearing made by liquid spraying. As shown in Figure 8,
bearings with MoS2 lubricating coating made by liquid spraying, and prepared with
Zhejiang CSB Co. and the ZYNP Co.
The widely used coating dopes in China are MoS2 and PTFE dopes, which wear
resistance and temperature resistance are poor, and the tribological properties
of composition elements such as resin and auxiliary are lower than that of Dow
Corning D7409 and Kawanori of Japan. However, self-lubricating coatings for
bearings under the medium (200°C) and high temperature (800°C) dopes are
lacking of. The special lubricating materials of coating dopes of American D7409
and Kawanori of Japan did not particularly be selected according to the special
alloys of bearing likewise the different aluminum alloys, copper alloys, and
babbitt alloys, and these coatings drop easily if the temperature varies with time.
Therefore, it is important to develop new coating dope for special alloys at different temperature.
The coating spraying technology includes coating dope preparation, liquid
dope spraying through spraying gun and solid coating formation. The coating dope
consists of self-lubricating materials, anti-wear materials, resins, auxiliaries and
solvents. The different lubrications and anti-wear materials easily mixed together
due to the liquid solution, and the coating made from dope will have the excellent
tribological properties. The principle of paint spraying is shown in Figure 9. There
are two ports on the spray gun connected to the spraying gas and dope respectively.
Figure 8.
Plain bearings with dope coating of China.
129
Friction, Lubrication and Wear
Figure 9.
Work principle of coating dope spraying
The paint dope is in a pressure tank with automatic stirring. It is driven into the
spraying gun by the action of the pump to adjust the size of the gas source, liquid
flow rate and spraying distance to control the amount of spraying dope.
2.2.3.1 Coating formation
Guo used epoxy resin as the binder, and MoS2 and PTFE were used as the
main lubricating materials to prepare the antifriction coating. The friction
mechanical properties of the coating were studied at different curing temperatures. The results showed that the coating performance was the best when the
coating formation temperature was 120°C. The coefficient of friction is 0.125,
and the adhesion is 16.73 N [39]. However, ordinary epoxy resins have poor
temperature resistance, and the coating thus prepared cannot be operated for
a long period of time at 200° C. Cao studied the spraying distance effects on
coating spraying efficiency and coating thickness uniformity. He pointed out
that reducing the spraying distance improves the adhesion between the coating
and the substrate. However, the shorter the distance was, the worse the coating
thickness uniformity could be [40]. Yang used sagging as the object of assessment, and studied the spraying distance and spraying temperature during the
PTFE coating preparation, but the principle and theory of sag phenomenon had
not studied [41].
2.2.3.2 Porosity
The heating temperature of the coating to form a coating is generally from 120
to 220°C. Under the action of materials such as resin and polyimide, the liquid
coating has a sealing effect on the solid coating process which leads to low coating
porosity. Li uses rare earth materials and a rapid thermosetting method to prepare a coating, and the porosity of coating is just only 0.35% [42]. The porosity of
sliding bearing produced by the powder metallurgy and electro-plating is high.
Lins et al. studied the effect of current density on the porosity of nickel deposited
with copper substrates. The porosity of nickel coatings was 6.22% according to
different current magnitude tests [43]. The films prepared by magnetron sputtering are relatively dense, and the porosity is generally from 0.5 to 5% [44, 45].
If 1–2% reduction in porosity, the fatigue strength of the workpiece will increase
from 10 to 30%, so low porosity is one of the necessary conditions for sliding
bearings [46].
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2.2.3.3 Bond strength
The initial state of the coating prepared on the surface of the bearing is liquid.
In order to avoid sagging of the coating, the coating thickness should not be too
thick. The optimum coating thickness of the coating method is less than 20 μm, and
the infiltration method and the brushing method are prepared. The thickness of
the coating should not exceed 120 μm. The bonding strength of the coating to the
substrate is influenced by surface roughness of the substrate, the type of coating
adhesive, the preheating and the curing temperature. Therefore, it is particularly
important to study the coating forming process to improve the bonding strength of
the coating. An used epoxy resin and polyvinyl butyral as binder to prepare coating with TiO2 as filler. The bond strength of the steel matrix is from 9 to 12 MPa
[47]. Mao prepared a coating of made by graphite, MoS2, PPS (polyphenylene
sulfide) and PES (polyethersulfone resin) by regression test. The optimum bonding strength of the tested coating was 42 MPa [48]. The self-lubricating coatings
with polyamide-imide used as the binder, and the main lubricants were MoS2 and
PTFE. The adhesive strength studied by Song according to the GB9286-88 paint
film rating test of China is poor as level 1, which does not reach the optimal bonding
strength [49].
2.2.3.4 Lubrication properties
Self-lubricating coatings are mainly composed of solid lubricating fillers such
as MoS2, PTFE, WS2, graphite, and some additives such as polyimide, epoxy resin,
phenolic resin, leveling agent, dispersing agent, defoaming agent, etc. Gao used PAI
(polyamide-imide polyamide-imide) as a binder, and the coating prepared by mixing 8% MoS2, 5.4% PTFE and 1.5% graphite had the best performance. The coating
had not changed which was tested at 80°C and −40°C, and it was not changed for
socking in 10% HCl over 3 months [50]. Li made PTFE coating which added MoS2
and graphite as the solid lubricants. The PTFE used as the main component, and
PEEK (polyether ether ketone), PI (polyamide) and PPS as binders. The coefficient
of friction of the PTFE coating was 0.12 [51]. The studies of self-lubricating sliding
bearing coatings are mainly concentrated in recent years, so there are few researches
of self-lubricating coatings which used at wide-temperature. Ordinary epoxy resins
and polyimide materials are generally used in coatings, however, they cannot work
for long under condition of 200°C. In addition, the sagging and leveling phenomenon of the sprayed sliding bearing have not been studied in detail. The theory of
optimal thickness of coating, optimum roughness of the substrate, optimum curing
temperature of the coating and cooling temperature of the coating are also very few.
Compared with the self-lubricating sliding bearings prepared by electroplating and magnetron sputtering, the paint-coated bearings have the advantages of
environmental protection and high production efficiency. The review of coating
research shows that the development of self-lubricating coatings under different
temperature is one of the best technologies for preparing sliding bearings due to the
excellent wear resistance and low friction performance.
2.3 Review of self-lubricating sliding bearing at high temperature
The work temperature of socket bearings in the missile launcher mechanism
is higher than 800°C. Materials such as resins used as components in dope coating cannot be operated under ultra-high temperature conditions. At present, the
maximum working temperature of grease-based lubricating materials generally
do not exceed 200°C, and the maximum using temperature of polymer-based
131
Friction, Lubrication and Wear
self-lubricating materials (single-phase) generally does not exceed 400°C [52]. The
ranges of optimum lubrication for single-phase materials are shown in Table 1.
The frictional coefficient of MoS2 is generally lower than 0.1 under room
temperature. The oxidations of Mo element will be generated if MoS2 working
temperature exceeds 200°C, that the self-lubricity of MoS2 is reduced. The MoS2
lubrication performance will be further reduced and the self-lubricating effect
will be lost if the temperature exceeds 350°C. In Table 1, B2O3 produced by BC4
under high temperature has self-lubricity, and its friction coefficient is from 0.10
to 0.30, while the BC4 friction coefficient is from 0.35 to 0.40 at room temperature
[55]. Single coatings are difficult to maintain self-lubricating performance over a
wide temperature range. Ouyang used BaSO4, BaCrO4, Ag as the main materials
to prepare self-lubricating materials. The results of friction and wear tests showed
that the friction coefficient was from 0.38 to 0.55 when the temperature was from
room temperature to 800°C [56]. Zhen studied a self-lubricating material mainly
consisted of CaF2, BaF2 fluoride and noble metal Ag, and the frictional coefficient
of the composite material is from 0.24 to 0.3 at the temperature from room temperature to 800°C [57]. The physical and phase change will vary with temperature,
for example, the structure and tribological properties of Ti2AlC coating made by
thermal spraying are different at room temperature and 800°C [58]. The coating
shown in Figure 10a is spongy and many pores, however, the coating was oxidized
and became dense at 800°C.
2.3.1 Powder metallurgy sintering
In order to make the bearings have self-lubricating performance under ultrahigh temperature conditions, the common method is to prepare self-lubricating
coating by powder metallurgy method. In the powder sintering method, the
self-lubricating powders often mixed with some functional powders, and placed
together in a high-temperature furnace to prepare a self-lubricating composite
material. In the preparation of self-lubricating composites by powder metallurgy,
local unevenness will be generated due to uneven powder mixing, uneven laying,
uneven powder size or incomplete sintering of the powder during sintering [59].
Chen studied the uneven microstructure of AlSi alloy powder. The study
showed that when the mass fraction of AlSi alloy powder is 50%, it can effectively
reduce the unevenness of the product and improve the stability of the alloy [60].
Ding studied the powder metallurgy oxidation behavior at different temperatures,
different processes and different atmospheres, and results pointed out that the
amino atmosphere was more protective than nitrogen [61]. Cao prepared Ti6Al4V
coating by sintering 23 μm Ti particles and 40 μm Al-V powder. The powder was
cold pressed to 180 MPa before sintering, and then sintered at 1250°C in vacuum to
prepare Ti6Al4V coating. The layer porosity was only 3.5% [62]. Studies had shown
Frictional coefficient
Max using temperature
Frictional coefficient
Max using temperature
Graphite
MoS2
WS2
WSe2
0.05–0.15
0.05–0.20
0.08–0.20
0.09–0.20
300°C
340°C
450°C
450°C
TaS2
PbO
BN
BC4
0.05–0.20
0.07–0.20
0.06–0.20
0.10–0.30
550°C
700°C
900°C
1200°C
Table 1.
The best frictional coefficient of single material [53, 54].
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Figure 10.
Structure and abrasion marks of Ti2AlC coating at different temperature: (a) room temperature; (b) 800°C.
that increasing pressure during powder metallurgy preparation of products, and
using an atmosphere to protect the environment or vacuum environment is conducive to the reduction of porosity.
As shown in Table 2, the frictional coefficient of self-lubricating materials
prepared by the powder sintering method is from 0.26 to 0.8 under different
temperature conditions. Although self-lubricating materials at wide temperature
domain had achieved some success, they had not been applied to sliding bearings.
Most of the results were in the laboratory stage, and the self-lubricating composite
materials prepared by powder sintering had defects such as high oxidation and high
porosity. In Table 2, in order to reduce the high temperature frictional coefficient,
a highly toxic fluoride material under high temperature conditions was used, which
was not conducive to safe production.
The CoFs (coefficients of friction) of self-lubricating materials studied in Table 2
is high and at 800°C. In order to satisfy the requirements of self-lubrication of sliding
bearings used at wide temperature range, the new process and method should be
used.
2.3.2 Thermal spraying
The solid self-lubricating powder particles are heated and molten by thermal
spraying, and then directly sprayed onto the surface of the sliding bearing to form a
coating. Since there is no resin, the prepared coating can be applied to a super-high
temperature working condition. The kerosene, propane, or hydrogen used as burn gas
during the supersonic flame spraying, and the molten or semi-molten alloy powders
are sprayed with high speed on the surface of substrate by flame spraying. The time
of alloys contact with oxygen in the air is very short due to the high spraying speed of
500 m/s. Supersonic flame spraying technology widely used as surface additive processing technology, and have high production efficiency and good coating bonding
strength. A variety of coatings had been successfully prepared by thermal spraying
Materials
Ag-Pb-Cu-Sn [63]
Lubrications
CoF at room
temperature
CoF at
800°C
Ag-Pb
0.35
0.3
—
MoS2-CaF2
0.3
0.8
0.27
Ni3Al-Ag-Mo-BaF2/CaF2 [65]
Ag, BaF2/CaF2
0.35
0.38
0.32
Ni-Ag-BaF2/CaF2 [66]
Ag, BaF2/CaF2
0.3
0.32
0.26
NiCr/Cr3C2-WS2 [67]
WS2
0.42
0.28
—
ZrO2-MoS2-CaF2 [64]
Table 2.
CoFs of self-lubricating composite materials at high temperature.
133
CoF at
600°C
Friction, Lubrication and Wear
technology, and which also can be used as sliding bearing materials. Thus, the preparation of sliding bearing coatings in combination with thermal spraying technology
is reliable. Supersonic flame spraying is shown in Figure 11. The self-lubricating
powders enter the spraying gun firstly, then, with the action of prismatic shock wave,
the molten powders are sprayed on the surface of substrate to form a coating.
High bonding strength is one of the advantages of supersonic flame spraying.
The bonding strength of WC-10Co-4Cr coating made by supersonic flame sprayed
and prepared by Zhu was 72.63 MPa, and the porosity was 1.5% [68]. WC–Co coating studied by Tang, and prepared on the surface of the screw material substrate
had a bonding strength of 65 MPa [69]. The bonding strength of MoSi2 coating
prepared by Wu was only 14.5 MPa, indicating that the material and spraying
parameters were important factors for the bonding strength of the coating. If
bonding strength is low, the bonding strength can be improved by optimizing the
spraying parameters [70].
The 54% Cr3C2 added with 34% NiCr and 12% CaF2/BaF2 mixed powders, and
sprayed as coating was studied by Xue. The frictional coefficient of coating was 0.75
and 0.37 at room temperature and 500°C respectively [71]. Hou used supersonic
flame spraying process to prepare aluminum bronze alloy coating on steel substrate,
and the frictional coefficient of coating was from 0.08 to 0.12 under different oil
lubrication conditions [72]. Copper alloy and aluminum alloy materials are also
suitable for supersonic spraying to prepare coatings. The studies like AgSnO2/Cu
coating prepared by Chong, Al-Si coating prepared by Wu, and Cu(ln, Ga)(S, Se)2
coating prepared by Park [73, 74].
2.3.3 Cold spraying
Cold spray technology is a new spray technology developed from thermal spray
technology in recent decades. The obvious spraying characteristics are low temperature and high speed. As shown in Figure 12, under the action of high pressure
gas, the powder particles are supersonic flying through the Lava tube and deposited
directly on the surface of the plain bearing to form a coating by the pure plastic
deformation.
The sliding bearing materials are generally copper alloys, aluminum alloys
and tin alloys. These metal materials have an ability of excellent plastic deformation during the formation of coating by cold spraying. Guo, Li and some scholars
studied the coating properties of bearing alloy materials such as CuSn6, CuSn8,
Cu5Sn95, AlSn5, AlSn10 and AlSn20 made by cold spraying, and the frictional
coefficient of bearing alloy materials under dry friction conditions were generally
Figure 11.
Principle of supersonic flame spraying.
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Figure 12.
Principle of supersonic cold spraying.
higher than 0.5 [75–79]. The preparation of supersonic cold spray coating is mainly
based on the plastic deformation ability of powder particles, so the material should
have excellent elastoplasticity [80]. The self-lubricating powder materials such as
MoS2, graphite and h-BN have poor elastoplastic deformation ability, and they are
difficult to deposit on the bearing to form a coating.
The material frictional tests of coatings made by powder sintering, supersonic
thermal spraying and supersonic cold spraying showed that the supersonic flame
spraying and cold spraying are the desired methods to prepare coating used at high
temperature. However, many materials lack of plastic deformation ability that the
liquid dope spraying is the best method to deposit coating used at temperature
lower than 200°C.
