The invention discloses a composite wing unmanned aerial vehicle and application thereof, belongs to the technical field of aircrafts, and can take off and land vertically and cruise economically at a high speed. The composite wing unmanned aerial vehicle is in a wing body fusion design and comprises a fixed wing system, a rotor wing system and an empennage which are in wing body fusion, a power device of the fixed wing system is mounted at the head of the wing body fusion wing; the rotor system is provided with eight shafts and eight propellers, and inner and outer rotors are arranged in a staggered manner, so that the outer rotors are closer to the middle, the stress of the wings is optimized, and the inner and outer rotors do not hit propellers to interfere with each other; when the unmanned aerial vehicle is applied to logistics transportation, the wing body fusion position of the unmanned aerial vehicle is detachably connected with the load cabin, the gravity center position of the load cabin coincides with the gravity center position of the flight platform in the vertical direction during connection, flight resistance of the unmanned aerial vehicle is reduced, and flight stability is enhanced.

    本发明公开了一种复合翼无人机及其应用,属于飞行器技术领域,即可以垂直起降,又可以高速经济巡航。本发明复合翼无人机为翼身融合设计,包括翼身融合的固定翼系统、旋翼系统、尾翼;所述固定翼系统的动力装置安装于翼身融合机翼的头部;所述旋翼系统为八轴八桨,内外旋翼交错式布置,使外旋翼更靠近中间,优化机翼受力,且内外旋翼不会打桨干涉;应用于物流运输时,无人机翼身融合处可拆卸连接载荷舱,连接时载荷舱重心位置与飞行平台重心位置在垂直方向重合,减少了无人机的飞行阻力,增强了飞行稳定性。


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    Title :

    Composite wing unmanned aerial vehicle and application thereof


    Additional title:

    一种复合翼无人机及其应用


    Contributors:
    BAI YALEI (author) / YANG BONING (author) / CHEN YILIANG (author) / LI CHAOJIE (author)

    Publication date :

    2024-03-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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