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.

    Un ensemble surmontoir est configuré pour être attaché entre une structure intérieure et une structure extérieure dans une cabine interne dun aéronef. Lensemble peut comprendre un corps principal comprenant un premier panneau raccordé à un deuxième panneau opposé au moyen dun panneau de base. Le corps principal est configuré pour limiter le passage de la lumière. Au moins trois éléments dancrage sont configurés pour fixer le corps principal à au moins trois structures réciproques des structures intérieure et extérieure.


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    Title :

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


    Additional title:

    ENSEMBLE SURMONTOIR ELECTROLUMINESCENT POUR ZONE DE TRANSITION, DANS UNE CABINE INTERIEURE D'UN AERONEF


    Contributors:

    Publication date :

    2021-03-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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