File:Cannular combustor on a Pratt & Whitney JT9D turbofan.jpg
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Summary
| Description |
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. |
| Date | |
| Source | Own work |
| Author | Olivier Cleynen |
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 09:12, 11 March 2012 | | 3,368 × 2,304 (1.52 MB) | Ariadacapo |
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