File:Jet engine.svg
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. |
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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 | ||
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Jeff Dahl, the copyright holder of this work, hereby publishes it under the following licenses:
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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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