Lotarev D-136

E1030528

The Lotarev D-136 is a powerful turboshaft engine developed in the Soviet Union, best known for powering the heavy-lift Mil Mi-26 helicopter.

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Label Occurrences
Lotarev D-136 canonical 1

Statements (44)

Predicate Object
instanceOf turboshaft engine
alsoKnownAs Progress D-136 NERFINISHED
applicationType rotorcraft
associatedWith Mil Moscow Helicopter Plant NERFINISHED
category Soviet aircraft engines
helicopter engines
turboshaft engines
compressorType axial-flow compressor
configuration axial-flow turboshaft
coolingMethod air-cooled
coolingSystem air-cooled turbine
countryOfOrigin Soviet Union
designBureau Ivchenko-Progress NERFINISHED
designGoal provide very high power for heavy-lift helicopters
developer Lotarev Design Bureau NERFINISHED
era Cold War
family Lotarev D-136 engine family NERFINISHED
fuelType jet fuel
intendedRole heavy-lift helicopter powerplant
manufacturer Motor Sich NERFINISHED
marketedBy Ivchenko-Progress NERFINISHED
mounting twin-engine installation on Mil Mi-26
notableFeature designed for very heavy-lift operations
high power-to-weight ratio
notableFor powering the world’s heaviest-lift production helicopter
numberOfCompressorStages 12
powerClass high-power turboshaft
powerTransmission to main rotor via gearbox
primaryApplication Mil Mi-26 NERFINISHED
regionOfUse Russia NERFINISHED
export markets
former Soviet republics
serviceEntry late 1970s
shaftPower 8200 kW
approximately 11000 shp
status in service
successor D-136-2 NERFINISHED
turbineType free power turbine
usedBy Russian Air Force NERFINISHED
Soviet Air Force NERFINISHED
various civilian operators
usedOnAircraft Mil Mi-26 NERFINISHED
Mil Mi-26T NERFINISHED
Mil Mi-26T2 NERFINISHED

Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

Mil Mi-26 engineModel Lotarev D-136