Flow control method and means

• US 5,340,271 A
• Filed: 01/14/1993
• Issued: 08/23/1994
• Est. Priority Date: 08/18/1990
• Status: Expired due to Term

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Wright, William B., Day, Ivor J., Freeman, Christopher
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): VERDIER, CHRISTOPHER M
• Application Number:
  US07/960,367
• Time in Patent Office: 586 Days
• Field of Search: 415/1, 415/17, 415/26-29, 415/47, 415/49, 415/51, 415/58.4, 415/58.5, 415/58.7, 415/116, 415/117, 415/118, 415/119, 60/39.091, 60/39.29
• US Class Current: 415/1
• CPC Class Codes: F04D 27/001 Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
• CPC Class Codes: F04D 27/0215 Arrangements therefor, e.g. bleed or by-pass valves
• CPC Class Codes: F04D 27/0238 Details or means for fluid reinjection
• CPC Class Codes: F05D 2270/101 Compressor surge or stall

Abstract

The method controls gas flow in an axial flow compressor in which the flow at one or more chosen station in the direction of flow through the compressor is sensed at a series of circumferentially spaced positions. Flow variations above a predetermined limit are evaluated to initiate a response if a disturbance above a predetermined acceptable level is detected. When such a disturbance is detected, higher pressure gas bled from downstream is injected at a station to supplement the main gas flow. An incipient rotating stall cell will appear as a variation occurring sequentially at the circumferentially spaced positions. By responding to such a condition with a pressure injection, it is found possible to suppress both rotating stall and surge conditions in the compressor before this disturbance develops fully. The same method can be arranged to counter steady state distortion.

Claims

1. A method of controlling gas flow in a compressor comprising the steps of sensing the flow at a series of circumferentially spaced positions at a chosen axial station in a direction of flow through the compressor to detect variations in the flow above a predetermined limit of variation and, upon at least one of the variations being detected, injecting higher-pressure gas from a region downstream of said chosen station into the flow through the compressor upstream of said region generally in said direction of flow and in a circumferentially selective manner dependent upon the circumferential origins of said variations, to act against flow disturbances indicated by said variations.

2. A method according to claim 1 wherein action is taken to terminate said injection after a fixed period.

3. A method according to claim 1 wherein the injection is tapered off after initiation.

4. A method according to claim 1 wherein the injection is shut off after a predetermined time.

5. A method according to claim 1, wherein flow variations above said predetermined limit are detected at one of a plurality of stations spaced from each other in the flow direction and said injection of higher-pressure gas is initiated adjacent said one station in response to said detection.

6. A method according to claim 5 wherein, flow variations are sensed at least a first station adjacent the entry of the compressor and at a second station intermediate the flow path through the compressor and higher-pressure gas is injected to act against flow variations detected at each said station, the higher-pressure gas for the first station being bled from adjacent said second station and the higher-pressure gas for the second station being bled from downstream of the second station.

7. A method according to claim 1 wherein the injection is performed in a series of different sectors around a circumference of the compressor, and the flow is independently sensed in each of said sectors.

8. A method according to claim 7 wherein the higher pressure gas is taken from the same sector as that into which it is injected.

9. A method according to claim 1 wherein a sensed signal of said variations at each said spaced position at the station is averaged over a rolling period corresponding to the sensing of the flow at least at three circumferentially successive locations to give a series of means values, from which a flow disturbance is detected.

10. A method according to claim 9 wherein a difference signal is formed between the sensed signal and the mean signal, a measure of a relative magnitude of the difference signal is obtained, and a detection of the relative magnitude above a predetermined level of the difference signal from each of a plurality of the sensing positions is arranged to produce an operative output for actuating the injection.

11. A method according to claim 1 wherein actuation of the injection is arranged to operate on sensing sequentially, for at least some of said circumferentially spaced positions of the station, the flow variations above the predetermined limit.

12. A method according to claim 1 wherein said direction of injection is at a radial angle not substantially more than 30°

.

13. A method according to claim 1 for controlling flow in an axial compressor in which said direction of injection has a circumferential component in opposition to a direction of rotation of the compressor rotor.

14. A method according to claim 1 wherein said limit of flow variation is not substantially less than 2% of a mean flow value sensed.

15. A method according to claim 1, wherein flow variations above said predetermined limit are detected at one of a plurality of stations spaced from each other in the flow direction and said injection of higher-pressure gas is initiated a substantial distance upstream of said station in response to said detection.

