The Turbomeca Arriel is a highly successful series of French turboshaft engines that first ran in 1974.[1] Weighing 109 kg (240 lb), the Arriel 1 has a power output of 520 kW (700 hp). 10,000 examples had been produced by 2012.
Applications
Specifications (Arriel 1)
Data from FAA Type Certificate Data Sheet.[2]
General characteristics
- Type: Twin-spool free turbine turboshaft
- Length: 44.2 in
- Diameter: 23.5 in
- Dry weight: 245 lb
Components
- Compressor: Single-stage axial plus single-stage centrifugal
- Combustors: Annular combustion chamber
- Turbine: Single-stage power turbine, two-stage gas generator turbine
- Fuel type: Jet A1
Performance
See also
- Related lists
References
- Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 166.
External links
|
---|
| General | |
---|
| Military | |
---|
| Accidents/incidents | |
---|
| Records | |
---|
|