Active clearance control for a centrifugal compressor

• US 8,087,880 B2
• Filed: 12/03/2008
• Issued: 01/03/2012
• Est. Priority Date: 12/03/2008
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Karafillis, Apostolos Pavlos, Loehle, Kenneth Allen, Tameo, Robert Patrick, Gutz, David Allen
• Primary Examiner(s): Blum, David S
• Application Number:
  US12/327,266
• Publication Number:
  US 20110002774A1
• Time in Patent Office: 1,126 Days
• Field of Search: 415/1, 415/118, 415/127, 415/174.1
• US Class Current: 415/118
• CPC Class Codes: F01D 11/22 by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
• CPC Class Codes: F04D 27/0246 by varying geometry within the pumps, e.g. by adjusting vanes
• CPC Class Codes: F04D 29/162 of a centrifugal flow wheel
• CPC Class Codes: F04D 29/4206 especially adapted for elastic fluid pumps
• CPC Class Codes: F04D 29/622 Adjusting the clearances between rotary and stationary parts
• CPC Class Codes: F05D 2270/301 Pressure

Abstract

Apparatus and method of operating a centrifugal compressor and active control system includes a centrifugal compressor with compressor blades mounted on an impeller, an annular cavity bounded in part by a shroud adjacent to the blades, and an active control system for controlling a clearance between the shroud and the blades by controlling a cavity pressure in the cavity. An electronic controller for controlling a control pressure valve for pressurizing using a source of compressor discharge pressure air and depressurizing the cavity respectively may open and close the valves using pulse width modulation. Pressure and clearance sensors positioned for measuring the cavity pressure the blade tip clearance respectively in signal supply communication with the electronic controller may be used. The shroud may be supported by radially spaced apart annular radially outer and inner supports connected to a casing by a bolted joint bounding the cavity.

Claims

1. A gas turbine engine centrifugal compressor and active control system assembly comprising:

a centrifugal compressor having a plurality of centrifugal compressor blades mounted on an annular centrifugal compressor impeller,

an annular blade tip shroud adjacent to blade tips of the blades,

a substantially sealed annular cavity bounded in part by the annular blade tip shroud, and

an active control system for controlling an annular blade tip clearance between the annular blade tip shroud and the blade tips by controlling a cavity pressure in the cavity.

2. An assembly as claimed in claim 1, further comprising valving controlled by an electronic controller for pressurizing and depressurizing the cavity.

3. An assembly as claimed in claim 2, further comprising the valving operably connected to a source of compressor discharge pressure air for pressurizing the cavity.

4. An assembly as claimed in claim 3, further comprising the valving including a control pressure valve for pressurizing the cavity and depressurizing the cavity.

5. An assembly as claimed in claim 4, further comprising the control pressure valve being connected to the cavity, the source of compressor discharge pressure air, and a vent line.

6. An assembly as claimed in claim 4, further comprising an electronic controller controllably connected to the control pressure valve.

7. An assembly as claimed in claim 6, further comprising the electronic controller being operable for pulsing a solenoid of the control pressure valve many times a second for rapidly cycling the control pressure valve between open and closed states of the control pressure valve.

8. An assembly as claimed in claim 7, further comprising the electronic controller being operable for controlling the pulsing of the solenoid using pulse width modulation.

9. An assembly as claimed in claim 2, further comprising:

one or more pressure sensors positioned for measuring the cavity pressure,

one or more clearance sensors positioned for measuring the blade tip clearance, and

the pressure and clearance sensors in signal supply communication with the electronic controller.

10. An assembly as claimed in claim 9, further comprising the valving operably connected to a source of compressor discharge pressure air for pressurizing the cavity.

11. An assembly as claimed in claim 10, further comprising the valving including a control pressure valve for pressurizing and depressurizing the cavity.

12. An assembly as claimed in claim 11, further comprising the control pressure valve being connected to the cavity, the source of compressor discharge pressure air, and a vent line.

13. An assembly as claimed in claim 11, further comprising an electronic controller controllably connected to the control pressure valve.

14. An assembly as claimed in claim 13, further comprising the electronic controller being operable for pulsing a solenoid of the control pressure valve many times a second for rapidly cycling the control pressure valve between open and closed states of the control pressure valve.

15. An assembly as claimed in claim 14, further comprising the electronic controller being operable for controlling the pulsing of the solenoid using pulse width modulation.

16. An assembly as claimed in claim 1, further comprising:

the shroud being supported by radially spaced apart annular impeller shroud radially outer and inner supports connected to a casing,

the cavity being bounded by the outer and inner supports and the annular blade tip shroud, and

the radially outer and inner supports attached to radially outer and inner ends of the shroud respectively.

17. An assembly as claimed in claim 16, further comprising the radially outer and inner supports connected to the casing by a bolted joint.

18. An assembly as claimed in claim 17, further comprising axial stop pads extending radially outwardly from the radially outer end of and distributed circumferentially about the shroud the stop pads.

19. An assembly as claimed in claim 17, further comprising valving controlled by an electronic controller for pressurizing and depressurizing the cavity.

20. An assembly as claimed in claim 19, further comprising the valving operably connected to a source of compressor discharge pressure air for pressurizing the cavity.

21. An assembly as claimed in claim 20, further comprising the valving including a control pressure valve for pressurizing and depressurizing the cavity.

22. An assembly as claimed in claim 21, further comprising the control pressure valve being connected to the cavity, the source of compressor discharge pressure air, and a vent line.

23. An assembly as claimed in claim 21, further comprising an electronic controller controllably connected to the control and blow off pressure valves.

24. An assembly as claimed in claim 23, further comprising the electronic controller being operable for pulsing a solenoid of the control pressure valve many times a second for rapidly cycling the valves between open and closed states of the control pressure valve.

