The invention relates to the technical field of unmanned aerial vehicles, in particular to a load type unmanned aerial vehicle structure which comprises a first shell, a second shell is mounted on one side of the first shell, the shape and size of the first shell are consistent with those of the second shell, and a load part is arranged on the side, away from the first shell, of the second shell. A cavity is formed between the first machine shell and the second machine shell, a connecting carbon pipe is arranged on the peripheral side of the first machine shell, a rotor wing pipe is arranged on the outer side of the connecting carbon pipe, an outer connecting piece used for connecting the connecting carbon pipe and the rotor wing pipe is arranged on the outer side of the rotor wing pipe, and a rotor wing assembly is arranged on the rotor wing pipe.

    本申请涉及无人机技术领域,尤其是涉及一种载重式无人机结构,包括第一机壳,所述第一机壳的一侧安装有第二机壳,所述第一机壳的形状大小与第二机壳的形状大小相一致,所述第二机壳背离第一机壳的一侧设有载重件,所述第一机壳与第二机壳之间形成空腔,所述第一机壳的周侧设置有连接碳管,所述连接碳管的外侧设置有旋翼管,所述旋翼管的外侧设有用于连接连接碳管与旋翼管的外连接件,所述旋翼管上设有旋翼组件。


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    Titel :

    Load type unmanned aerial vehicle structure


    Weitere Titelangaben:

    一种载重式无人机结构


    Beteiligte:
    GAO YUE (Autor:in) / LIU HUIYING (Autor:in) / PENG HUI (Autor:in) / HAN BO (Autor:in) / BIAN HAO (Autor:in)

    Erscheinungsdatum :

    2023-12-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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