A bulkhead (300) joint assembly (312) that includes a strap section (314) configured to secure to an aft section of a fuselage and forward section (308) of the fuselage and extend past a bulkhead (300) of the fuselage. The bulkhead joint assembly (312) also includes a chord (318) engaging and secured to the strap section (314), wherein the chord (318) is configured to extend along the bulkhead (300) to transfer a force from the bulkhead (300) in shear between the chord (318) and the strap section (314).


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    Title :

    BULKHEAD JOINT ASSEMBLY


    Additional title:

    DRUCKSCHOTTVERBINDUNGSANORDNUNG
    ENSEMBLE DE JOINT DE CLOISON


    Contributors:
    JOSEPH JOEL (author) / DIEP PAUL (author) / DOPKER BERNHARD (author) / BUCKLEY MARK J (author)

    Publication date :

    2022-07-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    BULKHEAD JOINT ASSEMBLY

    JOSEPH JOEL / DIEP PAUL / DOPKER BERNHARD et al. | European Patent Office | 2020

    Free access

    BULKHEAD JOINT ASSEMBLY

    JOEL JOSEPH / PAUL DIEP / BERNHARD DOPKER et al. | European Patent Office | 2020

    Free access

    BULKHEAD JOINT ASSEMBLY

    JOSEPH JOEL / DIEP PAUL / DOPKER BERNHARD et al. | European Patent Office | 2020

    Free access

    Bulkhead joint assembly

    JOSEPH JOEL / DIEP PAUL / DOPKER BERNHARD et al. | European Patent Office | 2020

    Free access

    Bulkhead joint assembly

    JOSEPH JOEL / DIEP PAUL / DOPKER BERNHARD et al. | European Patent Office | 2020

    Free access