Method of managing the power supply to a non-reversible actuator for a vehicle wheel brake
View Patent ↗A wheel brake for an aircraft, the brake comprising a support ( 2 ) that receives at least one electromechanical actuator ( 1 ) fitted with a pusher ( 8 ) facing friction elements ( 3 ) and movable under drive from an electric motor ( 6 ) to apply a braking force selectively against the friction elements. The actuator is non-reversible such that a reaction force applied on the pusher cannot cause the electric motor to turn, and the actuator is associated with elements ( 30, 31, 32, 33, 34 ) for selectively switching off an electric power supply to the electric motor, which elements allow power to be delivered to the actuator in normal circumstances, and switch off the power if (a) the measured speed of rotation (w mes ) of the electric motor drops below a first predetermined threshold (S 1 ); and (b) the commanded speed of rotation ( ω ) of the electric motor drops below a second predetermined threshold (S 2 ).
1. A wheel brake for an aircraft, the brake comprising a support that receives at least one electromechanical actuator fitted with a pusher facing friction elements and movable under drive from an electric motor to apply a braking force selectively against the friction elements, wherein the actuator is non-reversible such that a reaction force applied on the pusher cannot cause the electric motor to turn, at least when the reaction force is below a given limit force, and wherein the actuator is associated with means for selectively switching off an electric power supply to the electric motor, which means allow power to be delivered to the actuator in normal circumstances, and switch off said power if:
the measured speed of rotation (ω mes ) of the electric motor drops below a first predetermined threshold (S 1 ); and
the commanded speed of rotation ( ω ) of the electric motor drops below a second predetermined threshold (S 2 ).
2. A method of managing the electrical power supply to a non-reversible electromechanical actuator for a wheel brake of an aircraft, the electromechanical actuator being fitted with a pusher facing friction elements and movable under drive from an electric motor to apply a braking force selectively to the friction elements, the method including the step of switching off an electrical power supply to the actuator if:
the measured speed of rotation (ω mes ) of the motor drops below a first predetermined threshold (S 1 ); and
the commanded speed of rotation ( ω ) of the motor drops below a second predetermined threshold (S 2 ).