3. Comparisons and characteristics of different self-lubricating
treatment methods
According to the studies of self-lubricating sliding bearing and self-lubricating
composite materials at room temperature, medium temperature and high temperature, bearings with self-lubricating liners and bearings inlaying with solid
lubricating materials are used at room temperature commonly. Bearings treated
by electroplating, magnetron sputtering and liquid spraying are used at the temperature lower than 200°C. However, there are no bearings that have the continue
self-lubricating performance from room temperature to 800°C, though the coating
made by powder sintering, supersonic thermal spraying and cold spraying.
The production efficiency, oxidation rate, coating thickness, porosity and
bonding strength compared and shown in Table 3 according to the different surface
treatments and bearing using temperature. As shown in Table 3, the coating thicknesses prepared by electroplating, magnetron sputtering and liquid dope spraying
is thin. The electroplating is environment polluting.
The production efficiency of film produced by magnetron sputtering is low. It
takes more than 20 h to prepare a film which thickness is 10 μm. The film of large
sliding bearing cannot be prepared due to the structure limit. The self-lubricating
liner that added on the surface of bearing has low temperature resistance due to
the fail of adhesive glue and fiber braid. The structure strength is decreased as the
structure of bearing changing with inlaying solid materials. The oxidation and
high porosity of bearing will be generated by the method of powder sintering. The
structure of materials used for thermal and cold spraying should be spherical, and
the materials used for cold spraying should have plastic deformation performance.
135
Friction, Lubrication and Wear
Technologies
Production
efficiency
Oxidation
Coating
thickness
Porosity
Adhesive
strength
Shortages
Middle
Low
<15 μm
Middle
Low
Pollution
Magnetron
sputtering
Low
Low
<15 μm
Low
High
Less
utilization
of target
Fabric liner
Low
—
—
—
High
Woven
fabric
invalid
at high
temperature
Supersonic
flame
spraying
High
Middle
<1 mm
Low
High
Spherical
powders
Cold spraying
High
Low
>1 mm
Low
High
Powders
need plastic
deformation
ability
Powders
sintering
High
High
>1 mm
High
High
High
oxidation
Inlaying
lubrications
Low
Low
—
—
—
Structure
strength is
decreased
Liquid dope
spraying
High
Low
<20 μm
Low
Middle
—
Electroplating
Table 3.
Comparisons of different self-lubricating methods.
Figure 13.
Microstructure of Cu-Sn alloy of different manufacturing technologies: (a) centrifugal casting; (b) sintering;
(c) electroplating; (d) magnetron sputtering.
The ceramic materials such as WC, SiC, h-BN are limit to use by the thermal spraying and cold spraying. The coating made by liquid dope spraying has the advantages
of high production efficiency, green materials and good lubricity. The thickness
more than 1 mm of coating on bearing prepared by supersonic flame spraying can
be obtained, and it has the advantages of low porosity, good bonding strength and
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high production efficiency. Therefore, low- temperature and medium-temperature
self-lubricating coatings should be prepared by liquid dope spray method, and
ultra-high temperature wear-resistant anti-friction coatings should be prepared by
thermal spraying.
The micro structure of tin and cooper coating made by different manufacturing technologies are shown in Figure 13 [81–85]. The obvious cracks can be
found in Figure 13a, b which manufactured by centrifugal casting and powder
metallurgy sintering respectively. The coating made by magnetron sputtering
is more smooth than that of electroplating, and the porosity of coating made by
magnetron sputtering is little than that of electroplating. The tribological and
mechanical properties of alloy coating made by centrifugal casting and powder
metallurgy sintering are poor from the results shown in Figure 13. However,
the shortages of electroplating and magnetron sputtering are the pollutions and
low efficiency respectively. The new coating formation technologies such as
liquid dope spraying and supersonic flame spraying should be applied for sliding
bearings.
4. Current problems of self-lubricating plain bearings
The traditional self-lubricating treatments of sliding bearings are mainly electroplating, magnetron sputtering, bonding self-lubricating liners and inlaying solid
self-lubricating materials. The new self-lubricating preparation technologies of
sliding bearings are mainly the liquid dope spraying and supersonic flame spraying.
The problems of sliding bearings are listed as follows through above investigations
and discussions.
1. High friction coefficient and low fatigue life
Most of the sliding bearings have not been surface treated, and these bearings
have high dry frictional coefficients, low fatigue strength, low life and low bearing capacity. The frictional coefficient of copper alloy, aluminum alloy and tin
alloy of sliding bearings is generally higher than 0.5 under dry friction condition, and it does not have self-lubricity under a wide temperature range. The
traditional copper alloys of sliding bearings contain Pb metal, which is polluting
and harmful to human. The self-lubricating materials at ultra-high temperature
are still in the laboratory research stage, and the sliding bearing with self-lubricating cannot be produced on a large scale.
2. Environmental pollution and low production efficiency
The usage of acid, alkali and heavy metal solutions during the production of
self-lubricating sliding bearings will cause serious environmental pollution.
Magnetron sputtering takes long time during vacuuming and injection processes, and the efficiency of depositing thin films is lower than other processes.
The utilization efficiency of target materials of magnetron sputtering is generally less than 40%. The multiple modification treatment processes and bonding
processes are required for preparing self-lubricating bearings using of bonding
self-lubricating fabric liners and bearings with inlaid solid self-lubricating materials. The punching holes and inlaying solid lubricating materials are required
during the production. The production efficiency of inlaying solid lubrications
is low, which cannot satisfy the requirements of large-scale mass production.
3. The theory of spraying process for sliding bearing is not deep enough
137
Friction, Lubrication and Wear
The liquid dope spraying method is one of the best methods for preparing
self-lubricating sliding bearings which used at room temperature and medium
temperature. However, the spraying mechanisms such as leveling and sagging
coating on bearing surface have not been studied. The optimum thickness of the
coating, the optimum surface roughness of the substrate, the optimum curing
temperature of the coating, and the optimum cooling temperature of the coating
were not studied in details.
4. Poor tribological properties
The wear-resisting and self-lubricating performances of coatings are poor, and
their service life under the medium temperature (200°C) is short. There are no
special materials which have low difference of thermal expansion and similar
physical properties with the given materials of bearings. The self-lubricating
materials used at high temperature are currently in the state of laboratory research
stage, and have not been prepared for bearings at large production scale.
5. Conclusion
The processing technologies and material properties of self-lubricating
sliding bearings made by electroplating, magnetron sputtering, bonded selflubricating liners, and embedded solid self-lubricating materials are studied and
summarized in this paper. The advantages and disadvantages of self-lubricating
bearings made by different technologies are shown. The widely surface treatment
of sliding bearing is electro-plating, however, the bond strength is lower than
magnetron sputtering, supersonic flame spraying, cold spraying and powder
sintering technologies, and the solutions of electro-plating is pollution and
harmful to human. The properties of thin film made by magnetron sputtering is
excellent, however, the production efficiency is too low due to the vacuum and
deposition process. The large-scale size of bearings such as bearings used in ship
diesel engine cannot be deposited due to the structure limit of magnetron sputtering machine. The porosity of bearing made by powder sintering is high, and
the alloys are oxidized at the high sintering temperature. The mechanical properties of cold spraying are better than thermal spraying, however, the materials of
cold spraying should have excellent plastic deformation ability, that the materials
such as MoS2, C, h-BN and many ceramics materials are not able to be deposit on
the surface of bearing.
Through comparative analysis, liquid dope spraying method is suggested to be
adopted as the surface treatment process for bearing using at room temperature and
medium temperature. The solid powder thermal spraying is suggested to be used
for preparation of bearings working at high temperature. The liquid dope spraying
is used in the advanced sliding bearing manufacturing companies, and the materials of liquid dope should be improved due to the wide range temperature variation
at start and stop stage. The self-lubricating coating at high temperature is lacking,
and the tribological properties of bearings at high temperature are poor. There
were few materials that had continuous self-lubricating properties at the wide
range temperature. According to the review, the lubrication materials used at high
temperature mostly were the fluorides which were poisonous at high temperature.
According to the summaries of self-lubricating treatments, the green materials,
coating formation mechanisms, technology processes and tribological properties of
liquid dope spraying and supersonic flame spraying for sliding bearings should be
studied further.
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Acknowledgements
This research was supported by Shanghai Xiangsheng beco engine bearing Co,
Ltd. and its chairman of Shengxiang Zhu.
Author details
Jun Cao1,2*, Liang Qin3, Aibing Yu1,2, Haibo Huang1,2, Guoping Li1,2, Zhongwei Yin3
and Huiyu Zhou4
1 School of Mechanical Engineering, Ningbo University, Ningbo, China
2 Part Rolling Key Laboratory of Zhejiang Province, Ningbo, China
3 School of Mechanical Engineering, Shanghai Jiaotong University, Shanghai, China
4 School of Natural and Applied Science, Northwestern Polytechnical University,
Xi’an, China
*Address all correspondence to:
[email protected]
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
139
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145
Chapter 9
Tribology: The Tool to Design
Materials for Energy-Efficient and
Durable Products and Process
Amaya Igartua, Raquel Bayon, Ana Aranzabe
and Javier Laucirica
Abstract
This chapter describes a summary of the main tribological achievements carried
out in TEKNIKER during the last 37 years. It covers the description of commercial
and newly developed tribological test benches and case studies for a wide variety
of applications. The examples refer to different tribological characterization tools
for material selection (e.g., composition, surface treatments, lubricants). It makes
emphasis in the failure mechanisms (pitting, scuffing, abrasion, adhesion, thermal
fatigue, tribocorrosion, etc.) and friction simulation of a wide range of materials
(seals, textiles, steels, cast iron, light alloys, ceramic, composites), tribological
systems (mechanical components, biomaterials, tribolubrication), and environments (vacuum, ultrahigh vacuum, low or high temperature, and corrosive). A
huge range of new testing equipment and protocols have been developed to simulate
the mentioned failure mechanisms and working environments. This knowledge will
make possible, in the future, to simulate at laboratory a still wider list of tribological
systems and develop new standards. Tribology will help to implement materials
solutions into energy and resource efficient products and process, to reduce carbon
footprint.
Keywords: tribology, tribocorrosion, lubricants, materials, pitting, scuffing,
abrasion, adhesion, erosion, thermal fatigue, die soldering, vacuum,
ultrahigh vacuum, tribodesorption, outgassing, high temperature, corrosive
1. Introduction
TEKNIKER is a nonprofit applied research institution located in the armoring
city of Eibar specialized in manufacturing, precision engineering, and tribology,
with a history of 37 years. It is a founded member of the IK4 Research Alliance, a
private alliance of seven R&D centers with 1158 persons and 308 PHD, with the
mission to generate, capture, and transfer scientific and technological knowledge
to industries. The tribology unit from TEKNIKER is working on failure diagnosis,
surface characterization, and solving tribological problems in direct collaboration
with other units from TEKNIKER like surface physics and chemistry, lubricant
chemistry, laser, additive and micro-nano manufacturing, maintenance, mechanical design, sensors, and robotics. TEKNIKER is a European referent in the field of
tribology with participation in more than 130 projects (EU, Spanish, and regional)
147
Friction, Lubrication and Wear
with more than 250 scientific contributions in congresses, journals, and books and
3 patents. It has been active in several international working groups and associations, in some of them, acting as Spanish representative:
• The COST 516 about tribology (1995–2000)
• The COST 532 about tribotechnology of engines and transmissions
(2002–2007)
• The COST 533 on biotribology (2003–2008)
• The Virtual Tribology Institute (VTI) involving 22 centers of tribology
(2005–2016)
• The steering committee member (2005–now) of the European Materials
Platform (EuMaT) holding since 2017 the co-secretary
• The NANOMAT (Basque materials and nanotechnologies team (2005–2006))
• The E!-ENIWEP, the Eureka Network for wear prevention (2006–2010)
• The MATERPLAT Spanish Materials Platform (2009–now)
• The E!-SURF, the Eureka Umbrella on Surfaces (2010–2016)
• The Network 2B Funtex on Functional Textiles (2011–2014)
• The steering committee of EMIRI, the materials for Low Carbon Energy
Industrial Initiative (2012–now)
• The International Tribology Council (2014–now)
• The Austrian COMET Action X-Tribology (Excellence Center for Tribology
(2012–now))
• The BIC, Biobased Industries Consortium (2014–now)
• The Knowledge-based Multifunctional Materials Virtual Institute (KMM-VIN)
(2016–now)
• The ECP4 Network about plastics and composites (2015–now)
• The CAPTECH Materials for Defense of the European Defence Agency (EDA)
(2016–now)
• The Coordination and Support Action (CSA) MATCH, Materials Open House
(2014–2017), promoted by the Alliance of Materials A4M that was created by
Suschem, Nanofuture, EMRS, FEMS, EMIRI, and EUMAT
• The European Materials Modeling and European Materials Characterization
Councils (EMMC-EMCC) (2017–now)
• The materials for construction team of the ECTP Construction Platform
(2018–now)
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Tribology: The Tool to Design Materials for Energy-Efficient and Durable Products and Process
DOI: http://dx.doi.org/10.5772/intechopen.85616
• The European Pilot Projects Network (EPPN) (2017–now)
• The Basque Country representation in the materials for batteries S3P Smart
Specialization Region initiative (2018–now)
TEKNIKER has been active in the organization of Congress (LUBMAT,
IBERTRIB, COST 516, COST 532, COMADEM, EUMAT, NANOFILMS); international meetings in cooperation with MATERPLAT, EMRS, FEMS-SOCIEMAT,
EMCC, and EPPN; and courses such Marie Curie (Oct. 2011), LUBMAT (2012,
2016, 2018), or Erasmus+ (2018).
