File:Jet engine French.svg

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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。
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
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Jeff Dahl, French translation by Berrucomons, the copyright holder of this work, hereby publishes it under the following licenses:
GNU head Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License.
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Attribution: Jeff Dahl, French translation by Berrucomons
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current09:20, 13 February 2008Thumbnail for version as of 09:20, 13 February 20081,000 × 400 (462 KB)Berrucomons (talk | contribs)== 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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