[특허]Compressor with controllable recirculation and method therefor

Honeywell International Inc.

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특허 상세정보

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Compressor with controllable recirculation and method therefor

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F04D-029/66
미국특허분류(USC)	415/056.5; 415/057.1
출원번호	US-0628687 (2004-06-07)
등록번호	US-8287232 (2012-10-16)
국제출원번호	PCT/US2004/017819 (2004-06-07)
§371/§102 date	20080109 (20080109)
국제공개번호	WO2005/121559 (2005-12-22)
발명자 / 주소	Gu, Ronglei Yashiro, Masahiko
출원인 / 주소	Honeywell International Inc.
대리인 / 주소	Alston & Bird LLP
인용정보	피인용 횟수 : 10 인용 특허 : 1

초록
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There is provided a compressor (10) and an associated method for controlling a recirculation flow to control surging in the compressor. The compressor includes a housing (12) and a compressor wheel (16) mounted therein. A recirculation passage (41) receives compressed air from the compressor and recirculates the compressed air to an inlet passage (20) of the housing and, in particular, to leading edges (32) of blades (18) of the compressor wheel. An adjustable flow control device (60) is configured to control the flow of the compressed air through the re...

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1. A centrifugal compressor configured to provide a flow of recirculated air for surge control, the compressor comprising: a housing defining an axial inlet passage, a radial diffuser passage, an exit, and at least one injection port, each injection port extending to an outlet on an inner surface of the inlet passage;a compressor wheel defining a plurality of blades, each blade having a leading edge adjacent the inlet passage and a trailing edge adjacent the diffuser passage, the compressor wheel rotatably mounted in the housing such that the compressor wheel is configured to receive air flowing generally axially in the inlet passage at the leading edges of the blades and deliver the air from the trailing edges of the blades in a generally radial direction to the exit, the leading edges being configured proximate the outlet of the injection port;a recirculation passage fluidly connected to the exit and configured to receive a flow of compressed air from the compressor wheel and deliver the compressed air through the injection port to the leading edges of the blades of the compressor wheel; andan adjustable flow control device configured to control the flow of the compressed air through the recirculation passage to the injection port to thereby control a surge characteristic of the compressor, wherein the flow control device includes first and second valves in a fluidly parallel configuration, each of the valves being independently controllable between open and closed positions for controlling a respective flow of compressed air through each valve, such that the flow control device is configured to provide at least three different rates of flow of the compressed air to the at least one injection port, and wherein the flow control device is configured to combine the two flows of compressed air downstream of the valves and upstream of the at least one injection port. 2. A centrifugal compressor according to claim 1 wherein the first and second valves are configured to provide dissimilar rates of flow in the open configuration such that the control device is configured to provide at least four different rates of flow of the compressed air to the injection port. 3. A centrifugal compressor according to claim 1 wherein the flow control device comprises an electromagnetic actuator for each valve, configured to adjust the valve such that the flow of the compressed air to the injection port can be adjusted electronically. 4. A centrifugal compressor according to claim 1, further comprising an electronic controller configured to detect an operating parameter of an internal combustion engine and control the flow of the compressed air to the injection port according the operating parameter. 5. A centrifugal compressor according to claim 1 wherein the housing comprises an inlet duct defining a least a portion of the inner surface of the housing, wherein the inlet duct defines a circumferential chamber fluidly connecting the recirculation passage to the injection port. 6. A centrifugal compressor according to claim 1 wherein each injection port extends generally radially inward to the outlet. 7. A centrifugal compressor according to claim 6 wherein the housing defines a plurality of injection ports. 8. A centrifugal compressor according to claim 1 wherein each injection port is a bore. 9. A centrifugal compressor according to claim 1 wherein each injection port is disposed at an acute angle relative to the axial direction and directed toward the compressor wheel. 10. A centrifugal compressor according to claim 1 wherein the injection port is a slot extending circumferentially in the housing. 11. A centrifugal compressor according to claim 1 wherein the housing comprises a unitary body portion defining the at least one injection port and at least partially defining the inlet passage and the diffuser passage. 12. A centrifugal compressor according to claim 1 wherein the housing comprises first and second connected body portions, the first body portion defining the at least one injection port and the second body portion at least partially defining at least one of the group consisting of the inlet passage and the diffuser passage. 13. A centrifugal compressor according to claim 1 wherein each outlet is disposed proximate radially outer tips of the leading edges of the blades such that each injection port is configured to inject the compressed air into the inlet passage at a location proximate the radially outer tips of the leading edges. 14. A method for controlling a recirculation flow in a compressor, the method comprising: providing a rotatable compressor wheel in a housing defining an axial inlet passage and a radial diffuser passage;rotating a compressor wheel having a plurality of blades in a compressor housing such that the compressor wheel receives air flowing generally axially in the inlet passage at leading edges of the blades and delivers the air from trailing edges of the blades in a generally radial direction to the diffuser passage;recirculating a flow of the compressed air from the compressor wheel to the inlet passage of the compressor through at least one outlet proximate the leading edges of the blades of the compressor wheel, wherein said recirculating step comprises recirculating the flow of the compressed air through a flow control device comprising first and second valves in a fluidly parallel configuration, each valve having a flow of compressed air therethrough, and wherein the flow control device combines the two flows of compressed air downstream of the valves and upstream of the inlet passage; andadjusting the flow of the compressed air to thereby control a surge characteristic of the compressor, said adjusting step comprising selectively adjusting each of the first and second valves between open and closed positions. 15. A method according to claim 14 wherein said adjusting step comprises adjusting each valve with an electric actuator during operation of the compressor. 16. A method according to claim 14 wherein said adjusting step comprises selectively adjusting the flow of the compressed air according to an operating parameter of a combustion engine configured to receive compressed air from the compressor. 17. A method according to claim 16 wherein said adjusting step comprises adjusting the flow according to a speed of the combustion engine. 18. A method according to claim 14 wherein the recirculating step comprises injecting the flow of recirculated air through a chamber extending around the inlet passage of the compressor and from the chamber to the inlet passage via at least one injection port extending from the chamber to the outlet. 19. A method according to claim 14 wherein said recirculating step comprises injecting the recirculated air to the inlet passage in a generally radial direction. 20. A method according to claim 14 wherein said recirculating step comprises injecting the recirculated air to the inlet passage in a direction defining an acute angle relative to the inlet passage and directed toward the compressor wheel. 21. A method according to claim 14 wherein said recirculating step comprises injecting the recirculated air to the inlet passage through at least one bore. 22. A method according to claim 14 wherein said recirculating step comprises injecting the recirculated air to the inlet passage through a slot extending circumferentially around the inlet passage. 23. A method according to claim 14 wherein said providing step comprises forming the housing of a unitary body portion defining the at least one outlet and at least partially defining the inlet passage and the diffuser passage. 24. A method according to claim 14 wherein said providing step comprises forming the housing of at least two connected body portions, the first body portion defining the outlet and the second body portion at least partially defining at least one of the group consisting of the inlet passage and the diffuser passage. 25. A method according to claim 14 wherein said recirculating step comprises injecting the compressed air into the inlet passage at a location proximate radially outer tips of the leading edges of the blades.

이 특허에 인용된 특허 (1)

Grainger John K. (Liverpool GB2) Flaxington David (Formby GB2). Compressors. USP1992125173021.

이 특허를 인용한 특허 피인용횟수: 10

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Compressor with controllable recirculation and method therefor

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Compressor with controllable recirculation and method therefor

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