An apparatus for an aircraft structure comprising first and second stringers, each having a vertical stringer portion defining a lengthwise gap. The structure may include a fitting having a central rib attachment member and first and second extensions extending in opposite directions from said central rib attachment member. Stringer attachment portions extending up from said first and second extensions are inserted into the lengthwise gaps of the first and second stringer portions, respectively. The rib attachment member may be attached to a side-of-body rib.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    BONDED SPLICE JOINT


    Weitere Titelangaben:

    GEKLEBTE SPLEISSVERBINDUNG
    JOINT DE RECOUVREMENT COLLÉ


    Beteiligte:
    NORDMAN PAUL (Autor:in) / NELSON PAUL (Autor:in)

    Erscheinungsdatum :

    31.08.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    BONDED SPLICE JOINT

    PAUL NORDMAN / PAUL NELSON | Europäisches Patentamt | 2017

    Freier Zugriff

    Fatigue life prediction of a bonded splice joint

    LIU, C. / HELLER, R. | AIAA | 1980


    Splice joint terminal

    Europäisches Patentamt | 2019

    Freier Zugriff

    Splice joint terminal

    BAK SE YEONG | Europäisches Patentamt | 2019

    Freier Zugriff

    CRANE MAIN GIRDER WITH SPLICE JOINT

    PEIPPO JUHA / KALLIOKOSKI KIRSI | Europäisches Patentamt | 2024

    Freier Zugriff