The invention relates to an unmanned aerial vehicle airborne launching device capable of achieving continuous launching. The unmanned aerial vehicle airborne launching device comprises a turntable which is located in an XOY plane and is provided with a notch; the direction perpendicular to the XOY plane is the Z direction; a plurality of L-shaped throwing hooks are arranged at the periphery of theturntable, and each throwing hook is rotationally fixed on a shaft vertical to the Z direction; the width of throwing hooks is not greater than that of the notch; when the throwing hooks bear loads,the lower parts of the throwing hooks face the center of the turntable, and the upper parts of the throwing hooks press the side surfaces of the turntable; and when the turntable rotates until the notch is aligned with the corresponding throwing hook, the throwing hook is overturned under the driving of the gravity of the weight, and the upper part of the throwing hook can penetrate through the notch. According to the unmanned aerial vehicle airborne launching device, multiple times of throwing can be implemented by using a single executing mechanism and single flight, and compared with a multiple-time throwing scheme implemented by a plurality of executing mechanisms, the weight is effectively reduced, and the endurance time of an unmanned aerial vehicle is prolonged; and a single remotecontrol channel is adopted, a common steering engine is adopted, special control circuit design is not needed, and the unmanned aerial vehicle airborne launching device is conveniently and additionally arranged on the universal unmanned aerial vehicle.

    本发明涉及一种可连续投放的无人机机载投放装置,包括一转盘,转盘位于XOY平面内,其上设有一缺口;垂直于XOY平面的方向为Z向;转盘的四周设有多个L形的投放钩,各个投放钩转动固定在垂直于Z向的轴上;投放钩的宽度不大于缺口的宽度;投放钩承重时,投放钩的下部朝转盘中心的方向,上部压在转盘的侧面上;当转盘转动至缺口对准对应的投放钩时,在重物重力的带动下,投放钩翻转,其上部可穿过缺口。本发明使用单一执行机构,单次飞行,即可实施多次投放,与多个执行机构实现的多次投放方案相比,有效降低了重量,提高了无人机续航时间;单个遥控通道,采用普通舵机,无需专用控制电路设计,便于在通用的无人机上加装。


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    Titel :

    Unmanned aerial vehicle airborne launching device capable of achieving continuous launching and operation method


    Weitere Titelangaben:

    一种可连续投放的无人机机载投放装置及操作方法


    Beteiligte:
    SUN CHUNHUI (Autor:in) / LI RUIKUN (Autor:in) / XU WEIXING (Autor:in) / ZHANG MINGHUA (Autor:in) / LIANG MINGMING (Autor:in) / LIU XI (Autor:in)

    Erscheinungsdatum :

    2020-12-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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