The invention discloses an unmanned aerial vehicle mounting structure with a good heat dissipation effect, and relates to the technical field of unmanned aerial vehicles, the unmanned aerial vehicle mounting structure comprises a main frame in an unmanned aerial vehicle main body, two groups of mounting mechanisms are clamped below the main frame, and the two groups of mounting mechanisms are fixedly connected to the upper surface of a heat dissipation mechanism. Through mutual cooperation of the protective shell, the door plate, the clamping arms, the sliding blocks, limiting blocks, a lifting block, inserting rods, spring rods, limiting pieces, second springs and a pressing plate, when the unmanned aerial vehicle lifts off, an object downwards presses the pressing plate and the lifting block, and the lifting block drives the sliding blocks and the clamping arms on the two sides to slide towards the middle through the interaction of the inserting rods and inclined grooves on the two sides; the clamping arms are used for clamping and fixing articles, the articles are prevented from shaking in the transportation process, stable flight of the unmanned aerial vehicle is guaranteed, when the unmanned aerial vehicle falls to the ground, the bottom ends of the lifting blocks make contact with the ground and are lifted upwards, the clamping arms are driven to slide towards the two sides, fixing of the articles in the protection shell can be automatically relieved, the articles can be disassembled conveniently, and the taking efficiency is improved; the automation is higher.

    本发明公开了一种散热效果好的无人机挂载结构,涉及无人机技术领域,包括无人机主体中的主架,所述主架的下方卡接有两组安装机构,两组所述安装机构固定连接于散热机构的上表面。本发明通过防护壳、门板、夹臂、滑块、限位块、升降块、插杆、弹簧杆、限位片、第二弹簧、压板相互配合,无人机升空时,物品向下压迫压板和升降块,升降块利用两侧的插杆与斜槽相作用带动两侧的滑块和夹臂向中间滑动,利用夹臂对物品进行夹持固定,防止其在运输过程中晃动,保障无人机的飞行稳定,无人机落到地面时,升降块底端接触到地面向上抬升,带动夹臂向两侧滑动,可以自动解除对防护壳内部物品的固定,方便了物品的拆卸,提升拿取的效率,更自动化。


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    Titel :

    Unmanned aerial vehicle mounting structure with good heat dissipation effect


    Weitere Titelangaben:

    一种散热效果好的无人机挂载结构


    Beteiligte:
    ZENG HONGWEI (Autor:in) / PI JIANZHONG (Autor:in) / LI ZHENGYU (Autor:in) / LIANG XUEFEI (Autor:in)

    Erscheinungsdatum :

    2024-02-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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