Turbomeca Makila
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The Turbomeca Makila is a family of French turboshaft engines for helicopter use, first run in 1976 and flown in 1977.[1]
Typical power output is around 1,300 kW (1,700 hp).[2] As of 2012, some 2,200 had been built.[2]
Applications
- Puma HC Mk 2
- Aérospatiale Super Puma
- Denel Rooivalk
- Eurocopter AS532 Cougar
- Eurocopter EC225 Super Puma
- Eurocopter EC725
- IAR 330 SM
Variants
- Makila 1A
- Makila 1A1
- Makila 1A2
- Makila 1A4
- Makila 2A
- Makila 2A1
Specifications (Makila 2A)
Data from Turbomeca.[3]
General characteristics
- Type: Free-turbine turboshaft
- Length: 1,836 mm (72 in)
- Diameter: 498 mm (20 in)
- Dry weight: 278,9 kg (including FADEC)
Components
- Compressor: 3-stage axial flow LP, single-stage centrifugal flow HP
- Combustors: Annular
- Turbine: 2-stage axial flow free turbine
Performance
- Maximum power output: 1,801kW (2,415 shp)
- Power-to-weight ratio:
See also
- Related lists
References
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Wikimedia Commons has media related to Turbomeca Makila. |
- Notes
- ↑ Flight International - Turbomeca Makila www.flightglobal.com Retrieved: 3 January 2012
- ↑ 2.0 2.1 SAFRAN - Turbomeca Makila www.turbomeca.com Retrieved: 3 January 2012
- ↑ Turbomeca Makila - Manufacturer's data sheet. www.turbomeca.com Retrieved: 3 January 2012
- Bibliography
- Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens.
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