Method and apparatus for detecting rub in a turbomachine

• US 7,409,319 B2
• Filed: 11/24/2003
• Issued: 08/05/2008
• Est. Priority Date: 11/24/2003
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Badami, Vivek Venugopal, Kumar, Jitendra, Kant, Abhay Sudhakarrao, Giannakopoulos, Nicholas, Dimond, Mark M., Toth, Joseph Robert
• Primary Examiner(s): Lau; Tung S
• Application Number:
  US10/720,817
• Publication Number:
  US 20050114082A1
• Time in Patent Office: 1,716 Days
• Field of Search: 702/188, 702/38, 702/183, 324/207, 324/511, 621/41, 340/635, 340/647, 340/683, 340/679, 340/682, 208/157, 735/87, 735/93, 735/94
• US Class Current: 702/188
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: F01D 21/12 responsive to temperature
• CPC Class Codes: F01D 21/14 responsive to other specific conditions
• CPC Class Codes: F01D 21/20 Checking operation of shut-down devices

Abstract

An embodiment of the disclosed method and apparatus relates to a system for detecting a rub in a turbomachine. The system includes a turbomachine; sensors monitoring turbomachine conditions; and an on site monitor in communication with the sensors, and loaded with instructions to implement a method for detecting a rub in the turbomachine.

Claims

1. A system for detecting a rub in a turbomachine comprising;

a turbomachine comprising a rotor, a stator, and a plurality of blades extending radially from the rotor, or the stator, or a combination thereof;

sensors configured to monitor turbomachine conditions; and

an on site-monitor in communication with the sensors, wherein the on-site monitor is configured to analyze the turbomachine conditions to identify abnormal behavior indicative of a rub in at least near real time in the turbomachine between tip portions of the plurality of blades and corresponding seal portions of the turbomachine;

wherein the abnormal behavior comprises a high vibration amplitude relative to a baseline, or a high variation in vibration amplitude, or a sudden change in vibration amplitude, or a combination thereof.

2. The system of claim 1 further comprising a server in communication with the on site monitor via an internet.

3. The system of claim 1, wherein the plurality of blades is disposed on the rotor and the corresponding seal portions are disposed on the stator.

4. The system of claim 1, wherein the turbomachine conditions comprise bearing vibration, temperature, pressure, eccentricity, axial displacement, load, and condenser pressure values.

5. The system of claim 1, wherein the abnormal behavior comprises a sudden change in vibration values during steady speed operation, axial noisiness during coast down of the turbomachine, abnormal eccentricity value when the turbomachine returns to turning gear after a rub event during deceleration, abnormal vibration during start up followed by abnormal eccentricity when the turbomachine was on turning gear, abnormal vibration followed by abnormal upper and lower shell metal temperature difference, high vibration response to first critical speed, high vibration response to second critical speed, overall vibration affected by variation in load, overall vibration affected by variation in condenser pressure, or abnormal vibration during abnormal differential expansion of the stator and the rotor, or a combination thereof.

6. The system of claim 1, wherein the abnormal behavior comprises a sudden change in vibration amplitude.

7. A computer implemented method for detecting a rub in a turbomachine, the method comprising:

monitoring turbomachine conditions, wherein the turbomachine comprises a rotor, a stator, and a plurality of blades extending radially from the rotor, or the stator, or a combination thereof;

determining whether a rub is occurring between tip portions of the plurality of blades and corresponding seal portions of the turbomachine based at least in part on a high variation in vibration amplitude, or a sudden change in vibration amplitude, or a combination thereof; and

outputting an indication of the rub to a computer display.

8. The system of claim 7, wherein the blades are disposed on the rotor, or the stator, or any combination thereof and the seals are disposed on the rotor, or the stator, or any combination thereof.

9. The system of claim 7, wherein the turbomachine conditions comprise bearing vibration, temperature, and pressure.

10. A storage medium encoded with a machine-readable computer program code for detecting whether a rub is occurring in a turbomachine, the storage medium including instructions for causing a computer to implement a method comprising:

obtaining data indicating turbomachine conditions, wherein the turbomachine comprises a rotor, a stator, and a plurality of blades extending radially from the rotor, or the stator, or a combination thereof;

determining whether a rub is occurring between tip portions of the plurality of blades and corresponding seal portions of the turbomachine in at least near real time based at least in part on an abnormal vibration relative to a historical trend, wherein the abnormal vibration comprises a sudden change in vibration amplitude; and

outputting an indication of the rub to a computer display.

11. The system of claim 10, wherein the plurality of blades is disposed on the rotor and the corresponding seal portions are disposed on the stator.

12. The system of claim 10, wherein the turbomachine conditions comprise bearing vibration, or temperature, or axial displacement, or load, or condenser pressure values, or any combination thereof.

