A pressurized aircraft fuselage, comprising a pressure bulkhead (1) installed on a fuselage structure (2), which forms a barrier between an internal pressurized cabin area (3) and an outside area (4), wherein the edge of the pressure bulkhead (1) is circumferentially attached to the fuselage structure (2) by fastening means, wherein the fastening means comprise a pair of ring-shaped attachment frames (5a;5b) made of an open or hollow profile, which are disposed at each side of the pressure bulkhead (1) respectively, in order to form a clamping connection for the pressure bulkhead towards the fuselage structure (2).


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    Titel :

    A pressurized airplane fuselage, comprising a pressure bulkhead


    Weitere Titelangaben:

    Druckfester Flugzeugrumpf mit einem Druckschott
    Fuselage d'avion sous pression comprenant une cloison de pressurisation


    Beteiligte:
    GRASE KARIM (Autor:in) / ZUARDY ICHWAN (Autor:in) / SCHEEL HENNING (Autor:in) / HACHENBERG DIETER (Autor:in) / VULTAGGIO B CLAUDIO (Autor:in)

    Erscheinungsdatum :

    2020-11-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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