An aircraft light (12, 14) comprises at least one light source (26); at least one sensor (30), an operating mode selector (33), and a transmitter (34). The sensor (30) is configured for detecting current operational conditions and providing at least one corresponding sensor signal. The operating mode selector (33) configured for determining a suitable light emission of the at least one light source (26) based on the at least one sensor signal. The operating mode selector (33) is further configured for determining the amount of electrical power needed for generating the determined light emission. The transmitter (34) configured for transmitting a power request signal indicating the determined amount of electrical power to a power supply (16).


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    Title :

    AIRCRAFT LIGHT AND AIRCRAFT LIGHT ASSEMBLY


    Additional title:

    FLUGZEUGLICHT UND FLUGZEUGLICHTANORDNUNG
    LUMIÈRE D'AÉRONEF ET ENSEMBLE LUMINEUX D'AÉRONEF


    Contributors:

    Publication date :

    2021-04-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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