The invention discloses a multi-rotor manned vehicle, comprising man-carried cabin, lifting rotor, equipment bin and steering rudder; the upper part of the said man-carried cabin is provided with a window, the bottom edge is provided with a landing gear or taxiing wheels, the outer wall is provided with a cabin door, the outer wall of both sides or the top is provided with a side-push rotor separately, and the back end of the said side-push rotor is provided with a first power device to drive the said side-push rotor; the said lifting rotors are provided of a quantity of at least two, which are arranged side-by-side in parallel around or on both sides of the said man-carried cabin, and the lower end of each said lifting rotor is respectively provided with a second power device to drive the said lifting rotor; the said equipment bin is arranged at the bottom of the said man-carried cabin, in which a power source is provided for the operation of the said first power device and the second power device; the said steering rudder is arranged at the rear or top of the said man-carried cabin. The flight, take-off and landing of the invention is similar to the unmanned aerial vehicle, having the advantages of small and flexible, low altitude and low speed, vertical lifting, economic and practical.
Multi-rotor manned aircraft
2022-04-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |