A fuselage section of an aircraft has an inner surface with a non-circular contour. A pressure bulkhead for use in the fuselage section has a non-circular outer edge that is aligned with the non-circular contour of the inner surface of the fuselage section. The pressure bulkhead has a spherically-shaped inner section having radially arranged stiffening units and a non-spherically outer section having additional radially arranged stiffening units; the stiffening units corresponding to each section do no extend into the other section. The pressure bulkhead is attached to the fuselage section. A method of manufacturing a fuselage section having such a pressure bulkhead is also provided.


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    Titel :

    Pressure bulkhead adapted to non-circular fuselage section


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

    Erscheinungsdatum :

    31.03.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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