Variable turbine nozzle and valve
원문보기
IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
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출원번호 |
US-0762424
(2010-04-19)
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등록번호 |
US-8657568
(2014-02-25)
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발명자
/ 주소 |
- McAuliffe, Christopher
- Dehais, John M.
- Beers, Craig M.
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출원인 / 주소 |
- Hamilton Sundstrand Corporation
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대리인 / 주소 |
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인용정보 |
피인용 횟수 :
1 인용 특허 :
9 |
초록
▼
An air cycle machine includes a turbine wheel, a turbine inlet nozzle, a valve body, and a poppet member. The turbine wheel is mounted to rotate within the air cycle machine and the turbine inlet nozzle is positioned to direct airflow thereto. The poppet member selectively extends into the turbine i
An air cycle machine includes a turbine wheel, a turbine inlet nozzle, a valve body, and a poppet member. The turbine wheel is mounted to rotate within the air cycle machine and the turbine inlet nozzle is positioned to direct airflow thereto. The poppet member selectively extends into the turbine inlet nozzle and the valve body controls a pressure on the poppet member to move the poppet member relative to the turbine inlet nozzle to vary the size of the turbine nozzle directing airflow to the turbine wheel.
대표청구항
▼
1. An air cycle machine, comprising: a turbine wheel mounted to rotate within the air cycle machine;a turbine inlet nozzle in fluid communication with the turbine wheel to direct airflow thereto;a poppet member that selectively extends into the turbine inlet nozzle, the poppet member having a genera
1. An air cycle machine, comprising: a turbine wheel mounted to rotate within the air cycle machine;a turbine inlet nozzle in fluid communication with the turbine wheel to direct airflow thereto;a poppet member that selectively extends into the turbine inlet nozzle, the poppet member having a generally s-shaped cross-section; anda valve body that controls a pressure on the poppet member to move the poppet member relative to the turbine inlet nozzle to vary the size of the turbine inlet nozzle directing airflow to the turbine wheel. 2. The air cycle machine of claim 1, wherein the pressure comprises one of a turbine inlet pressure or an ambient pressure on the air cycle machine. 3. The air cycle machine of claim 1, wherein the air cycle machine has a cavity that is in fluid communication with the valve body. 4. The air cycle machine of claim 3, wherein the valve body selectively communicates air to the cavity from either a turbine inlet or a source external to the air cycle machine. 5. The air cycle machine of claim 3, wherein the poppet member is disposed within the cavity and selectively extends therefrom into the turbine inlet nozzle. 6. The air cycle machine of claim 5, wherein the air cycle machine has a second cavity that communicates with the turbine inlet nozzle immediately adjacent the turbine wheel. 7. The air cycle machine of claim 6, wherein the second cavity is defined by the poppet member and a shroud and the second cavity is maintained at a static pressure during operation. 8. The air cycle machine of claim 3, wherein the poppet member selectively extends from the cavity into the turbine inlet nozzle to contact an arcuate plate that is fixed to and divides the turbine inlet nozzle into at least two sections. 9. The air cycle machine of claim 8, wherein the poppet member and the arcuate plate restrict the airflow to a section of the turbine inlet nozzle when the cavity is a first pressure and the poppet member contacts the arcuate plate. 10. The air cycle machine of claim 8, wherein the arcuate plate and poppet member do not restrict a substantial portion of the airflow in the turbine nozzle when the cavity is a second pressure and the poppet member is not in contact with the arcuate plate. 11. An environmental control system, comprising: an air cycle machine having a compressor wheel and a turbine wheel mounted on a common shaft for rotation therewith, the air cycle machine including a poppet member disposed adjacent the turbine wheel, the poppet member including a first member extending towards a turbine nozzle inlet, the first member in contact with a first seal, a second member extending away from the turbine nozzle inlet, the second member in contact with a second seal, and a third member connecting a first end of the first member and a first end of the second member, the third member being outside the turbine nozzle inlet, and a valve body that controls a pressure on the poppet member to vary an amount of airflow to the turbine wheel. 12. The environmental control system of claim 11, wherein the pressure comprises one of a turbine inlet pressure or an ambient pressure external to the environmental control system. 13. The environmental control system of claim 11, wherein the air cycle machine has a cavity that is in fluid communication with the valve body. 14. The environmental control system of claim 13, wherein the valve body selectively communicates air to the cavity from either a turbine inlet or a source external to the environmental control system. 15. The environmental control system of claim 13, wherein the poppet member is disposed within the cavity and selectively extends therefrom into a turbine inlet nozzle adjacent the turbine wheel. 16. The environmental control system of claim 15, wherein the air cycle machine has a second cavity that communicates with the turbine inlet nozzle immediately adjacent the turbine wheel. 17. The environmental control system of claim 16, wherein the second cavity is defined by the poppet member and a shroud and the second cavity is maintained at a static pressure during operation. 18. The environmental control system of claim 15, wherein the poppet member selectively extends from the cavity into the turbine inlet nozzle to contact an arcuate plate that is fixed to and divides the turbine inlet nozzle into at least two sections. 19. The environmental control system of claim 18, wherein the poppet member and the arcuate plate restrict the airflow to a section of the turbine inlet nozzle when the cavity is a first pressure and the poppet member contacts the arcuate plate. 20. The environmental control system of claim 18, wherein the arcuate plate and poppet member do not restrict a substantial portion of the airflow in the turbine nozzle when the cavity is a second pressure and the poppet member is not in contact with the arcuate plate.
이 특허에 인용된 특허 (9)
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Sauterleute, Alfred; Schlagenhaft, Engelbert, Air conditioning system for airplanes.
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Merritt Brent J. (Westfield MA) Dziorny Paul J. (Manchester CT), Air cycle machine with heat isolation having back-to-back turbine and compressor rotors.
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Army ; Jr. Donald E. ; McAuliffe Christopher ; Greenberg Michael D., Integral bypass valves and air cycle machine.
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McAuliffe Christopher (Windsor CT) Maher ; Jr. John F. (Enfield CT), Turbine bypass working fluid admission.
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Trommer William C. (Rockford IL) Nohr Gary D. (Rockford IL), Turbine nozzle phasing device.
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Zollinger, Brent D.; Rayner, Patrick A.; Slupski, Kevin P., Variable geometry assembly for turbochargers.
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Lutz, Ernst; Spuler, Juerg, Variable geometry turbine.
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Arnold, Steven Don, Variable geometry turbocharger.
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Rannenberg George C. (Canton CT), Variable geometry turbosupercharger system for internal combustion engine.
이 특허를 인용한 특허 (1)
-
Hunt, Jason B., Method and system for varying the width of a turbine nozzle.
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