Turbomeca Turmo

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Turmo
Turbomeca Turmo IIIB
Type Turboshaft
Manufacturer Turbomeca
Major applications Aérospatiale Puma
Aérospatiale Super Frelon
Developed into Bristol Siddeley Nimbus

The Turbomeca Turmo is a French turboshaft engine developed for helicopter use. A descendant of Turbomeca's pioneering Artouste design, later versions delivered around 1,200 kW (1,610 shp).

Current versions are built in partnership with Rolls-Royce, and the engine is produced under license by the Chinese Changzhou Lan Xiang Machinery Works as the WZ-6 and Romanian Turbomecanica Bucharest as the Turmo IV-CA

Contents

[edit] Applications

[edit] Specifications (Turmo)

General characteristics

  • Type: Turboshaft
  • Length:
  • Diameter:
  • Dry weight:

Components

  • Compressor:

Performance

[edit] References

  • Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. pp. 163. 

[edit] External links

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