File:Cannular combustor on a Pratt & Whitney JT9D turbofan.jpg

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English: Cutaway of the annular combustion chamber on a Pratt & Whitney JT9-7D turbofan engine. The air flow is from left to right.

Discrete fuel injectors maintain flame zones which share a common ring (annulus) casing.

This engine is part of the exhibit of the Deutsches Museum.
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Author Olivier Cleynen

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19 July 2011

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current09:12, 11 March 2012Thumbnail for version as of 09:12, 11 March 20123,368 × 2,304 (1.52 MB)Ariadacapo

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