Disclosed is an aircraft interior lining arrangement wherein a gap cover having a visible portion and at least one rear retaining portions is installed from the frontside of lining panels in a first direction and then pushed in a second direction which is different to the first direction in order to get the gap cover in backside engagement with the panels, a gap cover, a panel and an installation method.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT INTERIOR LINING ARRANGEMENT, LONGITUDINAL GAP COVER, INTERIOR PANEL AND INSTALLATION METHOD


    Additional title:

    FLUGZEUGINNENVERKLEIDUNGSANORDNUNG, LÄNGSSPALTABDECKUNG, INNENVERKLEIDUNG UND INSTALLATIONSVERFAHREN
    AGENCEMENT DE REVÊTEMENT INTÉRIEUR D'AÉRONEF, COUVERCLE D'ESPACE LONGITUDINAL, PANNEAU INTÉRIEUR ET PROCÉDÉ D'INSTALLATION


    Contributors:
    ROTH INGO (author)

    Publication date :

    2025-03-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile