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D-136
IOC: 1983
Total Production: 560
Origin
Russia
Contractor/s
Ivchenko-Progress
Motor Sich
Applications
Mi-26
Derived from:
D-36
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Description:
The Ivchenko-Progress D-136 is a turboshaft engine derived from the D-36 turbine to power the massive Mi-26 and Mi-26T 'Halo' twin-engine heavy transport helicopters. A single D-136 engine develops 11,400-hp of power at the takeoff. In addition to the high power output, the D-136 turboshaft was designed to provide low specific fuel consumption. Engine development began in 1977 and series production at the Motor Sich plant started in 1982. The engine design consists of 10 line replaceable modules excepting the main module which is not replaceable. Five gas generator modules are identical to those in the D-36 engine.
Specifications
Dimensions: Height 1,382 mm, Length 3,715 mm, Width 1,124 mm
Weights: Dry Weight 1,077 kg (2,374 lb)
Power: Max Power at TakeOff 11,400 hp
Other: Service Life (Flight Hours) 3,000
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Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)
Last Updated: Friday, October 10, 2008
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