File:Jet engine numbered.svg

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Deutsch: Schemazeichnung eines typischen Gasturbinen-Triebwerks. Luft wird durch die Gebläsesschaufeln im Verdichterabschnitt komprimiert, wenn sie in die Turbine eintritt. Sie wird mit Kraftstoff gemischt und im Verbrennungsabschnitt verbrannt. Die heißen Abgase entwickeln Schub nach vorne und drehen die Turbinenschaufeln und damit die Gebläseschaufeln im Verdichterabschnitt.

Einlass
Niederdruckkompressor (Fan)
Hochdruckkompressor
Verbrennung
Turbine und Schubdüse
Heißer Abschnitt
Hoch- und Niederdruckturbine
Brennkammern
Kalter Abschnitt
Lufteinlass

English: Diagram of a typical gas turbine jet engine. 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.

Intake
Low pressure compression
High pressure compression
Combustion
Exhaust
Hot section
Turbines Low and High pressure
Combustion chambers
Cold section
Air inlet

Français : Schéma 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 génèrent une forte réaction vers l'avant, et font également tourner les turbines qui actionnent les pales de compression.

Admission de l'air
Compression - basse pression
Compression - haute pression
Combustion
Échappement
Section chaude
Turbines basse et haute pression
Chambres de combustion
Section froide
Bouche d'entrée de l'air

Español: Esquema de un motor estándar a reacción. El aire es comprimido por las palas del ventilador, para ser mezclado con el carburante y explosionado en la cámara de compresión. La salida de los gases realiza un fuerte empuje hacia delante y hacen girar las turbinas que accionan las palas de compresión.

Admisión
Compresión - baja presión
Compresión - alta presión
Combustión
Escape
Sección caliente
Turbina baja y alta presión
Cámaras de combustión
Sección fría
Entrada de aire

Català: Esquema d'un motor estàndard a reacció. L'aire d'entrada es comprimit per les pales o àleps del ventilador, per ser seguidament barrejat amb el combustible a la cambra de combustió. La sortida dels gasos provoca l'impuls i fa girar les turbines, les quals mouen les pales de compressió.

Admissió
Compressió - baixa pressió
Compressió - alta pressió
Combustió
Escapament
Secció calenta
Turbina baixa i alta pressió
Cambres de combustió
Secció freda
Entrada d'aire

Română: Schema unei turbine cu gaze. Aerul introdus este comprimat de paletele compresorului, după care intră în camera de ardere, unde este introdus combustibil. Amestecul este aprins, iar gazele de ardere se destind în turbină, efectuând lucru mecanic. În imagine sunt specificate următoarele părţi componente:

Zona de admisie
Zona de joasă presiune a compresorului
Zona de înaltă presiune a compresorului
Camera de ardere (combustie)
Turbina şi zona (conul) de evacuare
Zona caldă
Treptele de presiune înaltă, medie şi, respectiv, joasă ale turbinei
Camera de ardere (de combustie)
Zona rece
Admisia aerului

Русский: Схема турбореактивного двигателя. Воздух сжимается лопастями компрессора, смешивается с топливом, смесь поступает в камеру сгорания. Горячие выхлопные газы обеспечивают движение вперёд и приводят в действие компрессор.

Забор воздуха
Компрессор низкого давления
Компрессор высокого давления
Камера сгорания
Расширение рабочего тела в турбине и сопле
Горячая зона
Турбина
Зона сгорания топлива
Холодная зона
Входное устройство

Polski: Schemat jednoprzepływowego silnika turboodrzutowego. Powietrze pod ciśnieniem wtłaczane jest przez sprężarkę do komory spalania gdzie dostarczane jest paliwo i zachodzi proces spalania. Gorące spaliny napędzają turbinę połączona wałem ze sprężarką.

Dyfuzor wlotowy
Sprężarka niskiego ciśnienia
Sprężarka wysokiego ciśnienia
Komory spalania
Dysza wylotowa wraz z turbin
Część gorąca
Turbiny wysokiego i niskiego ciśnienia
Rura ogniowa
Część zimna
Wlot powietrza

Tiếng Việt: Sơ đồ của một động cơ turbin phản lực. Không khí được nén từ các quạt khi nó đi vào động cơ, và nó được trộn và bị đốt với nhiên nhiệu trong buồng đốt.

