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.
AIRCRAFT INTERIOR LINING ARRANGEMENT, LONGITUDINAL GAP COVER, INTERIOR PANEL AND INSTALLATION METHOD
FLUGZEUGINNENVERKLEIDUNGSANORDNUNG, LÄNGSSPALTABDECKUNG, INNENVERKLEIDUNG UND INSTALLATIONSVERFAHREN
AGENCEMENT DE REVÊTEMENT INTÉRIEUR D'AÉRONEF, COUVERCLE D'ESPACE LONGITUDINAL, PANNEAU INTÉRIEUR ET PROCÉDÉ D'INSTALLATION
2025-03-19
Patent
Electronic Resource
English
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 |
European Patent Office | 2025
|European Patent Office | 2025
|European Patent Office | 2019
|European Patent Office | 2017
|European Patent Office | 2016
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