The invention relates to a linkage mechanism and an unmanned aerial vehicle, the unmanned aerial vehicle comprises a fuselage assembly, a wing assembly and the linkage mechanism, the linkage mechanism comprises a wing locking assembly and an unlocking assembly, the wing assembly comprises a main wing, the main wing is rotatably arranged on the fuselage assembly, and the wing locking assembly comprises a wing locking piece. The wing locking piece is telescopically arranged in the main wing, the current-conducting plate is installed in the fuselage assembly, the unlocking assembly comprises the current-conducting plate, the current-conducting plate is installed in the fuselage assembly, and the wing locking piece can penetrate through the fuselage assembly through extension of the wing locking piece so as to lock the unfolded main wing and enable the wing locking piece to be connected with the current-conducting plate. Therefore, an activation circuit of the initiating explosive device is conducted. By means of the arrangement, the wing locking assembly is fully utilized, linkage of the wing locking assembly and the wing locking assembly is achieved, a triggering mechanism does not need to be additionally arranged to achieve conduction of an activation circuit of the initiating explosive device, the structure of the unmanned aerial vehicle is simplified, the manufacturing cost is reduced, and installation and maintenance of the unmanned aerial vehicle are facilitated.

    本发明涉及一种联动机构及无人机,无人机包括机身组件、机翼组件和联动机构,联动机构包括机翼锁定组件和解保组件,机翼组件包括主机翼,主机翼可转动地设置于机身组件上,机翼锁定组件包括机翼锁定件,机翼锁定件可伸缩地设置于主机翼内,导电板安装于机身组件内,解保组件包括导电板,导电板安装于机身组件内,通过机翼锁定件的伸长,能够使机翼锁定件穿过机身组件,以锁定展开的主机翼,并使机翼锁定件与导电板连接,以导通火工品的激活电路。这样的设置,充分利用了机翼锁定组件,实现了解保组件和机翼锁定组件的联动,不必额外设置触发机构来实现火工品的激活电路的导通,精简了无人机的结构,降低了制造成本,便于无人机的安装和维修。


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    Titel :

    Linkage mechanism and unmanned aerial vehicle


    Weitere Titelangaben:

    一种联动机构及无人机


    Beteiligte:
    CUI WEI (Autor:in) / LIU HAITAO (Autor:in) / JIN LIANG (Autor:in) / CHU XIANYING (Autor:in) / WANG QIANWEN (Autor:in) / LIU YANQI (Autor:in) / SHE ZHIYONG (Autor:in) / LI YANCHEN (Autor:in)

    Erscheinungsdatum :

    2023-12-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / F42C AMMUNITION FUZES , Munitionszünder



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