Aircraft braking system architecture comprising:a brake comprising electromechanical actuators (1, 2);a principal control channel (6) and an alternative control channel (7) comprising electrical components that are at least partly different and adapted to provide respectively a principal braking control function and an alternative braking control function that are at least partly different;power modules (15, 16) comprising electrical components that are at least partly different and adapted to generate electrical power supply currents (I1, I2) on the basis of principal control signals or alternative control signals;a surveillance unit (8) adapted to ensure that in normal operation the principal control signals are used and that in the event of a fault the alternative control signals are used to generate the electrical power supply currents.


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    Title :

    ARCHITECTURE DE SYSTÈME DE FREINAGE POUR AÉRONEF


    Additional title:

    ARCHITECTURE OF AN AIRCRAFT BRAKING SYSTEM
    AUFBAU EINES BREMSSYSTEMS FÜR LUFTFAHRZEUG


    Contributors:

    Publication date :

    2024-04-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF



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