The invention provides an unmanned aerial vehicle fuselage, a manufacturing method and an unmanned aerial vehicle with the unmanned aerial vehicle fuselage, the unmanned aerial vehicle fuselage comprises a head cover, a middle fuselage, a tail cabin and an air inlet channel, and the head cover is the head of the unmanned aerial vehicle and is fixedly connected with the front end of the middle fuselage; the middle fuselage comprises a fuselage covering cap, a fuselage skin, a fuselage frame and stringers, the fuselage frame is of a section identical to the cross sections of the middle fuselage in shape and fixed to the corresponding position through the stringers, the fuselage skin is of a full-length structure with an opening in the top, the length of the fuselage skin is equal to that of the middle fuselage, and the fuselage skin is fixed to the fuselage frame and the stringers with the opening facing upwards; the fuselage covering cap closes an opening in the top of the fuselage skin; the tail cabin is the tail of the unmanned aerial vehicle and is fixedly connected with the rear end of the middle fuselage; the air inlet is installed on the upper portion of the middle fuselage. According to the unmanned aerial vehicle fuselage structure, the general assembly and maintenance efficiency of the unmanned aerial vehicle is greatly improved through the openness and the operation space provided by the unmanned aerial vehicle fuselage structure.

    本发明提供一种无人机机身、制造方法及具有其的无人机,包括头罩、中机身、尾舱和进气道,头罩为无人机的头部,其与中机身前端固连;中机身包括机身口盖、机身蒙皮、机身框和桁条,机身框为与中机身各个横截面形状相同的截面,并通过桁条将机身框固定在相应的位置,机身蒙皮为顶部开口通长结构,长度为中机身的长度,机身蒙皮开口朝上固定在机身框和桁条上,机身口盖将机身蒙皮顶部的开口闭合;尾舱为无人机的尾部,其与中机身后端固连;进气道安装于中机身上部。本发明无人机机身结构提供的开敞性和操作空间大幅提升了无人机的总装和维护效率。


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    Titel :

    Unmanned aerial vehicle fuselage, manufacturing method and unmanned aerial vehicle with unmanned aerial vehicle fuselage


    Weitere Titelangaben:

    一种无人机机身、制造方法及具有其的无人机


    Beteiligte:
    LI JIANHUI (Autor:in) / HOU WEIKANG (Autor:in) / SHI XIAOFEI (Autor:in) / CHANG HAO (Autor:in) / TIAN XINFENG (Autor:in) / HE LIJUN (Autor:in) / YAO YUNFENG (Autor:in) / WEI CHANGQUAN (Autor:in)

    Erscheinungsdatum :

    29.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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