Visible built-in component for the interior fittings of an aircraft, comprising a partially transparent stone layer or glass layer and a luminous layer arranged thereunder for backlighting the stone layer or glass layer, wherein the luminous layer comprises a plurality of luminous strips and a partially transparent intermediate layer is provided between the luminous layer and the stone layer or glass layer.


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    Title :

    Built-in optical component for the interior fittings of an aircraft and correspondingly fitted aircraft


    Contributors:

    Publication date :

    2019-01-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60Q ARRANGEMENT OF SIGNALLING OR LIGHTING DEVICES, THE MOUNTING OR SUPPORTING THEREOF OR CIRCUITS THEREFOR, FOR VEHICLES IN GENERAL , Anordnung von Signal- oder Beleuchtungsvorrichtungen, deren Einbau oder Halterung oder deren Schaltkreise bei Fahrzeugen allgemein / F21W Index-Schema in Verbindung mit den Unterklassen F21K, F21L, F21S und F21V, betreffend den Gebrauch oder Einsatz von Leuchten oder Beleuchtungssystem , INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K,  F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS



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