13. A system, comprising:

a turbomachine comprising a rotor, a stator, and a plurality of blades extending radially from the rotor, or the stator, or a combination thereof;

means for monitoring turbomachine conditions; and

means for detecting whether a rub is occurring in the turbomachine between tip portions of the plurality of blades and corresponding seal portions of the turbomachine in at least near real time based on an abnormal vibration value, an abnormal eccentricity value, an abnormal response to a transient condition, an abnormal response to a variation in load, an abnormal response to a variation in pressure, or an abnormal differential expansion of the stator and the rotor, or a combination thereof.

14. The system of claim 13, wherein the plurality of blades is disposed on the rotor and the corresponding seal portions are disposed on the stator.

15. The system of claim 13, wherein the turbomachine conditions comprise temperature, eccentricity, load, and condenser pressure values.

16. A system, comprising:

a plurality of turbomachine sensors configured to couple to a turbomachine comprising a rotor, a stator, and a plurality of blades extending radially from the rotor, or the stator, or a combination thereof, wherein the plurality of turbomachine sensors is configured to sense operational parameters of the turbomachine; and

a rub detection system configured to monitor the plurality of turbomachine sensors and to detect a turbomachine rub event occurring between tip portions of the plurality of blades and corresponding seal portions of the turbomachine based on one or more abnormal conditions, wherein the abnormal conditions comprise an abnormal vibration value, an abnormal eccentricity value, an abnormal response to a transient condition, an abnormal response to a variation in load, an abnormal response to a variation in pressure, and an abnormal differential expansion of the stator and the rotor.

17. The system of claim 16, wherein the plurality of blades is disposed on the rotor and the corresponding seal portions are disposed on the stator.

18. The system of claim 16, wherein the rub detection system is configured to monitor in real time.

19. A system, comprising:

a rub detection system configured to monitor operational parameters of a turbomachine comprising a rotor, a stator, and a plurality of blades extending radially from the rotor, or the stator, or a combination thereof, wherein the rub detection system is configured to detect a turbomachine rub event occurring between tip portions of the plurality of blades and corresponding seal portions of the turbomachine based on one or more abnormal conditions, wherein the abnormal conditions comprise a high vibration amplitude relative to a baseline, a high variation in vibration amplitude, and a sudden change in vibration amplitude.

20. The system of claim 19, comprising a turbomachine, wherein the rub detection system is coupled to the turbomachine.

21. The system of claim 19, wherein the plurality of blades is disposed on the rotor and the corresponding seal portions are disposed on the stator.

22. The system of claim 19, wherein the operational parameters comprise eccentricity, or axial displacement, or load, or condenser pressure values, or any combination thereof.

23. The system of claim 19, wherein rub detection system is configured to monitor in real time.

24. A computer implemented method, comprising:

analyzing turbomachine operational data to detect a rub event based on one or more abnormal conditions in the turbomachine, wherein the turbomachine comprises a rotor, a stator, and a plurality of blades extending radially from the rotor, or the stator, or a combination thereof, the rub event occurs between tip portions of the plurality of blades and corresponding seal portions of the turbomachine, and the one or more abnormal conditions comprise a high vibration amplitude, a high variation in vibration amplitude, a sudden change in vibration amplitude, an abnormal eccentricity value, an abnormal response to a transient condition, an abnormal response to a variation in load, an abnormal response to a variation in pressure, and an abnormal differential expansion of the stator and the rotor, and a combination thereof; and

outputting an indication of the rub event to a computer display.

25. The method of claim 24, comprising monitoring a turbomachine to obtain the operational data.

26. The method of claim 24, wherein analyzing comprises detecting the rub event in real time with operation of a turbomachine.

27. The method of claim 24, wherein the plurality of blades is disposed on the rotor and the corresponding seal portions are disposed on the stator.

28. The method of claim 25, wherein monitoring comprises monitoring the turbomachine on-site.

29. The method of claim 25, wherein monitoring comprises monitoring the operational data in real time.

30. A system, comprising:

a turbomachine monitor configured to identify abnormal operational events as an indication of a rub in at least near real time between components of a turbomachine, wherein the abnormal operational events comprise an abnormal vibration value relative to a baseline.

31. The system of claim 30, wherein the abnormal operational events comprise a high vibration amplitude, a high variation in vibration amplitude, a sudden change in vibration amplitude, or a combination thereof.

32. The system of claim 30, wherein the abnormal operational events comprise an abnormal eccentricity amplitude and/or abnormal eccentricity change during turning of a component of the turbomachine.

33. The system of claim 30, wherein the abnormal operational events comprise abnormal behavior during the transient condition of a start up or a shut down of the turbomachine.

34. The system of claim 30, wherein the abnormal operational events comprise an abnormal load amplitude and/or abnormal load change associated with the turbomachine.

