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.


    Access

    Download


    Export, share and cite



    Title :

    REDUCED-WIRING CONTROLLER FOR AIRCRAFT USE


    Contributors:

    Publication date :

    2019-08-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Aircraft wiring

    Tema Archive | 1968


    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


    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