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A hybrid actuator assembly includes an actuator housing, an electromechanical actuator, and a hydraulic actuator. The electromechanical actuator is disposed at least partially within the actuator housing and is adapted to be controllably energized. The electromechanical actuator is configured, upon

A hybrid actuator assembly includes an actuator housing, an electromechanical actuator, and a hydraulic actuator. The electromechanical actuator is disposed at least partially within the actuator housing and is adapted to be controllably energized. The electromechanical actuator is configured, upon being controllably energized, to supply a first drive force. The hydraulic actuator is disposed at least partially within the actuator housing and is adapted to receive pressurized hydraulic fluid. The hydraulic actuator is configured, upon receipt of pressurized hydraulic fluid, to supply a second drive force.

대표청구항 ▼

1. An actuator assembly, comprising: an actuation element adapted to receive an actuation drive force;an electromechanical actuator adapted to be controllably energized and configured, upon being controllably energized, to supply a first drive force;a hydraulic actuator connected to the electromecha

1. An actuator assembly, comprising: an actuation element adapted to receive an actuation drive force;an electromechanical actuator adapted to be controllably energized and configured, upon being controllably energized, to supply a first drive force;a hydraulic actuator connected to the electromechanical actuator and adapted to receive pressurized hydraulic fluid, the hydraulic actuator configured, upon receipt of pressurized hydraulic fluid, to supply a second drive force;a link having a first end and a second end, the link rotationally connected to the electromechanical actuator at a position between the link first and second ends to receive the first drive force therefrom, the link first end rotationally connected to the hydraulic actuator to receive the second drive force therefrom, the link second end rotationally connected to the actuation element to supply the actuation drive force to the actuation element upon receipt, by the link, of the first drive force or the second drive force. 2. The assembly of claim 1, further comprising: an actuator housing that at least partially houses both the electromechanical actuator and the hydraulic actuator. 3. The assembly of claim 1, wherein the electromechanical actuator comprises: an electric motor adapted to be controllably energized and configured, upon being controllably energized, to supply a drive torque;an actuation mechanism coupled to receive the drive torque from the motor and configured, upon receipt thereof, to translate and supply the first drive force. 4. The assembly of claim 3, wherein the electromechanical actuator further comprises: a position sensor configured to sense actuation mechanism position and supply a position signal representative thereof. 5. The assembly of claim 3, wherein the electric motor comprises a brushless DC machine. 6. The assembly of claim 3, wherein the actuation element comprises a ballscrew-type actuator. 7. The assembly of claim 1, wherein the hydraulic actuator comprises: an actuation element adapted to selectively receive pressurized hydraulic fluid and configured, upon receipt thereof, to translate and supply the second drive force; anda directional control valve adapted to be controllably energized and configured, upon being controllably energized, to direct pressurized hydraulic fluid to the actuation element. 8. The assembly of claim 7, wherein the hydraulic actuator further comprises: a position sensor configured to sense actuation mechanism position and supply a position signal representative thereof. 9. The assembly of claim 7, wherein the actuation element comprises a piston-type actuator. 10. A flight control surface actuation system, comprising: an actuation element adapted to couple to a flight control surface and to receive an actuation drive force, the actuation element responsive to the actuation drive force to move the flight control surface to a commanded position;an electromechanical actuator adapted to be controllably energized and configured, upon being controllably energized, to supply a first drive force;a hydraulic actuator connected to the electromechanical actuator and adapted to receive pressurized hydraulic fluid, the hydraulic actuator configured, upon receipt of pressurized hydraulic fluid, to supply a second drive force;a link having a first end and a second end, the link rotationally connected to the electromechanical actuator at a position between the link first and second ends to receive the first drive force therefrom, the link first end rotationally connected to the hydraulic actuator to receive the second drive force therefrom, the link second end rotationally connected to the actuation element to supply the actuation drive force to the actuation element upon receipt, by the link, of the first drive force or the second drive force; andan actuator controller adapted to receive actuator position commands and operable, in response thereto, to controllably energize the electromechanical actuator or controllably direct pressurized hydraulic fluid to the hydraulic actuator. 11. The system of claim 10, comprising: an actuator housing that at least partially houses both the electromechanical actuator and the hydraulic actuator. 12. The system of claim 10, wherein the electromechanical actuator comprises: an electric motor adapted to be controllably energized by the actuator controller and configured, upon being controllably energized, to supply a drive torque;an actuation mechanism coupled to receive the drive torque from the motor and configured, upon receipt thereof, to translate and supply the first drive force; anda position sensor configured to sense actuation mechanism position and supply a position signal representative thereof to the actuator controller. 13. The system of claim 12, wherein the actuation element comprises a ballscrew-type actuator. 14. The system of claim 10, comprising: a bidirectional hydraulic pump adapted to be controllably energized and operable, in response thereto, to supply the pressurized hydraulic fluid to the hydraulic actuator. 15. The system of claim 14, wherein the hydraulic actuator comprises: an actuation element adapted to selectively the receive pressurized hydraulic fluid and configured, upon receipt thereof, to translate and supply the second drive force;a directional control valve in fluid communication with the bidirectional hydraulic pump, the directional control valve coupled to be controllably energized by the actuator controller and configured, upon being controllably energized, to direct pressurized hydraulic fluid to the actuation element; anda position sensor configured to sense actuation mechanism position and supply a position signal representative thereof to the actuator controller. 16. The system of claim 15, wherein the actuation element comprises a piston-type actuator.