A light assembly for an aircraft evacuation system may comprise a first casing (100) including a weighted portion. A light source (104) may be disposed within the first casing. A second casing (102) may be coupled to the first casing by a bearing. The first casing may be configured to rotate with respect to the second casing about an axis. A center of mass of the first casing may be offset from the axis.


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    Title :

    EXTERNAL AIRCRAFT EMERGENCY LIGHTING


    Additional title:

    EXTERNE FLUGZEUGNOTBELEUCHTUNG
    ÉCLAIRAGE D'URGENCE EXTERNE D'AÉRONEF


    Contributors:
    VOLNY JARO S (author) / HARTMAN DREW (author)

    Publication date :

    2022-09-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F21V FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF , Funktionsmerkmale oder Einzelheiten von Leuchten oder Beleuchtungssystemen / 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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