The invention discloses a detachable solar unmanned aerial vehicle structure design, and belongs to the technical field of modular design and solar aviation. The unmanned aerial vehicle comprises wings; the empennage and the wings are spaced by a preset distance; the fixing frame is detachably connected between the wings and the empennage and used for additionally installing the wings and the empennage of different lengths for the unmanned aerial vehicle and carrying all the function modules. Wherein the wing comprises a main wing middle section and a wing outer section which are spliced with each other; the empennage comprises a horizontal empennage and a vertical empennage which are spliced with each other; solar panels are installed on the surfaces of the wings, the empennage and the fixing frame. The wings and the empennage are spliced in a staggered mode through the concave parts and the convex parts, a user can be allowed to additionally install the wings and the empennage with different lengths for the unmanned aerial vehicle according to actual task requirements, rapid adjustment and optimal configuration of the wing structure are achieved, and it is ensured that the unmanned aerial vehicle can adapt to various complex task scenes.

    本发明公开了一种可拆卸太阳能无人机结构设计,属于模块化设计与太阳能航空技术领域;其包括:机翼;尾翼与机翼间隔预定距离;固定架可拆卸连接于机翼和尾翼之间,用于为无人机加装不同长度的机翼和尾翼以及运载各功能模块;其中,机翼包括:相互拼接的主翼中段和机翼外段;尾翼包括:相互拼接的水平尾翼和垂直尾翼;机翼、尾翼和固定架的表面均安装有太阳能板。本发明中机翼和尾翼各自通过凹部和凸部的交错拼接,可以允许使用者根据实际任务需求为无人机加装不同长度的机翼和尾翼,实现机翼结构的快速调整与优化配置,确保无人机能够适应各种复杂任务场景。


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    Title :

    Detachable solar unmanned aerial vehicle structure design


    Additional title:

    一种可拆卸太阳能无人机结构设计


    Contributors:
    SHANG ZHIGANG (author) / GONG ZIXU (author) / ZHOU NING (author) / ZHANG HONGWEI (author)

    Publication date :

    2025-04-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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