Embodiments of the present disclosure provide a wing element structure for an aircraft, a wing structure and an aircraft. The wing element structure comprises: a plurality of wing element units, wherein adjacent wing element units are connected by airfoil control 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 in the wing element unit is correspondingly connected to a wing support rod 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, wherein the movement of the wing element structure is driven by the movement of the wing support rods, and 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:
    LI WEI (Autor:in) / LUO BING (Autor:in) / CUI WEICHENG (Autor:in)

    Erscheinungsdatum :

    2024-01-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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