Helicopter collapsible and method of driving a rotor balancing torque of a helicopter UAV

摘要

Helicopter collapsible and method of driving a rotor balancing torque of a helicopter UAV.The present invention relates to a helicopter unmanned aerial vehicle (UAV) comprising a section of tail (3) including a rotor detachable compensation of torque (5), in which the power transmission of the engine (4) to the rotor torque compensation is carried out by (5) The provisions of the transmission pulley and belt (7, 8).