The invention provides a pressure bulkhead (1) for an aircraft comprising a pressurized zone, the pressure bulkhead (1) made of a composite material and comprising a front panel (2), which is intended to be faced towards the pressurized zone; and a rear panel (3), which is substantially parallel to the front panel (2) and is intended to be located farther from the pressurized zone than the front panel (2). The pressure bulkhead (1) further comprises a plurality of longerons (41) located between the front panel (2) and the rear panel (3), each one of them being attached to the front panel (2) and to the rear panel (3); and a plurality of stiffeners (43) some of them being attached to the front panel (2) and the rest of them being attached to the rear panel (3).


    Access

    Download


    Export, share and cite



    Title :

    PRESSURE BULKHEAD FOR AN AIRCRAFT


    Additional title:

    DRUCKSCHOTT FÜR EIN FLUGZEUG
    CLOISON DE PRESSURISATION POUR UN AVION



    Publication date :

    2019-12-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    PRESSURE BULKHEAD FOR AN AIRCRAFT

    BUCHER RAIMUND / EDELMANN KLAUS / MIARIS ANGELOS et al. | European Patent Office | 2019

    Free access

    Pressure bulkhead for an aircraft fuselage, and an aircraft comprising such a pressure bulkhead

    JÖRN PAUL / MÜLLER MARKUS | European Patent Office | 2019

    Free access

    Pressure bulkhead for an aircraft

    BUCHER RAIMUND / EDELMANN KLAUS / MIARIS ANGELOS et al. | European Patent Office | 2022

    Free access

    PRESSURE BULKHEAD FOR AN AIRCRAFT

    ZEEB SERGEJ / IRIMIE SERGIU | European Patent Office | 2019

    Free access

    PRESSURE BULKHEAD FOR AN AIRCRAFT FUSELAGE, AND AN AIRCRAFT COMPRISING SUCH A PRESSURE BULKHEAD

    JÖRN PAUL / MÜLLER MARKUS | European Patent Office | 2016

    Free access