The invention relates to a multi-rotor heavy-load unmanned aerial vehicle with equal force effect distribution. The multi-rotor large-load unmanned aerial vehicle comprises undercarriages (1), load bins (2), vehicle arms (3), a flight control system (4), large rotor wings (5), small rotor wings (6), a lithium battery (7), an electronic speed controller (8), a motor (9) and two reduction gear sets(10), and the force effect working points of the large rotor wings (5) and the small rotor wings (6) are the same. The unmanned aerial vehicle can increase the load, increase the endurance and reducethe overall boundary dimension of the unmanned aerial vehicle, and can be applied to the fields of agricultural aviation, forestry aviation, logistics transportation and the like.

    本发明涉及一种等力效分配的多旋翼大载重无人机,包括:起落架(1)、载荷仓(2)、机臂(3)、飞行控制系统(4)、大旋翼(5)、小旋翼(6)、锂电池(7)、电调(8)、电动机(9),2组减速齿轮组(10),大旋翼(5)与小旋翼(6)的力效工作点相同。本发明所无人机能够增加载荷,同时增加航时,减小无人机的整体外形尺寸,可应用于农业航空、林业航空、物流运输等领域。


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    Title :

    Multi-rotor heavy-load unmanned aerial vehicle with equal force effect distribution


    Additional title:

    一种等力效分配的多旋翼大载重无人机


    Contributors:
    LUO BING (author) / WANG MENGLONG (author) / ZHANG XIANMIN (author) / LU LIANGQING (author)

    Publication date :

    2021-01-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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