Aircraft flight control surface actuator
An actuator for a flight control surface of an aircraft, including: a fixed annulus for fixing to the fuselage, an rotatable annulus with respect to the fixed annulus about an axis of rotation, an output ring which can be fixed to the control surface, and a coupling mechanism having a disc with translational mobility with respect to the mobile annulus in a direction parallel to the axis of rotation, the disc able to move between an engaged position, and a disengaged position, in which the disc is disengaged from the mobile annulus to disconnect the output ring from the mobile annulus. A retaining piece keeps the disc in the engaged position, and a rupture member activates to break the retaining piece to allow the disc to move into the disengaged position.
1. An aircraft flight control surface actuator, comprising:
a fixed gear capable of being attached to a fuselage of the aircraft,
a gear rotatably movable with respect to the fixed gear around an axis of rotation,
an output ring capable of being attached to the flight control surface, and
a coupling mechanism comprising a disk movable in translation with respect to the movable gear in a direction parallel to the axis of rotation, the disk being movable between an engaged position in which the disk is in engagement both with the movable gear and the output ring so as to make the output ring secured to the movable gear, and a disengaged position in which the disk is disengaged from the movable gear, so as to decouple the output ring from the movable gear, a retaining part capable of retaining the disk in the engaged position, and a rupture member capable of being activated to rupture the retaining part, so as to allow displacement of the disk into the disengaged position.
2. The actuator according to claim 1 , wherein the rupture member comprises a block formed from a shape-memory material, the block being capable of changing shape when it is subjected to an electric or magnetic field, so as to apply a tensile stress to the retaining part, causing the rupture of the retaining part.
3. The actuator according to claim 1 , wherein the rupture member comprises a pyrotechnic composition capable of exploding when it is subjected to an electrical current, causing the rupture of the retaining part.
4. The actuator according to claim 1 , wherein the retaining part has a weakened area capable of rupturing in the event of activation of the rupture member.
5. The actuator according to claim 4 , wherein the weakened area is a thinned area of the retaining part.
6. The actuator according to claim 1 , wherein the coupling mechanism comprises an elastic return member capable of biasing the movable disk toward the disengaged position.
7. The actuator according to claim 1 , wherein the movable gear and the output ring each comprise a toothing, and the movable disk comprises a toothing capable of coming simultaneously into engagement with the toothing of the movable gear and of the output ring.
8. The actuator according to claim 7 , wherein the toothing of the movable gear, of the output ring and of the movable disk have a geometry such that the application of a torque between the movable gear and the output ring produces a separating force which biases the movable disk toward the disengaged position.
9. The actuator according to claim 1 , wherein the movable gear comprises a first gear portion and a second gear portion, the coupling mechanism comprising a first movable disk and a second movable disk, the first movable disk being in engagement with the first portion of the movable gear and the output ring so as to make the ring secured to the first portion of the movable gear when the first disk is in the engaged position, and the second movable disk being in engagement with the second portion of the movable gear and the output ring so as to make the ring secured to the second portion of the movable gear when the second disk is in the engaged position.
10. The actuator according to claim 9 , wherein the retaining part is capable of retaining the first disk and the second disk in the engaged position, the rupture of the retaining part allowing disengagement of the output ring, of the first portion of the movable gear and of the second portion of the movable gear.
11. The actuator according to claim 1 , further comprising:
an input shaft capable of being driven in rotation by a motor along the axis of rotation,
a planet carrier,
a plurality of planet gears, each planet gear being rotatably mounted on the planet carrier and being capable of meshing on the one hand with the input shaft and on the other hand with the fixed gear and the movable gear,
wherein the fixed gear and the movable gear have a different number of teeth from one another so that rotation of the input shaft with respect to the fixed gear drives rotation of the movable gear with respect to the fixed gear.
12. An assembly for actuating an aircraft flight control surface comprising an actuator conforming to claim 11 and the motor capable of driving the input shaft in rotation.