The invention discloses an unmanned aerial vehicle with an anti-collision structure. The unmanned aerial vehicle comprises a fuselage, a landing gear, a rotor wing, a first anti-collision device and a second anti-collision device, and the fuselage is an unmanned aerial vehicle main body and bears an unmanned aerial vehicle basic assembly; the four landing gears are distributed in a square shape and fixed to the four corners of the fuselage. The four rotor wings are distributed in a square shape and are rotationally fixed to the top of the landing gear. The four first anti-collision devices are distributed in a square mode, and the middle of each first anti-collision device is fixed to the top of the lifting device. The number of the second anti-collision devices is four, and the second anti-collision devices are distributed between the adjacent first anti-collision devices and fixed to the machine body. Compared with the prior art, the anti-collision device adopts the structural design of relieving and counteracting and a multi-rotating structure, so that the unmanned aerial vehicle deals with collision more flexibly and variably, and the loss of the unmanned aerial vehicle main body is reduced.

    本发明公开了一种带有防撞结构的无人机,包括:机身、起落装置、旋翼、第一防撞装置、第二防撞装置,所述机身为无人机主体,承载无人机基础组件;所述起落装置方形分布设置有四个,固定在机身四角;所述旋翼方形分布设置有四个,分别可转动固定在起落装置顶部;所述第一防撞装置方形分布设置有四个,且每个第一防撞装置的中部分别固定在起落装置的顶部;所述第二防撞装置设置有四个,分别分布在相邻的第一防撞装置之间,且固定在机身上。与现有技术相比,本发明中防撞装置采用缓解抵消的结构设计,多处转动结构,使无人机应对撞击更加灵活多变,降低无人机主体损耗。


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    Titel :

    Unmanned aerial vehicle with anti-collision structure


    Weitere Titelangaben:

    一种带有防撞结构的无人机


    Beteiligte:
    ZHANG XIAOJUN (Autor:in)

    Erscheinungsdatum :

    2022-03-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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