An aircraft structural assembly includes an area element which has a core and an outer layer. A first surface of the area element is convexly curved, at least in certain sections, relative to an imaginary central area of the area element extending through the core of the area element. By contrast, a second surface of the area element located opposite the first surface is oriented, at least in certain sections, parallel to the imaginary central area of the area element extending through the core of the area element. The area element is configured in the form of a floor panel of a floor system. The first or the second surface of the area element is designed to form a walkable floor surface of the floor system in the state of the aircraft structural assembly when mounted in an aircraft.


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    Titel :

    AIRCRAFT STRUCTURAL ASSEMBLY


    Weitere Titelangaben:

    STRUKTURANORDNUNG EINES FLUGZEUGES
    ENSEMBLE STRUCTURAL D'AÉRONEF


    Beteiligte:
    ZAHLEN PIERRE (Autor:in) / ZUARDY ICHWAN (Autor:in) / MUELLER MARKUS (Autor:in) / HERRMANN AXEL (Autor:in)

    Erscheinungsdatum :

    2019-11-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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