The invention discloses a multi-rotor mother-son unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles, the multi-rotor mother-son unmanned aerial vehicle comprises a mother unmanned aerial vehicle body and a son unmanned aerial vehicle, rotors are fixedly mounted on the side surface of the mother unmanned aerial vehicle body, a fixing plate is fixedly mounted on the bottom surface of the rotors, a fixing frame is arranged on the bottom surface of the fixing plate, and a radar detector is fixedly mounted on the bottom surface of the mother unmanned aerial vehicle body. A first motor is fixedly installed on the top face of the fixing frame, a first gear is installed at the output end of the first motor, and a rack is slidably connected into the fixing frame. According to the unmanned aerial vehicle, through the foldable design of the supporting frame, disturbance of airflow and resistance borne by the mother unmanned aerial vehicle body in the flight process are reduced, the endurance is prolonged, and the mother unmanned aerial vehicle body is prevented from being disturbed by an undercarriage and a large bearing cavity; and meanwhile, the size of the mother unmanned aerial vehicle body is reduced, and the mother unmanned aerial vehicle body is convenient to transport.

    本发明公开了一种多旋翼子母无人机,涉及无人机技术领域,包括:母无人机体和子无人机,所述母无人机体的侧面固定安装旋翼,所述旋翼的底面固定安装固定板,所述固定板的底面设置固定架,所述母无人机体的底面固定安装雷达探测仪,所述固定架的顶面固定安装第一电机,所述第一电机的输出端安装第一齿轮,所述固定架的内部滑动连接齿条;本发明,通过支撑架的可收纳式设计不仅起到了减少母无人机体在飞行过程中受到气流的扰动和受到的阻力,增加续航,避免母无人机体受到起落架和较大承载腔室的干扰,容易产生紊流而导致无人机的飞行姿态难以稳定控制的情况发生,同时也起到了减小母无人机体的体积,方便对其进行运输。


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    Titel :

    Multi-rotor child-mother unmanned aerial vehicle


    Weitere Titelangaben:

    一种多旋翼子母无人机


    Beteiligte:
    WANG TIANYOU (Autor:in) / YANG JING (Autor:in) / ZHENG XIAOXUE (Autor:in) / ZHAO CHUNHUA (Autor:in) / ZHOU HUI (Autor:in) / WANG LI (Autor:in)

    Erscheinungsdatum :

    11.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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