The invention discloses a multi-rotor unmanned aerial vehicle inclined lifting force device, and relates to the technical field of aircrafts, the device comprises a lifting force wing device and an unmanned aerial vehicle fixing device, the lifting force wing device comprises a frame connecting structure and a lifting force wing structure, the frame connecting structure is of a hollow design, and is used for connecting the unmanned aerial vehicle fixing device and the lifting force wing structure; through dynamic optimization of
aerodynamic lift assistance and an intelligent regulation and
control algorithm of a lift wing structure, rotor
energy consumption is reduced, battery film auxiliary power supply is matched, the cruising ability is improved, environment
airflow changes are captured in real time through a
sensing data acquisition
assembly, lift distribution and rotor rotating speed are rapidly adjusted through the
algorithm, and the reliability of the
system is improved. The stability of the
fuselage is enhanced by combining the aerodynamic characteristics of the lift wings, the
flight speed is increased, the wind resistance performance is optimized, rotor wing faults are detected through the fault response sub-module, emergency lift force distribution is triggered, the
fuselage balance is maintained by means of the emergency lift force of the lift wings, and the air
crash risk caused by the rotor wing faults is avoided.