Embodiments of the present disclosure provide a wing element structure for an aircraft, comprising a plurality of wing element units, wherein adjacent wing element units are connected by airfoil control units, hydraulic units and wing element outer edge connecting members, each of the wing element units comprises a plurality of wing element edge members connected to one another and a wing support rod connecting member, and the wing support rod connecting member located in a wing leading edge in the wing element unit is connected to a support rod structure on an aircraft main body. The embodiments of the present disclosure provide a wing element structure having a wide range of morphing airfoil features in terms of chord length and curvature; the embodiments of present disclosure have the capability of morphing airfoil and variable pitch angle in a wide range, and can make adjustment regarding complex flow fields or environments, which greatly improves the movement speed and movement efficiency and can achieve high-mobility actions.


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    Titel :

    Wing Element Structure for Aircraft, Wing Structure, and Aircraft


    Beteiligte:
    LUO BING (Autor:in) / LI WEI (Autor:in) / CUI WEICHENG (Autor:in)

    Erscheinungsdatum :

    21.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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