Turbomeca Artouste
The Turbomeca Artouste is a shaft gas turbine from the French manufacturer Turbomeca . The main customer was the Aérospatiale company , which installed the engines in helicopters . A reduction gear with a reduction ratio of around 6: 1 is flanged directly to the engine.
variants
Artouste II B1 / C / C5 / C6
These engine variants were built into the Aérospatiale Alouette II ; the first series-built helicopter powered by a shaft power turbine. The Artouste II was certified on May 2, 1957 and 1445 were built by 1964. It was also produced under license in the UK by Bristol Siddeley and in India by HAL .
Artouste III B
Version III B drives the helicopters Aérospatiale SA-315 "Lama" and Aérospatiale SA-319 "Alouette III". It was certified on December 15, 1961. This engine is still installed today.
Technical specifications
Parameter | Data Artouste II C6 | Data Artouste III B |
---|---|---|
Years of construction | 1955-1964 | 1969 – today |
Direction of rotation | Clockwise | in the direction of flight counterclockwise |
Max. rotational speed | 34,000 rpm | 33,500 rpm |
Fuel consumption | 150 kg / h | 195 kg / h |
Shaft power | 250 kW | 640 kW (unrestricted), 440 kW (throttled) |
Web links
- Type certificate of the Turbomeca Artouste II series - EASA-TCDS-E.137 (PDF; 255 kB)
- Type certificate of the Turbomeca Artouste III series - EASA-TCDS-E.091 (PDF; 174 kB)
- http://caea.free.fr/fr/coll/artouste.php?origine=coll
- http://www.tfd.uni-hannover.de/121.html
- http://www.tuag.ch
Individual evidence
- ^ A b Sylvain Tarrano: Turbomoteur ARTOUSTE IIC n ° 2121. Ailes Anciennes de Haute-Savoie, March 16, 2008, accessed December 27, 2010 (French).