File:Jet_engine_French.svg
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Summary
DescriptionJet engine French.svg |
English: Diagram of a typical gas turbine jet engine (in French). Air is compressed by the fan blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which drive the compressor fan blades.
Français : Schéma en français montrant un turboréacteur d'avion typique (simple flux, simple corps). L'air est comprimé par les pales en entrant dans le réacteur, puis est mélangé avec le carburant qui brule dans la chambre de combustion. Les gaz d'échappement donnent une forte poussée en avant et fait tourner les turbines qui actionnent les pales de compression.
中文:一个典型的燃气涡轮喷气发动机图解。 |
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Date | 16 December 2007, 07:15 (UTC) | ||
Source | Own work, vector version of en:Image:FAA-8083-3A Fig 14-1.PNG which comes from an FAA handbook | ||
Author | Jeff Dahl, French translation by Berrucomons | ||
Permission (Reusing this file) |
Jeff Dahl, French translation by Berrucomons, the copyright holder of this work, hereby publishes it under the following licenses:
This file is licensed under the Creative Commons Attribution-Share Alike Attribution-Share Alike 4.0 International, 3.0 Unported, 2.5 Generic, 2.0 Generic and 1.0 Generic license. Attribution: Jeff Dahl, French translation by Berrucomons
You may select the license of your choice. |
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SVG development InfoField | This vector image was created with Inkscape, or with something else. |
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16 December 2007
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 09:20, 13 February 2008 | 1,000 × 400 (462 KB) | Berrucomons | == Summary == {{Inkscape}} {{Information |Description={{en|Diagram of a typical gas turbine jet engine (in French). Air is compressed by the fan blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaus |
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Global file usage
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