- Source: Turbomeca Makila
The Turbomeca Makila is a family of French turboshaft engines for helicopter use, first run in 1976 and flown in 1977.
Typical power output is around 1,300 kW (1,700 hp). As of 2012, some 2,200 had been built.
Applications
Puma HC Mk 2
Aérospatiale Super Puma
Denel Oryx
Denel Rooivalk
Eurocopter AS532 Cougar
Eurocopter EC225 Super Puma
Eurocopter EC725
IAR 330 SM
Turboliner
Variants
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.
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
Performance
Maximum power output: 1,801kW (2,415 shp)
See also
Related lists
List of aircraft engines
References
Notes
Bibliography
Kata Kunci Pencarian:
- Airbus Helicopters H225M
- Eurocopter AS 532
- Eurocopter AS332 Super Puma
- Turbomeca
- Mesin Turboshaft free turbin
- Eurocopter EC225 Super Puma
- Eurocopter EC 725
- NAS-332 dalam TNI Angkatan Udara
- Denel Rooivalk
- Turbomeca Makila
- Eurocopter AS332 Super Puma
- Eurocopter AS532 Cougar
- Aérospatiale SA 330 Puma
- Eurocopter EC725
- Eurocopter EC225 Super Puma
- Rolls-Royce Turbomeca RTM322
- Rolls-Royce Turbomeca
- Safran Helicopter Engines
- Turbomeca Marboré
