IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
UP-0236345
(2008-09-23)
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등록번호 |
US-7775120
(2010-09-06)
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발명자
/ 주소 |
- Owens, Kevin Eugene
- Blome, Robert Jay
- Benson, Dwayne M.
- Forrest, Steven Talbert
- Quitmeyer, James Neil
- McDowell, Hugh Scott
|
출원인 / 주소 |
- Honeywell International Inc.
|
대리인 / 주소 |
Ingrassia Fisher & Lorenz, P.C.
|
인용정보 |
피인용 횟수 :
1 인용 특허 :
18 |
초록
▼
An electromechanical actuator test system includes an inertia simulator, a first load actuator, a second load actuator, and a test system control. The inertia simulator simulates the inertia of at least a portion of a system that is moved by a test actuator. The first load actuator supplies a first
An electromechanical actuator test system includes an inertia simulator, a first load actuator, a second load actuator, and a test system control. The inertia simulator simulates the inertia of at least a portion of a system that is moved by a test actuator. The first load actuator supplies a first load to the inertia simulator to simulate at least one or more dynamic system loads, and the second load actuator supplies a second load to the inertia simulator to simulate at least one or more steady-state system loads. The test system control supplies the first actuator commands and the second actuator commands.
대표청구항
▼
What is claimed is: 1. An electromechanical actuator test system, comprising: an inertia simulator adapted to be coupled to a test actuator and configured to simulate the inertia of at least a portion of a system moved by the test actuator; an electromechanical actuator coupled to the inertia simul
What is claimed is: 1. An electromechanical actuator test system, comprising: an inertia simulator adapted to be coupled to a test actuator and configured to simulate the inertia of at least a portion of a system moved by the test actuator; an electromechanical actuator coupled to the inertia simulator and operable to be selectively energized, the electromechanical actuator operable, upon being energized, to supply a first load to the inertia simulator to simulate at least one or more dynamic system loads; a motor controller in operable communication with the electromechanical actuator, the motor controller coupled to receive first actuator commands and operable, in response thereto, to selectively energize the electromechanical actuator; a second load actuator coupled to the inertia simulator, the second load actuator coupled to receive second actuator commands and operable, in response thereto, to supply a second load to the inertia simulator to simulate at least one or more steady-state system loads; and a test system control operable to supply the first actuator commands and the second actuator commands. 2. The system of claim 1, further comprising: a command generator operable to at least selectively supply test actuator commands to a test actuator. 3. The system of claim 2, wherein the command generator is adapted to receive input commands and is operable, in response thereto, to at least selectively supply the test actuator commands. 4. The system of claim 1, wherein the inertia simulator comprises: a rotationally disposed element including a mass mounted on an end thereof 5. The system of claim 1, wherein the electromechanical actuator comprises: a linear motor operable to be selectively energized and, upon being energized to supply a drive force; and a force transfer member coupled to receive the drive force from the linear motor and operable, upon receipt thereof, to supply the first load to the inertia simulator. 6. The system of claim 1, wherein the second load actuator comprises: a fluid-operated actuator responsive to control fluid to supply the second load to the inertia simulator; and a control valve in operable communication with the test system control, the control valve responsive to the second actuator commands to control the supply of control fluid to the fluid-operated actuator. 7. The system of claim 6, wherein the fluid-operated actuator comprises a pneumatic actuator. 8. The system of claim 1, further comprising: a sensor coupled to the inertia simulator, the sensor operable to sense the first and second loads and supply a load signal representative thereof to the test system control. 9. The system of claim 8, wherein the test system control is coupled to receive the load signal from the sensor and is responsive thereto to supply the first actuator commands and the second actuator commands. 