16. A method of controlling gas flow in a compressor comprising the steps of sensing the flow at a series of circumferentially spaced positions at a chosen axial station in the direction of flow through the compressor to detect variations in the flow above a predetermined limit of variation, the sensing of said variations at a series of said positions in circumferential sequence actuating the injection of gas at a higher pressure than that prevailing at said station to act against a flow disturbance indicated by said variations, and performing the gas injection in a series of different sectors around the compressor, said injection being generally in said direction of flow through the compressor and the flow being independently sensed in each of said sectors.

17. A method of controlling gas flow in a compressor comprising the steps of sensing the flow at a series of circumferentially spaced positions to detect a variation in the flow in one circumferential region relative to another and, upon the variation being detected injecting, generally in the direction of flow through the compressor, higher-pressure gas from a region downstream of said series of circumferentially spaced positions toward a circumferential region in which said variation has been detected.

18. Apparatus for controlling gas flow in a compressor comprising flow sensing means for a series of circumferentially spaced positions at a chosen axial station in a direction of flow through the compressor, means for detecting from signals from the sensing means at the individual positions flow variations above a predetermined limit of variation, means for injecting gas at a higher pressure than that prevailing at said station and generally in the direction of flow, means for actuating said injection means in response to the sensing of said variations at a series of said positions in circumferential sequence thereby to act against a flow disturbance indicated by said variations.

19. Apparatus for controlling gas flow in compressor comprising sensing means for sensing variations in flow at a series of circumferentially spaced positions at a chosen axial station in a direction of main flow through the compressor, means for tapping higher-pressure gas from a region downstream of said chosen station, means for injecting said higher-pressure gas into the compressor generally in said direction of flow, to act against a flow disturbance indicated by said variations, and control means for controlling said injection, the sensing means actuating said injection through said control means in a circumferentially selective manner dependent upon the circumferential origins of said variations.

20. Apparatus according to claim 19 wherein said sensing means are provided at a plurality of stations spaced from each other in the flow direction and said injection means are provided one of at and adjacent said stations, the control means being arranged to initiate said injection in response to the direction of said flow variations at said station.

21. Apparatus according to claim 19 comprising a first station adjacent the entry to the compressor and a second station intermediate the flow path trough it, first injection means one of at and adjacent said first station, second injection means a substantial distance upstream of said second station, first conduit means for connecting said first injection means to the main compressor flow downstream of the first station and second conduit means for the injection to said second station having means for connecting said second injection means to the main compressor flow downstream of said second station.

22. Apparatus according to claim 21 wherein a common valve means is provided to selectively block said injection and either of said conduit means.

23. Apparatus according to claim 19 wherein the flow control means is biased to a normally closed position.

24. Apparatus according to claim 19 wherein there are tapping means and injection means for each of a plurality of different sectors of the compressor, and there are sensing means for each of said sectors, control means actuable by the sensing means being operable for injection into each of said sectors.

25. Apparatus according to claim 24 wherein there are at least six said sectors.

26. Apparatus according to claim 19 wherein the injection means comprises outlets directed at a radial angle of not substantially more than 30°

.

27. Apparatus according to claim 26 wherein said outlets comprise nozzles in which a projecting portion at each nozzle exit deflects the injection in a downstream direction.

28. Apparatus according to claim 19 wherein said control means comprises at least one semirotary valve comprising a cylindrical stator and a cylindrical rotor in close sliding fit with said stator, the stator and rotor each having a series of circumferentially spaced openings that are brought into and out of registration by rotation of the rotor to open and close the valve.

29. Apparatus according to claim 28 wherein electromagnetic drive means determine the end positions of the rotary movement of the rotor.

30. Apparatus according to claim 19 comprising means for one of reducing and stopping said injection in a predetermined time period.

31. Apparatus according to claim 19 wherein the control means comprises means for averaging the signal sensed at each said spaced position over a rolling period corresponding to the sensing of the flow at least at three circumferentially successive locations to give a series of mean values from which a flow disturbance is detected.

32. Apparatus according to claim 31 comprising means for forming a difference signal between the instantaneous sensed signal and the mean signal, means for measuring the relative magnitude of said difference signal and output means for producing an actuating signal for the injection upon detection of a relative magnitude above a predetermined level from each of a plurality of the sensing positions.

33. An apparatus according to claim 19, wherein said sensing means are provided at a plurality of stations spaced from each other in the flow direction and said injection means are provided a substantial distance upstream of one of said stations, the control means being arranged to initiate said injection in response to the detection of said flow variations at said one station.