A pressure bulkhead of an aircraft with a fuselage shell and a pressure bulkhead disposed therein preferably in the rear region for forming a fuselage-internal pressure region, which pressure bulkhead is attached on the edge in the interior of the fuselage shell, wherein the pressure bulkhead has a lenticular cross-section and a sandwich construction that comprises a foam core sandwiched between two opposing exterior shells.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Pressure fuselage of an aircraft with a fuselage shell and a pressure bulkhead disposed therein


    Beteiligte:
    ZUARDY M ICHWAN (Autor:in) / GRASE KARIM (Autor:in) / ROWEDDER CARSTEN (Autor:in) / DE JONG CLAAS (Autor:in) / MUELLER MARKUS (Autor:in) / JESSRANG MATHIAS (Autor:in)

    Erscheinungsdatum :

    2017-12-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    PRESSURE BULKHEAD FOR AN AIRCRAFT FUSELAGE

    ZUARDY ICHWAN / HOFFMEISTER THOMAS / HERRMANN AXEL SIEGFRIED et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    PRESSURE BULKHEAD FOR AN AIRCRAFT FUSELAGE

    ZUARDY ICHWAN / HOFFMEISTER THOMAS / HERRMANN AXEL SIEGFRIED et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    Pressure bulkhead for an aircraft fuselage

    ZUARDY ICHWAN / HOFFMEISTER THOMAS / HERRMANN AXEL SIEGFRIED et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    PRESSURE BULKHEAD FOR AN AIRCRAFT FUSELAGE

    JORN PAUL / GRASE KARIM | Europäisches Patentamt | 2017

    Freier Zugriff

    PRESSURE BULKHEAD FOR AN AIRCRAFT FUSELAGE

    ZUARDY ICHWAN / HOFFMEISTER THOMAS / HERRMANN AXEL SIEGFRIED et al. | Europäisches Patentamt | 2020

    Freier Zugriff