A light assembly for an aircraft evacuation system may comprise a first casing including a weighted portion. A light source may be disposed within the first casing. A second casing 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.


    Access

    Download


    Export, share and cite



    Title :

    EXTERNAL AIRCRAFT EMERGENCY LIGHTING


    Additional title:

    ECLAIRAGE D'URGENCE D'EXTERIEUR D'AERONEF


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

    Publication date :

    2018-05-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    External aircraft emergency lighting

    VOLNY JARO S / HARTMAN DREW | European Patent Office | 2018

    Free access

    EXTERNAL AIRCRAFT EMERGENCY LIGHTING

    VOLNY JARO S / HARTMAN DREW | European Patent Office | 2022

    Free access

    Aircraft emergency lighting

    RUST DANIEL | European Patent Office | 2019

    Free access

    AIRCRAFT EMERGENCY LIGHTING SYSTEM

    EDQUIST JOHN / FREDRICH JEREMY | European Patent Office | 2021

    Free access

    AIRCRAFT EMERGENCY LIGHTING SYSTEM

    EDQUIST JOHN / FREDRICH JEREMY | European Patent Office | 2023

    Free access