A braking system architecture for aircraft, the architecture comprising:a brake (20) comprising a plurality of electromechanical actuators (26), each electromechanical actuator including a digital communication module;at least one power supply unit (21, 22);two control units (23, 24), each control unit being connected to a distinct group of one or more electromechanical actuators and comprising an upstream digital communication module (27), a control module (28) arranged to generate digital control signals (Sn1, Sn2), and a downstream digital communication module (29) connected to the digital communication modules of the electromechanical actuators of said group in order to transmit the digital control signals to the power modules of said electromechanical actuators; anda digital communication network (25) to which the upstream digital communication modules (27) of both control units are connected.
DISTRIBUTED ARCHITECTURE OF AIRCRAFT BRAKING SYSTEM
2023-07-20
Patent
Electronic Resource
English