An aircraft navigation light (8; 9) with integrated redundancy having at least a selected minimum light output, comprises a first light source (81; 91); a second light source (82; 92); and a common optical element (84; 94), which is configured for shaping an output light intensity distribution (89; 99) of the aircraft navigation light (8; 9). The light emitted by each of the first light source (81; 91) and the second light source (82; 92) is modified by the common optical element (84; 94). Each of the first and second light sources (82; 92) has an individual light output capacity, wherein the individual light output capacity of each of the first and second light sources (82; 92) alone is sufficient for providing the selected minimum light output (89; 99) of the aircraft navigation light (8; 9).


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    Title :

    AIRCRAFT NAVIGATION LIGHT AND AIRCRAFT COMPRISING THE SAME


    Additional title:

    FLUGZEUGNAVIGATIONSLICHT UND FLUGZEUG DAMIT
    LUMIÈRE DE NAVIGATION D'AÉRONEF ET AÉRONEF LA COMPRENANT


    Contributors:

    Publication date :

    2021-05-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung



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