An internally powered, e.g. battery powered, emergency exit sign for an aircraft is provided which is portable and provided with an adhesive layer 3 to enable the internally powered sign to be adhered to a surface. An aircraft cabin requires cabin emergency exit signs which are electrically illuminated using an aircraft electricity supply. However, in the event of the failure of one of these cabin emergency exit signs, the internally powered sign may be adhered in the vicinity to act as a temporary replacement. In this way the flight worthiness of an aircraft may be maintained by a method involving the temporary replacement of a failed cabin emergency exit sign by an internally powered emergency exit sign.


    Access

    Download


    Export, share and cite



    Title :

    Lighting system for aircraft


    Contributors:

    Publication date :

    2024-12-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G09F DISPLAYING , Anzeigewesen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Aircraft lighting system

    KHAWAM MAURICE A | European Patent Office | 2019

    Free access

    Aircraft lighting system

    BUSHELL TIMOTHY GEORGE / LOGAN PHILLIP / EDWARDS GEOFFREY STEPHEN | European Patent Office | 2017

    Free access

    Aircraft lighting system

    TILLOTSON BRIAN J | European Patent Office | 2020

    Free access

    Aircraft lighting system

    KHAWAM MAURICE A | European Patent Office | 2018

    Free access

    Aircraft lighting system

    KHAWAM MAURICE A | European Patent Office | 2018

    Free access