25. An assembly as claimed in claim 24, further comprising the electronic controller being operable for controlling the pulsing of the solenoid using pulse width modulation.

26. An assembly as claimed in claim 19, further comprising:

one or more pressure sensors positioned for measuring the cavity pressure,

one or more clearance sensors positioned for measuring the blade tip clearance, and

the pressure and clearance sensors in signal supply communication with the electronic controller.

27. An assembly as claimed in claim 26, further comprising the valving operably connected to a source of compressor discharge pressure air for pressurizing the cavity.

28. An assembly as claimed in claim 27, further comprising the valving including a control pressure valve for pressurizing and depressurizing the cavity.

29. An assembly as claimed in claim 28, further comprising the control pressure valve being connected to the cavity, the source of compressor discharge pressure air, and a vent line.

30. An assembly as claimed in claim 28, further comprising an electronic controller controllably connected to the control pressure valve.

31. An assembly as claimed in claim 30, further comprising the electronic controller being operable for pulsing a solenoid of the control pressure valve many times a second for rapidly cycling the valves between open and closed states of the control pressure valve.

32. An assembly as claimed in claim 31, further comprising the electronic controller being operable for controlling the pulsing of the solenoid using pulse width modulation.

33. An assembly as claimed in claim 3, further comprising the valving including a control pressure valve for pressurizing the cavity and a blow off pressure valve for depressurizing the cavity.

34. An assembly as claimed in claim 33, further comprising the control and blow off pressure valves being inline and connected to a pressure line extending between the cavity and the source of compressor discharge pressure air.

35. An assembly as claimed in claim 34, further comprising an electronic controller controllably connected to the control and blow off pressure valves.

36. An assembly as claimed in claim 35, further comprising the electronic controller being operable for pulsing solenoids of the control and blow off pressure valves many times a second for rapidly cycling the valves between open and closed states.

37. An assembly as claimed in claim 36, further comprising the electronic controller being operable for controlling the pulsing of the solenoids using pulse width modulation.

38. An assembly as claimed in claim 37, further comprising:

one or more pressure sensors positioned for measuring the cavity pressure,

one or more clearance sensors positioned for measuring the blade tip clearance, and

the pressure and clearance sensors in signal supply communication with the electronic controller.

39. An assembly as claimed in claim 33, further comprising:

the shroud being supported by radially spaced apart annular impeller shroud radially outer and inner supports connected to a casing,

the cavity being bounded by the outer and inner supports and the annular blade tip shroud, and

the radially outer and inner supports attached to radially outer and inner ends of the shroud respectively.

40. An assembly as claimed in claim 39, further comprising the radially outer and inner supports connected to the casing by a bolted joint.

41. An assembly as claimed in claim 40, further comprising axial stop pads extending radially outwardly from the radially outer end of and distributed circumferentially about the shroud the stop pads.

42. An assembly as claimed in claim 40, further comprising valving controlled by an electronic controller for pressurizing and depressurizing the cavity.

43. An assembly as claimed in claim 42, further comprising the valving including a control pressure valve connected to a source of compressor discharge pressure air for pressurizing the cavity and a blow off pressure valve for depressurizing the cavity.

44. An assembly as claimed in claim 43, further comprising an electronic controller controllably connected to the control and blow off pressure valves.

45. An assembly as claimed in claim 44, further comprising the electronic controller being operable for pulsing solenoids of the control and blow off pressure valves many times a second for rapidly cycling the valves between open and closed states.

46. An assembly as claimed in claim 45, further comprising the electronic controller being operable for controlling the pulsing of the solenoids using pulse width modulation.

47. A method for controlling an annular blade tip clearance between an annular blade tip shroud and adjacent blade tips mounted on an annular centrifugal compressor impeller of a gas turbine engine centrifugal compressor and active control system, the method comprising controlling a cavity pressure in a cavity bounded in part by the annular blade tip shroud.

48. A method as claimed in claim 47 further comprising using valving connected to a source of compressor discharge pressure air for increasing the cavity pressure in the cavity.

49. A method as claimed in claim 48, further comprising using a control pressure valve for the increasing and the decreasing of the cavity pressure in the cavity.

50. A method as claimed in claim 49, further comprising using an electronic controller for controlling the control pressure valve for the controlling of the cavity pressure.

51. A method as claimed in claim 50, further comprising opening the control pressure valve for pressurizing the cavity with the source of compressor discharge pressure and venting the control pressure valve for depressurizing the cavity with a pressure sink.

52. A method as claimed in claim 51, further comprising pulsing a solenoid in the control pressure valve for opening and closing the control pressure valve many times a second for rapidly cycling the control pressure valve between open and closed states of the control pressure valve for the controlling of the cavity pressure.

53. A method as claimed in claim 52, further comprising using pulse width modulation for the pulsing of the solenoid.

54. A method as claimed in claim 50, further comprising:

measuring the cavity pressure using one or more pressure sensors positioned for measuring the cavity pressure and in signal supply communication with the electronic controller,

measuring the blade tip clearance using one or more clearance sensors positioned for measuring the blade tip clearance and in signal supply communication with the electronic controller, and

using output from the pressure and clearance sensors to the electronic controller for further controlling the control pressure valve for the controlling of the cavity pressure.

55. A method as claimed in claim 54, further comprising opening the control pressure valve for pressurizing the cavity with the source of compressor discharge pressure and venting the control pressure valve for depressurizing the cavity with a pressure sink.

56. A method as claimed in claim 55, further comprising pulsing a solenoid in the control pressure valve for opening and closing the control pressure valve many times a second for rapidly cycling the control pressure valve between open and closed states of the control pressure valve for the controlling of the cavity pressure.

57. A method as claimed in claim 56, further comprising using pulse width modulation for the pulsing of the solenoid.