The invention relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle and an unmanned aerial vehicle cruise system. The unmanned aerial vehicle comprises a fuselage, wing structures and a power device, the wing structure comprises a main wing and an empennage; the main wings are fixed to the fuselage, and the empennages are connected to the main wings through supporting rods. The power device comprises a vertical power assembly used for providing vertical take-off and landing power and a tail pushing power assembly used for providing level flight forward pushing power. The vertical power assembly is arranged on the supporting rod, and the tail pushing power assembly is arranged on the machine body. Through different operations on the vertical power assembly and the tail thrust power assembly, the unmanned aerial vehicle can simply and quickly realize vertical take-off and landing and flat flight modes, safety and high speed can be ensured, and the unmanned aerial vehicle is compact in structure and high in adaptability to different environments.

    本发明涉及无人机技术领域,且公开了一种无人机及无人机巡航系统。其中包括:机身、机翼结构以及动力装置;机翼结构包括主翼和尾翼;主翼固定于机身,尾翼通过撑杆连接于主翼;动力装置包括用于提供垂直起降动力的垂直动力组件以及用于提供平飞前推动力的尾推动力组件;垂直动力组件设置于撑杆上,尾推动力组件设置于机身。通过对垂直动力组件和尾推动力组件的不同操作,使无人机简单快速地实现垂直起降和平飞模式,可以保证安全高速,该无人机的结构紧凑,对不同环境的适应性强。


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    Title :

    Unmanned aerial vehicle and unmanned aerial vehicle cruise system


    Additional title:

    一种无人机及无人机巡航系统


    Contributors:
    YU WENGUANG (author) / YANG SHUNCHAO (author) / ZHANG BINGLEI (author)

    Publication date :

    2022-11-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




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