Fuselage sections having tapered wing rib interfaces are disclosed. A disclosed example apparatus includes a rib associated with a fuselage section, and a wing interface surface defined by the rib, where the wing interface surface is tapered relative to a longitudinal axis of the fuselage section from an aft end of the fuselage section to a fore end of the fuselage section.


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    Titel :

    Fuselage sections having tapered wing rib interfaces


    Beteiligte:
    ROSMAN RICHARD R (Autor:in) / COMINSKY KENNETH D (Autor:in) / LAKIC BRANKO (Autor:in)

    Erscheinungsdatum :

    02.08.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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    FUSELAGE SECTIONS HAVING TAPERED WING RIB INTERFACES

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    FUSELAGE SECTIONS HAVING TAPERED WING RIB INTERFACES

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