A pressure bulkhead for the pressure-tight axial closure of a pressurized fuselage of an aircraft or spacecraft that is capable of being put under internal pressure includes dome segments, having an integrated reinforcement, in particular a peripheral reinforcement, which are in each case made integrally from a fiber-reinforced thermoplastic plastics material, and are joined to one another so as to form a pressure dome.


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    Titel :

    PRESSURE BULKHEAD FOR AN AIRCRAFT


    Beteiligte:
    BUCHER RAIMUND (Autor:in) / EDELMANN KLAUS (Autor:in) / MIARIS ANGELOS (Autor:in) / RATH DOMINIK (Autor:in) / STELLBERGER FRANK (Autor:in)

    Erscheinungsdatum :

    05.09.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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