Fayl Faylin tarixcesi Faylin istifadesi Faylin qlobal istifadesi MetamelumatlarBu SVG faylin PNG formatindaki bu gorunusunun olcusu 800 334 piksel Diger olculer 320 134 piksel 640 267 piksel 1 024 428 piksel 1 280 535 piksel 2 560 1 069 piksel 910 380 piksel Faylin orijinali SVG fayli nominal olaraq 910 380 piksel faylin olcusu 447 KB Bu fayl Vikianbarda yerlesir Aciqlama sehifesindeki melumatlar asagida gosterilib Vikianbar azad lisenziyali media anbaridir Siz de tohfe vere bilersiniz Xulase IzahJet engine numbered svg Eger ede bilseniz bu tesviri diger dillere tercume ederek hami ucun elcatan etmesine komek edin Tesekkur edirem Deutsch Schemazeichnung eines typischen Gasturbinen Triebwerks Luft wird durch die Geblasesschaufeln 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 Geblaseschaufeln im Verdichterabschnitt Einlass Niederdruckkompressor Fan Hochdruckkompressor Verbrennung Turbine und Schubduse 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 Francais nbsp Schema montrant un turboreacteur d avion typique simple flux simple corps L air est comprime par les pales en entrant dans le reacteur puis est melange avec le carburant qui brule dans la chambre de combustion Les gaz d echappement generent une forte reaction vers l avant et font egalement tourner les turbines qui actionnent les pales de compression Admission de l air Compression basse pression Compression haute pression Combustion Echappement Section chaude Turbines basse et haute pression Chambres de combustion Section froide Bouche d entree de l air Espanol Esquema de un motor estandar a reaccion El aire es comprimido por las palas del ventilador para ser mezclado con el carburante y explosionado en la camara de compresion La salida de los gases realiza un fuerte empuje hacia delante y hacen girar las turbinas que accionan las palas de compresion Admision Compresion baja presion Compresion alta presion Combustion Escape Seccion caliente Turbina baja y alta presion Camaras de combustion Seccion fria Entrada de aire Catala Esquema d un motor estandard a reaccio L aire d entrada es comprimit per les pales o aleps del ventilador per ser seguidament barrejat amb el combustible a la cambra de combustio La sortida dels gasos provoca l impuls i fa girar les turbines les quals mouen les pales de compressio Admissio Compressio baixa pressio Compressio alta pressio Combustio Escapament Seccio calenta Turbina baixa i alta pressio Cambres de combustio Seccio freda Entrada d aire Romană Schema unei turbine cu gaze Aerul introdus este comprimat de paletele compresorului după care intră in camera de ardere unde este introdus combustibil Amestecul este aprins iar gazele de ardere se destind in turbină efectuand lucru mecanic In imagine sunt specificate următoarele părţi componente Zona de admisie Zona de joasă presiune a compresorului Zona de inaltă presiune a compresorului Camera de ardere combustie Turbina si zona conul de evacuare Zona caldă Treptele de presiune inaltă medie si respectiv joasă ale turbinei Camera de ardere de combustie Zona rece Admisia aerului Russkij Shema turboreaktivnogo dvigatelya Vozduh szhimaetsya lopastyami kompressora smeshivaetsya s toplivom smes postupaet v kameru sgoraniya Goryachie vyhlopnye gazy obespechivayut dvizhenie vperyod i privodyat v dejstvie kompressor Zabor vozduha Kompressor nizkogo davleniya Kompressor vysokogo davleniya Kamera sgoraniya Rasshirenie rabochego tela v turbine i sople Goryachaya zona Turbina Zona sgoraniya topliva Holodnaya zona Vhodnoe ustrojstvo Polski Schemat jednoprzeplywowego silnika turboodrzutowego Powietrze pod cisnieniem wtlaczane jest przez sprezarke do komory spalania gdzie dostarczane jest paliwo i zachodzi proces spalania Gorace spaliny napedzaja turbine polaczona walem ze sprezarka Dyfuzor wlotowy Sprezarka niskiego cisnienia Sprezarka wysokiego cisnienia Komory spalania Dysza wylotowa wraz z turbin Czesc goraca Turbiny wysokiego i niskiego cisnienia Rura ogniowa Czesc zimna Wlot powietrza Tiếng Việt Sơ đồ của một động cơ turbin phản lực Khong khi được nen từ cac quạt khi no đi vao động cơ va no được trộn va bị đốt với nhien 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 