A header assembly is configured to be secured between an inboard structure and an outboard structure within an internal cabin of an aircraft. The header assembly may include a main body including a first panel connected to an opposed second panel by a base panel. The main body is configured to limit light from passing therethrough. At least three anchoring members are configured to securely connect the main body to at least three reciprocal structures of the inboard and outboard structures.


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    Titel :

    LIGHT-LIMITING HEADER ASSEMBLY FOR A TRANSITION AREA WITHIN AN INTERIOR CABIN OF AN AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    16.06.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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