The design of the gearbox of a single-engine aircraft has been developed ( Transport )
The design of the gearbox of a single-engine aircraft has been developed.
Specifications: -Gear ratio U=17.5;
-The power of the gas turbine engine N = 500kW;
-Center distance Aw=225mm;
-The direction of rotation of the input and output shafts is multidirectional.
Rated torque: Hm. Gear ratio number:
Specifications: -Gear ratio U=17.5;
-The power of the gas turbine engine N = 500kW;
-Center distance Aw=225mm;
-The direction of rotation of the input and output shafts is multidirectional.
Characteristics:
Fotos
