A control method of an electrical braking system for aircraft includes a plurality of electromechanical actuators capable of applying a braking force on friction members. Each electromechanical actuator includes an electric motor equipped with one or more windings. The braking system further includes at least one power module configured to send to each electric motor winding a phase current and at least one control module configured to control, in response to a braking setpoint, the sending by the power module of a setpoint phase current determined depending on the braking force to be applied. The method further includes the variation of the phase current transmitted to each winding of the electric motor so as to cause the phase current to oscillate around the setpoint phase current.


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    Title :

    PROCEDE DE PILOTAGE D'UN SYSTEME DE FREINAGE ELECTRIQUE ET SYSTEME DE FREINAGE ELECTRIQUE POUR AERONEF


    Additional title:

    METHOD FOR CONTROLLING AN ELECTRIC BRAKING SYSTEM AND ELECTRIC BRAKING SYSTEM FOR AIRCRAFT
    STEUERVERFAHREN EINES ELEKTRISCHEN BREMSSYSTEMS UND ELEKTRISCHES BREMSSYSTEM FÜR LUFTFAHRZEUG


    Contributors:

    Publication date :

    2022-03-23


    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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