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Early French turboshaft engine From Wikipedia, the free encyclopedia
The Turbomeca Artouste is an early French turboshaft engine, first run in 1947. Originally conceived as an auxiliary power unit (APU), it was soon adapted to aircraft propulsion, and found a niche as a powerplant for turboshaft-driven helicopters in the 1950s. Artoustes were licence-built by Bristol Siddeley (formerly Blackburn) in the UK, Hindustan Aeronautics Limited in India, and developed by Continental CAE in the US as the Continental T51. Two major versions of the Artouste were produced. The Artouste II family, mainly used in the Aérospatiale Alouette II helicopter, had a one-stage centrifugal compressor and a two-stage turbine, with gearbox-limited power of 300 kW (400 hp). The Artouste III family, mainly used in Aérospatiale's Alouette III and Lama helicopters, had a two-stage axial-centrifugal compressor and a three-stage turbine, with gearbox-limited power of 420–440 kW (560–590 hp).
| Artouste | |
|---|---|
| |
| Turbomeca Artouste IIIB | |
| Type | Turboshaft |
| National origin | France |
| Manufacturer | Turbomeca |
| First run | 1947 |
| Major applications | Aérospatiale Alouette II Aérospatiale Alouette III |
| Developed into | Continental T51 |
A Turbomeca Artouste is on public display at:
Data from Aircraft engines of the World 1970[7]
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