File:Jet engine numbered.svg
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Size of this PNG preview of this SVG file: 800 × 334 pixels. Other resolutions: 320 × 134 pixels | 640 × 267 pixels | 1,024 × 428 pixels | 1,280 × 535 pixels | 2,560 × 1,069 pixels | 910 × 380 pixels.
Original file (SVG file, nominally 910 × 380 pixels, file size: 447 KB)
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Summary
| DescriptionJet engine numbered.svg |
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.
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.
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.
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.
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.
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:
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.
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.
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:
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| 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 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 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 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. 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. 中文: 一个典型的燃气涡轮喷气发动机图解 |
This image was selected as picture of the day on Vietnamese Wikipedia.
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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.http://www.gnu.org/copyleft/fdl.htmlGFDLGNU Free Documentation Licensetruetrue |
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.
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You may select the license of your choice.
| Annotations InfoField | This image is annotated: View the annotations at Commons |
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Intake
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Low pressure compression
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High pressure compression
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Combustion
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Ambient Air
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Cold Section
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Hot Section
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Turbine
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Exhaust Nozzle
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Combustion Section
Captions
nederlands
Items portrayed in this file
depicts
7 January 2008
457,868 byte
image/svg+xml
b71ce76e9fa4a03010c93f7464e0d7399ddebdb1
File history
Click on a date/time to view the file as it appeared at that time.
| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 04:25, 8 January 2008 | 910 × 380 (447 KB) | wikimediacommons>Jeff Dahl | Label fixes |
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| Width | 910 |
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| Height | 380 |
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