The invention relates to the technical field of aircrafts, in particular to an anti-torsion miniature unmanned aerial vehicle which comprises an upper shell, a bearing plate and a lower shell, a first connecting piece is arranged in the upper shell and used for being connected with the bearing plate, and a second connecting piece is arranged on the lower shell and used for being connected with the bearing plate. A plurality of front rotor wings are installed on the side wall of the upper machine shell in a folding mode, a plurality of rear rotor wings are installed on the side wall of the lower machine shell in a folding mode, and a plurality of folding undercarriages are installed at the bottom of the lower machine shell. The unmanned aerial vehicle has the effect of optimizing the structure of the unmanned aerial vehicle.

    本申请涉及飞行器的技术领域,尤其是涉及一种抗扭式微型无人机,其包括上机壳、承重板、下机壳,所述上机壳内设置有第一连接件,所述第一连接件用于与承重板连接,所述下机壳设置有第二连接件,所述第二连接件用于与承重板连接,所述上机壳的侧壁折叠安装有多个前旋翼,所述下机壳的侧壁折叠安装有多个后旋翼,所述下机壳的底部安装有多个折叠起落架。本申请具有对无人机的结构进行优化的效果。


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    Titel :

    Torsion-resistant miniature unmanned aerial vehicle


    Weitere Titelangaben:

    一种抗扭式微型无人机


    Beteiligte:
    SONG WENHAO (Autor:in) / LIU HUIYING (Autor:in) / HAO CHUNYAN (Autor:in) / GAO YUE (Autor:in)

    Erscheinungsdatum :

    2023-12-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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