AI-136T /D-136T-2/AI-136T-2 turboshaft engine family


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.

Engine AI-136Т D-136Т-2/АІ-136Т-2
2.5 minutes power with one engine running out of power
Power, hp. 40
Maximum 30-minute power H=0, Vn=0, ICA
Power, hp. 11 400
Up to temperature supported, 0С. 30 40
Takeoff power H=0, Vn=0, ICA
Power, hp. 10 000
Up to temperature supported, 0С. 22 40
Specific fuel consumption, kg/hp/h 0,210
Weight, dry, kg 1150
Dimensions, mm 3703 x 1124 x 1146
Assigned resource, h 6 000 12 000

Applicability

  • Mi-26

    Mi-26

  • Mi-26Т

    Mi-26Т