中文：一个典型的燃气涡轮喷气发动机图解。上面流程标识为：

吸入
低压压缩
高压压缩
燃烧
排气
热区域
涡轮机
燃烧室
冷区域
进气口

Date

7 January 2008, 07:09 (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

Other versions

[edit]

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English (English)
español (Spanish)
français (French)
svenska (Swedish)
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मराठी (Marathi)
हिन्दी (Hindi)
অসমীয়া (Assamese)
বাংলা (Bangla)
ગુજરાતી (Gujarati)
తెలుగు (Telugu)
ಕನ್ನಡ (Kannada)
മലയാളം (Malayalam)
বাংলা (Bangla)
தமிழ் (Tamil)
日本語 (Japanese)
עברית (Hebrew)
العربية (Arabic)
پښتو (Pashto)
فارسی (Persian)
русский (Russian)

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Picture of the year
	This file was a candidate in Picture of the Year 2008. This is a featured picture on Wikimedia Commons (Featured pictures) and is considered one of the finest images. See its nomination here. If you have an image of similar quality that can be published under a suitable copyright license, be sure to upload it, tag it, and nominate it.

This image was selected as picture of the day on Wikimedia Commons for 2 April 2008. It was captioned as follows:

English: Diagram of a typical gas turbine jet engine.

Other languages:

Afrikaans: Diagram van 'n tipiese gasturbine stralerenjin

Alemannisch: Äs Diagram vom a nä Strautriebwärch

Asturianu: Cadarma d'un reautor.

Bosanski: Dijagram tipičnog avionskog benzinskog motora.

Čeština: Schematické znázornění proudového motoru

Dansk: Diagram over en typisk jetmotor (gasturbine)

Deutsch: Diagramm eines Strahltriebwerks

English: Diagram of a typical gas turbine jet engine.

Español: Diagrama de un reactor.

Euskara: Erreakzio-motore baten diagrama.

Français : Schéma montrant un turboréacteur d'avion typique

Íslenska: Skýringarmynd sem sýnir dæmigerðan þotuhreyfil.

Italiano: Schema di un motore a getto.

Lietuvių: Tipiška dujų turbinos reaktyvinio variklio diagrama.

Magyar: Gázturbinás sugárhajtómű felépítése

Nederlands: diagram van een tunnelschroefturbine

Polski: Diagram typowej turbiny gazowej w silniku odrzutowym.

Português: Diagrama esquemático de uma típica turbina a gás.

Română: Schemă numerotată a celei mai comune turbinei cu gaze folosită în aviație.

Svenska: Schematisk bild av en turbinjetmotor.

Türkçe: Jet motoru gaz türbininin çizimi

Беларуская: Схема газавай турбіны рэактыўнага рухавіка

Русский: Схема турбореактивного двигателя.

Српски / srpski: Дијаграм типичне авионске бензинске турбине (мотора).

한국어: 전형적인 가스 터빈 제트 엔진의 다이어그램.

日本語：ガスタービンジェットエンジンの動作原理(詳細図)

中文：一个典型的燃气涡轮喷气发动机图解

中文（繁體）：一個典型的燃氣輪機噴射發動機圖解

This image was selected as picture of the day on Vietnamese Wikipedia.

Licensing

Jeff Dahl, the copyright holder of this work, hereby publishes it under the following licenses:

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.

This file is licensed under the Creative Commons Attribution-Share Alike 4.0 International, 3.0 Unported, 2.5 Generic, 2.0 Generic and 1.0 Generic license.

Attribution: Jeff Dahl

You are free:

to share – to copy, distribute and transmit the work
to remix – to adapt the work

Under the following conditions:

attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
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You may select the license of your choice.

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File history

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	Date/Time	Dimensions	User	Comment
current	04:25, 8 January 2008	910 × 380 (447 KB)	Jeff Dahl	Label fixes
	18:45, 7 January 2008	910 × 380 (444 KB)	Jeff Dahl	stroke to path
	18:43, 7 January 2008	910 × 380 (444 KB)	Jeff Dahl	Bracket fixes
	18:40, 7 January 2008	910 × 380 (443 KB)	Jeff Dahl	Bracket fixes
	18:37, 7 January 2008	910 × 380 (443 KB)	Jeff Dahl	bracket fixes
	18:32, 7 January 2008	910 × 380 (443 KB)	Jeff Dahl	rm whitespace
	07:09, 7 January 2008	1,000 × 400 (444 KB)	Jeff Dahl	{{Inkscape}} {{Information \|Description={{en\|Diagram of a typical gas turbine jet engine.}} \|Source=self-made \|Date=~~~~~ \|Author= Jeff Dahl \|Permission= \|other_versions=100px }}