A rib (44) is disclosed for use in a torque box assembly (120) of a wing structure provided on an aircraft (20). The wing structure has a skin panel (72, 74) and a stringer (82) coupled to the skin panel. The rib includes a web (60) defining at least one stringer hole (90) sized to receive the stringer, a shear tie (70) coupled to the web and configured to engage the skin panel, and a clip (100) positioned adjacent the at least one stringer hole. The clip has a base (102) coupled to and aligned with the web, a head (104) extending at an angle relative to the base and configured to engage the stringer, and a transition portion (106) extending between the base and the head.


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    Titel :

    COMPOSITE RIB FOR AN AIRCRAFT


    Weitere Titelangaben:

    VERBUNDRIPPE FÜR EIN FLUGZEUG
    NERVURE COMPOSITE POUR UN AVION


    Beteiligte:
    DOBBERFUHL JAMES P (Autor:in) / UHLMAN MATT D (Autor:in) / MOON WILLIAM J (Autor:in)

    Erscheinungsdatum :

    2019-03-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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