The invention discloses a lightweight unmanned aerial vehicle framework and an unmanned aerial vehicle thereof, relates to the technical field of unmanned aerial vehicles, and solves the problem that the unmanned aerial vehicle framework is poor in structural strength and cruising ability, and the technical scheme is characterized in that the lightweight unmanned aerial vehicle framework comprises a carrying frame used for carrying an aircraft, and four groups of flight force arms connected to the peripheral side of the carrying frame; the carrying frame is rectangular, and the four sets of flight force arms are arranged corresponding to the four sets of side walls of the carrying frame. The flying force arm comprises two groups of side force arms and a load seat for carrying aircraft wings, one ends of the two groups of side force arms are respectively connected to fulcrums at two tail ends of the same side wall of the carrying frame, and the other ends of the two groups of side force arms are connected with the load seat; the distance between the two sets of side force arms is gradually reduced in the direction from the carrying frame to the load seat. After the unmanned aerial vehicle framework is subjected to lightweight design, the cruising ability of an unmanned aerial vehicle can be improved, meanwhile, the unmanned aerial vehicle framework has good structural strength, and the overall flight stability of the unmanned aerial vehicle can be well kept.

    本发明公开了一种轻量化无人机骨架及其无人机,涉及无人机技术领域,解决了无人机骨架结构强度以及续航能力不佳的问题,其技术方案要点是:其包括用于搭载飞行器的搭载架、连接在所述搭载架周侧的四组飞行力臂,所述搭载架为矩形,四组所述飞行力臂对应所述搭载架的四组侧壁设置;所述飞行力臂包括有两组侧力臂以及用于搭载飞行器机翼的荷载座,两组所述侧力臂的一端分别连接在所述搭载架同一侧壁的两末端的支点上,两组所述侧力臂的另一端与所述荷载座相接,两组所述侧力臂之间的间距沿着所述搭载架指向所述荷载座的方向逐渐减小。本发明对无人机骨架进行轻量化设计后能够提高无人机的续航能力的同时具有较好的结构强度,能够较好的保持无人机整体飞行的稳定性。


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    Titel :

    Lightweight unmanned aerial vehicle framework and unmanned aerial vehicle thereof


    Weitere Titelangaben:

    一种轻量化无人机骨架及其无人机


    Beteiligte:
    ZHU FEI (Autor:in) / LIANG HAOJUN (Autor:in) / GUO BILIN (Autor:in) / WANG JIAN (Autor:in) / XIE CHENGYUAN (Autor:in) / GAO XIUJIE (Autor:in) / WEI YEGUO (Autor:in) / XIE RUXUAN (Autor:in) / YU FEILONG (Autor:in) / GAN RONGWEI (Autor:in)

    Erscheinungsdatum :

    2023-03-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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