An aircraft interior fitting component system (10) comprises an aircraft interior fitting component (12), a support element (20) attached to the aircraft interior fitting component (12) and an aircraft primary structure component (16). The support element (20) is dimensioned in such a way and is attached to the aircraft interior fitting component (12) in such a position that, in an assembled state of the aircraft interior fitting component (12) in an aircraft, it is supported on the aircraft primary structure component (16) at least when a predetermined load acts on the aircraft interior fitting component (12) along the x-axis of the aircraft in flight direction.


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    Titel :

    AIRCRAFT INTERIOR FITTING COMPONENT SYSTEM AND METHOD FOR MANUFACTURING AN AIRCRAFT INTERIOR FITTING COMPONENT SYSTEM


    Weitere Titelangaben:

    FLUGZEUGINNENAUSBAUKOMPONENTENSYSTEM UND VERFAHREN ZUR HERSTELLUNG EINES FLUGZEUGINNENAUSBAUKOMPONENTENSYSTEMS
    SYSTÈME DE COMPOSANTS D'ÉQUIPEMENT INTÉRIEUR D'AVION ET PROCÉDÉ DE FABRICATION D'UN SYSTÈME DE COMPOSANTS D'ÉQUIPEMENT INTÉRIEUR D'AVION


    Beteiligte:
    ROTH INGO (Autor:in)

    Erscheinungsdatum :

    2017-05-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT