The invention discloses a parachute opening mechanism and an unmanned aerial vehicle, and belongs to the technical field of parachute bay parachute opening, the parachute opening mechanism comprises a locking assembly and an unlocking assembly, the locking assembly comprises a base mechanism and a parachute bay lock hook mechanism, the base mechanism is rotatably connected with the parachute bay lock hook mechanism, the unlocking assembly is matched with the parachute bay lock hook mechanism, the parachute bay lock hook mechanism comprises a lock hook body, and the lock hook body is rotatably connected with the base mechanism. The lock hook body is provided with a movable groove hole, the unlocking assembly comprises an end face cam, the end face cam is provided with a rotating bearing, the rotating bearing is matched with the movable groove hole, and the rotating bearing is arranged in the movable groove hole.

    开伞机构及无人机,属于伞舱开伞技术领域,包括锁定组件和解锁组件,所述锁定组件包括底座机构与伞舱锁钩机构,所述底座机构与所述伞舱锁钩机构转动连接,所述解锁组件与所述伞舱锁钩机构配合,所述伞舱锁钩机构包括锁钩主体,所述锁钩主体上设置有活动槽孔,所述解锁组件包括端面凸轮,所述端面凸轮上设有旋转轴承,所述旋转轴承与所述活动槽孔配合,所述旋转轴承设置在所述活动槽孔中。


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    Titel :

    Parachute opening mechanism and unmanned aerial vehicle


    Weitere Titelangaben:

    开伞机构及无人机


    Beteiligte:
    CHEN GUOQI (Autor:in) / HAN BO (Autor:in) / GAO YAJING (Autor:in)

    Erscheinungsdatum :

    05.05.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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