About: Allison J35     Goto   Sponge   NotDistinct   Permalink

An Entity of Type : yago:WikicatAllisonAircraftEngines, within Data Space : dbpedia.org associated with source document(s)
QRcode icon
http://dbpedia.org/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FAllison_J35

The General Electric/Allison J35 was the United States Air Force's first axial-flow (straight-through airflow) compressor jet engine. Originally developed by General Electric (GE company designation TG-180) in parallel with the Whittle-based centrifugal-flow J33, the J35 was a fairly simple turbojet, consisting of an eleven-stage axial-flow compressor and a single-stage turbine. With the afterburner, which most models carried, it produced a thrust of 7,400 lbf (33 kN). Like the J33, the design of the J35 originated at General Electric, but major production was by the Allison Engine Company.

AttributesValues
rdf:type
rdfs:label
  • Allison J35 (cs)
  • General Electric J35 (de)
  • Allison J35 (en)
  • Allison J35 (fr)
  • Allison J35 (it)
  • アリソン J35 (ja)
  • Allison J35 (pl)
  • Allison J35-A-35 (pt)
rdfs:comment
  • Das General Electric J35 (auch Allison J35 und General Electric TG-180) ist ein Turbojet-Triebwerk des US-amerikanischen Herstellers General Electric Company. Das Triebwerk wurde 1947 serienreif und war das erste Strahltriebwerk in den USA, das sowohl über einen axialen Verdichter als auch eine axiale Turbine verfügte. Es wurde ausschließlich für militärische Zwecke verwendet und wurde mit einem Nachbrenner ausgeliefert. (de)
  • The General Electric/Allison J35 was the United States Air Force's first axial-flow (straight-through airflow) compressor jet engine. Originally developed by General Electric (GE company designation TG-180) in parallel with the Whittle-based centrifugal-flow J33, the J35 was a fairly simple turbojet, consisting of an eleven-stage axial-flow compressor and a single-stage turbine. With the afterburner, which most models carried, it produced a thrust of 7,400 lbf (33 kN). Like the J33, the design of the J35 originated at General Electric, but major production was by the Allison Engine Company. (en)
  • Il General Electric/Allison J35 era un motore aeronautico turbogetto sviluppato nella seconda metà degli anni quaranta negli Stati Uniti dalla General Electric e poi prodotto dalla Allison Engine Company. Fu il primo motore con il compressore a flusso assiale usato dalla United States Air Force. (it)
  • アリソンJ35(Allison J35)は、アメリカ合衆国の軸流式圧縮機を備えたターボジェットエンジン。 (ja)
  • O Alison J35-A-35 foi uma turbina turbojato desenvolvida pela General Electric (designado como TG 180 pela empresa) mas fabricado primariamente pela . Era o motor utilizado nos caças a jata F-89 Scorpion, um dos primeiros caças a jato do mundo. Tinha empuxo de 24.26 kN e com pós-combustor, 32.11 kN. (pt)
  • General Electric/Allison J35 byl proudový motor původně vyvinutý firmou General Electric (tovární označení TG-180) paralelně s motorem s J33 (který byl založen na výzkumu Franka Whittlea s radiálním kompresorem) a první motor s axiálním kompresorem, který sloužil u amerického letectva. J35 byl poměrně jednoduchý motor skládající se z jedenáctistupňového axiálního kompresoru a jednostupňové turbíny. S přídavným spalováním, kterým byla většina motorů vybavena, poskytoval tah 7 400 lbf (32,92 kN). (cs)
  • Le General Electric/Allison J35 était un turboréacteur simple flux monocorps, conçu originellement aux États-Unis par l'entreprise General Electric (désignation interne TG-180), en parallèle au turboréacteur à flux centrifuge de style « Whittle » Allison J33. Il fut le premier réacteur à flux axial de l’US Air Force. Le J35 était d'une conception très simpliste, avec un compresseur axial à onze étages, huit chambres de combustion tubulaires et une turbine à étage unique. Avec la postcombustion, ce que la plupart des modèles possédaient, il produisait une poussée de 32,92 kN. (fr)
  • Allison J35 – amerykański silnik turboodrzutowy produkowany w zakładach , pierwszy silnik United States Air Force ze sprężarka osiową, opracowany w tym samym czasie miał sprężarkę odśrodkową. Silnik opracowany był w zakładach General Electric, gdzie znany był pod odznaczeniem TG-180. (pl)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/Allison_J35.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/GE-Allison-J35-Engine.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/J-35-A-4_Turbojet_Combustor_Dome.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/J-35-A-4_Turbojet_Fuel_Atomizer.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/General_Electric-Allison_J35_turbojet_in_Aalborg_Forsvars-_og_Garnisonsmuseum,_pic3.jpg
dcterms:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
Link from a Wikipage to an external page
sameAs
Faceted Search & Find service v1.17_git139 as of Feb 29 2024


Alternative Linked Data Documents: ODE     Content Formats:   [cxml] [csv]     RDF   [text] [turtle] [ld+json] [rdf+json] [rdf+xml]     ODATA   [atom+xml] [odata+json]     Microdata   [microdata+json] [html]    About   
This material is Open Knowledge   W3C Semantic Web Technology [RDF Data] Valid XHTML + RDFa
OpenLink Virtuoso version 08.03.3330 as of Mar 19 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (378 GB total memory, 60 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software