2. Commercial equipment
The philosophy from TEKNIKER has been to buy commercial equipment when
available and to develop and construct new testing benches, when they are not easily available. Thus, TEKNIKER is equipped with the most advanced commercial
equipment covering a huge range of testing standards such as:
• FALEX high-performance and FALEX multispecimen test machines (ASTM
G99, ASTM D3702, ASTM D5183, ASTM D2266, ASTM D4172)
• FALEX Four-Ball Machine to measure antiwear properties (ASTM D 2266 for
greases, ASTM D 4172 for oils) and extreme pressure properties (ASTM D
2596 for greases, ASTM D 2783 and ASTM D-7421 for lubricants)
• FALEX tapping torque test machines (ASTM D5619)
• OPTIMOL SRV-III machine to measure antiwear properties (ASTM D 5707
for greases, ASTM D 6425 and DIN 51834 for lubricants) and extreme pressure
properties (ASTM D 5706 for greases, ASTM D 74121 for lubricants)
• CETR UMT-3 reciprocal tribological test, Block on Ring Test (ASTM G77),
scratch test (ASTM D7027, ASTM G171, ISO 20502), Ball on Flat (ASTM
G-133), Friction dissipation (ASTM G-203), Pin Abrasion (ASTM G132), Pin
on Disc (ASTM G99), Scratch hardness (ASTM G171), Thrust washer (ASTM
D3702), Rolled web friction (ASTM G143), Viscoelastic properties (DIN
53513), Indentation hardness (ISO 14577), Adhesion and mechanical failures
(ASTM C 1640)
• CSM nanotribometer (Load from 20μN-2N)
• Twin disc machine with Block on Ring configuration (e.g., ASTM G176,
ASTM G77)
• STRAMA FZG gear test machine, wear (ASTM D 4998), Micropitting (FVA
54/I-IV), DGMK 575), Pitting (FVA 2/V), Scuffing (DIN 51354-1/2, ISO
14635-1, CEC-L-07-96, IP 334/93, ASTM D5182-91), grease (DIN 74), Extreme
Pressure test (FVA 243)
• Two bearing tests by Elgeti Engineering to characterize bearings lubricated
with greases and oils (DIN51819) and to develop new lubricants, coatings,
rolling bearings designs, and predictive maintenance activities
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Friction, Lubrication and Wear
• Ducom Erosion Tester (ASTM G-76)
• TABER abrasion machine (many standards, e.g., ASTM 4060 (paints), ASTM
D3884 (textiles))
• Pendulum slip safety testing (UNE-ENV 12663, CEN/TS 16165, BS7976-2,
ASTM E303, BS EN 13748-1)
• GMG tribometer test for flooring security (DIN 51131, CEN/TS 16165)
• Microtest tribometer transformed by TEKNIKER in a tribocorrosion device
• NEURTEK Washability Test, humid rubbing test (UNE-EN ISO 11998, DIN
53778, ASTM D 2486, ASTM D 4213)
• CORMET stress corrosion cracking in liquid media with electrochemical
control until 300°C and autoclave to test stress corrosion at high temperature
(800°C) and gaseous media (SO2, NO2, CO2, O2) (ASTM Practice G 129, ASTM
Test Method E8). NACE Standards (TM0198, TM0177)
• Corrosion test salt spray (ISO 9227, ASTM B117)
• Metrohm Autolab potentiostats, Electrochemical corrosion (ISO 16773-1-4),
liquid corrosion (ISO 2812-1, ISO 2812-2), corrosion classification
(ISO 12944-6), others (ASTM G1, ASTM G3, ASTM G5, ASTM G61, ASTM
G96, ASTM G102, ASTM G106)
• Climatic chambers (UV, temperature, humidity, condensation), (e.g., ISO
6270, ASTM D4329, ASTM D4587, ASTM D4799, ASTM D5208, ASTM G151,
ASTM G154, DIN EN 12224, DIN EN 1297, DIN EN 13523-10, DIN EN ISO
4892-1, EN 927-6, ISO 11997-2, ISO 16474-3, ISO 4892-3, ISO 20340 (Off
shore, Norsok), D4585)
• INSTRON mechanical tests at different temperatures at 1–50 kN with speed
range 0.005–500 mm/min (many, e.g., tear test (ISO 13937-2:2000))
• Compatibility of seals with lubricants (ASTM D471)
• Complete laboratory for paint characterization to measure impact (e.g.,
ISO 6272), falling sand abrasive test (e.g., ASTM D 968, ASTM D333; ASTM
D1395; ASTM D 2205), crosscut test (e.g., ASTM 3359), bend test (e.g., ISO
6860), Persoz and Kónig hardness (e.g., ISO 1522), pencil scratch test (e.g.,
ISO 1518-4), cupping test (e.g., EN ISO 1520), pull off test (ISO 4624; ASTM
D4541), brightness loss (Crock meter)
When possible, round robin tests have been carried out (pin on disc tests, tribocorrosion tests) with different organizations having similar commercial machines.
3. New testing benches
The differential from TEKNIKER is the capability to develop unique tribological test machines and new testing configurations to design a wide variety of working conditions (temperature, load, speed) in different environments (atmospheric,
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inert, vacuum, ultrahigh vacuum, corrosive, etc.) in order to cover different
tribological problems to analyze the tribomechanism taking place on the rubbed
surfaces (adhesion, die soldering, galling, abrasion, pitting, micropitting, fretting,
tribocorrosion, tribodesorption, tribolayer formation, impact, erosion, tactile friction, corrosion, fatigue corrosion, fretting-corrosion, thermal fatigue, fading, etc.).
The objective of the measurements carried out with the tribological testing
machines is to measure differences in the material behavior. For that, a reference is
always used that corresponds to a material with a well-known behavior. The standard
deviation of the measurement is established with the reference material. The value
of the standard deviation depends on (a) the working conditions (pressure, velocity,
temperature, etc.) and (b) the properties (roughness, texturing, composition, etc.).
The difference between two materials is significative, if it is higher than three times
the standard deviation of the measurements. In some cases, also standard protocols
have been developed (e.g., tribocorrosion tests) in collaboration with ISO/CEN
groups.
The new test benches developed by TEKNIKER have been the following:
• New atmospheric, vacuum, and ultrahigh vacuum tribometer with capacity
to test friction and wear at different temperatures and also analyze the tribodesorption of gases, assisted by mass spectra.
• New DEMETRA machine, to measure the outgassing of the lubricants,
polymeric materials, and coatings that need to work under vacuum conditions
(ASTM E 595, ECSS-Q-ST-70-02C).
• New drag friction tester to measure drag friction for different applications
(e.g., paints in the ships, friction losses in heat exchangers).
• Tribocorrosimeters under oscillatory and rotatory conditions, where it is possible to calculate mechanical wear, corrosive (chemical) wear, and the synergy
between mechanical wear and chemical wear (UNE 112086, ASTM G119 and
internal protocols).
• Bearing tests (radial and axial), to measure torque and wear (now in MecautoWisco Company).
• Real bearing friction and wear test configuration adapted to a Twin Disc and
Falex machines.
• Ball on rod machine to test point contact fatigue at high pressure and speeds
(12000prm, reference STP 771).
• Cylinder on cylinder to test line contact fatigue at high pressure and speeds
(reference STP 771).
• Thermal fatigue test bench, to simulate cycles of high temperature (up to
900°C) and low temperature (the T°C depends on cooling unit selected). One
machine is available in TEKNIKER and another in AUDI.
• Gravelometer to test the stone-chip (abrasives, screws) resistance to impact
of coatings (paints, varnish) (reference ISO 20567-1:2005). Internal protocols
have been developed to test impact resistance in polymer injection molds.
• Clutch dynamometer test, to measure torque and wear (now in GOIZPER
Company).
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• Disc brake dynamometer test bench, to measure the friction, wear, and
thermal fatigue of disc brakes (now in Edertek-Fagor Ederlan company).
• Testing configurations of engine component wear and friction test have been
adapted to the SRV, FALEX, and CETR machines (e.g., ASTM G181-11, ASTM
G206-17). Several new protocols have been developed to simulate valve stem/
guide, gudgeon pin/piston, piston ring/cylinder liner, piston ring/piston,
piston skirt/cylinder liner, impact of valve seat/valve head, etc.
• New seals test bench under reciprocating and oscillatory movement
with capacity to test with different lubrication systems and different
temperatures.
• Prosthesis simulators involving real components for evaluating tribological
properties of hip prosthesis coatings and synovial fluids, adapted to FALEX
and SRV machines.
• Car wash type test, cleaning and abrasive testing of glass (ISO 20566) and
solar mirrors (internal protocols).
4. Description of the main new test benches
4.1 CATRI (CA3UHV) machine
CATRI (CA3UHV) machine has been developed by TEKNIKER to determine
the friction and wear properties in atmospheric, vacuum, and ultrahigh vacuum
conditions. It is also possible to measure the gas tribodesorption detected by
mass spectra, during friction and wear tests. Both the force sensor and sample
holder of the experimental system have been patented, PCT/ES2009/070635 and
PCT/ES2010/07273, respectively [1–4]. In this machine, the patents from CSIC
ES200700480 and ES2320513B1 have also been validated. This machine allows
complex tribological characterization of materials and coatings in a wide range
of gas pressures from atmospheric to ultrahigh vacuum and loads (0.1–20 N).
This system can be used to study tribological behavior of the coatings under
gradually varying gas pressure and composition, simulating the environments on
the various stages of the service life of the real aerospace systems. The machine
can work under ultrahigh vacuum (5 × 10−10 mbar) and inert gas in controlled
atmosphere (from 103 to 5 × 10−9 hPa). T°C can reach up to 350°C. It can be possible to quantify the gas tribodesorption from materials and coatings (Figure 1).
Figure 1.
(a) CATRI machine, (b) detail of the sample holder, TEKNIKER©.
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4.2 DEMETRA machine
DEMETRA machine is developed for the analysis of the outgassing from lubricants and materials (e.g., coatings, textiles, and plastics) in vacuum conditions.
The bench test has been built using the ASTM E595-07 and ECSS-Q-ST-70-02C
Reference Protocols. In the test, the volatile components of the materials and lubricants are determined at 125°C in vacuum conditions. The flexibility of the machine
allows to modify working conditions. According to the standard, the Recovered
mass loss (RML) should be <1% and the Collected volatile condensable material
(CVCM) should be <0.1% (Figure 2) [3].
Figure 2.
Details of (a) vacuum chamber, (b) evaporation unit with four testing stations, and (c) DEMETRA machine
developed by TEKNIKER.
4.3 Drag friction test
Drag friction test is for the determination of the drag friction torque of antifouling
paints or surface treatments (e.g., texturing). The test samples are hollowed cylinders of
200 × 200 m that can be either located in ships or in the port to be covered with fouling
after a specific time period. The torque before and after fouling and with different surface treatments can be compared at different rotating speeds, simulating either laminar
or turbulent flow. Two test configurations are available with gaps of 5 and 10 mm. The
machine has been developed by TEKNIKER in the frame of EU Project Foul X PEL
(https://cordis.europa.eu/project/rcn/101484/reporting/en) (Figure 3) [5, 6].
Figure 3.
(a) Drag friction tester, TEKNIKER©. (b) The image shows the testing cylinder location in a ship.
4.4 Tribocorrosion testers
Tribocorrosion testers have been developed combining a tribometer and a potentiostat. The test equipment allows monitoring and control both mechanical and
electrochemical parameters. A tribometer creates relative motion, either unidirectional (rotatory) or bidirectional (reciprocating), rubbing two surfaces against each
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other. The electrochemical cells are used to record and control the electrochemical
parameters. These cells are usually composed of three electrodes: a reference electrode, a counter-electrode, and the working electrode. The reference electrode has a
stable, well-defined potential, and it is used to register the potential of the working
electrode, i.e., the test sample. Typical reference electrodes are saturated calomel
electrodes (SCE) and silver/silver chloride electrodes (Ag/AgCl). The counter-electrode is used to measure or control the current and is usually made of inert materials
such as platinum, gold, or graphite. The electrodes are connected to a potentiostat
to register the potential between the reference electrode and the working electrode
or the current between the counter-electrode and the working electrode. A typical
tribocorrosion test setup is schematically shown in Figure 4 [7–16].
Figure 4.
Experimental setup of a tribocorrosion device for a unidirectional tribometer under ball on disc configuration,
TEKNIKER©.
4.5 Test bench for plain bearings
A test bench is built with the objective to carry out friction test and wear test
in plain bearings. Alternative movement has a stroke of 120–125 mm, a speed of
1–40 m/min, and a maximum load of 3000 kgf (Figure 5) [17, 18].
Figure 5.
Plain bearing testing machine, designed and constructed by TEKNIKER for Mecauto-Wisco company.
4.6 Ball on rod machine
Ball on rod machine is built with the objective to study the point rolling contact
fatigue of the bearing materials and coatings, to apply to ball rolling bearings. It follows
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the protocol from Douglas Glover, “A Ball-Rod Rolling Contact Fatigue Tester”
(ASTM STP 771, J. J. C. Hoo, D., American Society for Testing and Materials, 1982,
pp. 107–124). It has a variable speed, reaching up to 12,000 rpm instead of 3000 rpm
of the documented protocol. The typical pressure applied is 5.5 MPa. The lubrication
is an air/oil system with controlled flow, typical lubrication regime for high-speed
rolling bearings. Alternatively, other lubrication systems can be selected. The balls
can be made from steel and ceramic and with or without coatings with a diameter of
12.7 mm. The roller has a diameter of 10 mm and length of 125 mm. The ball on rod
machine has a double testing device for parallel testing. The time to reach the micropitting or pitting is recorded and monitored by an increase of the vibrations. The machine
was developed by TEKNIKER in collaboration with SNR, in the frame of EU Project
Eurobearing (https://cordis.europa.eu/project/rcn/6657/factsheet/es) (Figure 6) [19].
Figure 6.
Ball on rod machine, TEKNIKER©.
4.7 Cylinder on cylinder machine
Cylinder on cylinder machine, built to study the pitting phenomena in roller
bearings, simulates the line contact rolling fatigue behavior of the materials. The
machine is based on ASTM STP 771 protocol, with the advantage of reaching a maximum speed of 12,000 rpm with air/oil lubrication. The roller’s size is 12x12mm. The
duration of the test until reaching the micropitting or pitting phenomena is recorded
for different types of materials and coatings of the rollers. The test stops, when the
level of vibration increases, due to generation of pitting in the contact. The machine
was developed by TEKNIKER in collaboration with SKF, in the frame of EU Project
REFINE (Figure 7) (https://cordis.europa.eu/project/rcn/36428/factsheet/en).
Figure 7.
(a) Cylinder on cylinder machine, TEKNIKER©, (b) pitting in a roller.
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4.8 The thermal fatigue
The thermal fatigue test bench has been built to simulate thermal cycles of high
temperature generated by induction heating and low temperature cooled with
spray. There is one machine in TEKNIKER and one in AUDI. The machine has been
developed to simulate the heating and cooling cycles of the high pressure die casting
dies. The time to thermal fatigue crack failure mainly depends on (a) the maximum
temperature, (b) the temperature gradient, (c) the geometry, and (d) the designed
cooling channels inside the mold (testing block). The machine can simulate a time
to thermal fatigue failure similar to the real applications (Figure 8) [20].
Figure 8.
(a) Cooling process, (b) heating process of the thermal fatigue machine TEKNIKER©.
4.9 Brake disc testing machine
Brake disc testing machine is built with the objective of carrying out friction,
wear, and thermal fatigue tests of disc brakes and brake drums. The maximum
velocity is 2500 rpm and the maximum load is 105 kg/m2. During the test, the
torque and the temperature and wear are recorded. Different protocols from automotive suppliers can be applied (e.g., AUDI, Volkswagen) (Figure 9) [21].
Figure 9.
Disc brake testing machine, designed and constructed by TEKNIKER for Fagor Ederlan company.
4.10 Clutch dynamometer test
Clutch dynamometer test has been built with the objective to measure the
friction and wear of the clutches at fixed or variable conditions of load and speed.
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Measurement of force, the friction loss between the cylinder and braking films,
and temperatures at different points, forces, torque, and speeds are recorded. The
specific power, specific energy, the dynamic and static torques, the sliding time,
and initial speed can be monitored during breaking or evaluated during the test
(Figure 10) [22].
Figure 10.
(a) Clutch dynamometer test bench. (b) Control unit of the dynamometer, constructed by TEKNIKER for
GOIZPER company.
4.11 The TESSA machine
The TESSA machine has been developed by TEKNIKER to measure the friction,
wear, and leakage of the dynamic seals [23–28]. It can reach a maximum speed of
6 m/s. The machine has been adapted to work under variable temperature integrating a climatic chamber. The test chamber is modular, and it has the capability to
measure the differential pressure between the two sides of the seals for pistons
and rollers and evaluate the leakage. Oils sensors, developed by TEKNIKER (www.
tekniker.es/en/ and ATTEN2 (https://atten2.com/en/), can be used to monitor the
generation of wear particles in lubricated seals (Figure 11).
Figure 11.
(a) New seal test bench constructed by TEKNIKER with two units with oscillatory and reciprocal movements
and climatic temperature control (low and high temperatures). (b) Example of test conditions.