10. An electromechanical actuator test system, comprising: an inertia simulator adapted to be coupled to a plurality of test actuators and configured to simulate the inertia of at least a portion of a system moved by the test actuators; a first axis first load actuator coupled to the inertia simulator, the first axis first load actuator coupled to receive first axis first actuator commands and operable, in response thereto, to supply a first load to the inertia simulator along a first axis; a first axis second load actuator coupled to the inertia simulator, the first axis second load actuator coupled to receive first axis second actuator commands and operable, in response thereto, to supply a second load to the inertia simulator along the first axis; a second axis first load actuator coupled to the inertia simulator, the second axis first load actuator coupled to receive second axis first actuator commands and operable, in response thereto, to supply a third load to the inertia simulator along a second axis, the second axis perpendicular to the first axis; a second axis second load actuator coupled to the inertia simulator, the second axis second load actuator coupled to receive second axis second actuator commands and operable, in response thereto, to supply a fourth load to the inertia simulator along the second axis; and a test system control operable to supply the first axis first and second actuator commands and the second axis first and second actuator commands. 11. The system of claim 10, further comprising: a command generator adapted to receive input commands and operable, in response thereto, to at least selectively supply test actuator commands to a plurality of test actuators. 12. The system of claim 10, wherein the first and second axis first load actuators each comprise: an electromechanical actuator operable to be selectively energized and, upon being energized, to supply a load to the inertia simulator; and a motor controller in operable communication with the test system control and the electromechanical actuator, the motor controller responsive to actuator commands to selectively energize the electromechanical actuator. 13. The system of claim 12, wherein each of the electromechanical actuators comprises: a linear motor operable to be selectively energized and ,upon being energized to supply a drive force; and a force transfer member coupled to receive the drive force from the linear motor and operable, upon receipt thereof, to supply the first load to the inertia simulator. 14. The system of claim 10, wherein the inertia simulator comprises: a gimbal element including a mass mounted on an end thereof 15. The system of claim 10, wherein the first and second axis second load actuators each comprise: a fluid-operated actuator responsive to control fluid to supply the second load to the inertia simulator; and a control valve in operable communication with the test system control, the control valve responsive to the second actuator commands to control the supply of control fluid to the fluid-operated actuator. 16. The system of claim 10, further comprising: a first axis sensor coupled to the inertia simulator, the first sensor operable to sense the first and second loads and supply a load signal representative thereof to the test system control; and a second axis sensor coupled to the inertia simulator, the second axis sensor operable to sense the third and fourth loads and supply a load signal representative thereof to the test system control. 17. The system of claim 16, wherein the test system control is coupled to receive the load signals from the first and second axis sensors and is responsive thereto to supply the first axis first and second actuator commands and the second axis first and second actuator commands. 18. The system of claim 10, further comprising: a support structure having mounted thereon at least the inertia simulator, the first axis first load actuator, the first axis second actuator, the second axis first load actuator, and the second axis second actuator; and a plurality of test actuator supports mounted on the support structure, each test actuator support adapted to couple to a test actuator, each test actuator support further adapted to adjust at least a back stiffness supplied thereby to a test actuator. 19. An electromechanical actuator test system, comprising: an inertia simulator adapted to be coupled to a test actuator and configured to simulate the inertia of at least a portion of a system moved by the test actuator; a first load actuator coupled to the inertia simulator, the first load actuator coupled to receive first actuator commands and operable, in response thereto, to supply a first load to the inertia simulator to simulate at least one or more dynamic system loads; a fluid-operated actuator coupled to the inertia simulator and responsive to control fluid to supply a second load to the inertia simulator to simulate at least one or more steady-state system loads; a control valve coupled to receive second actuator commands and operable, in response thereto, to control the supply of control fluid to the fluid-operated actuator; and a test system control operable to supply the first actuator commands and the second actuator commands. 20. The system of claim 19, wherein the first load actuator comprises: an electromechanical actuator operable to be selectively energized and, upon being energized, to supply the first load to the inertia simulator; and a motor controller in operable communication with the test system control and the electromechanical actuator, the motor controller responsive to the first actuator commands to selectively energize the electromechanical actuator.
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