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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    Title :

    A pressurized airplane fuselage, comprising a pressure bulkhead


    Additional title:

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


    Contributors:

    Publication date :

    2020-11-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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