High-pressure rotor driver of aviation turbine engine

The high-pressure rotor driver of the aviation turbine engine comprises a main machine, a man-machine interaction interface, a motor assembly and a remote controller, the motor assembly is mainly composed of a closed-loop stepping motor, a speed reducer and a coiling mechanism, the output end of the closed-loop stepping motor is connected with the input end of the speed reducer, the output end of the speed reducer is connected with a square shaft, and the square shaft is connected with a motor. The winding mechanism comprises a winding roll, a wire sliding ring arranged on the top face of the winding roll and a cable wound on the winding roll, one end of the cable is connected to the wiring end of the closed-loop stepping motor, and the other end of the cable penetrates through the wire sliding ring to be connected with the main machine. According to the utility model, the turbine engine rotor is electrically driven to rotate, so that the uniformity of the rotating speed of the turbine engine rotor is improve