In order to simplify an integration of systems on an aircraft fuselage, the invention provides a production method for producing a supporting fuselage panel (10) for a fuselage portion of an aircraft fuselage in a region of an aircraft cabin (14), comprising: manufacturing the fuselage panel (10) in a sandwich construction with an inner panel (24) and an outer skin (28) as shells (18, 20) and with a filler panel (30), which is embedded between the shells (18, 20), as a core (22), with the outer skin (28) being designed as part of a fuselage structure (12) and of the outer boundary of the aircraft fuselage, the inner panel (24) being designed for an interior boundary (26) of the cabin (14) and functional elements (32) of the fuselage structure (12) and of the cabin (14) and/or of the aircraft being integrated in the filler panel (30). The shells (18, 20) and the filler panel are preferably connected by a joining process, with covalent bonds being produced.


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    Title :

    PRODUCTION METHOD FOR PRODUCING A SUPPORTING FUSELAGE PANEL AND FUSELAGE PANEL PRODUCIBLE THEREWITH


    Additional title:

    PROCEDE DE FABRICATION D'UN PANNEAU DE FUSELAGE PORTEUR AINSI QUE PANNEAU DE FUSELAGE POUVANT ETRE FABRIQUE PAR CE PROCEDE


    Contributors:

    Publication date :

    2015-06-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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