The present invention provides a pressure bulkhead device (1) for an aircraft fuselage (10), the pressure bulkhead device (1) comprising: a first side (2) extending along a vertical direction (Zb) and facing a pressurizable compartment; a second side (3) arranged opposite the first side (2), wherein the first side (2) is pressurizable with an internal pressure that is higher than an ambient pressure being present at the second side (3); and an energy absorbing section (4) [or energy absorbing mechanism, respectively], which is configured to absorb impact energy, and is arranged at least at a lower end region (5) of the first side (2) and the second side (3) in relation to the vertical direction (Zb). Further the present invention provides an aircraft fuselage (10) comprising such a pressure bulkhead device (1) as well as an aircraft (100) comprising such an aircraft fuselage (10).


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    Titel :

    PRESSURE BULKHEAD DEVICE, AIRCRAFT FUSELAGE AND AIRCRAFT


    Weitere Titelangaben:

    DRUCKSCHOTT, FLUGZEUGRUMPF UND FLUGZEUG
    CLOISON DE PRESSURISATION, FUSELAGE D'AÉRONEF ET AÉRONEF


    Beteiligte:
    SIEMANN MARTIN (Autor:in) / BENTHIEN HERMANN (Autor:in)

    Erscheinungsdatum :

    06.08.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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