The structure has a power module (7) for sending phase currents to electromechanical actuators (3) such that the actuators exert braking efforts. A control module (8) controls the power module in response to a braking command such that the appropriate phase currents are sent to the actuators to increase the desired braking efforts. A power supply box (20) comprises a high-voltage converter (21) generating high voltages for providing high power to the power module. The box comprises a low-voltage converter (22) generating low voltages for supplying low voltages to the control module.


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    Title :

    Architecture de système de freinage pour aéronef


    Additional title:

    Architecture of an aircraft braking system
    Aufbau eines Bremssystems für ein Luftfahrzeug


    Contributors:

    Publication date :

    2016-08-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF



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