4.12 Glass and mirror wash test
Glass and mirror wash test has been built to evaluate the scratch abrasion resistance of coatings used in glass of the cars and solar mirrors. In automotive sector, the
glass car wash resistance is assessed. A machine-based washing is simulated in the
laboratory environment using a rotating brush and synthetic dirt. The test conditions
have been designed to be as close as possible to the real conditions in a car wash and
solar mirrors, in order to evaluate the cleanability, the abrasion resistance, and their
durability. Protocols for solar mirror evaluation are under development by TEKNIKER
in the frame of EU Project In Power (http://in-power-project.eu/) (Figure 12).
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Figure 12.
Glass and solar mirror testing device TEKNIKER©.
5. Case studies
Different case studies have been selected to cover examples of different tribological characterization tools and equipment used for material selection (composition, topography, surface treatments, lubricants), making emphasis in the failure
mechanism and friction simulation of a wide variety of materials, tribological
systems, and environments.
5.1 Tribology for aggressive environments
5.1.1 Vacuum and ultrahigh vacuum tribology
The CATRI tribometer (see Figure 1) has been used to screen the tribological
properties under vacuum and ultrahigh vacuum of the steel/coating and titanium
materials lubricated with different fluids (oils, greases, or ionic liquids). For
example, it has been observed that it is possible to find non-halogen ionic liquids to
lubricate steel under vacuum and ultrahigh vacuum conditions (e.g., phosphonium
phosphate) and to lubricate titanium; up to now, better results have been obtained
with halogen-containing ionic liquids or lubricants (e.g., [Bu3MeP][Tf 2N]). The
desorption of CF3 detected in the mass spectra occurred just in the moment when the
friction was reduced (see Figure 13a). During the test, a TiFx tribolayer was generated. Titanium and inorganic F and S(II) were detected by XPS. The reaction mechanism that explained the TiFx layer generation was elucidated (see Figure 13c) thanks
to the fragments of the mass spectra (see Figure 13b) detected during the tribodesorption process. The machine and protocols have been used in the National Project
CATRI [1], the EU Project MINILUBES [2], the Austrian X-Tribology COMET
Initiative [3], the Eurostars Project VACUUM DLC [4], and industrial projects.
Figure 13.
(a) Friction coefficient during ultrahigh vacuum tribotest (b) mass spectra, highlighting the hydrogen and CF3
fragments from the F-containing lubricant. (c) Proposed tribomechanism for the TiFx generation.
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5.1.2 The DEMETRA machine
The DEMETRA machine (see Figure 2) was built to measure the outgassing
under vacuum to screen and select the materials and lubricants that can work
under these conditions. The volatility data of the outgassing measurements of
the ionic liquid [Bu3MeP][Tf 2N] has been compared to the reference lubricant, a
perfluoropolyether (PFPE). It can be stated that the ionic liquid exhibits acceptable
outgassing data according to the requirements of the standard ASTM E595 (RML
<1.0% and CVCM <0.1%) [3]. The machine has been used in EU Projects VACUUM
DLC and Austrian X-Tribology COMET Initiative. It has also been used to study
dependence of outgassing of thermal fluids in function of the viscosity for heat
exchangers (see Section 11.2) in EU Project SUSPIRE (http://suspire-h2020.eu/)
(Figure 14).
Figure 14.
Outgassing data of the PFPE oil and the ionic liquid (ASTM E595).
5.1.3 Drag friction tribology in marine environments
The development of the drag friction test (see Figure 3) has been carried out
in the frame of EU Project FOUL X PEL [5, 6]. In this study, the torque of different antifouling paints before and after immersion in a ship or in the Motrico
Port has been compared. The tests have been carried out with artificial sea water
fluid (ASTM D1141) in a container under rotation at different speed, generating
laminar or turbulent regime, using different gaps of 5 and 10 mm. The effect of
biofouling, roughness, and fluid properties can be measured. In the example,
two fluids FX1 and FX2 were tested and being selected FX2 due to their lower
drag friction in all the range of speeds tested. The machine has also been used in
the EU Project SUSPIRE to test thermal fluids with different viscosities to select
those with lower drag friction loss and higher energy efficiency (see Section 11.2)
(Figure 15).
Figure 15.
Comparative drag friction measurement of two antifouling coatings, before and after 1-year sea exposure in a ship.
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5.1.4 Tribocorrosion
The coupling of standard tribometers with a potentiostat has been done to
measure wear-corrosion behaviour, that means to study the mechanical, the
chemical wear and the synergy between both phenomena. In the frame of RAMPE
Project [11], the tribocorrosion properties of Inconel + Cr electrodeposited coating is compared with CrN+TiN coating deposited by Physical Vapour Deposition
(PVD) developed by TEKNIKER. It is observed that the impedance (corrosion
resistance) after the wear test, is considerably reduced for Inconel + Cr Coating.
In case of CrN+TiN PVD coating, the impedance curve resulted unaltered after
wear test. These results correlate well with the wear scars measured after the
test, for both coatings (see Figure 16). The technique has been used also in EU
Projects FUNCOAT [7, 29–31], FRONTIERS [10], NADIA [32], in Regional project
TRICONDEX [8], FRONTIERS [12], and National project NANOTRIBOCOR [9].
Figure 16.
Impedance measurements before and after wear test for (a) Inconel + Cr coating and (b) Inconel + PVD
TiN + CrN coating. Wear scars: (c) Inconel + Cr and (d) Inconel + TiN/CrN coating.
5.1.5 Tribocorrosion in marine and offshore environments
High-strength low-alloy (HSLA) steels employed in offshore applications suffer
high degradation due to their high corrosivity in seawater and the wear generated
during mooring chain movement. The results, obtained in the frame of the FONDEO
Adhoc project financed by the Spanish Minister of Science, showed an acceleration
of corrosion during wear experiments, as consequence of the synergism generated
between wear and corrosion. In Figure 17(i), it can be seen, how the sliding has
modified the electrochemical behavior of both steels. The effect of several parameters
such as seawater temperature or salinity have also been studied to understand their
Figure 17.
(i) Potentiodynamic polarization curves obtained for two HSLA steel grades (R4 and R5) under corrosion
(without sliding) and under tribocorrosion (with sliding) in synthetic seawater. (j) Topography of the wear
tracks obtained after tribocorrosion tests on: (a) the TSA and (b) PEO-treated TSA.
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influence in the steel degradation [13, 14]. In order to protect steels in mooring lines of
floating structures, it has been developed some surface treatments based on thermally
sprayed aluminum (TSA) coating with and without post-treatment by plasma electrolytic oxidation (PEO). In Figure 17(j), it can be highlighted the reduction of wear scar
after tribocorrosion tests, can be highlighted and produced when the TSA coating on
the steel is additionally treated by plasma electrooxidation (Figure 17(jb)) [15, 16].
5.2. Tribology of mechanical components
5.2.1 Tribology of journal bearings
Two testing benches have been constructed (see Figure 4) for Mecauto company
to study the torque and wear in axial and radial bearings. Also, a standard tribotest
has been adapted to study the limits of pressure and velocity of the tribological
pair. In the frame of BELEADFREE Project, a test has been designed to evaluate
the tribological properties of real bearings. In the frame of EREBIO EU Project,
the reduction of friction and contact temperature has been proven when using a
biodegradable low-viscosity and environmentally friendly engine oil for the lubrication of bearings using a basic thrust washer configuration [17]. In the project
ECOBEARINGS [18] and BELEADFREE, the lead content of the bearings have been
reduced or eliminated (Figure 18).
Figure 18.
Evolution of temperature when using biodegradable and mineral lubricants to lubricate journal bearings.
5.2.2 Tribology of rolling bearings
As described before, the ball on rod (Figure 6) and cylinder on cylinder
machines (Figure 7) have been constructed by TEKNIKER to study point and
line contact rolling fatigue to understand the pitting failure behavior of rolling
bearing materials, under high contact loads and high speeds. In the frame of
EUROBEARING project, different PVD coatings were studied, measuring the
load-carrying capacity, the adherence, the abrasion resistance, and the hardness,
as shown in the next table. Their fatigue resistance was also tested using the ball
on rod machine. The long fatigue lifetime (1000 million cycles duration) of the
TiN + C coating and their good behavior against abrasion and adhesion make this
coating a promising alternative to be applied in high-speed rolling bearings [19]
(Table 1). In this subject, (a) the relationship between vibration generation and
oil particle generation (EU Projects TESS) [33], (b) the fatigue behavior of roller
bearings (REFINE), and (c) the behavior of different PVD coatings and lubricants
for rolling bearings (National Project HIEFBE) have been studied, and (d) a test
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configuration to study the tribology of real bearings has been developed, adapted to
FALEX tribological test (Project BIOMON).
Coating type
Loadcarrying
capacity
Adherence
Wear
protection
Hardness
Fatigue
resistance
CrN
Good
Good
Good
Medium
Bad
Mo
Good
Good
Bad
Low
Bad
TiAlN
Good
Medium–good
Good
High
Good
TiCN
Bad-medium
Bad
Good
High
Good
TiAlCN
Medium
Medium
Good
High
Good
TiN + C (C
sputtered)
Medium–good
Good
Medium–
good
Medium–
high
Very good
Table 1.
Qualitative behavior of coatings to increase lifetime of rolling bearings [19].
5.2.3 Tribology of clutches and brakes
Brakes and clutches require high stable friction coefficient. To understand the
tribology phenomena of these systems, testing protocols have been developed for
the standard FALEX (high-performance and multispecimen) tribometers to study
the friction wear mechanism of brakes and clutches (high temperature abrasion,
adhesion, and fading) and to study the relationship of the friction coefficient
with the squeal generation. Additionally, a dynamometer test bench has been
constructed to test disc brakes (Figure 9) and clutches (Figure 10). In the frame
of the i-SINTER Project, the correlation between the friction measured in pin on
disc tests and the torque measured in clutch tests has been studied, observing very
similar values, especially at low loads (Figure 19). These conditions were selected
for screening of the materials with pin on disc tests, before final validation in the
clutch test. The tribological knowledge on dry friction has been used in the projects
M-eranet JOLIE (brakes) [21], Manunet BRAKE SQUEAL (clutches) [22], and
Industrial Project I-SINTER (clutches).
Figure 19.
Coefficient of friction during clutch test and pin on disc test carried out with the same materials.
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5.2.4 Tribology of gears and transmissions
In the frame of the EU Project OPTIMIZE, TEKNIKER has upgraded the FZG
machine, to measure the vibrations, noise, and transmission losses and to complement the study of micropitting, pitting, or scuffing phenomena (Figure 20).
In this topic, the team has been working in the EU Projects TESS [33], OPTIMIZE
[34], EREBIO [35–37], VOSOLUB [38], SUNOIL [39], LUBRICOAT [40],
BIOGREASE [39], and BIOMON [41] and the industrial projects AEROHUMs
and SELENA.
Figure 20.
a) Upgrading of FZG machine to monitor vibration, transmission error, power losses, noise, temperature, and
drive motor intensity and (b) sensors and signals collected [34].
5.3 High-temperature tribology
5.3.1 Tribology of high-pressure die casting (HPDC) and polymer injection molds
(PIM)
In the frame of MUSIC Project, a thermal fatigue machine has been constructed
to reproduce the main failure of the high-pressure die casting molds. In Figure 21a,
the thermal cycles can be seen in high-pressure die casting process reproduced in
the thermal fatigue machine, and in Figure 21b, the thermal fatigue mechanism
can be observed, reproduced in a flat specimen with internal cooling circuits,
representing the die. The thermal fatigue mechanism can also be reproduced in 3D
complex geometries. Setup of testing protocols has been carried out to simulate also
other failure mechanisms of HPDC and PIM molds such as mechanical and chemical die soldering, abrasion and erosion resistance, and the corrosion behavior. The
knowledge generated in MUSIC project has been applied to the EUROSTAR Project
Figure 21.
(a) Thermal cycles in the thermal fatigue machine TEKNIKER©, (b) thermal cracks reproduced in the tested
block of the mold material after 10,000 thermal cycles.
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SUPERSLIP (to select surface treatments for polymer injection molds) and to the
industrial projects HARCO, ALEPRE, MEFOLUB and MMPUL [20, 42–45].
5.3.2 Tribology of engine and turbine components
The development of testing configurations adapted to standard tribological testing machines can be highlighted in order to test real parts of engine and
turbine components (e.g., valve/guide contact, piston ring/cylinder liner contact,
the piston skirt/cylinder liner contact, valve head/valve inserts, gudgeon pin/
piston, gland/piston rod, piston rod/seal, turbine support, etc.). In Figure 22,
the results of scuffing tests of the piston ring/cylinder liner used to screen suitable biodegradable oils compatible with bioethanol for two stroke engine oils can
be seen. Most of the lubricants suffered scuffing, except the one called SEMO36
that was suitable for the application. The testing protocols developed has been
used in the EU Projects POWERFUL [46], EREBIO [47, 48], Nano-HVOF [49],
EFCAP [50], COST [51], CLEANENGINE [52, 53], NANOMAG, and NADIA [32];
in the regional project TRIBORE and MOTOLURE [47]; in the industrial projects
REMTRAL [51], AUMORE, RECOLURE, EQUIMOTOR and EQUIMOTOR
PLUS [54], ABADIE, and 2 MW engine; and in the national projects RAMPE and
ALELLA.
Figure 22.
(a) Piston ring/cylinder liner configuration developed by TEKNIKER. (b) Selection of SEMO 36 oil to avoid
scuffing of bioethanol/biolubricant mixture, in piston ring/cylinder liner tests.
5.4 Tribology of special materials
5.4.1 Tribology of seals and elastomers
As already described (see Figure 11), a test bench has been constructed to test
real seals to study their friction, wear, and leakage under oscillatory and reciprocal motions. A simplified tribological test has also been developed to reproduce
the failure mechanism and the friction and wear of the seals. In the frame of EU
Project KRISTAL, the laser texturing was applied by TEKNIKER directly on seals
materials or transferred through the molds. In Figure 23a, it can be observed the
effect of surface laser texturing on seals materials reducing significantly the friction coefficient. In the EU project STOKES, different surface texturing geometries
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were tested in the seals test bench constructed by TEKNIKER, selecting also the
most appropriate texturing geometry. This knowledge has been applied to EU
Projects FUNDTRIBO [26], ISSELUB, the regional projects MODELOST [23] and
EMAITEK [24, 25], and the industrial projects 3D FLEX and ELASWEAR.
Figure 23.
(a) Effect of texturing to improve the tribological properties of different types of seals. (b) Results of the
TESSA seal test bench TEKNIKER© with different texturing geometries and selection of the one reaching a
minimum torque.
5.4.2 Tribology of anti-slippery floorings
In this context a test protocol has been developed to evaluate the friction (static
and dynamic) and wear of the floorings determining the anti-slippery properties
simulating the lifetime of the floor (Figure 24). This knowledge has been used in
the national project TRIBOSTAND, in the EU Project SLIP SAFE, and in a regional
project SEGURPAV [55].
Figure 24.
Test protocols have been developed to evaluate the durability, the cleanliness, and the comfort of the floorings
(a) involving persons, (b) tribometers, and (c) contact angle measurements.
5.4.3 Tribology of textiles
Testing protocols have been set up to evaluate mechanical properties, abrasion,
and tactile properties of the textiles (Figure 25). This knowledge has been used in
the EU Project 2B FUNTEX [56].
