Turbomeca Turmo

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

Applications

• Aérospatiale Puma
• Aérospatiale Super Frelon
• Aérospatiale Super Puma
• IAR 330
• Bölkow Bo 46
• Breguet 940
• Breguet 941
• Breguet 941S

Specifications (Turmo)

General characteristics

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

Components

• Compressor:

Performance

• Maximum power output: 1,200 kW (1,610 shp)
• Power-to-weight ratio:

References

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

External links

• Turbomeca website