The invention provides a high-lift wing suitable for a long-endurance fixed-wing unmanned aerial vehicle and the unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The flap is arranged on the rear edge, close to the wing root, of the main wing, a gap is formed between the flap and the main wing, and at least one of the front edge and the rear edge of the flap is of a wavy structure in the spanwise direction; the problems that in the prior art, a long-endurance fixed-wing unmanned aerial vehicle high lift device is small in maximum lift coefficient and large in take-off distance are solved.

    本发明提供一种适用于长航时固定翼无人机的增升机翼及无人机,涉及无人机技术领域,包括:主翼;襟翼,襟翼设置在主翼靠近翼根部位的后缘,襟翼与主翼之间形成缝道,襟翼的前缘和后缘至少其中之一在展向上为波浪形结构;解决现有技术中长航时固定翼无人机增升装置最大升力系数较小,起飞距离较大的问题。


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    Titel :

    High-lift wing suitable for long-endurance fixed-wing unmanned aerial vehicle and unmanned aerial vehicle


    Weitere Titelangaben:

    一种适用于长航时固定翼无人机的增升机翼及无人机


    Beteiligte:
    ZHANG YANTAI (Autor:in) / FU YIWEI (Autor:in) / ZHAO JIAXIANG (Autor:in)

    Erscheinungsdatum :

    24.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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