The invention relates to the technical field of unmanned aerial vehicles, in particular to an airborne launching pad and an unmanned aerial vehicle, and the airborne launching pad comprises a mounting seat, a connecting arm assembly and a launching assembly which are connected in sequence; the connecting arm assembly comprises a first rotation driving part used for driving the transmitting assembly to rotate relative to the mounting base, the axis of an output shaft of the first rotation driving part is a first axis, the transmitting assembly comprises a main transmitting tube, the axis of the main transmitting tube is a transmitting axis, and the first axis intersects with the transmitting axis. The invention aims to provide the airborne launching pad and an unmanned aerial vehicle to solve the problem that an existing unmanned aerial vehicle weapon system is large in recoil force during ammunition launching, large-amplitude vibration can be generated relative to a motor, and then the striking accuracy is affected.

    本申请涉及无人机技术领域,具体而言,涉及一种机载发射台及无人机,包括依次连接的安装座、连接臂组件和发射组件;所述连接臂组件包括用于带动所述发射组件相对所述安装座转动的第一转动驱动件,所述第一转动驱动件的输出轴的轴线为第一轴线,所述发射组件包括主发射管,所述主发射管的轴线为发射轴线,所述第一轴线与所述发射轴线相交。本申请的目的在于针对现有无人机武器系统在发射弹药时后坐力较大,会相对电动机产生较大幅度震动,进而影响打击的准确性的问题,提供一种机载发射台及无人机。


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    Titel :

    Airborne launching pad and unmanned aerial vehicle


    Weitere Titelangaben:

    机载发射台及无人机


    Beteiligte:
    LIU GENGPENG (Autor:in)

    Erscheinungsdatum :

    2022-02-25


    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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