A distributed controller of an aircraft includes a first communication device, a second communication device, and at least one processor. The first communication device is configured to transmit heater status data and receive heater command data via radio waves or power-line communication. The second communication device is configured to transmit at least one heater control signal and to receive heater sensor data. The at least one processor is configured to provide heater control based upon the heater command data and the heater sensor data and to provide heater status information based upon the received heater sensor data.


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    Titel :

    REDUCED-WIRING CONTROLLER FOR AIRCRAFT USE


    Beteiligte:
    AESCHLIMAN CARL (Autor:in) / HARR JOHN A (Autor:in)

    Erscheinungsdatum :

    2019-08-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H04Q Wähltechnik , SELECTING



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    Cox, R.H.W. / Hill, W.E. | Engineering Index Backfile | 1945


    Aircraft wiring system

    Cox, R.H.W. / Hill, W.E. | Engineering Index Backfile | 1944


    Aircraft wiring system

    Cox, R.H.W. / Hill, W.E. | Engineering Index Backfile | 1945


    Aircraft wiring system

    Cox, R.H.W. / Hill, W.E. | Engineering Index Backfile | 1944