Door assemblies for aircraft interiors are described. Such door assemblies may comprise a door for opening and closing an aperture between zones of the aircraft interior and an interface configured to couple the door to the aircraft interior. A pressure-relief element may form at least a portion of the door wherein the pressure-relief element is retained by a magnetic force calibrated to permit release of the pressure-relief element upon presence of a predetermined pressure differential across the pressure-relief element. Components and mechanisms useful in reducing light bleed across doors for aircraft interiors are also disclosed.


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    Titel :

    DOOR ASSEMBLY FOR AIRCRAFT INTERIOR


    Weitere Titelangaben:

    TÜRANORDNUNG FÜR FLUGZEUGINNENRAUM
    ENSEMBLE PORTE POUR L'INTÉRIEUR D'UN AVION


    Beteiligte:
    GUIMONT JEAN-FRANÇOIS (Autor:in) / ROSA YVAN (Autor:in) / TREMBLAY BENJAMIN (Autor:in) / BOXER USHER (Autor:in)

    Erscheinungsdatum :

    17.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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