An aircraft electric taxi health management system includes a right electric motor drivingly connected to at least one wheel on a right landing gear assembly, a left electric motor drivingly connected to at least one wheel on a left landing gear assembly, a right motor controller configured to electrically drive the right electric motor, monitor the right motor current and voltage, and generate right motor signals as a function of the right motor current and voltage; a left motor controller configured to electrically drive the left electric motor, monitor the left motor current and voltage, and generate left motor signals as a function of the left motor current and voltage; and a health management controller configured to compare the right motor signals to the left motor signals; and generate electric taxi system maintenance signals based on the comparison.


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    Title :

    AIRCRAFT ELECTRIC TAXI HEALTH MANAGEMENT SYSTEM AND METHOD


    Contributors:
    GORDON GRANT (author) / ABEL STEVE (author) / KIM KYUSUNG (author)

    Publication date :

    2016-02-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte



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