File:Jet engine.svg

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Summary

Description
English: 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 exhaust gases provide forward thrust and turn the turbines which drive the compressor fan blades.
Deutsch: Schematischer Aufbau eines Strahltriebwerkes. Einströmende Luft wird durch die Rotorblätter komprimiert, gelangt in die Brennkammer, wo sie zusammen mit einem Treibstoffgemisch verbrannt wird. Die ausströmenden Abgase sorgen für den Schub und treiben zugleich die Turbine an, die die Rotorblätter in Bewegung hält.
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。
Русский: Схема типичного газотурбинного реактивного двигателя. Поступающий в двигатель воздух сжимается в компрессоре, смешивается с топливом и сжигается в камерах сгорания. Горячие выхлопные газы обеспечивают тягу и вращают турбину, которые приводят в движение компрессор.
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
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This is a featured picture on Wikimedia Commons (Featured pictures) and is considered one of the finest images. See its nomination here.
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United States Navy

jet engine

inception

16 December 2007

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Date/TimeThumbnailDimensionsUserComment
current18:21, 5 June 2022Thumbnail for version as of 18:21, 5 June 20221,000 × 400 (82 KB)wikimediacommons>SemperVincoReduced source complexity; converted traced text to actual text (all translations should really be done using <switch>); size could be reduced much further by exploiting symmetry

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