TALK OF VERTICAL TAKEOFF AND LANDING AIRCRAFT-TYPE PROPELLER REMOVAL AND BALANCING DEVICE COMBINATION

摘要

The present invention relates to a torque removal and balancing device of a propeller type vertical taking-off and landing aircraft. In other words, a body support frame (110) to support a body (100) is provided, and at least one main rotor blade (120) to generate necessary lift for taking-off and landing is provided in both sides or central part of the body support frame (110). A propeller type vertical taking-off and landing aircraft (A) includes a main rotor rotating motor (150) installed in a lower part of a rotation driving shaft (140) extended from a rotor (130) of the center of the main rotor blade (120) to the bottom. In a lower part of the body support frame (110), a torque removal and balancing reaction wheel (200), operated in the opposite way to the rotation of the main rotor blade (120) according to the operation of a torque removal reaction motor (210) provided separately from the main rotor rotating motor (150) while effectively offsetting torque by rotation moment while helping balance the body with a gyro effect, is installed. The torque removal and balancing reaction wheel (200) is not exposed to the outside and closed.