The invention provides a heavy-load unmanned aerial vehicle hoisting mounting damping mechanism which solves the problem of unmanned aerial vehicle hoisting motion stability and the like and comprises a fixed mounting plate, an unmanned aerial vehicle connecting frame is connected to the upper end of the fixed mounting plate, and a stepping assembly is movably connected to the lower end of the fixed mounting plate. The lower end of the stepping assembly is in transmission connection with the claw assembly through the linkage assembly, and the damping assembly is installed between the fixed installation plate and the linkage assembly. The device has the advantages of good structural stability, high safety and the like.

    本发明提供了一种大载重无人机吊装挂载阻尼机构,它解决了无人机吊装运动稳定性等问题,其包括固定安装板,固定安装板上端连接有无人机连接架,固定安装板下端活动连接有步进组件,步进组件下端通过联动组件与钩爪组件传动连接,固定安装板与联动组件之间安装有阻尼组件。本发明具有结构稳定性好、安全性高等优点。


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    Titel :

    Hoisting and mounting damping mechanism for heavy-load unmanned aerial vehicle


    Weitere Titelangaben:

    一种大载重无人机吊装挂载阻尼机构


    Beteiligte:
    NI HONGYU (Autor:in) / YAN WENXU (Autor:in) / XU LEIMIN (Autor:in) / ZHAO FENG (Autor:in) / LI SHANGYU (Autor:in) / WANG LITING (Autor:in) / YANG NING (Autor:in) / ZHANG LIZONG (Autor:in) / ZHANG YONGJIAN (Autor:in) / LI HUA (Autor:in)

    Erscheinungsdatum :

    18.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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