Autodesk Inventor professional

Titlurile au inserat link direct catre descrierea cursurilor de la http://www.softedu.eu Cursuri Autocad, Inventor, 3D Studio Max, Desen tehnic, Adobe Premiere, After Effects, Photoshop, Illustrator, Dreamweaver, Corel Draw, Web Design, Soft Educational tehnic si teste computerizate.

Currently, the gantry crane in LAPAN Garut still uses steel material. The steel material is protected using a coating to minimize the impact of corrosion. However, this method is less efficient, considering the corrosion rate in LAPAN Garut is very high because it is located on the coast of Cilauteureun. It also creates problems in terms of maintenance because it has to be done regularly and periodically repainting. In addition, not all equipment is available maintenance funds every year. The objective of this paper is to design and analyze the stress of a gantry crane with a capacity of 9 tons using Aluminum 6061 material. The material used is three units of JIS G 3192 H standard frame (I-shape) with a size of 150 x 150 x 7 mm, four units of JIS G 3466 frame (square profile) with a size of 150 x 150 x 6 mm, and four units of JIS G 3466 frame (square profile) with a size of 125 x 125 x 6 mm. Finite element analysis is performed using Autodesk Inventor Professional 2017 software. The simulation results show that the gantry crane has a mass, von Mises stress, deformation, and safety factors respectively at 165.36 kg; 132.9 MPa; 13.67 mm; and 2.07.

Chassis is a main component of the vehicle. This work involves static and dynamics analysis to determine the key characteristics of a Bolero Maxi-Truck chassis. The modelling of the chassis was done by using the modelling software AUTODESK INVENTOR PROFESSIONAL 2016 and then imported into finite element package ANSYS 14.5. The analysis was done by using one of the most important numerical methods is FEA and the software used is ANSYS 14.5.The static characteristics include identifying location of high stress area and maximum deformation area of the chassis. The dynamic characteristics of maxi-truck chassis such as the natural frequency and mode shape were determined by using finite element (FE) method. In the analysis, the behaviour of the chassis will be shown in 6 mode shapes. Modal updating of the truck chassis model was done by adjusting the selective properties such as mass density and Poisson's ratio. Modifications have been suggested on the current chassis. Finally, the modification of the bolero maxi-truck chassis model was proposed to reduce the stress, deformation & weight of the truck chassis. The static structural analysis was done at different mesh conditions and results will be tabulated and graphs were plot. The results obtained from the modified chassis are compared with the original chassis, and the most optimized chassis is presented.

Penelitian ini mengkaji tentang ketahanan beban dinamis material CFRP dan Aluminium 6061 untuk material turbin angin terhadap kecepatan putar rotor (rpm). Desain 3 (tiga) bilah turbin angin menggunakan airfoil NACA 2415 dengan panjang 500 mm. Analisis dilakukan secara numerik dengan menggunakan software Autodesk Inventor Professional 2017. Variasi kecepatan rotor yang digunakan yaitu 100 rpm, 200 rpm, 300 rpm, dan 400 rpm. Hasil penelitian menunjukkan material CFRP memiliki faktor keamanan yang lebih baik daripada material Aluminium 6061 saat pengujian dengan menggunakan kecepatan rotor 400 rpm.

Kata kunci: turbin angin, naca 2415; metode elemen hingga; carbon fiber reinforced polymer (cfrp); aluminium 6061; rpm.

The article is devoted to the formation of students' information competence in the study of the discipline "Resistance of materials". This paper presents a systematic review of models and methodologies that integrate information and communication technologies (ICT) and education. An important component in the formation of information competence is the ability to use readymade software products in their professional activities. The article shows the relevance of the development of students of applied programs that contribute to improving the readiness of students for engineering activities. Emphasis is placed on improving understanding of the subject area when integrating experimental research and finite element modelling. The paper gives an example of using the application module of the Autodesk Inventor software package to calculate one of the problems of material resistance. One of the main goals of education at the global level has reduced the educational gap by bringing education to all people around the world [6].

This study examined the effect of material selection on the strength of the main landing gear frame for UAV aircraft using the finite element method. Linear static analysis was carried out using Autodesk Inventor Professional 2017 software. Main landing gear frame using Aluminum 5052-H38, Aluminium 5083 87 Cold Formed, Aluminium 6061, and CFRP. UAV aircraft was weighing 85 kg with a landing speed of 10 m/s and impact time of 0,5 second. The simulation results show that the landing gear frames of the lightest in a row were CFRP, Al 5083 87 Cold Formed, Al 5052-H38, and Al 6061. Materials that have the greatest safety factor were CFRP, Al 5083 87 Cold Formed, Al 6061, and Al 5052-H38.

Penelitian ini mengkaji tentang ketahanan beban dinamis material CFRP dan Aluminium 6061 untuk material turbin angin terhadap kecepatan putar rotor (rpm). Desain 3 (tiga) bilah turbin angin menggunakan airfoil NACA 2415 dengan panjang 500 mm. Analisis dilakukan secara numerik dengan menggunakan software Autodesk Inventor Professional 2017. Variasi kecepatan rotor yang digunakan yaitu 100 rpm, 200 rpm, 300 rpm, dan 400 rpm. Hasil penelitian menunjukkan material CFRP memiliki faktor keamanan yang lebih baik daripada material Aluminium 6061 saat pengujian dengan menggunakan kecepatan rotor 400 rpm.