Tarix 7 yanvar 2008 07 09 UTC Menbe Oz isi vector version of en Image FAA 8083 3A Fig 14 1 PNG which comes from an FAA handbook Muellif Jeff Dahl Diger versiyalar redakte Numbered version Deutsch alman English ingilis espanol ispan francais fransiz svenska isvec Turkce turk मर ठ marathi ह न द hind অসম য assam ব ল benqal ગ જર ત qucarat త ల గ teluqu ಕನ ನಡ kannada മലയ ള malayalam ব ল benqal தம ழ tamil 日本語 yapon עברית ivrit العربية ereb پښتو pustu فارسی fars russkij rus This SVG file contains embedded text that can be translated into your language using any capable SVG editor text editor or the SVG Translate tool For more information see About translating SVG files SVG nbsp genesisInfoField nbsp The SVG code is valid nbsp This vector image was created with Inkscape or with something else Goruntu 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 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 stralerenjinAlemannisch As Diagram vom a na StrautriebwarchAsturianu Cadarma d un reautor Bosanski Dijagram tipicnog avionskog benzinskog motora Cestina Schematicke znazorneni proudoveho motoruDansk Diagram over en typisk jetmotor gasturbine Deutsch Diagramm eines StrahltriebwerksEnglish Diagram of a typical gas turbine jet engine Espanol Diagrama de un reactor Euskara Erreakzio motore baten diagrama Francais Schema montrant un turboreacteur d avion typiqueIslenska Skyringarmynd sem synir daemigerdan thotuhreyfil Italiano Schema di un motore a getto Lietuviu Tipiska duju turbinos reaktyvinio variklio diagrama Magyar Gazturbinas sugarhajtomu felepiteseNederlands diagram van een tunnelschroefturbinePolski Diagram typowej turbiny gazowej w silniku odrzutowym Portugues Diagrama esquematico de uma tipica turbina a gas Romană Schemă numerotată a celei mai comune turbinei cu gaze folosită in aviație Svenska Schematisk bild av en turbinjetmotor Turkce Jet motoru gaz turbininin cizimiBelaruskaya Shema gazavaj turbiny reaktyynaga ruhavikaRusskij Shema turboreaktivnogo dvigatelya Srpski srpski Diјagram tipichne avionske benzinske turbine motora 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 Lisenziya Jeff Dahl the copyright holder of this work hereby publishes it under the following licenses Bu senedi GNU Azad Senedlesdirme Lisenziyasi Versiya 1 2 ve ya Azad Proqram Fondu terefinden nesr olunan her hansi sonraki versiya sertlerine esasen deyismez bolmeler on qapaq metnleri ve arxa qapaq metnleri olmadan kocurmek yayimlamaq ve ve ya deyisdirmek ucun icaze verilir Lisenziyanin bir nusxesi GNU Azad Senedlesdirme Lisenziyasi adli hisseye daxil edilmisdir http www gnu org copyleft fdl html GFDL GNU Free Documentation License true true Bu fayl Creative Commons Attribution Share Alike 4 0 International 3 0 Unported 2 5 Generic 2 0 Generic ve 1 0 Generic lisenziyasi altinda yayimlanmisdir Atribut Jeff DahlSiz hec bir mehdudiyyet olmadan paylasa bilersiniz eseri kocure paylaya ve oture bilersiniz remiks ede bilersiniz eseri adaptasiya ede bilersiniz Asagidaki sertlere emel etmekle istinad vermek Muvafiq istinad vermeli lisenziyaya kecid elave etmeli ve deyisiklikler edilib edilmediyini bildirmelisiniz Siz bunu istenilen sekilde ede bilersiniz lakin lisenziya verenin size sexsen icaze verdiyini gosteren formada yox benzer paylasma Eseri remix edirsinizse deyisdirirsinizse ve ya uzerinde is aparirsinizsa oz tohfelerinizi orijinalda oldugu kimi eyni ve ya uygun lisenziya altinda yayimlamalisiniz https creativecommons org licenses by sa 4 0 CC BY SA 4 0 Creative Commons Attribution Share Alike 4 0 true true Istediyiniz lisenziyani sece bilersiniz AnnotationsInfoFieldThis image is annotated View the annotations at Commons57 8 9 9 910 380 Intake 137 8 9 9 910 380 Low pressure compression 299 9 9 9 910 380 High pressure compression 508 6 9 9 910 380 Combustion 19 309 9 9 910 380 Ambient Air 210 357 9 9 910 380 Cold Section 678 361 9 9 910 380 Hot Section 615 312 9 9 910 380 Turbine 713 10 9 9 910 380 Exhaust Nozzle 403 307 9 9 910 380 Combustion SectionBasliqlarazerbaycancaBu faylin neyi temsil etdiyine dair bir setirlik izahat elave etingilisnederlandsBu faylda tesvir olunan elementlertesvir edirReaktiv muherrikyaradiciVikidata