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Figure 25.
(a) Friction measurements as indicator of textile tactility in dry and wet conditions for cotton, polyester, and
the 50% mixture. (b) Material used to simulate the skin at laboratory. (c) Real skin.
5.5 Biotribology
5.5.1 Tribology of autologous bones
The use of impact and compression tests to understand the effect of thermal treatments in artificial bones and inserts has been studied in the frame of the EU Project
AUTOBONE. In Figure 26, it can be appreciated that the thermal treatment reduces
the wear caused by the impact, improving the toughness of the artificial inserts
composed of hydroxyapatite and collagen [57].
Figure 26.
(a) Configuration of impact test. (b) Impact resistance of the hydroxyapatite/collagen bone inserts with and
without thermal treatments.
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5.5.2 Tribology of hip and knee implants
A testing configuration has been designed adapted to a commercial FALEX
tribometer to simulate the wear of hip/acetabular cup. Friction, wear, and tribocorrosion protocols have also been developed to simulate the lifetime of the hip and
knee prosthesis. In Figure 27, it is possible to see how the TiCN-2 coating deposited
by Physical vapor deposition (PVD) by TEKNIKER can enhance the tribocorrosion properties and antibacterial properties. The antibacterial properties are still
enhanced when adding a sacrificial silver top layer, also applied by PVD. The Ag
layer might be active as anti-infection layer, during implantation, since it will be
easily removed due to their poor wear resistance. The protocols have been used in
the national projects FUNCOAT, DELECA, SINOVIAL, FUNMAT in the industrial
BIOTIDE project, and the Eurostars INNOVATIDE Project [29–31].
Figure 27.
(a) Program for coating evaluation. (b) Tribocorrosion resistance of Ti6Al4V alloy before and after coating
with TiCN-1 and TiCN-2. (c) Antibacterial properties of Ti6Al4V, after coating with TiCN-2 without and
with a top silver layer.
5.5.3 Dental tribology
The development of testing protocols can be highlighted to simulate friction,
wear, impact, and tribocorrosion in dental implants. In Figure 28, the results of
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Friction, Lubrication and Wear
tribocorrosion tests carried out to compare the behavior of titanium before and
after treatment with different plasma electrooxidation coatings (PEO) developed
by TEKNIKER using different process conditions are represented. The behavior
of the coatings improved when increasing the plasma intensity. Also, the wear
volume of a reference and new electrolyte was compared observing a significative
improvement with the new electrolyte developed in TEKNIKER. This knowledge
has been applied to the national project FUNCOAT and industrial projects [58].
Figure 28.
(a) Tribocorrosion test of titanium (Ti) coated with two types of PEO coatings. (b) Wear volume of
tribocorrosion test of Ti and PEO coatings using two electrolytes.
5.5.4 Tactile properties of steel
A similar test protocol mentioned in Section 5.4.3 has also been used to evaluate
the steel sheet tactility. The effect of the textured surface geometries of steel sheet
surfaces transferred by lamination with laser textured rollers has been studied. The
laser texturing was carried out by TEKNIKER. This knowledge has been used in the
EU Project STEELTAC [59].
5.6 Tribolubrication
5.6.1 Tribology of environmentally friendly lubricants for cutting and forming
applications
Testing protocols has been developed to compare tapping torque results and
center of numeric control (CNC) machines to screen torque and wear of cutting
and forming fluids and different coatings to increase the efficiency. In the EU
Figure 29.
Comparison of mineral and vegetable lubricants measuring (a) relative efficiency in tapping torque machine
and (b) flank wear in CNC grinding machine.
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Project VOSOLUB [60], similar tribological properties have been shown between
mineral- and vegetable-based cutting lubricants. Both the efficiency of the fluids
measuring the torque with the tapping torque machine and the flank wear with a
CNC controlled grinding machine have been evaluated (Figure 29). The knowledge
has been applied to EU Projects IBIOLAB [60], DECOLUB [61], and other related
projects such as ECOLUBRO, NANOCOMP, MEFOLUB, and CLAREFOSS.
5.6.2 Tribology of biolubricants for bearings and gears
Testing protocols have been developed to compare the behavior of the biolubricants
as alternative to mineral-based oils to lubricate mechanical components (e.g., wind mills,
hydraulic pumps, excavators). In the example, a glycol-free lubricant has been developed increasing their load-carrying capacity in comparison with the glycol-containing
one. The glycol-free lubricant is biodegradable, and it can be an interesting alternative
as a fire-resistant hydraulic oil (Figure 30). The protocols have been used in the EU
Projects VOSOLUB [38], SUNOIL and BIOGREASE, [39], LUBRICOAT [40], CTVONET and LLINCWA [62], BIOMON and IBIOLAB [41], the national projects LUVE and
BIOVESIN [63, 64], and the industrial projects ADIVINA, PAVIA, and NANOINTECH.
Figure 30.
(a) Load-carrying capacity of glycol and glycol-free lubricants. (b) Biodegradability of glycol-free lubricants >60%.
5.6.3 Tribology of ionic liquids
Testing protocols has been developed also to evaluate the behavior of ionic liquids as
lubricants in different environments studying friction, wear, and tribocorrosion behavior. In Figure 31, it is represented the friction and wear scar of the Ionic Liquids DIL3 and
Figure 31.
In the figure, the friction and wear scar of the ionic liquids DIL3 and DIL7, patented by TEKNIKER, are
compared with the hybrid ionic liquid synthetized by TEKNIKER.
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Friction, Lubrication and Wear
DIL7, patented by TEKNIKER (EFS/ID/12720945) and developed in the frame of EU
Project MINILUBES Project has been compared with a hybrid ionic liquid synthetized
by TEKNIKER, developed in the EMAITEK project, are represented. In this subject, the
activity carried out in Eurostar Project VACUUM DLC, the EMAITEK Basque Country
Initiative, and the Austrian COMET Project can be also mentioned [65–67].
5.7 Tribology of materials for energy
5.7.1 Tribology for biogas, biodiesel, and bioethanol
Testing protocols has been set up to determine the durability of fuel injectors
and other critical engine components of engines working with biogas or suffering
lubricant dilution with biodiesel, bioethanol, or their mixtures. In Figure 32, it is
represented the friction coefficient of the PVD coating Ti-DLC coating deposited
by TEKNIKER on injectors, comparing the behavior between diesel and biodiesel
(B50, 50% diesel and 50% biodiesel). The protocols have been used in the EU
Project Cleanengine and in the industrial project IDEA [68].
Figure 32.
(a) Tribological properties of the Ti-DLC coating, simulating the contact of injector nozzles with diesel and
biodiesel B50; and (b) testing configuration.
5.7.2 Tribology in energy-efficient systems
Testing protocols have been set up to compare the lifetime of critical components of heat exchangers, compressors, gensets, and microturbines. In the example,
Figure 33.
Average main torque obtained with the drag friction test with different heat exchange fluids of different
viscosities (mPa). Error bars represent average standard deviation.
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the drag friction test developed by TEKNIKER (Figure 3), has been used to evaluate the average torque of different heat exchanger fluids, named as HTF-800 and
HTF-200. The last one was tested at different viscosities from 10 to 100 mPa s. The
minimum torque was measured for the HT-800 fluid, being finally selected for the
application in SUSPIRE Project (Figure 33). The protocols have been applied to EU
Project HEGEL [68] and to the industrial project ABADIE PLUS [69].
6. Conclusions
Attention to tribological problems would imply worldwide annual savings
of 970,000 M€ (1.39% GDP) [69]. A huge range of new testing equipment and
protocols have been developed to simulate the friction and wear (mechanical
and chemical) of a wide range of mechanical components and systems, in different environments. The knowledge about the working conditions and the failure
mechanisms will make possible in the future to simulate at laboratory a still wider
list of tribological systems. This will also help us to make a step forward, toward
modeling the extrapolation of research results to real systems and the generation of
new standards. Artificial intelligence can be also a tool that can facilitate this step
forward. Tribology will help to design low carbon footprint materials and implement them in a cost-efficient, predictive, and safe way [70–75]. Tribology will assist
also the development of energy- and resource-efficient products and processes, in
real systems.
Acknowledgements
The authors acknowledge the financing from the European Commission,
the Spanish Minister of Science and Technology and CDTI, the Basque Country
Government SPRI and InnoBasque, the Gipuzkoa Provincial Council and the
X-Tribology Austrian COMET Program. The authors also acknowledge the cooperation and/or financing of the industries and research institutions participating in
each project. The authors made special mention to those members of the tribology
team, that completed their Doctoral Thesis for their contribution to the knowledge generated: Bihotz Pinedo (Tribology of seals 2016) [23-25, 27], Borja Zabala
(high Temperature Tribology (eg. moulds, engines) 2017) [20, 22, 42, 43, 46, 52],
Francesco Pagano, (tribology of ionic liquids and vacuum tribology, 2017) [2–4, 13,
57–65], Beatriz Fernandez-Diaz (tribology of polymers, 2017) [28, 34, 63], Virginia
Saenz de Viteri (biotribology, 2016) [30, 31, 56, 57], Sofia Alves (dental tribology,
2017) [58], Cristina Cerrillo (ecotoxicity of nanoparticles, 2016) [71–75], Ainara
López (marine and off shore tribology, 2018) [12–16]. Also, to all the members
of the tribology team that dedicate their professional work to tribology activity
Elena Fuentes [17, 18, 30, 40, 56, 57], Xana Fernandez [9, 11, 29, 31, 46–48, 54,
65], Gemma Mendoza [5, 11, 32, 49, 50, 60, 63, 71–73], Xanti Almandoz [34], Juan
Carlos Rodriguez [8, 9, 16, 34], Olatz Areitioaurtena [48, 67, 68, 71–73], Marcello
Conte [1, 2, 23–25, 27, 54], and Roman Nevshupa [1, 4, 7, 8, 46, 52, 54], and the
other members of the research group that contributed to the generation of the
results.
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Author details
Amaya Igartua1*, Raquel Bayon1, Ana Aranzabe1 and Javier Laucirica2
1 Fundación TEKNIKER, Eibar, Spain
2 IK4, Eibar, Spain
*Address all correspondence to:
[email protected]
A summary of 37 years’ experience in TEKNIKER.
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
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DOI: http://dx.doi.org/10.5772/intechopen.85616
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178
Chapter 10
High-Temperature SelfLubricating Metal Nitride-Based
Nanostructure Composite Films
Hongbo Ju
Abstract
The film technology is one of the most efficient methods of modifying the
surface properties of materials. The focus of recent attention in the solid lubricating
materials is on the hard transition metal nitride films’ excellent high-temperature
tribological properties applied in powertrains and cutting tools. This chapter
reviewed the formation mechanism of Magnéli phases and the influence of Magnéli
phases on the high-temperature tribological properties of hard transition metal
nitride films synthesized using magnetron sputtering. The self-lubricating behavior
and wear mechanism of the Magnéli phases are discussed from the point of view
of crystallography. Some methods to enhance the wear resistance property of the
metal nitride film are also discussed.
Keywords: transition metal nitride films, magnetron sputtering,
tribological properties, self-lubricating, Magnéli phase
1. Introduction
Recently, a solid lubrication known as Magnéli phases was reported in the application of oxide materials with “easy” crystallographic shear phases, and numerous
related research activities have been carried out to investigate the function mechanism of Magnéli phases. Molybdenum, tungsten, and vanadium as the additional
elements were initially incorporated into transition metal nitride (TMN)-based hard
films, since the molybdenum oxide, tungsten oxide, and vanadium oxide are common
Magnéli phases and exhibit the excellent lubricating property. The TMN matrix as the
hard phase with a columnar structure could retain the strength and bearing capacity
during the wear test. Both the environment heat and friction heat induce the complex
tribo-chemistry reaction and the formation of Magnéli phases. The binary molybdenum nitride, the scientists have already attached importance to tungsten nitride
and vanadium nitride film in solid lubricating films in recent years. In this part, the
high-temperature self-lubricating property of TMN-based hard films was discussed.
2. Binary molybdenum nitride, tungsten nitride, and vanadium nitride
films
The crystal structure of the molybdenum nitride film shows a little influence on
the deposition parameters such as nitrogen partial pressure, substrate temperature,
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Friction, Lubrication and Wear
and target power. A single fcc-Mo2N phase is usually investigated in the molybdenum nitride film deposited using magnetron sputtering system.
Hardness of the molybdenum nitride film is ~26 GPa. The film exhibits the
excellent friction property at high temperature at the expense of wear resistance
property. Tribo-film MoO3 is considered as the main factor attributing to the
relatively low friction coefficient. MoO3 is composed of double layers of distorted
edge-sharing MoO6 octahedra parallel to (010) planes. The MoO3 has low shear
strength because weak van der Waals forces hold the successive layers together. The
counterpart is easy to wear away the MoO3 under the wear test.
The crystal structure of the tungsten nitride film depends on the deposition
parameters significantly. Tungsten nitride films could present a variety of phases
such as cubic W2N and hexagonal WN with large nitrogen to tungsten ratios, and
the film consisting of a single phase of fcc-W2N exhibits the highest hardness
and lowest friction coefficient. The tungsten or nitrogen vacancies in the binary
tungsten nitride films are a common phenomenon [1, 2]. The vacancies in the films
could enhance the mechanical properties. The hardness of fcc-W2N film is ~30 GPa,
whose value is higher than that of molybdenum nitride and vanadium nitride films.
Binary tungsten nitride film also exhibits the excellent friction property at the
expense of wear resistance property. During the wear test, WO3 could easily form
induced by the counterpart at high temperature, and it could play an excellent lubricating role. WO3 is described as crystallographic shear structure in normal as a type
of typical Magnéli phases. Reeswinkel et al. [3] expounded the structure of WO3
by the calculation results according to the density functional theory. The results
show that there are three different types of W-O bonds co-exist in WO3 owing to the
distorted octahedron WO6 and the shifted W cation in the WO3. It is showed that
these three types of W-O bonds represent extraordinary lubrication properties.
The crystal structure of vanadium nitride film is also influenced by the deposition parameters significantly. The vanadium nitride-based film is seldom applied in
the cutting tools on account of the relative low value of hardness and poor thermal
stability of the vanadium nitride film. Vanadium oxide phases could lubricate the
film during the wear test at high temperature, and VnO2n + 1 was defined as Magnéli
phase because of its excellent lubricant properties. The increase in temperature
was reported to induce the change of VO2 to V2O5 [4]. Erdemir [5] establishes the
relationship between the phase lubricity of oxide and its ionization potential based
on the principle of crystal chemistry. Based on this principle, oxides with high ionic
potential values will show a low coefficient of friction. Because the ionic potential
of V2O5 (10.2) is higher than that of VO2 (6.8) [6], the V2O5 shows a better lubricant
property than that of VO2.
3. Molybdenum nitride, tungsten nitride, and vanadium nitride-based
composite films
In view of the poor thermal stability and high wear rate, V-N, W-N, and Mo-Nbased films are comparatively less applied in cutting tool field. As reported [7, 8],
alloying metallic/nonmetallic elements into metal nitride matrix to deposit ternary,
quaternary, and multicomponent hard films could combine the benefits of individual components. Therefore, the incorporation of some additional elements into
the V-N, W-N, and Mo-N film could be an efficient method to improve the thermal
stability and wear resistance property.
