A draft design of the aircraft's turbine engine has been developed ( Transport )

A draft design of the aircraft's turbine engine has been developed. The input and output shafts rotate in the same direction.

Technical specifications:
-Gear ratio U=26
-Capacity of the air turbine N=350 hp
-The speed of rotation of the input shaft n = 40000 rpm.

Characteristics:

Weight: 0 kg.

Rated torque: Hm.

Gear ratio number: