The invention discloses a novel cooperative control unmanned aerial vehicle docking mechanism which comprises a first docking assembly and a second docking assembly. A guide module, a rotating module and a linear driving module are arranged in a first butt-joint assembly, a guide seat, a locking rail and a locking tongue are arranged in a second butt-joint assembly, so that the first butt-joint assembly and the second butt-joint assembly can be locked or loosened in a butt-joint mode, and after locking is completed, the rotating module can enable the two butt-joint assemblies to relatively rotate around a locking shaft. The problem of interference caused by the fact that the guiding device cannot move in the docking process of multiple unmanned aerial vehicles is effectively solved.

    本发明公开了一种新型协同控制无人机对接机构,包含第一对接组件和第二对接组件;通过在第一对接组件设置导向模块、旋转模块和直线驱动模块,在第二对接组件中设置导向座、锁止轨道和锁止舌,使得第一对接组件、第二对接组件能够对接锁定或松开,且锁定完成后,旋转模块能够两对接组件绕锁定轴相对转动。本发明有效解决了多无人机对接过程中由于导引装置无法移动造成的干涉问题。


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    Titel :

    Novel cooperative control unmanned aerial vehicle docking mechanism


    Weitere Titelangaben:

    一种新型协同控制无人机对接机构


    Beteiligte:
    LI CHUANPENG (Autor:in) / YUAN XIAOCHEN (Autor:in) / LIU RUNZE (Autor:in) / WANG ZHIQIANG (Autor:in) / HU JUN (Autor:in) / TU BAOFENG (Autor:in) / WANG YINGFENG (Autor:in)

    Erscheinungsdatum :

    2023-08-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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