35. The system of claim 30, wherein the abnormal operational events comprise an abnormal pressure amplitude and/or abnormal pressure change associated with the turbomachine.

36. The system of claim 30, wherein the abnormal operational events comprise an abnormal amplitude and/or an abnormal change in a property of steam in the turbomachine.

37. The system of claim 30, wherein the abnormal operational events comprise the abnormal differential expansion of a stator and a rotor of the turbomachine.

38. The system of claim 30, wherein the abnormal operational events comprise the abnormal vibration value, the abnormal eccentricity value, the abnormal behavior associated with the transient condition, the abnormal behavior associated with the variation in load, the abnormal behavior associated with the variation in pressure, the abnormal steam characteristic of the turbomachine, and the abnormal differential expansion, each individually and in combinations with one another.

39. The system of claim 30, comprising the turbomachine having a plurality of sensors communicative with the turbomachine monitor.

40. The system of claim 30, wherein the turbomachine monitor is configured to monitor for the rub in at least near real time.

41. The system of claim 30, wherein the abnormal operational events comprise an abnormal eccentricity value, an abnormal behavior associated with a transient condition, an abnormal behavior associated with a variation in load, an abnormal behavior associated with a variation in pressure, an abnormal steam characteristic of the turbomachine, an abnormal differential expansion, or a combination thereof.

42. The system of claim 39, wherein the turbomachine comprises a rotor, a stator, and a plurality of blades extending radially from the rotor, or the stator, or a combination thereof, wherein the turbomachine monitor is configured to monitor the possibility of the rub between tip portions of the plurality of blades and corresponding seal portions of the turbomachine.

43. A system, comprising:

a turbomachine monitor configured to identify abnormal operational events as an indication of a rub between components of a turbomachine, wherein the abnormal operational events comprise a sudden change in vibration relative to a first baseline, a large variance in vibration relative to a second baseline, or a large vibration amplitude relative to a third baseline, or a combination thereof.

44. The system of claim 43, comprising the turbomachine having a plurality of sensors communicative with the turbomachine monitor.

45. The system of claim 43, wherein the turbomachine monitor is configured to monitor for the rub in at least near real time.

46. The system of claim 43, wherein the first, second, and third baselines are based on past data.

47. The system of claim 44, wherein the turbomachine comprises a rotor, a stator, and a plurality of blades extending radially from the rotor, or the stator, or a combination thereof, wherein the turbomachine monitor is configured to monitor the possibility of the rub between tip portions of the plurality of blades and corresponding seal portions of the turbomachine.

48. A system, comprising:

a turbomachine monitor configured to monitor for abnormal operational events to identify a possible rub between components of a turbomachine in at least near real time, wherein the abnormal operational events comprise a sudden change relative to a first baseline, or a high variation relative to a second baseline, or a high value relative to a third baseline, or a combination thereof, of an operational parameter of the turbomachine, wherein the operational parameter comprises vibration amplitude.

49. The system of claim 48, wherein the abnormal operational events comprise an abnormal eccentricity value, an abnormal behavior associated with a transient condition, an abnormal behavior associated with a variation in load, an abnormal behavior associated with a variation in pressure, an abnormal steam characteristic of the turbomachine, or an abnormal differential expansion, or a combination thereof.

50. The system of claim 48, wherein the abnormal operational events comprise an abnormal eccentricity value, an abnormal behavior associated with a transient condition, an abnormal behavior associated with a variation in load, an abnormal behavior associated with a variation in pressure, an abnormal steam characteristic of the turbomachine, and an abnormal differential expansion, each individually and in combinations with one another.

51. The system of claim 48, wherein the abnormal operational events comprise an abnormal eccentricity amplitude and/or abnormal eccentricity change during turning of a component of the turbomachine.

52. The system of claim 48, wherein the abnormal operational events comprise abnormal behavior during the transient condition of a start up or a shut down of the turbomachine.

53. The system of claim 48, wherein the abnormal operational events comprise an abnormal load amplitude and/or abnormal load change associated with the turbomachine.

54. The system of claim 48, wherein the abnormal operational events comprise an abnormal pressure amplitude and/or abnormal pressure change associated with the turbomachine.

55. The system of claim 48, wherein the abnormal operational events comprise an abnormal amplitude and/or an abnormal change in a property of steam in the turbomachine.

56. The system of claim 48, wherein the abnormal operational events comprise the abnormal differential expansion of a stator and a rotor of the turbomachine.

57. The system of claim 48, comprising the turbomachine having a plurality of sensors communicative with the turbomachine monitor.

58. The system of claim 57, wherein the turbomachine comprises a rotor, a stator, and a plurality of blades extending radially from the rotor, or the stator, or a combination thereof, wherein the turbomachine monitor is configured to monitor for the possible rub between tip portions of the plurality of blades and corresponding seal portions of the turbomachine.