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The General Electric/Allison J33 is a development of the General Electric J31, enlarged to produce significantly greater thrust, starting at 4,000 lbf (18 kN) and ending at 4,600 lbf (20 kN) with an additional low-altitude boost to 5,400 lbf (24 kN) with water-alcohol injection.

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rdf:type
rdfs:label
  • Allison J33 (cs)
  • General Electric J33 (de)
  • Allison J33 (en)
  • Allison J33 (es)
  • Allison J33 (it)
  • Allison J33 (fr)
  • アリソン J33 (ja)
rdfs:comment
  • General Electric/Allison J33 byl americký proudový motor, který vznikl jako vývojový stupeň motoru . Byl mj. zvětšen za účelem významného zvýšení tahu. Nejprve na 18 kN (4 000 lbf), poté na 20 kN (4 600 lbf) a s dodatečným vstřikování směsi vody a alkoholu v nižších letouvých hladinách poskytoval tah až 24 kN (5 400 lbf). (cs)
  • The General Electric/Allison J33 is a development of the General Electric J31, enlarged to produce significantly greater thrust, starting at 4,000 lbf (18 kN) and ending at 4,600 lbf (20 kN) with an additional low-altitude boost to 5,400 lbf (24 kN) with water-alcohol injection. (en)
  • Das General Electric J33 (auch General Electric I-40 und Allison J33) war ein Turbojet-Triebwerk auf Basis des General Electric J31. Im Gegensatz zu diesem wurde die Anströmung der Turbine jedoch dadurch vereinfacht, dass die Brennkammern gerade verliefen. In seiner Ausführung entspricht es dem de Havilland Goblin. (de)
  • El General Electric/Allison J33 fue un desarrollo estadounidense de los primeros Rolls-Royce Derwent de Frank Whittle, agrandados para producir mucha más potencia, desde 18 kN (1837 kgf) a 20 kN (2040 kgf), con una potencia adicional a baja altitud de 24 kN (2450 kgf) con inyección de agua-alcohol. (es)
  • Le General Electric / Allison J33 était un développement du General Electric J31, élargi pour produire beaucoup plus de poussée, de 4 000 lbf (18 kN) à 4 600 lbf (20 kN) avec, à faible altitude un boost supplémentaire à 5 400 lbf (24 kN) par injection d'eau-alcool. (fr)
  • アリソンJ33はアメリカ合衆国の遠心式圧縮機を備えたターボジェットエンジンである。 (ja)
  • Il General Electric/Allison J33 era un motore aeronautico turbogetto con compressore centrifugo sviluppato dalla statunitense General Electric negli anni quaranta. Fu sviluppato a partire dal motore Rolls-Royce Derwent di Frank Whittle, maggiorandolo in modo da fornire una spinta compresa tra 18 e 20,4 kN con la possibilità di una extra potenza fino a 24 kN a bassa quota utilizzando l'iniezione di una miscela di acqua ed alcol. (it)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/2020-09-061-J33.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/ALLISON_J33.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/Allison_J33-A-35_Keski-Suomen_ilmailumuseo_1.jpg
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sameAs
similar engines
  • * de Havilland Ghost * Rolls-Royce Derwent (en)
thrust
  • static dry at 11,750 rpm at sea level for take-off (en)
  • ::::Take-off thrust, static wet: at 11,750 rpm at sea level ::::Normal thrust, static: at 11,000 rpm at sea level (en)
thrust/weight
turbine
  • single-stage axial (en)
turbinetemp
  • TIT: ; JPT: (en)
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