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General Electric H80

Aircraft Engines

The General Electric H80 is the initial engine of the H-Series, a family of turboprop aircraft engines produced by GE Aviation Czech. The H80 is an updated derivative of the Walter M601 that was launched in 2009, and the H75 and H85 are later derivatives. GE added a new compressor, blisks, blades and new stators to raise power by 3 percent and efficiency by 10 percent, so the engine reaches 597 kilowatts of shaft power against 580 kilowatts for the M601-F, with better hot and high performance. It has a two-shaft reverse flow layout with a two-stage axial and single-stage centrifugal compressor, an annular combustor and a two-stage planetary gearbox. EASA certificated it on 13 December 2011 and the FAA followed on 13 March 2012.

Facts
Year
2009 1
Power (kW)
597 1
Classification
Fuel or Cycle
Jet Fuel / Turbine 1
Connections

Of Make

Source General Electric H80 (Wikipedia)
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Source General Electric H80 (Wikipedia)Lead, maker
Quote, Lead, maker
is a family of turboprop aircraft engines produced by GE Aviation Czech
Sources
1. General Electric H80 (Wikipedia)
  • Lead, engine kind, cycle
    is a family of turboprop aircraft engines produced by GE Aviation Czech
  • Development, launch
    The H80 was launched in 2009 based on the M601
  • Development, H80 power
    It reaches 597 kW (801 hp) (shaft horsepower)
  • Lead, maker
    is a family of turboprop aircraft engines produced by GE Aviation Czech
  • Part Of: Dornier Do 28, Applications
    Dornier Do-28 G92 (H75-200)
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