Addition of Al into transition metal nitride thin films has been regarded as an
effective method to improve the hardness, crystalline orientation, wear resistance,
oxidation resistance, and thermal stability of the materials [9, 10]. AlN alloys are
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DOI: http://dx.doi.org/10.5772/intechopen.86124
usually considered as a superior oxidation resistant due to the formation of Al2O3
layers, which prevent oxygen diffusion toward the coating interior. In addition, Al
and Al alloys exhibit low wear resistance although they are used in a wide range of
automobile and aerospace industries [11]. Yang et al. [12] prepared Mo1-x Alx N
thin films on stainless steel coins, alumina sheet, and silicon wafer substrates by
using dc reactive magnetron sputtering technique and studied the effect of N2 and
Al content (0.06–0.33) on the coating properties including structural, hardness,
and oxidation resistance. The maximum hardness of 29 GPa was found at x = 0.06,
and by further increasing of Al content, a decrease in hardness was detected owning to the weakness of fine grain strengthening. The oxidation resistance temperature increased gradually by increasing the concentration of Al. Our group [13]
fabricated Mo-Al-N thin films with various Al contents (3.7–18.3 at.%) on stainless
steel (06Cr19Ni10) and Si (100) wafer substrate by using reactive magnetron sputtering and studied the effect of Al content on microstructure, mechanical oxidation
resistance, and tribological properties of the films. The result showed that the
oxidation resistance of MoAlN thin films increased by increasing the Al content,
while hardness and young modulus first increased and then started decreasing by
increasing the Al content. The highest values of hardness and elastic modulus were
32.6 and 494 GPa, respectively, at 3.7 at.% Al. The film showed the lowest average
friction coefficient and wear at the range between 4.1 and 9.5 at.% of Al content.
Besides this, we also add the Al into the vanadium nitride film using the magnetron
sputtering. The influence of Al content on the micro-structure, oxidation resistance, mechanical, and tribological properties of V-Al-N films were investigated.
The crystal structure of V-Al-N film is always a single face-centered cubic structure
no matter what the aluminum content is. When the content of aluminum was lower
than 4.7 at.%, the hardness of the film represented an obvious increase. At the
same time, the friction coefficient and wear rate showed a decrease at room temperature. The elevated Al content increases the oxidation resistance while reducing
the fracture toughness. The high temperature tribological properties of the film at
4.7 at.% aluminum, which showed the highest hardness, lowest friction coefficient,
and wear rate were investigated. The increase in temperature caused a change in the
wear mechanism and a phase transition of the tribo-film vanadium oxides. The friction coefficient first increases to 0.7 at 300°C and decreases to 0.28 at 700°C with
the wear rate gradually increases. As a result, the film at 4.7 at.% Al represented the
most suitable properties in cutting tool application.
Based on above investigation, the addition of Al into the Mo2N, VN matrix to
the formation of the substitutional solid solution could enhance the mechanical properties. Besides this, the addition of Al also could improve the oxidation
resistance temperature. The oxidation behavior of the films containing Al is mainly
controlled by the Al content in the films. Al3+ diffuses outward to the surface of
the films with the inward diffusion of oxygen will form Al2O3 layer during the
oxidation process. Al2O3 phase is stable over a wide temperature range and easy to
be formed. At low temperature ranging from 400 to 600°C, amorphous Al2O3 is
formed [9]. The amorphous Al2O3 layer on the surface of the films is more effective
to prevent the diffusion of oxygen into the films. However, the further increase in
temperature induces the Al2O3 from amorphous to crystalline. Compared with the
amorphous Al2O3, oxygen is easily diffused internally due to the grain boundary
[10, 13, 14] of the crystalline oxide layer, while Al2O3 and MoO3 grow rapidly. The
oxidation diffusion mechanism is transferred from atomic diffuse to mass transfer.
At the same time, the exchange of Al caused an increase in Al-N covalent bonds in
the films, which represents excellent thermal stability property. The addition of Al
could improve the wear resistance property of the films due to the enhancement of
thermal stability and the decrease in the Magnéli elements in the films.
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Friction, Lubrication and Wear
Figure 1.
HRTEM image of W-Si-N film with a Si content of 23.5 at %.
Silicon is another additional element to improve the mechanical, thermal stability, and wear resistance properties of the films. Limited solid solubility of Si in the
TMN matrix induces the formation of amorphous Si3N4 phase. Figure 1 shows the
TEM image of the W-Si-N composite film with a Si content of 23.5 at.%. As shown
in the figure, the nanograins of fcc-W2N are embedded into the amorphous phases.
The amorphous Si3N4 exhibits an excellent thermal stability property, and its oxidation resistance temperature is above 1200°C. Therefore, the addition of Si into the
TMN matrix could increase the oxidation resistance temperature. The nanograins
of tungsten nitride are wrapped up by the amorphous phase. This microstructure
could provide better protection for tungsten nitride against oxidation and prolong
the service life during the wear test.
Some other additional elements such as titanium and niobium also could
improve the wear resistance properties of molybdenum nitride, tungsten nitride,
and vanadium niride-based films [15–17]. For instance, the incorporation of titanium into the tungsten nitride matrix could form a solid solution of (W1−xTix)2−yNy
and exhibited a single face-centered cubic (fcc) W2N structure. Both the substoichiometric nitrogen content and solid solution strengthening could enhance the
mechanical properties. The incorporation of titanium also drops the wear rate at
room temperature significantly. This could be attributed to the increase of hardness
to elastic modulus ratio, elastic recovery, and hardness. Besides this, the addition of
titanium into the tungsten nitride matrix decreases the tungsten content in the film,
and this finally induces the decrease in the content of Magnéli phase on the wear
track surface. The decrease in the poor wear resistance Magnéli phase also attributes
to the decline of wear rate. Tungsten titanium nitride film exhibits the higher working temperature than the binary W2N film.
4. TMN-based composite films containing Magnéli elements
The molybdenum, tungsten, and vanadium Magnéli elements have been widely
incorporated into some traditional TMN-based films to improve the high-temperature self-lubricating property. For instance, V was incorporated into the Nb-Si-N
matrix, and the Nb-V-Si-N composite films were synthesized using the magnetron
sputtering to improve the high-temperature tribological properties. The results
show that the incorporation of V into the matrix could form the substitutional
solid solution of (Nb, V)N. Figure 2 shows the HRTEM image of the Nb-V-Si-N
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DOI: http://dx.doi.org/10.5772/intechopen.86124
Figure 2.
HRTEM image and its corresponding SAED pattern of Nb-V-Si-N film at 3.7 at.% vanadium.
Figure 3.
Friction coefficient and wear rate of Nb-V-Si-N films as a function of vanadium content.
film with a vanadium content of 3.7 at.%. The amorphous Si3N4 phases enclose the
substitutional solid solution. This microstructure could provide better protection
for Nb-V-N against oxidation at the high temperature environment. The solution
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Friction, Lubrication and Wear
of V could improve the mechanical properties such as the hardness and toughness.
Figure 3 illustrates the friction coefficient and wear rate of the films at different
testing temperatures. The incorporation of V into the film could improve the friction property at elevated temperatures at the expense of wear resistance property
due to the Magnéli phase with weakly bonded lattice planes.
Molybdenum can also bring positive influence to high-temperature friction
performance of the film. We add molybdenum into the classic titanium nitride film
in order to improve its tribological properties. The result shows that the Ti-Mo-N
film exhibits a single face-centered cubic structure, as same as binary TiN film. With
the increase of molybdenum content, the Mo2N phase appears in the film because of
the precipitated molybdenum. Figure 4 illustrates the SAED pattern of the Ti-Mo-N
film at 46.0 at.% Mo. Calculated the data given in Figure 4, it can be seen that the
selected electron diffraction pattern matches fcc-Mo2N. The composite film represents the highest hardness and the lowest friction coefficient in room temperature
at 46.0 at.% Mo. Figure 5 shows the average friction coefficient and wear rate of
Ti-Mo-N films at 46.0 at.% Mo under different testing temperatures. Figure 6
shows the relative mass fraction of Ti-Mo-N, MoO3, and TiO2 on the wear tracks of
Ti-Mo-N films at testing temperatures. When the texting temperature is higher than
Figure 4.
The SAED patterns of Ti-Mo-N films with 46.0 at % Mo content.
Figure 5.
The average friction coefficient and wear rate of Ti-Mo-N films at different temperatures.
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DOI: http://dx.doi.org/10.5772/intechopen.86124
Figure 6.
The relative mass fraction of Ti-Mo-N, MoO3, and TiO2 on the wear tracks of Ti-Mo-N films at testing
temperatures.
Figure 7.
The friction coefficient and wear rate of Ti-W-N composite films at different temperatures.
400°C, the Magnéli phase MoO3 and oxidized phase TiO2 appeared contributes to the
decrease of average friction coefficient, and the relative mass fraction of the friction phase in the film wear marks increases gradually with the increase of ambient
temperature, which can lubricate the wear marks and friction pairs and make the
interaction between them tend to ease, so the average friction coefficient of the film
decreases gradually with the increase of ambient temperature. However, the MoO3
layers are only combined by van der Waals force. MoO3 is very diffusive and easy to
be worn by counterpart during the wear test, so MoO3 is not wear-resistant although
it can decrease the friction coefficient.
In addition, there are similar conclusions in Ti-W-N composite film. TiN incorporating tungsten can form the substitutional solid solution of (Ti, W) N as well and precipitate W2N when the content of tungsten reaches a specific value. Figure 7 illustrates
the friction coefficient and wear rate of Ti-W-N composite films at 35.29 at.% W under
different temperatures. When the temperature rises to 400°C, the friction coefficient
decreases sharply because the TiWN composite film is oxidized, and the oxidation
phases of Ti and W are formed on the surface of the film, which means TiO2 and WO3.
WO3 with layered structure plays a role in the lubricant under the high-temperature
friction. When the content of WO3 increases, the coefficient of friction decreases. WO3
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Friction, Lubrication and Wear
has a melting point of about 730°C, and when the temperature continues to rise to
800°C, the melted WO3 has better lubricating properties than the dry friction, which
leads to the further decrease of friction coefficient. Beside this, the friction coefficient
will keep a low value due to the constant formation of liquid WO3 during the friction
process.
5. Conclusion
1. The Magnéli phase exhibits the excellent lubricating properties at high temperatures; however, it could be worn away easily by the counterpart during the
wear test due to its weakly bonded lattice planes.
2. Addition of aluminum and silicon into the TMN-based films containing
Magnéli elements could improve the thermal stability and decrease in the
content of Magnéli phase on the wear track surface. It could enhance the wear
resistance property to some extent.
Author details
Hongbo Ju
School of Materials Science and Engineering, Jiangsu University of Science
and Technology, Zhenjiang, Jiangsu Province, China
*Address all correspondence to:
[email protected]
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
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DOI: http://dx.doi.org/10.5772/intechopen.86124
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Chapter 11
Testing of the Resistance to
Scuffing of Spiral Bevel Gears:
Test Rig, Method, and Results of
Verification Testing
Waldemar Tuszynski, Marek Kalbarczyk, Bartosz Kiser,
Michal Michalak, Remigiusz Michalczewski, Jerzy Mydlarz,
Witold Piekoszewski, Marian Szczerek and Jan Wulczynski
Abstract
In spite of long-term development of the technology of bevel gear production,
the automotive industry reports various operational demands such as the need of
the size and mass reduction of gears without lowering their durability and reduction of friction leading to a decrease in the energy losses and a decrease of the
tendency to scuffing. What is more expected, EU regulations may impose the use
of new generation gear oils (ecological-friendly) providing the proper operational
properties of the transmission. In view of these demands, a new, bevel gear test rig
and scuffing test method have been developed at ITeE-PIB. The idea resulted from
a necessity to improve reliability of tests—popular gear tests are run mostly on
spur gears having the tooth geometry significantly different than bevel gears. The
test rig, test method, and results of verification testing are presented. The effect
of various gear oils and the deposition of a low-friction coating on the resistance
to scuffing were investigated. It is shown that the new test rig fulfils the research
requirements and that the new test method has a good resolution.
Keywords: bevel gear, test rig, scuffing, gear oil, coating
1. Introduction
1.1 Types of automotive drivetrains
In modern motor vehicles, like cars, lorries, and buses, the design of the drivetrain depends on the function of a given vehicle. For small- and medium-sized cars,
the automotive engineers pay attention to design such a drivetrain that occupies as
small space as possible. In this case, the motor and gearbox are located crosswise
in the front part of the vehicle; thus, it is the front wheels that are driven, and the
functionality of the transmission, differential, and associated components of the
driven axle is integrated into one assembly called the transaxle. This design is very
compact; however, it limits the maximum motor power to approximately 150 kW,
which is a result of offloading the front wheels when the vehicle accelerates.
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A diagram of the described drivetrain is shown in Figure 1 [1]. In this and the
next few figures, the rectangle with the four circles represents the motor and its
cylinders.
In the vehicles of a higher class, being larger in size, the criterion of the compactness of the drivetrain is not so important. In such vehicles, as well as in vans
and lorries, the so-called classic drivetrain is employed. In this case, the motor is
located longitudinally in the front part of the vehicle, and the rear wheels are driven
(Figure 2) [1].
In the solution portrayed in Figure 2, the driving torque is transmitted from the
motor via the clutch, gear box, and drive shaft to the axle with a final drive, differential, shafts, and finally to the wheels.
In motor vehicles having the classic drivetrain, during acceleration, the back
wheels are loaded; thus, the problem of the adherence of the driven wheels to the
Figure 1.
Diagram of a transverse drivetrain [1].
Figure 2.
Diagram of a classic drivetrain [1].
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Figure 3.
Diagram of a drivetrain with all wheels driven [1].
road does not limit the motor power. It is very important in high-class cars (e.g.
BMW, Mercedes), as well as in lorries.
The highest acceleration and off-road functionality are exhibited by vehicles
having all wheels driven. In such vehicles, the number of final drives equals the
number of the driven axles. A scheme of the “state-of-the-art” drivetrain used in,
e.g. Nissan GT-R sports vehicles, is presented in Figure 3 [1].
Unique features of this design are two driving shafts. The first one transmits the
driving torque from the motor to the gearbox. Then, the torque is transmitted to the
rear axle final drive (transaxle). The second driving shaft transmits the torque from
the gearbox via the distribution box to the final drive of the front axle. This sophisticated design makes it possible to uniformly load both axles and achieve a neutral
vehicle behaviour when turning.
Another example of a drivetrain that drives all the vehicle wheels is a famous
Willys-Overland used by the US Army during the World War II. Its numerous
“clones” are still produced in the world. It is interesting that its original version
Willys-Overland is still employed by the Indian Army. The described drivetrain is
shown in Figure 4 [1].
The drivetrain shown in Figure 4 is equipped with two axles. The driving torque
produced by the motor is transmitted from the gearbox via the distribution box to
the two driving shafts and then to the front and rear axles.
1.2 Final drives
A typical axle consists of the final drive, differential, and half shafts, which
transmit the driving torque to the wheels.
The final drive is to transmit the driving torque to the wheels, at the same time,
reducing the transmitted rotational speed, very often changing its direction, and
increasing the driving torque. In most cases, the final drive consists of a pair of
toothed gears.
The final drive can be one-stage, two-stage, and multistage, depending on the
number of the reduction gears. Concerning the simplest, one-stage final drives for
the automotive purposes, four of these types are applied (Figure 5) [2].
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Friction, Lubrication and Wear
Figure 4.
