File:Jet engine-Persian.svg

Summary

Description
فارسی: اصول کار توربوجت
English: Diagram of a typical gas turbine jet engine (in French). 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 français 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 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 16 December 2007, 07:15 (UTC)
Source Category:Deprecated template usage: AttribSVG#Jet%20engine-Persian.svg
 
This vector image includes elements that have been taken or adapted from this file:
 Jet engine.svg (by Jeff Dahl).
Category:Vector images using elements from other vector images#Jet%20engine-Persian.svg
Author Jeff Dahl, Persian translation by Ali Zifan (28 July 2016)
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Jeff Dahl, Persian translation by Ali Zifan (28 July 2016)
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Category:Jet engine schematic diagrams Category:Persian-language SVG diagrams Category:Cutaway diagrams of aircraft engines
Category:CC-BY-SA-4.0,3.0,2.5,2.0,1.0 Category:Created with Inkscape-undef Category:Cutaway diagrams of aircraft engines Category:Deprecated template usage: AttribSVG Category:GFDL Category:Jet engine schematic diagrams Category:License migration redundant Category:Persian-language SVG diagrams Category:Self-published work Category:Translation possible - SVG Category:Valid SVG created with Inkscape Category:Vector images using elements from other vector images