Electromechanical actuator with dual excitation

1. A braking actuator for an aircraft brake, the actuator comprising:

a casing integrating:

an electric motor comprising a stationary portion and a movable portion that is movable relative to the stationary portion, the stationary portion carrying an exciter member adapted to drive the movement of the movable portion when the exciter member is electrically powered;

a pusher that is movable in translation relative to the casing along a pusher travel axis;

mechanical means for transforming travel movement of the movable portion of the motor into movement in translation of the pusher; and

a position sensor for sensing the position of the movable portion relative to the stationary portion; the position sensor comprising a transmitter member and a receiver member, the transmitter member being adapted, when powered electrically, to excite said receiver member at least when the movable portion is moving relative to the stationary portion, the receiver member being adapted to generate at least one signal representative of the position of the movable portion when said receiver member is excited by said transmitter member;

wherein:

the exciter member of the motor comprises at least first and second exciters, each exciter being adapted, when powered, to drive the movement of the movable portion relative to the stationary portion, the exciters being arranged to be capable of being powered electrically independently from each other;

the transmitter member of the position sensor comprises at least first and second transmitters, each transmitter being adapted, on being powered, to cause at least one signal representative of the position of the movable portion to be sent by the receiver member, the transmitters being arranged to be capable of being electrically powered independently of each other;

the actuator further includes an integrated inverter inside the casing of the actuator and being adapted to power said first exciter, said integrated inverter being connected to first terminals of the actuator so as to be capable of being powered by a common power source external to the actuator; and

the second exciter is wired to second terminals of the actuator so as to be powerable by an external inverter external to the actuator.

2. A braking actuator according to claim 1 , wherein the stationary portion is a stator and the movable portion is a rotor mounted to rotate relative to the stator, wherein the mechanical means for transforming travel movement are adapted to transform rotation of the rotor into a movement in translation of the pusher, and wherein said position sensor is an angular position sensor for sensing the angular position of the rotor relative to the stator.

3. A braking actuator for aircraft according to claim 2 , wherein the angular position sensor is an inductive sensor:

the transmitter member of the sensor comprising first and second transmitter coils respectively forming the first and second transmitters; and

the receiver member of the sensor including first and second receivers each formed by a receiver coil, the first and second receivers being adapted to generate respective first and second signals representative of the angular position of the rotor when at least one of said transmitters is powered with an alternating voltage.

4. An actuator according to claim 2 , wherein said actuator includes an integrated processor unit inside said casing of the actuator and suitable for controlling said integrated inverter as a function of at least one signal representative of the angular position of the rotor.

5. An actuator according to claim 1 , wherein the stationary portion is a stator and the movable portion is a rotor mounted to rotate relative to the stator, wherein the mechanical means for transforming travel movement are adapted to transform rotation of the rotor into a movement in translation of the pusher, and wherein said position sensor is an angular position sensor for sensing the angular position of the rotor relative to the stator, wherein said at least one signal representative of the position of the movable portion is a signal representative of the angular position of the rotor, wherein said receiver member of the sensor is connected to third terminals of the actuator in such a manner as to be capable of sending said signal representative of the angular position of the rotor to an external calculation unit external to the actuator, which unit is suitable for controlling said external inverter as a function of the signal representative of the angular position of the rotor.

6. A braking actuator for an aircraft brake, the actuator comprising:

a casing integrating:

an electric motor comprising a stationary portion and a movable portion that is movable relative to the stationary portion, the stationary portion carrying an exciter member adapted to drive the movement of the movable portion when the exciter member is electrically powered;

a pusher that is movable in translation relative to the casing along a pusher travel axis;

mechanical means for transforming travel movement of the movable portion of the motor into movement in translation of the pusher; and

a position sensor for sensing the position of the movable portion relative to the stationary portion; the position sensor comprising a transmitter member and a receiver member, the transmitter member being adapted, when powered electrically, to excite said receiver member at least when the movable portion is moving relative to the stationary portion, the receiver member being adapted to generate at least one signal representative of the position of the movable portion when said receiver member is excited by said transmitter member;

wherein:

the exciter member of the motor comprises at least first and second exciters, each exciter being adapted, when powered, to drive the movement of the movable portion relative to the stationary portion, the exciters being arranged to be capable of being powered electrically independently from each other;

the transmitter member of the position sensor comprises at least first and second transmitters, each transmitter being adapted, on being powered, to cause at least one signal representative of the position of the movable portion to be sent by the receiver member, the transmitters being arranged to be capable of being electrically powered independently of each other,

the stationary portion is a stator and the movable portion is a rotor mounted to rotate relative to the stator, and

the mechanical means for transforming travel movement are adapted to transform rotation of the rotor into a movement in translation of the pusher, and wherein said position sensor is an angular position sensor for sensing the angular position of the rotor relative to the stator, and

wherein

it includes a blocking member for blocking the pusher in position, said blocking member being adapted to cause the pusher to be blocked on receiving a blocking control signal and to release said pusher on receiving an unblocking control signal, the blocking member being:

firstly electrically connected to an internal relay for controlling the blocking member; and

secondly electrically connected to external blocking terminals of said actuator so as to be capable of receiving the blocking and unblocking control signals via said external blocking terminals without passing via said internal relay.

7. An aircraft brake including at least one actuator according to claim 1 , the brake further including a stack of disks suitable for being selectively pressed together by the actuator in order to brake a wheel associated with the brake.

8. A braking device for aircraft including at least one brake comprising (1) a stack of disks suitable for being selectively pressed together by the actuator in order to brake a wheel associated with the brake, (2) a braking actuator for an aircraft brake, the actuator comprising:

a casing integrating:

an electric motor comprising a stationary portion and a movable portion that is movable relative to the stationary portion, the stationary portion carrying an exciter member adapted to drive the movement of the movable portion when the exciter member is electrically powered;

a pusher that is movable in translation relative to the casing along a pusher travel axis;

mechanical means for transforming travel movement of the movable portion of the motor into movement in translation of the pusher; and

a position sensor for sensing the position of the movable portion relative to the stationary portion; the position sensor comprising a transmitter member and a receiver member, the transmitter member being adapted, when powered electrically, to excite said receiver member at least when the movable portion is moving relative to the stationary portion, the receiver member being adapted to generate at least one signal representative of the position of the movable portion when said receiver member is excited by said transmitter member;

wherein:

the exciter member of the motor comprises at least first and second exciters, each exciter being adapted, when powered, to drive the movement of the movable portion relative to the stationary portion, the exciters being arranged to be capable of being powered electrically independently from each other;

the transmitter member of the position sensor comprises at least first and second transmitters, each transmitter being adapted, on being powered, to cause at least one signal representative of the position of the movable portion to be sent by the receiver member, the transmitters being arranged to be capable of being electrically powered independently of each other,

the stationary portion is a stator and the movable portion is a rotor mounted to rotate relative to the stator, and

the mechanical means for transforming travel movement are adapted to transform rotation of the rotor into a movement in translation of the pusher, and wherein said position sensor is an angular position sensor for sensing the angular position of the rotor relative to the stator, and

further comprising:

an external inverter external to the actuator and connected to the second exciter in order to power it selectively; and

an integrated inverter integrated in the actuator and connected to the first exciter of the motor in order to power it.

9. An actuator according to claim 1 , wherein the integrated inverter and the first transmitter of the transmitter member of the sensor are connected to said first terminals of the actuator so as to be capable of being powered by said common power source external to the actuator.