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


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    Titel :

    PRESSURE BULKHEAD ADAPTED TO NON-CIRULAR FUSELAGE SECTION


    Beteiligte:
    ORLOV DIMITRI (Autor:in) / RICHTER DIRK (Autor:in) / TIRYAKI MEMIS (Autor:in) / REINHOLD RALF (Autor:in) / EILKEN WOLFGANG (Autor:in)

    Erscheinungsdatum :

    08.09.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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