Diagram of a drivetrain with all wheels driven used in the Willys-Overland off-road vehicles [1].
Figure 5.
The typical, one-stage final drives produced by the automotive industry: (a) spiral bevel gears (offset = 0),
(b) hypoid gears (offset >0), (c) worm gears, and (d) helical gears [2].
A hypoid gear is a type of a spiral bevel gear whose axis does not intersect with
the axis of the meshing gear. This is why the distance between these axes, called the
offset, is higher than 0. In spiral bevel gears, the offset is exactly 0.
Spiral bevel gears or hypoid gears are used in the final drives of the drivetrains
shown in Figures 2–4, while in the drivetrain presented in Figure 1, helical gears
constitute the final drive.
Although nowadays, in vehicles, practically only helical gears (e.g. in the
drivetrain from Figure 1) or hypoid gears (e.g. in the drivetrain from Figure 2) are
used, spiral bevel gears are still very important, because they are broadly applied in
lorries, special vehicles, and buses, where the axle size and the noise emission are
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Figure 6.
Scuffed area on the tooth flank of a spiral bevel gear.
of minor importance but the gear efficiency is a priority. For example, spiral bevel
gears are employed for the final drives in the drivetrain of the Willys-Overland offroad vehicles (Figure 4); their “clones” are still produced throughout the world.
It should be emphasised here that spiral bevel gears are used not only in motor
vehicles. It can be estimated that, in case of, e.g. speed reducers with bevel-shaped
gears, spiral bevel gears are applied in 90% of such devices, leaving only 10% to
hypoid gears.
In spite of long-term development of the manufacturing technology and service
of spiral bevel gears, there are still problems related to friction. The following
problems, coming from excessive friction in such gears, still exist: an increase in the
oil temperature followed by a rise in the tendency to scuffing. A typical scuffed area
on the flank of the spiral bevel gear tooth is shown in Figure 6.
For the purpose of research on spiral bevel gears, the authors have developed
a new test rig and a method for testing scuffing of such gears. The new testing
machine and the test method will be a subject of the body of this chapter.
1.3 Automotive gear lubrication
Comprehensive characteristics of the automotive gear oils were provided in the
former authors’ chapter, being a part of the book [3]. Generally, the characteristics
of the automotive gear oils were based on the source document provided by the
American Petroleum Institute (API) [4].
However, to help the reader to analyse the data in this chapter, the authors
decided to repeat information given in the book [3].
As in the book [3], emphasis was put on the classification of manual transmission fluids (MTF), i.e. automotive gear oils, excluding oils for automatic transmissions, called the automatic transmission fluids (ATF) and excluding oils for off-road
vehicles (e.g. tractors). For simplification, manual transmission fluids (MTF) will
be called the equivalent name—“automotive gear oils”—that will be used throughout the text.
There are two different classifications of automotive gear oils.
The first one specifies lubricant service designations or the “performance levels”
of automotive gear oils. These have been provided by the American Petroleum
Institute (API) [4]. The API classification divides automotive gear oils into seven
performance levels. Four performance levels are in current use, three are not. The
reason for the performance level not to be in current use results from changes of
manufacturers’ recommended tests or the unavailability of test equipment, and it
does not mean that such products have been withdrawn from the market.
The API classification is described in Tables 1 and 2.
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API service
designation
Application areas and short characterisation
GL-1
Manual transmissions operating under such mild conditions that straight petroleum or
refined petroleum oil may be used satisfactorily
Not satisfactory for many passenger car manual transmissions
GL-1 oils may contain oxidation and rust inhibitors, defoamers, and pour depressants.
Friction modifiers (FM) and extreme pressure (EP) additives shall not be used in GL-1 oils
GL-4
Axles with spiral bevel gears operating under moderate to severe conditions of speed and
load or axles with hypoid gears operating under moderate speeds and loads
GL-4 oils may be used in selected manual transmission and transaxle applications where
MT-1 lubricants are unsuitable
GL-4 oils contain up to 4% of extreme pressure (EP) additives
GL-5
Gears, particularly hypoid gears, in axles operating under various combinations of highspeed/shock-load and low-speed/high-torque conditions
GL-5 oils contain up to 6.5% of extreme pressure (EP) additives
MT-1
Nonsynchronised manual transmissions used in buses and heavy-duty lorries
API MT-1 does not address the performance requirements of synchronised transmissions
and transaxles in vehicles and heavy-duty applications
API MT-1 oils provide protection against the combination of thermal degradation,
component wear, and oil seal deterioration, which is not provided by lubricants in current
use meeting only the requirements of API GL-1, 4, or 5
Table 1.
API service designations (performance levels) of automotive gear oils in current use, according to the source document—
API Publication 1560 [4].
API service
designation
Application areas and short characterisation
GL-2
Automotive worm-gear axles operating under such conditions of load, temperature, and
sliding velocities that lubricants, satisfactory for API GL-1 service, will not suffice
GL-2 oils contain antiwear or film strength improvers specifically designed to protect
worm gears
Currently, it is very difficult to find products designed as “GL-2” in the automotive market
GL-3
Manual transmissions operating under moderate to severe conditions and spiral bevel
axles operating under mild to moderate conditions of speed and load
GL-3 oils provide load-carrying capacities exceeding those satisfying API GL-1 but below
the requirements of API GL-4 oils
GL-3 oils are not intended for axles with hypoid gears
They contain up to about 3% of antiwear (AW) additives
GL-6
Hypoid gears designed with a very high pinion offset
Their EP properties are typically better than of GL-5 oils
GL-6 oils contain up to 10% of extreme pressure (EP) additives
Table 2.
API service designations (performance levels) of automotive gear oils not in current use, according to the source
document—API Publication 1560 [4].
Apart from the designations from Tables 1 and 2, there is also one denoted as
API GL-5(LS) or GL-5+. Gear oils that meet the requirements of this class contain
special additives, called friction modifiers (FM), preventing the stick–slip phenomenon under conditions of limited slip (LS). As such, GL-5(LS) oils are intended for
lubrication of limited slip differentials.
To reduce the number of various gear oils in the market and, in turn, simplify oil
selection, many lubricant manufacturers implement more universal (“multi-class”)
gear oils. In this group, gear oils denoted as API GL-4/GL-5 or GL-4+ predominate.
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Maximum temperature
for viscosity of
150,000 cP [°C]
Kinematic viscosity
at 100°C, cSt [mm2/s]
Minimum
Kinematic viscosity
at 100°C, cSt [mm2/s]
Maximum
70 W
−55
4.1
—
75 W
−40
4.1
—
80 W
−26
7.0
—
85 W
−12
11.0
—
SAE viscosity
grade
80
—
7.0
<11.0
85
—
11.0
<13.5
90
—
13.5
<18.5
110
—
18.5
<24.0
140
—
24.0
<32.5
190
—
32.5
<41.0
250
—
41.0
—
Table 3.
Automotive gear oil viscosity classification according to the source document—SAE J306:2005 [5].
The second classification was provided by the Society of Automotive Engineers
(SAE) [5]. It is a viscosity classification. It divides automotive gear oils into 11
grades based on their rheological properties (Table 3).
For lubrication of automotive gears, multiviscosity grade oils are mostly employed,
e.g. SAE 80W-90. This designation means that such an oil meets the requirements of
both low-temperature (SAE 80W) and high-temperature grades (SAE 90).
1.4 Scuffing
The comprehensive analysis of the scuffing phenomenon was provided in the
former authors’ chapter, being a part of the book [6]. However, to help the reader
analyse this chapter, the authors decided to extract the most important information
and present it here.
1.4.1 Some definitions of scuffing
Despite long tradition of research on scuffing, its terminology has not been
systemised so far. The term scuffing has many synonyms, e.g. seizure, scoring,
galling, and seizing.
The variety of terms presented here makes interpretation of literature data
difficult. Additionally, many terms are very often used as equivalents, e.g. scuffing
and seizure.
The lack of consensus on the origin of scuffing as well as its symptoms is
reflected by numerous definitions of the phenomenon. Some of them associate
scuffing with wear, the others—with friction. The former are the definitions given
or quoted by, e.g. Enthoven and Spikes, Dyson, Ludema, and Sadowski. Among the
latter, one can classify the definition given by Nosal.
Enthoven and Spikes [7] have quoted the definition suggested by the
Organisation for Economic Co-operation and Development, characterising scuffing as “localized damage caused by the occurrence of solid-phase welding between
sliding surfaces, without local surface melting”.
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Dyson [8] has adopted the definition presented by The Institution of Mechanical
Engineers: scuffing is “gross damage characterized by the formation of local welds
between the sliding surfaces”.
Ludema [9] has considered scuffing to be “a roughening of surfaces by plastic
flow whether or not there is material loss or transfer”.
Sadowski [10] has interpreted scuffing as “an interference of stabilised wear and
a boundary example of such wear”.
However, according to Nosal [11], scuffing is “a collection of phenomena taking
place in the sliding pair, localized mainly deep inside the surface layer, producing an
increased and unstabilised friction which is likely to result in seizure”.
1.4.2 What does initiate scuffing?
Practical lubrication in most of the sliding pairs, e.g. high-speed toothed gears,
is neither a purely hydrodynamic (HD) nor an elastohydrodynamic (EHD) process.
Despite either HD or EHD, film supports most of the loading applied to the tribosystem elements, collisions between the highest surface asperities cannot be excluded.
Therefore, besides fully lubricated friction, dry and boundary friction may also
appear. Their common action is called the mixed friction or mixed lubrication [12].
The lubricating film, being produced at mixed friction, compared to such
created at fully lubricated friction, is significantly thinner. Collisions of surface
asperities give rise to a local load increase, then the lubricating film collapses, and
scuffing takes place. It is a serious practical problem, because scuffing can appear in
tribosystems creating apparently good conditions for lubrication.
A kinetic model, proposed by Nosal [11], presents scuffing to be a sequence of
the following phenomena: collapse of the lubricating film ⇨ removal of oxides layers in microareas of contact, leading to direct metal–metal contacts ⇨ appearance
of adhesive bonds due to a temperature increase or plastic deformation ⇨ development of adhesive bonds deeper and deeper inside the surface layer ⇨ shearing
of adhesive bonds, tearing out and transfer of metal particles from one element
onto the other, due to their relative movement ⇨ rapid development of the above
phenomena ⇨ macroscopic range of destruction (scuffing).
The kinetic model of scuffing assumes that the transition from stabilised friction
to scuffing requires some time, rejecting the idea that it takes place very rapidly, i.e.
during t → 0.
Scuffed areas on the tooth flank of a spiral bevel gear were presented earlier in
Figure 6.
It is very important to differentiate between the terms scuffing and scoring.
Scuffing has a physical nature and is a result of shearing adhesive bonds, which
appear between the rubbing surfaces. Scoring has a rather mechanical nature and
appears at very high loads. Under such conditions abrasion of the surface takes
place—by the action of the very hard wear particles [13].
1.5 Some reasons for the bevel gear testing
In spite of long-term development of the technology of bevel gear production, the automotive industry reports various operational demands. The main one
concerns the need of the size and mass reduction of gears without lowering their
durability. The second demand relates to the reduction of friction, leading to the
decrease in heat emission, lowering the energy losses, and above all, resulting in a
decrease of the tendency to scuffing. The abovementioned effect can be achieved by
the deposition of a thin, hard, and low-friction coating on the operating surface of
the gears, although the present-day research is limited to spur gears [14–22].
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The third important aspect is environmental protection, which is addressed by the
use of new generation gear oils (ecological-friendly) providing the proper operational properties of the gear. In addition, the new EU law requirements, concerning
the biodegradability of lubricants in various fields, are expected to be implemented
soon. This is why numerous research investigations are now being conducted, which
consider the application of ecological oils for various technological areas [23–26].
Apart from the demands mentioned above, an equally important issue is the
diversification of automotive gear oils in respect to API GL performance levels.
Present research concerns the simple specimens [27–29], such as the four-ball
tribosystem, as well as spur gear investigation [30, 31]. However, there is a striking
lack of research performed in this direction on spiral bevel gears.
The mentioned demands could be fulfilled only by a new tribotester, intended
for testing bevel gears. There are some tribotesters of this type. The first one is the
hypoid/bevel gear test rig [32, 33] developed in the Gear Research Centre (FZG) at
the Technical University of Munich. The second one is the test rig [34] designed at
NASA Glenn Research Center. This machine is intended for aeronautics purposes.
However, these test rigs are not widely available.
Poor availability of bevel gear test rigs is probably the reason why most of the
publications in this area focus on the two aspects:
• Optimisation of the geometry of bevel gears, optimisation of the conditions
of meshing teeth of bevel gears, as well as improvement of the production
technology—by using the tools of mathematical modelling [35–38]
• Case studies, focusing on the explanation of operational causes of bevel gear
scuffing, surface fatigue wear (pitting), and teeth breakage in various vehicles,
machines, and devices, i.e. lorry transmission, turbojet gearboxes, or in the
transmissions of industrial conveyors [39–41]
In spite of the test rig, for the investigation of bevel gears, a necessary factor is the
usage of proper test methods. Unfortunately, a review of the most common standards
indicates that there is a complete lack of any standardised methods for testing scuffing of bevel gears. The existing standards concern the means of construction calculations for providing the proper resistance to scuffing (ISO/TR 13989-1,2), and it has
to be underlined that these calculation methods are treated as controversial. For this
reason, the American Gear Manufacturers Association (AGMA) has not published
such a method as a standard yet. The lack of research in this area is clearly visible.
In contradiction to the calculation methods, available as standards or computer
programmes, the proposals of authorial methods for friction and wear testing of
hypoid or bevel gears are presented very rarely in publications [32, 33, 42, 43].
As it was mentioned before, answering to the issues specified above at the
Tribology Department of the Institute for Sustainable Technologies (ITeE-PIB), a
new test rig for the investigation of bevel gears was developed, and the authorial
method for testing scuffing of bevel gears was designed. The testing machine and
the test method are the subjects of the chapter.
2. Bevel gear test methodology
2.1 New bevel gear test rig
The kinematic scheme of the developed test rig is presented in Figure 7. In the
line of testing equipment for tribological research, developed at ITeE-PIB, the bevel
gear testing machine is denoted as T-30.
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Friction, Lubrication and Wear
Figure 7.
Kinematic scheme of the T-30 back-to-back bevel gear test rig.
The main part of the T-30 test rig consists of three gears—a test bevel gear, slave
bevel gear, and slave cylindrical (helical) gear—and in the figure, all the teeth were
presented as if they were straight for simplification. The test bevel gear consists of a
pinion and a gear wheel, which are immersed in the investigated oil. Before the test,
the test chamber is preheated to the required temperature by means of a heating unit.
The test chamber is equipped with cooling channels (in Figure 7 called the cooler)
connected with a heat exchanger working in a closed water circulation system. This
construction makes it possible to cool the oil before the gear inspection. Furthermore,
it extends the application area of the T-30 test rig for investigation under conditions
of constant oil temperature (necessary for surface fatigue testing).
The testing machine is equipped with a circulating power system. After the
application of the required load and fixing the shafts and the clutch, the torque
circulates in the shaft-gear system. The load (shaft torsion) is applied by means of
the lever unit with the number of weights, providing the possibility of obtaining a
torque up to 720 Nm. The applied torque and its changes during the test are measured by means of the loading torque transducer.
