The invention relates to a power driven
system of the aircraft, which is characterized in that the power driven
system comprises a power supply, a motor and a bearing support. The motor is vertically arranged in the bearing support by a bearing. Both the
stator and the rotor of the motor are extending upwards and are respectively provided with propellers. The upper ends of the
stator and the rotor where the propellers are arranged are coaxially sleeved, and the lower end of the rotor is fixed with a rotary disc after stretching out of the bearing support, an
electromagnet with the magnetic pole part near the rotary disc is fixed-arranged outside the bearing support. When the motor is electrified, both the rotor and the
stator drive the propellers to rotate to acquire power at the same time, and the power is transmitted to the frame by the bearing support to drive the aircraft to rise or advance. Meanwhile the electromagnetic moment between the
electromagnet and the rotary disc is used to counteract the
friction torque, and control the size of the electromagnetic moment to achieve the turning of the aircraft. The power driven
system has the advantages of solving the problem of anti-torque of the
propeller, satisfying the design requirements of miniature, simplification and
lightness of the aircraft, and being beneficial to the popularization and manufacturing of the aircraft.