The present disclosure discloses a multi-rotor aircraft with multi-shaft dislocation layout. The multi-rotor aircraft includes a frame, a plurality of upper-layer power sources, a plurality of lower-layer power sources, a plurality of upper-layer propeller blades and a plurality of lower-layer propeller blades. The plurality of upper-layer propeller blades are disposed at intervals, and are connected to the upper side of the frame through the plurality of upper-layer power sources. The plurality of lower-layer propeller blades are disposed at intervals, and are connected to the lower side of the frame through the plurality of lower-layer power sources. The plurality of upper-layer propeller blades and the plurality of lower-layer propeller blades are staggered along a projection direction of the frame. The centers of the plurality of upper-layer propeller blades and the centers of the plurality of lower-layer propeller blades are located on the same flat geometric figure along the projection direction of the frame. Under the same loading capacity, the multi-rotor aircraft can obviously reduce the flight resistance and volume, and improve the propeller efficiency. The multi-rotor aircraft can also meet a higher loading requirement in the case of less influence on the volume and weight, and the multi-rotor aircraft has a relatively low requirement for transportation equipment.


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    Title :

    MULTI-ROTOR AIRCRAFT WITH MULTI-SHAFT DISLOCATION LAYOUT


    Additional title:

    MEHRROTORFLUGZEUG MIT MEHRWELLENVERSETZUNGSANORDNUNG
    AÉRONEF À ROTORS MULTIPLES AVEC AGENCEMENT DE DISLOCATION À ARBRES MULTIPLES


    Contributors:
    TIAN YU (author)

    Publication date :

    2024-05-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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