The invention provides a multi-rotor combined type unmanned aerial vehicle. The multi-rotor combined type unmanned aerial vehicle comprises a fuselage; the multiple rotor wing assemblies are connected with the fuselage, are arranged in the circumferential direction of the fuselage in a surrounding mode and can provide lift force in the vertical stage and provide thrust in the level flight stage; the wing assemblies are fixed to the two longitudinal sides of the fuselage respectively and can provide lift force in the level flight stage; wherein the rotor assemblies are fixedly arranged relative to the inclination angle of the fuselage. According to the arrangement, through the mode that the rotor wing assemblies and the wing assemblies are matched, the cruising speed is increased, energy consumption is reduced, the flight range is increased, the inclination angle of the rotor wing assemblies relative to the fuselage does not need to be controlled, the control logic is simple, the structure is stable and reliable, the manufacturing cost is saved, and the failure rate is reduced.

    本申请提供了一种多旋翼复合式无人机,包括:机身;多个旋翼组件,与所述机身连接并沿所述机身的周向环绕设置,并能够在垂起阶段提供升力、在平飞阶段提供推力;多个机翼组件,分别固定在所述机身的纵向两侧,并能够在平飞阶段提供升力;其中,所述旋翼组件相对于所述机身的倾角固定设置。如此设置,通过旋翼组件和机翼组件相配合的形式,有利于提升巡航速度,减少能耗并提升飞行航程,而且不需要对旋翼组件相对于及机身的倾角进行控制,控制逻辑简单,结构稳定可靠,有利于节省制造成本并降低故障率。


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    Title :

    Multi-rotor combined type unmanned aerial vehicle


    Additional title:

    一种多旋翼复合式无人机


    Contributors:
    DU HAO (author) / TANG RUOCHEN (author) / LIU HENG (author) / YUAN DEJIE (author)

    Publication date :

    2025-05-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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