An aircraft lighting health monitoring system is disclosed. Aircraft lights include each include one or more sensors. Multiple lights having such a sensor(s) are operatively interconnected with this common aircraft lighting health monitoring system. A CPU of this aircraft lighting health monitoring system may be maintained in a sleep mode until needed to assess sensor data of a first data classification, at which time the CPU is used for this assessment and outputs an appropriate health status communication to one or more displays. A DMA controller of the aircraft lighting health monitoring system may be used to handle sensor data of a second data classification (e.g., to control storage of such sensor data).


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    Title :

    AIRCRAFT LIGHTING HEALTH MONITORING SYSTEM


    Contributors:

    Publication date :

    2021-10-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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