| 摘要 |
The invention relates to a braking system architecture for an aircraft having wheels 1 braked by means of respective brakes 2, each brake having a plurality of electromechanical actuators 3a, 3b, the braking system having controllers 8a, 8b for distributing electric power Ps to the actuators 3a, 3b in response to a braking setpoint, each controller 8a, 8b being associated with some of the actuators of any given brake. According to the invention, each controller 8a, 8b has an input Ev for receiving information about the rotary speed of the wheel 1 braked by the actuators associated with said controller, the controller including processor means 13 for modulating the power transmitted to the actuators as a function of the speed of rotation of the wheel in order to provide anti-skid protection. |
| 主权项 |
1. A braking system architecture for an aircraft having wheels (1) braked by means of respective brakes (2), each brake having a plurality of electromechanical actuators (3), the braking system having controllers (8) for distributing electric power (Ps) to the actuators (3) in response to a braking setpoint, each controller (8) being associated with some of the actuators of any given brake, the architecture being characterized in that each controller (8) has an input (Ev) for receiving information about the rotary speed of the wheel (1) braked by the actuators associated with said controller, the controller including processor means (13) for modulating the power transmitted to the actuators as a function of the speed of rotation of the wheel in order to provide anti-skid protection. |
