The invention belongs to the technical field of unmanned aerial vehicle height control, and particularly relates to a combined height control method for an unmanned aerial vehicle, and the unmanned aerial vehicle comprises an unmanned aerial vehicle body, two wings and a height control mechanism. The height control mechanism comprises an air pump, an air cavity, a fixing plate, a sliding plate and an angle adjusting part; the angle adjusting part comprises a sliding rail, a sliding block, a connecting rod, a toothed plate, a gear and a rotating rod. The two wings are installed on the front side and the rear side of the aircraft body through bearings correspondingly. The air pump is fixedly installed in the machine body and connected with an external pipeline, the air cavity is fixedly installed below the air pump, the lower end of the air cavity is open and located below the machine body, the fixing plate is fixedly installed on the inner wall of the air cavity, a through hole is formed in the middle of the fixing plate, and the sliding plate is slidably connected to the inner wall of the air cavity. The device solves the problem that when a current unmanned aerial vehicle controls the flight height, vertical rising and climbing cannot be synchronously controlled, so that the height control of the unmanned aerial vehicle is unstable.

    本发明属于无人机高度控制技术领域,具体涉及一种无人机用组合高度控制方法,其中包括无人机,所述无人机包括机体、两根机翼以及高度控制机构;所述高度控制机构包括气泵、气腔、固定板、滑板以及角度调节部;所述角度调节部包括滑轨、滑块、连接杆、齿板、齿轮以及转杆,两根所述机翼分别轴承安装于机体的前后两侧;所述气泵固定安装于机体的内部,且与外界管道连接,所述气腔固定安装于气泵的下方,且下端为开口状,且下端位于机体的下方,所述固定板固定安装于气腔的内壁,且中间开设有通孔,所述滑板滑动连接于气腔的内壁,该装置解决了当前无人机在控制飞行高度时,无法同步控制垂直升起和爬升导致无人机高度控制不平稳的问题。


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    Titel :

    Combined height control method for unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机用组合高度控制方法


    Beteiligte:
    WANG FEI (Autor:in) / CHEN LINGFENG (Autor:in) / LIN YANXI (Autor:in) / YANG YI (Autor:in)

    Erscheinungsdatum :

    2024-02-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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