elementi olmayan bir nece deyerURL https commons wikimedia org wiki user Jeff DahlVikimedia istifadeci adi Jeff Dahlobyektin rolu fotoqrafmuellifin qisa adi Jeff Dahlcopyright status nbsp ingiliscopyrighted nbsp ingilislisenziyaCreative Commons Attribution ShareAlike 2 5 Generic nbsp ingilisCreative Commons Attribution ShareAlike 1 0 Generic nbsp ingilisCreative Commons Attribution ShareAlike 4 0 International nbsp ingilisGNU Free Documentation License version 1 2 or later nbsp ingilisCC BY SA 3 0Creative Commons Attribution ShareAlike 2 0 Generic nbsp ingilisCommons quality assessment nbsp ingilisWikimedia Commons featured picture nbsp ingilissource of file nbsp ingilisoriginal creation by uploader nbsp ingilisyaranma tarixi7 yanvar 2008 Faylin tarixcesi Faylin evvelki versiyasini gormek ucun gun tarix bolmesindeki tarixlere klikleyin Tarix VaxtMiniaturOlculerIstifadeciSerh hal hazirki04 25 8 yanvar 2008910 380 447 KB Jeff DahlLabel fixes 18 45 7 yanvar 2008910 380 444 KB Jeff Dahlstroke to path 18 43 7 yanvar 2008910 380 444 KB Jeff DahlBracket fixes 18 40 7 yanvar 2008910 380 443 KB Jeff DahlBracket fixes 18 37 7 yanvar 2008910 380 443 KB Jeff Dahlbracket fixes 18 32 7 yanvar 2008910 380 443 KB Jeff Dahlrm whitespace 07 09 7 yanvar 20081 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 Faylin istifadesi Asagidaki sehife bu fayli istifade edir Reaktiv muherrik Faylin qlobal istifadesi Bu fayl asagidaki vikilerde istifade olunur ar wikipedia org layihesinde istifadesi إسقاطات عمودية ba wikipedia org layihesinde istifadesi Eske yanyuly dvigatel be wikipedia org layihesinde istifadesi Reaktyyny ruhavik bn wikipedia org layihesinde istifadesi উইক প ড য আজক র ন র ব চ ত ছব এপ র ল ২০০৮ ca wikipedia org layihesinde istifadesi Turbina de gas crh wikipedia org layihesinde istifadesi Sablon Potd 2008 04 cv wikipedia org layihesinde istifadesi Shablon Potd 2008 04 de wikipedia org layihesinde istifadesi Benutzer Lychee CBDJ08 Diskussion Turbinen Strahltriebwerk Archiv 1 Portal Luftfahrt BildergalerieHistorie en wikipedia org layihesinde istifadesi Multiview orthographic projection Components of jet engines es wikipedia org layihesinde istifadesi Forjado isotermico Turbina axial eu wikipedia org layihesinde istifadesi Erreakzio motor Lankide Mikel Olabarria Proba orria hu wikipedia org layihesinde istifadesi Wikipedia A nap kepe 2008 04 Wikipedia Kezdolapmuhely A nap kepe 2008 04 hy wikipedia org layihesinde istifadesi Տուրբոռեակտիվ շարժիչ id wikipedia org layihesinde istifadesi Komponen mesin jet it wikipedia org layihesinde istifadesi Turbogetto Proiezioni ortogonali Impianti velivolo Utente 3Pappa3 Multiview orthographic projection ko wikipedia org layihesinde istifadesi 위키백과 오늘의 그림 2008년 4월 단면 lbe wikipedia org layihesinde istifadesi Shablon Potd 2008 04 mg wikipedia org layihesinde istifadesi Wikipedia Sary Sarin 039 ny anio 28 Jiona 2026 Wikipedia Sary taona 2026 nl wikipedia org layihesinde istifadesi Turbojet nl wiktionary org layihesinde istifadesi turbojet no wikipedia org layihesinde istifadesi Lokomotiv os wikipedia org layihesinde istifadesi Shablon Potd 2008 04 outreach wikimedia org layihesinde istifadesi WikiArS Tips and Resources Ref Technical illustration pl wikipedia org layihesinde istifadesi Silnik odrzutowy Wikiprojekt Ilustrowanie Odkrycia Wikiprojekt Ilustrowanie Medalowe zasoby Commons Styczen 2008 Wikiprojekt Ilustrowanie Medalowe zasoby Commons 9 pt wikipedia org layihesinde istifadesi Wikipedia Imagem em destaque Abril de 2008 Wikipedia Imagem em destaque 2 de Abril de 2008 Portal Aviacao Imagem em Destaque Usuario Luz28 Testes 12 Portal Aviacao Imagem em Destaque 64 Wikipedia Discussao Projetos Aviacao 2018 Polo UFSC ru wikipedia org layihesinde istifadesi Dvigatel vnutrennego sgoraniya Vozdushno reaktivnyj dvigatel Turboreaktivnyj dvigatel Shablon Potd 2008 04 Obsuzhdenie Reaktivnyj dvigatel Bu faylin qlobal istifadesine baxin Metamelumatlar Bu faylda fotoaparat ve ya skanerle elave olunmus melumatlar var Eger fayl sonradan redakte olunubsa bezi parametrler bu sekilde gosterilenlerden ferqli ola biler Genislik910Hundurluk380 Menbe https az wikipedia org wiki Fayl Jet engine numbered svg