The invention relates to a fuselage section comprising an inner surface (15) with a non-circular contour and a pressure bulkhead (11) comprising a non-circular outer edge (16). The non-circular outer edge (16) of the pressure bulkhead (11) is aligned with the non-circular contour of the inner surface (15) of the fuselage section (10) when the pressure bulkhead (11) is attached to the fuselage section (10). The invention further relates to an aircraft with a fuselage section (10) and a method for manufacturing a fuselage section (10).


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    Title :

    Pressure bulkhead adapted to non-circular fuselage section


    Additional title:

    Druckschott für unrunde Rumpfsektion
    Cloison de pressurisation adaptée à une section de fuselage non circulaire


    Contributors:

    Publication date :

    2016-09-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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