Fuel metering valve assembly including thermal compensation mechanism
IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
UP-0923343
(2007-10-24)
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등록번호 |
US-7784487
(2010-09-20)
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발명자
/ 주소 |
|
출원인 / 주소 |
- Honeywell International Inc.
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대리인 / 주소 |
Ingrassia Fisher & Lorenz, P.C.
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인용정보 |
피인용 횟수 :
4 인용 특허 :
3 |
초록
▼
A metering valve assembly is provided for metering a fluid. The metering valve assembly includes a position sensor, metering valve, and a thermal compensation mechanism. The metering valve includes a valve housing having a flow passage therethrough, and a valve element movably mounted within the val
A metering valve assembly is provided for metering a fluid. The metering valve assembly includes a position sensor, metering valve, and a thermal compensation mechanism. The metering valve includes a valve housing having a flow passage therethrough, and a valve element movably mounted within the valve housing. The thermal compensation mechanism is coupled between the position sensor and the valve element and configured to adjust the displacement of the position sensor relative to the valve element as a function of fluid temperature.
대표청구항
▼
What is claimed is: 1. A metering valve assembly for metering fuel and for use in conjunction with a valve actuator, a controller operably coupled to the valve actuator, and an aircraft engine combustor, the metering valve assembly comprising: a position sensor configured to be operably coupled to
What is claimed is: 1. A metering valve assembly for metering fuel and for use in conjunction with a valve actuator, a controller operably coupled to the valve actuator, and an aircraft engine combustor, the metering valve assembly comprising: a position sensor configured to be operably coupled to the controller; a metering valve, comprising: a valve housing having a flow passage therethrough configured to be fluidly coupled to the aircraft engine combustor; and a valve element movably mounted within the valve housing and configured to be moved axially by the valve actuator in accordance with commands received from the controller to provide the aircraft engine combustor with a metered fuel supply; and a thermal compensation mechanism coupled between the position sensor and the valve element, the thermal compensation mechanism configured to adjust the displacement of the position sensor relative to the valve element as a function of fluid temperature. 2. A metering valve assembly according to claim 1 wherein the thermal compensation mechanism increases the displacement of the position sensor relative to the valve element as fluid density decreases over an operative temperature range. 3. A metering valve assembly according to claim 1 wherein the position sensor comprises: a sensor body coupled to the valve housing; and a sensor input movably coupled to the sensor body and fixedly coupled to the thermal compensation mechanism. 4. A metering valve assembly according to claim 3 wherein the position sensor is a linear variable differential transducer. 5. A metering valve assembly according to claim 1 wherein the thermal compensation mechanism maintains a displacement gap between the position sensor and the valve element, the thermal compensation mechanism configured to adjust the width of the displacement gap in relation to changes in fluid temperature. 6. A metering valve assembly according to claim 5 wherein the thermal compensation mechanism is configured to increase the width of the displacement gap in a substantially linear manner as fluid temperature increases over a predetermined temperature range. 7. A metering valve assembly according to claim 6 wherein the predetermined temperature range comprises approximately −46° Celsius to approximately 93° Celsius. 8. A metering valve assembly according to claim 1 wherein the metering valve includes an exponential port. 9. A metering valve assembly according to claim 3 wherein the valve housing comprises a sleeve, and wherein the valve element comprises a piston slidably mounted with the sleeve. 10. A metering valve assembly according to claim 9 wherein the piston is configured to translate along an axis of motion, and wherein the thermal compensation mechanism is configured to adjust the displacement of the sensor input relative to the piston along the axis of motion. 11. A metering valve assembly according to claim 10 wherein the thermal compensation mechanism is configured to expand along the axis of motion as fluid temperature increases. 12. A metering valve assembly according to claim 9 wherein the thermal compensation mechanism is fixedly attached to the sensor input. 13. A metering valve assembly according to claim 1 wherein the thermal compensation mechanism comprises a bi-metallic body. 14. A metering valve assembly according to claim 13 wherein the bi-metallic body comprises a disc. 15. A metering valve assembly for metering a fluid, comprising: a metering valve, comprising: a valve sleeve having a flow passage therethrough; and a valve piston mounted within the valve sleeve and configured to translate therein to control fluid flow through the flow passage, the valve piston configured to move in a first direction from a closed position to an open position; a position sensor, comprising: a sensor body coupled to the valve sleeve; and a sensor input movably coupled to the sensor body; and a thermal compensation mechanism coupled between the sensor input and the valve piston, the thermal compensation mechanism configured to be heated by the fluid and, when so heated, to move the sensor input away from the metering valve piston in a second direction substantially opposite the first direction, and an actuator responsive to sensor input moving the valve piston in an axial direction. 16. A metering valve assembly according to claim 15 wherein the thermal compensation mechanism comprises a bi-metallic disc. 17. A metering valve assembly according to claim 16 wherein the bi-metallic disc is at least partially concave and increases its concavity as fuel temperature rises. 18. A fuel delivery and control system for supplying a metered amount of fuel to an aircraft engine combustor having an engine controller associated therewith, the fuel delivery and control system comprising: a fuel source; a metering valve fluidly coupled between the fuel source and the aircraft engine combustor, the metering valve comprising: a valve housing having a flow passage therethrough; and a valve element movably mounted within the valve housing; a position sensor coupled to the valve element and separated therefrom by a displacement gap, the position sensor further coupled to the engine controller and configured to relate thereto the sensed position of the valve element; a valve actuator coupled to the valve element and to the engine controller, the valve actuator configured to axially adjust the position of the valve element in accordance with command signals received from the engine controller; and a thermal compensation mechanism coupled between the valve element and the position sensor, the thermal compensation mechanism configured to increase the width of the displacement gap as the fuel's temperature increases over an operative temperature range. 19. A fuel delivery and control system according to claim 18 wherein the thermal compensation mechanism is configured to expand, as measured along a first axis, as the fuel's temperature increases. 20. A fuel delivery and control system according to claim 19 wherein the valve element is configured to translate within the valve housing along a second axis, the second axis being substantially parallel with the first axis.
이 특허에 인용된 특허 (3)
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Smith Trevor Stanley,GB2, Flow sensor and fuel control system.
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Dyer Gerald P. (Enfield CT) Donnelly Brian G. (Suffield CT), Fuel control utilizing a multifunction valve.
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Reuter Charles E. ; Gaudet Timothy J., Hydromechanical control for a variable delivery, positive displacement fuel pump.
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Hodinot, Laurent Gilbert Yves; Issert, Celine Marie Anne; Marly, Pascal Laurent, Method and device for feeding a turbomachine combustion chamber with a regulated flow of fuel.
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Richardson, Brandon, System for tire inflation.
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Dimascio, Paul Stephen; Arnett, Michael Douglas; Hefner, Rebecca Evelyn, Thermally-controlled component and thermal control process.
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