The measurement of friction torque is realised with the use of a friction torque
transducer mounted between the motor and the slave cylindrical gears. The purpose
of using friction torque measurement is to make it possible to compare materials
from which the test gears are produced from the point of view of a possible friction
reduction. The motor is supplied through a power inverter, providing the possibility
of speed regulation.
A photograph of the T-30 bevel gear testing rig, equipped with the control and
measuring system, is presented in Figure 8.
The control system makes it possible to regulate the motor speed to change
the lubrication conditions of the tested gear by changing the motion direction, to
regulate the temperature of the oil, and to automatically turn off the motor after
reaching the required number of test pinion revolutions or after exceeding the
selected level of vibrations. The main elements of the control system are mounted
in the measuring cupboard (Figure 8—left side).
The measuring system (Figure 8) consists of a digital amplifier, the set of measuring transducers, and a computer equipped with specialised software. During the test,
the following quantities are measured and registered: the loading torque between the
gears, the friction torque, the motor speed, the number of test pinion revolutions, the
temperature of the tested oil, the level of vibrations, and the test duration.
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Figure 8.
Photograph of the T-30 back-to-back bevel gear test rig with its control and measuring system (on the left) and
water circulating cooling system (on the right) [44].
The measured signals from the transducers are amplified and transferred to the
computer. The specialised software developed at ITeE-PIB makes it possible to display
the curves of measured values in relation to test duration. At the end of the test, the
measurements are saved on the hard disc, and then research reports can be printed.
The new test rig was designed with the cooperation between ITeE-PIB and
Invenio Ltd. and manufactured by ITeE-PIB.
2.2 New bevel gear scuffing test
A simplified scheme of the geometric configuration of the test bevel gears is
presented in Figure 9.
The pinion and the wheel have a spiral line of teeth. The direction of motion
shown in Figure 9 is defined by the authors as “normal” viewed from the test
chamber’s front cover, and the wheel rotates counterclockwise. From the same point
Figure 9.
Simplified scheme of the geometric configuration of the test bevel gears [44].
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of view, the pinion is mounted behind the wheel, which was skipped in Figure 9 in
order to simplify the scheme.
Under the load action direction, which results from the test rig construction, the
convex flank of the pinion tooth is pressed to the concave flank of the wheel. As a
consequence, the convex flank of the pinion is recognised as the investigated one. The
pinion and the wheel are immersed in the tested oil up to the level of the gear axis.
The developed test method consists in performing research on the lubricated
spiral bevel gears, operating under the conditions presented below, at the constant
rotational speed, gradually increasing load, with a starting temperature the same
for every test, until the failure load stage (FLS) is reached, which is a basic indicator
of the resistance to scuffing, or until the 12th load stage is reached. FLS is the load
stage under which the area, which is damaged by polishing, scratches, and scoring,
exceeds the area of one pinion tooth (≥ 450 mm2). Therefore, the FLS is a measure
of the anti-scuffing properties of the investigated oil or the scuffing resistance of
the coating deposited on one or both test gear elements.
Test conditions
• Type of test gears
Bevel gears with spiral teeth line
• Rotational speed of the motor
3000 rpm
• Average circumferential speed
7.7 m/s
• Single run duration
15 min
• The motion rotational direction
“Normal” (Figure 9)
• Min. and max. Load stage
From 1 to 12 (the 13th and 14th stage is
allowed)
• Loading torque
From 3 to 535 Nm, gradually increasing
• Hertzian contact stress
From 0.1 to 1.5 GPa
• Oil starting temperature
90°C (not stabilised during the test)
• Type of lubrication
Immersive (approx. Volume of oil: 2 l)
• Level of oil
To the axis of the test gear elements
Depending on the requirements, beside the basic scuffing resistance indicator,
which is FLS, for evaluation of anti-scuffing properties, an additional criterion can
be used, which is the damage progression of the pinion teeth flanks. For this purpose, during every pinion inspection, apart from the total damaged area, the most
common mode of wear is also notified in the report sheet—according to Table 4.
When testing a low-friction hard coating deposited on one of the test gears, the
coated element “polishes” the uncoated one due to a mild abrasive action of the
coating surface. Therefore, polishing areas on the teeth flank of the uncoated gear
can be neglected when inspecting test gears for the sings of damage.
2.3 Test spiral bevel gears
The pair of test spiral bevel gears is shown in Figure 10.
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Mode of wear
Symbol
Polishing
W
Scratches
R
Scoring
B
Scuffing
Z
Appearance
Table 4.
Possible modes of wear of the test pinion.
Figure 10.
Test spiral bevel gears.
The spiral bevel gears were manufactured in a high, fifth grade of precision,
defined in DIN 3965. They were made of 18CrNi8 steel. The material was carburised
(0.6–0.9 mm in depth). Then it was tempered to achieve the hardness of 56–60
HRC. Machining was performed using Klingelnberg’s method.
Technical specifications of the test spiral bevel gears are presented in Table 5.
2.4 Oils tested
For the research, the following oils were used: the commercial mineral-based oils of
API GL-1 and GL-5 performance level, intended for vehicle mechanical gears, and VG
220 viscosity grade, ecological oil, intended for industrial gears (this oil has been developed at ITeE-PIB). The characteristics of the investigated oils are presented in Table 6.
2.5 Materials tested
Two material configurations were tested. The first one consisted of a steel pinion
and steel wheel, and the second one consisted of a steel pinion and a-C:H:W coated
steel wheel. The photographs of both configurations are presented in Figure 11.
The a-C:H:W coating is a multilayer coating. The structure of the coating is
presented in Figure 12, showing the results of the depth profile quantitative analysis
obtained by a glow discharge optical emission spectrometer (GDOES). The reference
sample was deposited on the Armco Fe substrate material (technically pure Fe).
As it is shown in Figure 12, on the Fe-based substrate, the layer of Cr is deposited to
increase adhesion of the tungsten carbide (WC) layer to the substrate. The hard WC is
of crucial importance to achieve the high load-carrying capacity, and in case when the
outer layer wears out, the WC layer protects the substrate material from abrasive wear.
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Description
Pinion
Wheel
Manufacturing process
Klingelnberg
Material
18CrNi8 steel
Heat treatment
Case hardening
Case depth
0.6–0.9 mm
Surface hardness
56–60 HRC
Core hardness
33–45 HRC
Gear quality
5 according to DIN 3965
Number of teeth
7
Normal module
8.70 mm
Normal pressure angle
20°
Mean spiral angle
35°
Shaft angle
90°
Working tooth flank
Convex
18
Concave
Table 5.
Main material and geometrical characteristics of the test spiral bevel gears.
Symbol
API GL
service
designation
Viscosity
grade
Type of base oil
Application and short
characteristics
GL-1 90
GL-1
SAE 90
Mineral
Manual transmissions operating
under such mild conditions that
straight petroleum or refined
petroleum oil may be used
satisfactorily
GL-1 oils do not contain any
lubricating additives
GL-5
80W-90
GL-5
SAE
80W-90
Mineral
Gears, particularly hypoid gears,
in axles operating under various
combinations of high-speed/shockload and low-speed/high-torque
conditions
GL-5 oils contain up to 6.5% of
extreme pressure (EP) additives
Eko VG
200
—
VG 220
Natural
(vegetable)—
mixture of
rapeseed and
castor oils
Industrial transmissions and
transmissions in machine tools and
in machines working especially in the
paper industry
The oil contains 2% (wt.) of
sublimated sulphur, performing as an
EP additive
Table 6.
Characteristics of the tested gear oils.
The outer layer is responsible for the interaction with the mating element of the
tribosystem. It is a multilayer structure (colloquially named WC/C) that consists of
WC-reach DLC layers with DLC interlayers. The presence of nickel is required for
technological reasons. Low-friction properties are a result of a high concentration
of amorphous carbon (sp2) in the outer layer.
202
Testing of the Resistance to Scuffing of Spiral Bevel Gears: Test Rig, Method, and Results…
DOI: http://dx.doi.org/10.5772/intechopen.84848
Figure 11.
Material configurations of the test bevel gears: (a) steel pinion, steel wheel, and (b) steel pinion, a-C:H:W
coated wheel.
Figure 12.
Structure of the a-C:H:W coating; the results of the quantitative GDOES depth profiling (hydrogen was not analysed).
3. Results of verification testing of the T-30 bevel gear test rig
In Figure 13, the FLS values obtained for investigated oils and material configurations are presented. The expected repeatability intervals are added to the bars.
The failure load stage result analysis indicates that the resolution of the scuffing test
method is very high—the FLS differences between all the tested cases are statistically
significant. It is also of great importance that, for all the tested cases, the 12th load
stage was not exceeded. The maximal obtained FLS level is not higher than 10, which is
an additional confirmation of the very high resolution of the developed test method.
In the steel pinion/steel wheel configuration, the GL-1 90 oil without additives
exhibits low resistance to scuffing (represented by very low—3rd—FLS), whereas
the GL-5 80 W-90 oil, with significant concentration of EP additives, makes it possible to reach much higher FLS value (eighth). The Eko VG 220 oil is characterised
by an intermediate value of failure load stage, which indicates that it can be used as
a lubricant only for bevel gears, which operate under conditions of low and moderate loads, still providing a measurable ecological effect.
According to the facts presented by the researchers [17–22] who performed
scuffing tests on spur gears, there is a possibility to improve the resistance to
scuffing of gear elements by deposition of a thin, hard coating, i.e. a-C:H:W,
on at least one of the gears. This thesis is fully confirmed by the results of the
203
Friction, Lubrication and Wear
Figure 13.
Failure load stage (FLS) for the tested gear oils and material configurations.
bevel gear scuffing test performed on the configuration of a steel pinion mating
a-C:H:W coated steel wheel for which the highest value of FLS was obtained
(tenth). This test result indicates that the thin hard coatings represent a very high
application potential for scuffing resistance improvement in the area of heavily
loaded gears.
As stated before, considering the assessment of the anti-scuffing properties of oils
and the resistance to scuffing of various material combinations of gear elements, in particular with coatings, one more important criterion can be used, which is the progression of wear, occurring on the flanks of pinion teeth under stepwise increasing load.
The detailed analyses comprised the modes of wear that occurred on most of the
pinion teeth. The results of the analyses are compiled in Table 7. Below the symbols
of the wear mode, the total damaged area of the pinion teeth is presented, expressed
in mm2. The description of wear modes is provided earlier in Table 4.
It can be observed that, as the load increases, the progression of tooth wear is
the fastest for the gears lubricated with GL-1 90 oil, because the scuffing is initiated
just after the test at the first load stage.
When considering the wear modes during two tests on two different material
combinations lubricated with GL-5 80 W-90 oil, the eighth load stage causes the
scuffing of the steel-steel pair, while on the steel pinion meshing with a-C:H:W
coated wheel, only scoring (in a form of groves) appears. It is because the presence of the coating causes a lower level of affinity than in the steel-steel case.
Additionally, the high hardness of the coating, decreasing the tendency to adhesive
bonding, significantly mitigates scuffing. As an effect of these factors, the steelcoating material configuration reached a high tenth load stage.
Thus, the additional criterion (i.e. progression of wear on the teeth flanks) constitutes a very useful supplement to the basic criterion, which is the failure load stage, and
it can provide additional and valuable information on the damage process of the teeth.
Concerning the coating-steel material combination of bevel gear teeth, it is
very difficult to compare the wear results reported in this chapter with the results
obtained by other researchers, because such papers are extremely rare. For example,
204
205
7
6
5
4
3
2
1
Load stage
910 mm2
295 mm2
216 mm2
1225 mm2
54 mm2
31 mm2
16 mm2
7 mm2
≈0
116 mm2
70 mm2
≈0
≈0
≈0
≈0
≈0
72 mm2
≈0
≈0
≈0
≈0
≈0
≈0
GL-5 80 W-90
GL-5 80 W-90
GL-1 90
Eko VG 200
Steel—a-C:H:W
Steel—steel
Testing of the Resistance to Scuffing of Spiral Bevel Gears: Test Rig, Method, and Results…
DOI: http://dx.doi.org/10.5772/intechopen.84848
206
1575 mm2
960 mm2
164 mm2
130 mm2
GL-5 80 W-90
GL-5 80 W-90
GL-1 90
Eko VG 200
Steel—a-C:H:W
Steel—steel
Table 7.
The wear modes found on the teeth of the test pinion at increasing stages of load; the research was performed using various gear oils and material combinations.
10
9
8
Load stage
Friction, Lubrication and Wear
Testing of the Resistance to Scuffing of Spiral Bevel Gears: Test Rig, Method, and Results…
DOI: http://dx.doi.org/10.5772/intechopen.84848
Basiniuk et al. [45] studied the behaviour of coated bevel gears, however, from a
point of view of a noise and friction reduction.
The authors plan to continue their research on the coated bevel gears. The aim
will be to identify mechanisms of interaction between the surface and the gear oil
of different chemistry in the steel-coating and coating-coating friction zones of the
meshing teeth. Scientific publications, relating to this aspect, concern mainly testing
on simple model specimens. The most recent papers in this field are, e.g. [46–58].
4. Conclusions
Based on the carried out research, the following conclusions can be drawn:
• The developed method for testing scuffing of spiral bevel gears exhibits a good
resolution.
• It is possible to improve the resistance to scuffing by the application of a thin,
low-friction coating on one of the elements of the spiral bevel gear.
The developed test rig with the test method can be used for the assessment of the
anti-scuffing properties of oils intended for bevel gear lubrication and also for the
determination of the resistance to scuffing of bevel gears from the perspective of materials used for gears and possibly the tooth surface processing. Thus, they can be applied
in R&D industrial laboratories of lubricant producers, manufacturers of devices that
contain bevel gears, automotive industry, as well in laboratories of technical universities
where the aspects of bevel gear tribology and design are studied and investigated.
Acknowledgements
The research was financed by the National Centre for Research and
Development (NCBiR) within the scope of Research Project No. N R03 0019 06.
Author details
Waldemar Tuszynski1*, Marek Kalbarczyk1, Bartosz Kiser2, Michal Michalak1,
Remigiusz Michalczewski1, Jerzy Mydlarz2, Witold Piekoszewski1, Marian Szczerek1
and Jan Wulczynski1
1 Tribology Department, Institute for Sustainable Technologies—National Research
Institute (ITeE-PIB), Radom, Poland
2 Invenio Ltd, Tychy, Poland
*Address all correspondence to:
[email protected]
© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms
of the Creative Commons Attribution License (http://creativecommons.org/licenses/
by/3.0), which permits unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.
207
Friction, Lubrication and Wear
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211
Edited by Mohammad Asaduzzaman Chowdhury
Tribology has rapidly expanded in recent years as the demand for improved materials
has increased. The good function of numerous electrical, electrochemical, mechanical,
and biological systems or components depends on suitable friction, lubrication, and wear
as well as tribological values. In this context, the study of friction, wear, and lubrication
is of tremendous pragmatic importance. The reduction of friction and loss of materials in
relative motion are important challenges to improveing energy efficiency.
This book guides the rational design of material for technological application. Chapters
cover topics such as the resistance of dry abrasive wear, the role of a brand-new additive
in the minimization of friction and wear, the structural-energy model of elastic-plastic
deformation, the influence of micro-abrasive wear modes, tribological characteristics
of magneto-rheological fluids (MRFs) and magneto-rheological elastomers (MREs), and
different treatment technologies to improve tribological properties, among others.
ISBN
ISBN978-1-83962-346-2
978-1-78984-287-6
Published in London, UK
© 2019 IntechOpen
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