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The Turbomeca Palas is a diminutive centrifugal flow turbojet engine used to power light aircraft. An enlargement of the Turbomeca Piméné, the Palas was designed in 1950 by the French manufacturer Société Turbomeca, and was also produced under licence by Blackburn and General Aircraft in the United Kingdom and Teledyne Continental Motors in the United States as the Continental Model 320.

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dbo:abstract
  • Le Turbomeca Palas est un petit turboréacteur à flux centrifuge français, utilisé pour propulser des avions légers. (fr)
  • TheTurbomeca Palas adalah sebuah mesin pesawat turbojet sentrifugal kecil digunakan untuk daya lampu. Ini dirancang pada tahun 1950 oleh pabrik Prancis Société Turbomeca, dan juga diproduksi dengan lisensi oleh Blackburn and General Aircraft di Britania Raya dan Teledyne Continental Motors di Amerika Serikat. (in)
  • The Turbomeca Palas is a diminutive centrifugal flow turbojet engine used to power light aircraft. An enlargement of the Turbomeca Piméné, the Palas was designed in 1950 by the French manufacturer Société Turbomeca, and was also produced under licence by Blackburn and General Aircraft in the United Kingdom and Teledyne Continental Motors in the United States as the Continental Model 320. (en)
  • パラス(Palas )は小型機に使用された小型の遠心圧縮式ターボジェットエンジンである。1950年にフランスのチュルボメカで設計され、英国のブラックバーン・エアクラフトと米国のコンチネンタル・モータースでライセンス生産された。 (ja)
  • Il Turbomeca Palas era un motore turbogetto a compressore centrifugo utilizzato su velivoli leggeri. Venne progettato nel 1950 dal produttore francese Société Turbomeca e successivamente prodotto sotto licenza dalla Blackburn and General Aircraft in Gran Bretagna e dalla negli Stati Uniti. (it)
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dbo:wikiPageRevisionID
  • 1124876947 (xsd:integer)
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dbp:combustion
  • annular with rotary fuel injection (en)
dbp:compression
  • 4 (xsd:integer)
dbp:compressor
  • single-stage centrifugal (en)
dbp:date
  • 2007-10-07 (xsd:date)
dbp:developedFrom
dbp:fueltype
dbp:lists
  • * List of aircraft engines (en)
dbp:majorApplications
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dbp:nationalOrigin
dbp:oilsystem
  • dry sump with Turbomeca gear pump at (en)
dbp:ref
  • Aircraft engines of the World 1953 (en)
dbp:thrust
  • ::Take-off: ::Max Continuous: ::Cruising: (en)
dbp:thrust/weight
  • 2.200000 (xsd:double)
dbp:turbine
  • single-stage with 24 or 25 blades (en)
dbp:turbinetemp
  • ::TIT: ::JPT: (en)
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rdfs:comment
  • Le Turbomeca Palas est un petit turboréacteur à flux centrifuge français, utilisé pour propulser des avions légers. (fr)
  • TheTurbomeca Palas adalah sebuah mesin pesawat turbojet sentrifugal kecil digunakan untuk daya lampu. Ini dirancang pada tahun 1950 oleh pabrik Prancis Société Turbomeca, dan juga diproduksi dengan lisensi oleh Blackburn and General Aircraft di Britania Raya dan Teledyne Continental Motors di Amerika Serikat. (in)
  • The Turbomeca Palas is a diminutive centrifugal flow turbojet engine used to power light aircraft. An enlargement of the Turbomeca Piméné, the Palas was designed in 1950 by the French manufacturer Société Turbomeca, and was also produced under licence by Blackburn and General Aircraft in the United Kingdom and Teledyne Continental Motors in the United States as the Continental Model 320. (en)
  • パラス(Palas )は小型機に使用された小型の遠心圧縮式ターボジェットエンジンである。1950年にフランスのチュルボメカで設計され、英国のブラックバーン・エアクラフトと米国のコンチネンタル・モータースでライセンス生産された。 (ja)
  • Il Turbomeca Palas era un motore turbogetto a compressore centrifugo utilizzato su velivoli leggeri. Venne progettato nel 1950 dal produttore francese Société Turbomeca e successivamente prodotto sotto licenza dalla Blackburn and General Aircraft in Gran Bretagna e dalla negli Stati Uniti. (it)
rdfs:label
  • Turbomeca Palas (fr)
  • Turbomeca Palas (in)
  • Turbomeca Palas (it)
  • チュルボメカ パラス (ja)
  • Turbomeca Palas (en)
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