The invention discloses an unmanned aerial vehicle wing structure and a light flying wing layout unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The wing body comprises a wing front beam, a wing rear beam, a plurality of wing truss ribs and a plurality of fuselage truss ribs, the wing front beam and the wing rear beam are connected to a fuselage main beam, and the fuselage truss ribs are arranged on the fuselage main beam at equal intervals in the length direction of the fuselage main beam; the wing truss ribs are vertically connected to the main beam web at equal intervals in the length direction of the main beam web, and the two ends of each wing truss rib extend out of the main beam web; the wing front beam is a D-shaped section beam formed by a wing front edge stress skin and a main beam web, the wing front edge stress skin is connected to one end, close to the wing front edge, of the wing truss rib, the wing rear beam is arranged on one side of the wing rear edge and is parallel to the main beam web, and the wing rear beam is fixedly connected with the wing truss rib. According to the invention, the unmanned aerial vehicle with the super-high aspect ratio can execute a flight task in a complex environment in a long-endurance manner.

    本申请公开了一种无人机机翼结构及轻型飞翼布局无人机,涉及无人机技术领域,包括翼身以及机身主梁;翼身包括机翼前梁、机翼后梁、若干机翼桁架肋以及若干机身桁架肋,机翼前梁和所述机翼后梁均连接于机身主梁,若干机身桁架肋沿所述机身主梁长度方向等间距设置在机身主梁上,若干机翼桁架肋沿所述主梁腹板的长度方向等间距垂直连接于主梁腹板,机翼桁架肋的两端延伸至主梁腹板外;机翼前梁为机翼前缘应力蒙皮和主梁腹板构成的D形截面梁,机翼前缘应力蒙皮承接于机翼桁架肋靠近于机翼前缘的一端,机翼后梁设置于机翼后缘一侧且与主梁腹板平行,机翼后梁与机翼桁架肋固定连接。本申请使得超大展弦比无人机能够于复杂环境下长续航执行飞行任务。


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    Titel :

    Wing structure of unmanned aerial vehicle and light flying wing layout unmanned aerial vehicle


    Weitere Titelangaben:

    无人机机翼结构及轻型飞翼布局无人机


    Beteiligte:
    CHENG JIALIN (Autor:in) / ZHI YAFEI (Autor:in) / WANG JUE (Autor:in) / YANG WEN (Autor:in) / WU PENGCHENG (Autor:in) / HE YAN (Autor:in) / DENG ZHONG (Autor:in) / JI TUO (Autor:in) / OH SONG TAEK (Autor:in)

    Erscheinungsdatum :

    2024-05-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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