The illustrative embodiments disclose a pressure bulkhead system comprising an aft pressure bulkhead, skin splice angles, and stringer splice angles. The aft pressure bulkhead has an outer compression ring. The skin splice angles are positioned adjacent to one another and joined to the outer compression ring. The skin splice angles form a joint between a first section of a fuselage, a second section of the fuselage, and the aft pressure bulkhead. The stringer splice angles join the skin splice angles to a stringer in the second section of the fuselage.


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    Titel :

    PRESSURE BULKHEAD SYSTEM


    Weitere Titelangaben:

    DRUCKSCHOTTSYSTEM
    SYSTÈME DE CLOISON DE PRESSURISATION


    Beteiligte:
    DIEP PAUL B (Autor:in) / DOPKER BERNHARD (Autor:in) / VINGIANI ROSARIO (Autor:in)

    Erscheinungsdatum :

    29.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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