A wing of a vehicle can include a rigid spar. The wing can include beams configured to inflate with a gas. The beams can be disposed from a leading edge of the wing to a trailing edge of the wing. The wing can include a component coupled with the rigid spar and coupled with the trailing edge of the wing, the component to deflect the trailing edge of the wing relative to the leading edge and curve the plurality of beams.


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    Titel :

    Inflatable wing with deflection


    Beteiligte:
    SEAVER KAEL (Autor:in)

    Erscheinungsdatum :

    08.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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