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[update], some 2,200 had been built.[2]
Applications
Variants
[4]
- Makila 1A 1240 kW (1662shp)
- Makila 1A1 1357 kW (1820shp)
- Makila 1A2 1376 kW (1845shp)
- Makila 1A4
- Makila 2A 1801 kW (2415shp)
- Makila 2A1
- Makila 2B
Specifications (Makila 2A)
Data from Turbomeca.[5]
[6]
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 (both mounted on HP shaft)
- Combustors: Annular
- Turbine: 2-stage axial flow HP turbine, 2-stage axial flow free power turbine with rearwards output shaft
- Maximum power output: 1,801kW (2,415 shp)
See also
Related lists
References
- Notes
- Bibliography
- Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens.