About: Turbomeca Orédon (1947)

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The Turbomeca Orédon was a small French turbo-shaft / Auxiliary Power Unit (APU) engine produced by Turbomeca in the late 1940s. Developed as a turbo-shaft / APU derivative of the TR 011 turbojet, the Orédon drove an alternator and was used as an aircraft auxiliary power unit. “Orédon” was reused for a later helicopter turboshaft design. The Turbomeca Piméné, a larger turbojet version of the TR 011 / TT 782 / Orédon, was developed with greater mass-flow and single-stage turbine.

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dbo:abstract
  • The Turbomeca Orédon was a small French turbo-shaft / Auxiliary Power Unit (APU) engine produced by Turbomeca in the late 1940s. Developed as a turbo-shaft / APU derivative of the TR 011 turbojet, the Orédon drove an alternator and was used as an aircraft auxiliary power unit. “Orédon” was reused for a later helicopter turboshaft design. The Turbomeca Piméné, a larger turbojet version of the TR 011 / TT 782 / Orédon, was developed with greater mass-flow and single-stage turbine. (en)
dbo:wikiPageExternalLink
dbo:wikiPageID
  • 36162593 (xsd:integer)
dbo:wikiPageLength
  • 4230 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1101618902 (xsd:integer)
dbo:wikiPageWikiLink
dbp:aircon
  • at 35,000 rpm at sea level (en)
dbp:combustion
  • single annular combustion chamber with rotary disc fuel injector (en)
dbp:compression
  • 3.440000 (xsd:double)
dbp:compressor
  • 1 (xsd:integer)
dbp:developedInto
dbp:firstRun
  • 1947 (xsd:integer)
dbp:fueltype
dbp:length
  • without alternator (en)
dbp:manufacturer
dbp:nationalOrigin
dbp:oilsystem
  • dry sump with Turbomeca gear pump at (en)
dbp:power
  • maximum, at 36,000 rpm / sea level ::::normal at 35,000 rpm / sea level (en)
dbp:ref
  • Aircraft engines of the World 1953 (en)
dbp:thrust
  • ::Max continuous: at 34,000 rpm / sea level ::Cruising: at 33,000 rpm / sea level (en)
dbp:thrust/weight
  • 2 (xsd:integer)
dbp:turbine
  • 2 (xsd:integer)
dbp:turbinetemp
  • ::Before turbine: ::After turbine: (en)
dbp:type
dbp:weight
  • with gearbox, with alternator (en)
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dcterms:subject
rdfs:comment
  • The Turbomeca Orédon was a small French turbo-shaft / Auxiliary Power Unit (APU) engine produced by Turbomeca in the late 1940s. Developed as a turbo-shaft / APU derivative of the TR 011 turbojet, the Orédon drove an alternator and was used as an aircraft auxiliary power unit. “Orédon” was reused for a later helicopter turboshaft design. The Turbomeca Piméné, a larger turbojet version of the TR 011 / TT 782 / Orédon, was developed with greater mass-flow and single-stage turbine. (en)
rdfs:label
  • Turbomeca Orédon (1947) (en)
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