D-136-2 Turboshaft Engine


For the purpose of improving the Mi-26T2 transport helicopter flight performance under higher environmental temperature and highland conditions designed is being a turboshaft gas turbine engine, designated D-136-2, based on the advanced D-436 turbofan gas generator, with a new full authority automatic control system of FADEC type, which now is passing bench tests.

Takeoff (SLS, ISA)
N, hp. 12,200
C, kg/hp/h 0.210
Dimensions, mm 3,715 x 1,382 x 1,124
Weight, dry, kg 1,150

Applicability

  • Mi-26

    Mi-26

  • Mi-26Т

    Mi-26Т


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