Actuator assembly includes a housing assembly, a ball screw, a ball nut, and a lock. The ball screw is rotationally mounted on and extends from the housing assembly, is coupled to receive an actuator drive torque, and is configured, upon receipt thereof, to rotate. The ball nut is rotationally suppo
Actuator assembly includes a housing assembly, a ball screw, a ball nut, and a lock. The ball screw is rotationally mounted on and extends from the housing assembly, is coupled to receive an actuator drive torque, and is configured, upon receipt thereof, to rotate. The ball nut is rotationally supported on the ball screw and is configured, in response to rotation of the ball screw, to translate thereon between a stowed position and a deployed position. The lock is disposed at least partially within the housing assembly and is configured to move between a lock position and an unlock position. The lock prevents the ball nut from translating out of the stowed position when the lock is in the lock position and the ball nut is in the stowed position.
대표청구항▼
1. An actuator assembly, comprising: a housing assembly;a ball screw rotationally mounted on and extending from the housing assembly, the ball screw coupled to receive an actuator drive torque and configured, upon receipt thereof, to rotate;a ball nut rotationally supported on the ball screw and con
1. An actuator assembly, comprising: a housing assembly;a ball screw rotationally mounted on and extending from the housing assembly, the ball screw coupled to receive an actuator drive torque and configured, upon receipt thereof, to rotate;a ball nut rotationally supported on the ball screw and configured, in response to rotation of the ball screw, to translate thereon between a stowed position and a deployed position, the ball nut including a first tapered surface; anda lock disposed at least partially within the housing assembly and configured to move between a lock position and an unlock position,wherein: the lock comprises a main body having an actuation end and an engagement end, the engagement end including a second tapered surface, the main body rotationally mounted on the housing assembly between the actuation end and the engagement end and adapted to receive a lock actuation force on the actuation end, the main body configured, upon receipt of the actuation force, to rotate between the lock and unlock position,the engagement end engages the ball nut and thereby prevents the ball nut from translating out of the stowed position when (i) the lock is in the lock position and (ii) the ball nut is in the stowed position, andthe second tapered surface engages the first tapered surface when the ball nut translates from any deployed position back to the stowed position, and allows the ball nut to translate from any deployed position back to the stowed position even when the lock is in the lock position and without having to first apply the lock actuation force to rotate the lock to the unlock position. 2. The actuator assembly of claim 1, wherein the lock does not prevent the ball nut from translating when the lock is in the unlock position. 3. The actuator assembly of claim 1, wherein the lock further comprises: a lock actuator mounted on the housing assembly and coupled to the main body, the lock actuator configured to supply the lock actuation force to the actuation end of the main body. 4. The actuator assembly of claim 3, wherein the lock actuator comprises: an actuation rod coupled to the actuation end and configured to supply the lock actuation force thereto;a solenoid assembly coupled to the actuation rod and configured, upon being energized, to cause the actuation rod to rotate the main body to the unlock position; anda spring coupled to the solenoid assembly and configured to supply a bias force thereto that urges the actuation rod to rotate the main body to the lock position. 5. The actuator assembly of claim 1, further comprising: a lock position sensor mounted on the housing assembly and configured to sense lock position. 6. An aircraft thrust reverser actuation system, comprising: at least one power source;at least two synchronization mechanisms; andat least two actuators each coupled to at least one of the synchronization mechanisms, at least one of the actuators comprising: a housing assembly;a ball screw rotationally mounted on and extending from the housing assembly, the ball screw coupled to receive an actuator drive torque and configured, upon receipt thereof, to rotate;a ball nut rotationally supported on the ball screw and configured, in response to rotation of the ball screw, to translate thereon between a stowed position and a deployed position, the ball nut including a first tapered surface; anda lock disposed at least partially within the housing assembly and configured to move between a lock position and an unlock position,wherein: the lock comprises a main body having an actuation end and an engagement end, the engagement end including a second tapered surface, the main body rotationally mounted on the housing assembly between the actuation end and the engagement end and adapted to receive a lock actuation force on the actuation end, the main body configured, upon receipt of the actuation force, to rotate between the lock and unlock position,the engagement end engages the ball nut and thereby prevents the ball nut from translating out of the stowed position when (i) the lock is in the lock position and (ii) the ball nut is in the stowed position, andthe second tapered surface engages the first tapered surface when the ball nut translates from any deployed position back to the stowed position, and thereby allows the ball nut to translate from any deployed position back to the stowed position even when the lock is in the lock position and without having to first apply the lock actuation force to rotate the lock to the unlock position. 7. The system of claim 6, wherein the lock does not prevent the ball nut from translating when the lock is in the unlock position. 8. The system of claim 6, wherein: the lock further comprises a lock actuator mounted on the housing assembly and coupled to the main body, the lock actuator configured to supply the lock actuation force to the actuation end of the main body. 9. The system of claim 8, wherein the lock actuator comprises: an actuation rod coupled to the actuation end and configured to supply the lock actuation force thereto;a solenoid assembly coupled to the actuation rod and configured, upon being energized, to cause the actuation rod to rotate the main body to the unlock position; anda spring coupled to the solenoid assembly and configured to supply a bias force thereto that urges the actuation rod to rotate the main body to the lock position. 10. The system of claim 6, further comprising: a lock position sensor mounted on the housing assembly and configured to sense lock position.
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이 특허에 인용된 특허 (13)
Davies, Stephen Harlow; Harvey, John Herbert; Blakemore, Steven; Hill, Edward George, Actuator.
Bristol, Brent L.; Chakkera, Kevin K.; Auer, Peter J.; Neri, Remo N., Bi-directional locking ring assembly for aircraft thrust reverser manual drive unit.
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