An aircraft interior lining component is formed at least partially of a thermoplastic foam material and includes a first surface which faces an interior of an aircraft cabin when the aircraft interior lining component is mounted in an aircraft, and a second surface which faces away from the interior of the aircraft cabin when the aircraft interior lining component is mounted in an aircraft. The second surface of the aircraft interior lining component includes at least one supporting section and at least one surface section adjacent to the supporting section and recessed relative to the supporting section. The supporting section is dimensioned and arranged so that it is supported, when the aircraft interior lining component is mounted in an aircraft, on an element of a primary structure of the aircraft at least when a predetermined load acts on the first surface of the aircraft interior lining component.


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    Titel :

    AIRCRAFT INTERIOR LINING COMPONENT, METHOD FOR PRODUCING AN AIRCRAFT INTERIOR LINING COMPONENT, AND AIRCRAFT ASSEMBLY


    Weitere Titelangaben:

    FLUGZEUGINNENVERKLEIDUNGSBAUTEIL, VERFAHREN ZUR HERSTELLUNG EINES FLUGZEUGINNENVERKLEIDUNGSBAUTEILS UND FLUGZEUGANORDNUNG
    COMPOSANT DE GARNITURE INTÉRIEURE D'AÉRONEF, PROCÉDÉ DE PRODUCTION D'UN COMPOSANT DE GARNITURE INTÉRIEURE D'AÉRONEF, ET ENSEMBLE D'AÉRONEF


    Beteiligte:
    ROTH INGO (Autor:in)

    Erscheinungsdatum :

    02.01.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge