File:Jet engine arabic.svg

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العربية: رسم توضيحي لمحرك توربين غاز (بالعربية). يضغط الهواء خلال دخول إلى التوربين بشفرات المروحة ويحرق مع الوقود في قسم الاحتراق. تعطي الغازات العادمة الساخنة المنبعثة من العادم العزم اللازم لتحريك التوربين والذي يحرك شفرات الضاغط.
English: Diagram of a typical gas turbine jet engine (in Arabic). 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 anglais 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 à 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 (UTC)
Source self-made, vector version of en:Image:FAA-8083-3A Fig 14-1.PNG which comes from an FAA handbook
Author Jeff Dahl
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current20:56, 1 April 2008Thumbnail for version as of 20:56, 1 April 20081,000 × 400 (490 KB)Jak (talk | contribs)== Summary == {{Inkscape}} {{Information |Description={{en|Diagram of a typical gas turbine jet engine (in English). 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 exhau

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