Systems and methods for aircraft electric taxi brake optimization are provided. The system may comprise an aircraft having a landing gear comprising a wheel, a friction brake having a brake material coupled to the wheel, a regenerative brake comprising a reversible taxi motor coupled to the wheel, a sensor configured to measure a wheel parameter of the wheel and a temperature of the friction brake, a tangible, non-transitory memory configured to communicate with a controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising: receiving, by the controller, a command signal and the friction brake temperature and calculating, by the controller, a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal.


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    Titel :

    System and method for aircraft electric taxi brake optimization


    Beteiligte:
    KIPP RICHARD A (Autor:in) / KELLER STEVEN T (Autor:in)

    Erscheinungsdatum :

    2020-01-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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