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, wherein 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.

    本发明涉及具有锥形机翼肋接口的机身部段。公开了具有锥形机翼肋接口的机身部段。公开的示例性设备包括与机身部段相关联的肋,以及由该肋限定的机翼接口表面,其中机翼接口表面相对于机身部段的纵向轴线从机身部段的尾端到机身部段的前端成锥形。


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    Titel :

    FUSELAGE SECTIONS HAVING TAPERED WING RIB INTERFACES


    Weitere Titelangaben:

    具有锥形机翼肋接口的机身部段


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

    Erscheinungsdatum :

    2021-04-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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