Method for managing a braking system for an aircraft fitted with electromechanical brakes
View Patent ↗A braking system for an aircraft with electric brakes comprising plural electromechanical actuators ( 2 ). The system comprises a braking control unit ( 20 ) delivering a normal braking setpoint ( 21 ) for one or more controllers ( 10 ) of the actuators, and selection logic ( 15 ) for causing the braking system to operate in a plurality of modes. The system includes: a normal braking mode where the control unit generates a normal braking setpoint ( 21 ) for the controller(s); an ultimate braking mode, having priority over the normal braking mode, being responsive to a parking control member, and controlling actuators to respond to the actuation of the parking control member; and a parking braking mode, applied in response to the parking control member and only if the aircraft is stationary, in which the actuators are controlled to apply a force in response to the parking control member being actuated and are then blocked in position.
1. A braking system for an aircraft with electric brakes comprising:
at least one electromechanical actuator ( 2 ),
at least one controller ( 10 ) for said at least one electromechanical actuator,
a braking control unit ( 20 ) delivering a normal braking setpoint ( 21 ) for one or more of said at least one controller ( 10 ) of the at least one actuator, and
selection means ( 15 ) for causing the braking system to operate in a plurality of modes, including:
a normal braking mode during which the braking control unit generates a normal braking setpoint ( 21 ) for the at least one controller;
an ultimate braking mode, having priority over the normal braking mode, that is applied in response to actuation of a parking control member, and in which the at least one actuator is controlled to apply a force in response to the actuation of the parking control member, but in which they are not blocked in position; and
a parking braking mode, applied in response to actuation of a parking control member and only if the aircraft is stationary, in which the at least one actuator is controlled to apply a force in response to the parking control member being actuated and is then blocked in position.
2. A braking system according to claim 1 , wherein the parking control member is a parking selector ( 12 ), and wherein the selection means ( 15 ) select the operating mode to apply as a function of various signals including: the normal braking setpoint ( 21 ); a parking setpoint ( 22 ) delivered by parking logic ( 13 ) for which a parking order ( 23 ) is transmitted on actuation of the parking selector; and a signal ( 17 ) representative of the speed of the aircraft.
3. A braking system according to claim 1 , wherein the parking control member is a parking lever ( 12 ) delivering a parking order proportional to a stroke of the lever, and wherein the selection means ( 15 ) select the operating mode to be applied as a function of various signals, including: the normal braking setpoint ( 21 ); a parking setpoint ( 22 ) delivered by a parking logic ( 13 ) to which a parking order ( 23 ) is transmitted on actuation of the parking control member; and the parking order.