Braking system for an aircraft provided with electromechanical brakes.

摘要

The architecture has electromechanical brakes (2) respectively with electromechanical actuators (3), and a proximity casing (50) placed near each brake at the bottom of a landing gear (5). The proximity casing includes an input-output unit for collecting and calibrating a signal from each sensor associated to each brake and for transmitting the processed signal to each controller (10) using a communication bus along the landing gear. The proximity casing includes a control logic for managing blocking units of the actuators. The controllers are respectively linked to the actuators by cables.