The invention relates to an architecture of an aircraft braking system, comprising:-a brake (20) comprising a plurality of electromechanical actuators (26), each having a digital communication module; at least one power supply unit (21, 22); two control units (23, 24), each connected to a separate set of one or more electromechanical actuators and comprising an upstream digital communication module (27) arranged to generate digital control signals (Sn1, Sn2), sn2), and a downstream digital communication module (29) connected to the digital communication modules of the electromechanical actuators in the group to transmit digital control signals to the power modules of the electromechanical actuators; -a digital communication network (25) to which the upstream digital communication modules (27) of the two control units are connected.

    本发明涉及一种飞行器制动系统的架构,包括:‑包括多个机电致动器(26)的制动器(20),每个机电致动器具有数字通信模块;至少一个供电单元(21,22);两个控制单元(23,24),每个控制单元连接到单独一组一个或多个机电致动器并且包括上游数字通信模块(27)、被布置成生成数字控制信号(Sn1,Sn2)的控制模块(28)、以及连接到所述组中的机电致动器的数字通信模块以将数字控制信号传输到所述机电致动器的功率模块的下游数字通信模块(29);‑数字通信网络(25),两个控制单元的上游数字通信模块(27)连接到该数字通信网络。


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    Titel :

    Distributed architecture of aircraft brake system


    Weitere Titelangaben:

    飞行器刹车系统的分布式架构


    Beteiligte:
    ENFLOY DAVID (Autor:in) / FREY OLIVIER (Autor:in) / GOYEZ BRIAN (Autor:in)

    Erscheinungsdatum :

    2022-12-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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