A pressure bulkhead for the pressure-tight axial closure of a pressurized fuselage of an aircraft or spacecraft that can be put under an internal pressure, comprises a pressure dome, which is designed with a concave inner surface and a convex outer surface; inspection hatches, which each form an aperture in the pressure dome from the inner surface to the outer surface; and pressure covers for pressure-tight closure of the inspection hatches, wherein the pressure covers each have a cover and a pressure seal, wherein the cover is designed for the repeatedly releasable fixing of the pressure cover on the concave inner surface over the inspection hatch and wherein the pressure seal is formed at the edge of the cover for the pressure-tight closure of the cover with the pressure dome.


    Access

    Download


    Export, share and cite



    Title :

    PRESSURE BULKHEAD FOR AN AIRCRAFT


    Contributors:
    ZEEB SERGEJ (author) / IRIMIE SERGIU (author)

    Publication date :

    2019-07-11


    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 FUSELAGE, AND AN AIRCRAFT COMPRISING SUCH A PRESSURE BULKHEAD

    JÖRN PAUL / MÜLLER MARKUS | European Patent Office | 2016

    Free access

    Pressure bulkhead for an aircraft

    JÖRN PAUL / GRASE KARIM / ZUARDY ICHWAN et al. | European Patent Office | 2020

    Free access

    Pressure bulkhead for an aircraft

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

    Free access