Method and apparatus for detecting and compensating for compressor surge in a gas turbine using remote monitoring and diagnostics

• US 6,438,484 B1
• Filed: 05/23/2001
• Issued: 08/20/2002
• Est. Priority Date: 05/23/2001
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Yeung, Chung-hei Simon, Hill, James Michael, Andrew, Philip Lynn, Stampfli, John David, Schirle, Steven Mark, Cotroneo, Joseph Anthony
• Primary Examiner(s): NGUYEN, TAN QUANG
• Application Number:
  US09/863,021
• Time in Patent Office: 454 Days
• Field of Search: 701/100, 415/118, 415/57.4, 415/55.2, 415/55.7, 415/55.1, 340/966, 416/26
• US Class Current: 701/100
• CPC Class Codes: F04D 27/02 Surge control surge detection F04D27/001
• CPC Class Codes: F05D 2270/101 Compressor surge or stall

Abstract

A method is disclosed for monitoring and controlling a compressor including (a) monitoring at least one compressor parameter; (b) storing data indicative of the monitored parameter in a database system; (c) processing the collected data using a stall precursor detection algorithm to determine a stall precursor; (d) comparing the stall precursor with at least one of a corresponding average compressor value, and a corresponding unit specific value to determine the level of compressor operability, and (e) if the stall precursor varies from at least one of the average compressor value and the unit specific value, performing corrective actions to vary the level of compressor operability to prevent a surge condition.

Claims

1. A method for monitoring and controlling a compressor, comprising:

(a) monitoring at least one compressor parameter;

(i) storing data indicative of the monitored parameter in a database system;

(b) processing the collected data using a stall precursor detection algorithm to determine a stall precursor;

(c) comparing the stall precursor with at least one of a corresponding average compressor value, and a corresponding unit specific value to determine the level of compressor operability, and

(d) if the stall precursor varies from at least one of said average compressor value and said unit specific value, performing corrective actions to vary the level of compressor operability to prevent a surge condition.

2. The method of claim 1 further comprising step (e) of iterating steps (a) to (d) until the monitored at least one compressor parameter is within predetermined thresholds.

3. The method of claim 1, wherein step (b) further comprising:

(i) computing a stall precursor signal magnitude to generate stall precursor characteristic; and

(ii) storing stall precursor characteristic data in said database system.

4. The method of claim 1, wherein step (d) further comprises:

(i) increasing the output of the compressor if the level of operation of the compressor is superior to at least one of said average value and said unit specific characteristic; and

(ii) lowering the output of the compressor if the level of operation of the compressor is inferior to at least one of said average value and said unit specific characteristic.

5. The method of claim 4, wherein said output is varied by varying the operating line parameters.

6. The method of claim 5, wherein said output is varied by varying the compressor loading.

7. The method of claim 5, wherein said operating line parameters are set to a near-threshold value.

8. The method of claim 1 wherein the storage of data and database system are remote from the compressor.

9. An apparatus for monitoring a compressor, comprising:

at least one sensor operatively coupled to the compressor for monitoring at least one compressor parameter;

a processor system for computing stall precursors from the monitored data;

a database system for storing said at least one compressor parameter and said computed stall precursors, said database system further comprising a look-up-table comprising average compressor values for similar compressors;

a comparator for comparing the computed stall precursors with at least one of an average precursor value and a previously computed stall measure of the compressor; and

a control system for initiating corrective actions to prevent a compressor surge if the computed stall precursors deviate from at least one of said average precursor value and said previously computed stall measure.

10. The apparatus of claim 9, wherein the corrective actions are initiated by varying operating limit line parameters.

11. The apparatus of claim 9, wherein said operating limit line parameters are set to a near-threshold value.

12. The apparatus of claim 9, wherein the compressor is in a gas turbine.

13. In a gas turbine of the type having a compressor, a combustor, and a turbine, a method for monitoring the compressor comprising:

(a) monitoring at least one compressor parameter and collecting data indicative of the compressor parameter;

(b) processing the monitored data using a stall precursor detection algorithm to determine a stall precursor;

(c) comparing the stall precursor with at least one of a corresponding average compressor value, and a corresponding unit specific value to determine the level of compressor operability, and

(d) if the stall precursor varies from at least one of said average compressor value and said unit specific value, performing corrective actions to vary the level of compressor operability to prevent a surge condition.

14. The method of claim 13 further comprising step (e) of iterating steps (a) to (d) until the monitored at least one compressor parameter is within predetermined thresholds.

15. The method of claim 13, wherein step (b) further comprising:

(i) computing a stall precursor signal magnitude to generate stall precursor characteristic; and

(ii) storing stall precursor characteristic data.

16. The method of claim 13, wherein step (d) further comprises:

(i) increasing the output of the compressor if the level of operation of the compressor is superior to at least one of said average value and said unit specific characteristic; and

(ii) lowering the output of the compressor if the level of operation of the compressor is inferior to at least one of said average value and said unit specific characteristic.

17. The method of claim 16, wherein said output is varied by varying the operating line parameters.

18. The method of claim 17, wherein said output is varied by varying the compressor loading.

19. The method of claim 17, wherein said operating line parameters are set to a near-threshold value.

20. An apparatus for monitoring and controlling a compressor, comprising:

means for monitoring at least one compressor parameter;

means for computing stall measures;

means for comparing the stall measures with at least one of an average stall measure of similar compressors or a previously computed stall measure for the compressor; and

means for initiating corrective actions if the computed stall measure deviates from at least one of said average stall measure or said previously computed stall measure.

21. The apparatus of claim 20, wherein the corrective actions are initiated by varying operating limit line parameters.

22. The apparatus of claim 21, wherein said operating limit line parameters are set to a near-threshold value.

23. A method for detecting and compensating for a compressor surge in a gas turbine of the type having a compressor, comprising:

remotely monitoring at least one compressor parameter;

computing stall measures;

comparing the stall measures with at least one of an average stall measure of similar compressors or a previously computed stall measure for the compressor; and

initiating corrective actions if the computed stall measure deviates from at least one of said average stall measure or said previously computed stall measure.

24. A method for remotely monitoring and controlling a compressor to prevent a compressor surge condition, the method comprising:

(a) monitoring at least one compressor parameter and storing data indicative of the monitored parameter in a remote database system;

(b) processing the monitored data using a stall precursor detection algorithm to determine a stall precursor;

(c) comparing the stall precursor with at least one of a corresponding average compressor value, and a corresponding unit specific value to determine the level of compressor operability, and

(d) if the stall precursor varies from at least one of said average compressor value and said unit specific value, performing corrective actions to vary the level of compressor operability to prevent a surge condition.

25. The method of claim 24 further comprising step (e) of iterating steps (a) to (d) until the monitored at least one compressor parameter is within predetermined thresholds.

26. The method of claim 24, wherein step (b) further comprising:

(i) remotely computing a stall precursor signal magnitude to generate stall precursor characteristic; and

(ii) storing stall precursor characteristic data in said remote database system.