A wing assembly for a modular aircraft 2 comprises a central wing structure 12 having inboard wing sections 20a, 20b which extend laterally on opposing sides of the central wing structure and a plurality of pairs of outboard wing sections 14, 16, 18. Each outboard wing section is arranged to be removably mounted to a respective one of the inboard wing sections such that each pair of outboard wing sections is mountable to the central wing structure to provide a respective alternative wing configuration. The plurality of pairs of outboard wing sections comprises: a first pair having a first outboard sweep angle; and a second pair having a second outboard sweep angle, wherein a leading edge of each second outboard wing section is arranged to extend at a second outboard sweep angle and the second outboard sweep angle is greater than the inboard sweep angle.


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    Titel :

    Aircraft wing assembly


    Beteiligte:
    PETER CURTIS (Autor:in)

    Erscheinungsdatum :

    12.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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