The invention relates to a fuselage (10) comprising a fuselage section (11) with an inner surface (12) having a non-circular contour and a spherical pressure bulkhead (13) with an outer edge (16). The outer edge (16) of the spherical pressure bulkhead (13) is attached to the inner surface (12) of the fuselage section (11) and extends along a line, which is non-circular. The line (17) is a three-dimensional curve extending parallel to the inner surface (12) of the fuselage section (11). The invention further relates to an aircraft (40) and to a method for manufacturing a fuselage (10).


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    Titel :

    Extended rear pressure bulkhead


    Weitere Titelangaben:

    Erweitertes Heckdruckschott
    Cloison de pressurisation arrière étendue


    Beteiligte:
    ORLOV DIMITRI (Autor:in)

    Erscheinungsdatum :

    2018-11-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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