Diagnostic method and system for turbine engines

• US 20030045992A1
• Filed: 08/31/2001
• Published: 03/06/2003
• Est. Priority Date: 08/31/2001
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Humerickhouse, Charles Edward, Vorwerk, Ryan Kenneth, Lethander, Charles Eric
• Granted Patent: US 6,687,596 B2
• Time in Patent Office: Days
• US Class Current: 701/100
• CPC Class Codes: F02C 9/00 Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants controlling air intakes F02C7/057; controlling turbines F01D; controlling compressors F04D27/00; controlling in general G05
• CPC Class Codes: F05D 2270/05 to affect the output of the engine
• CPC Class Codes: F05D 2270/309 Rate of change of parameters
• CPC Class Codes: G01M 15/00 Testing of engines
• CPC Class Codes: G01M 15/14 Testing gas-turbine engines or jet-propulsion engines
• CPC Class Codes: G05B 23/0281 Quantitative, e.g. mathematical distance; Clustering; Neural networks; Statistical analysis

Abstract

A method and system for evaluating whether faults detected during the testing of a gas turbine engine are related to the performance problems of the engine or to some other abnormality unrelated to engine performance. One performance parameter of the engine is evaluated under one performance condition to generate a first set of current engine data that is then compared to a first set of prior engine data to determine if there is an abnormality. If one is detected, this performance parameter is then evaluated under at least two different performance conditions to generate a second set of current engine data that is compared to a second set of prior engine data to determine if there is an abnormality. If one is detected, the abnormality is evaluated to see if the fault is unrelated to the performance of the engine. If one is not detected, this performance parameter is evaluated relative to at least one other performance parameter to generate a third set of current engine data that is compared to a third set of prior engine data to determine if there is an abnormality. If one is detected after this comparison of the third set of current to prior engine data, the abnormality is then evaluated to see if it is unrelated to engine performance. If one is not detected, the abnormality is then evaluated to determine if the fault is related to engine performance.

Claims

1. A method for evaluating whether faults detected during the testing of a gas turbine engine are related to engine performance problems or to problems unrelated to engine performance, the method comprising the steps of:

(A) comparing a first set of current engine data to a first set of prior engine data for one performance parameter of the engine under one performance condition to determine if there is an abnormality;

(B) if an abnormality is detected after comparing the first set of current engine data to the first set of prior engine data, comparing a second set of current engine data to a second set of prior engine data for at least two different performance conditions to determine if there is an abnormality;

(C) after comparing the second set of current engine data to the second set of prior engine data to determine if there is an abnormality;

(1) if an abnormality is detected, evaluating whether the abnormality is a fault unrelated to the performance of the engine;

(2) if an abnormality is not detected, comparing a third set of current engine data to a third set of prior engine data for at least one other engine performance parameter under at least one performance condition to determine if there is an abnormality.

2. The method of claim 1 which comprises the further step of:

(D) after comparing the third set of current engine data to the third set of prior engine data to determine if there is an abnormality;

(1) if an abnormality is detected, evaluating whether the abnormality is a fault unrelated to the performance of the engine;

(2) if an abnormality is not detected, evaluating whether the abnormality detected in step (B) is a fault related to performance of the engine.

3. The method of claim 2 wherein the one engine performance parameter in step (A) is exhaust gas temperature, specific fuel consumption, compressor rotor speed, fan rotor speed, engine air flow, cooling flow, bleed flow, leakage flow, thrust at rated power, compression pressure ratio, turbine pressure ratio, fan pressure ratio, engine pressure ration, turbine clearance control, compression temperature ratio, variable stator angle, variable bleed door position, vibration, oil consumption or acceleration time.

4. The method of claim 3 wherein the one engine performance parameter during step (A) is exhaust gas temperature or specific fuel consumption.

5. The method of claim 2 wherein the engine performance condition is an engine power level.

6. A method for evaluating whether faults detected during the testing of a gas turbine engine are related to engine performance problems or to problems unrelated to engine performance, the method comprising the steps of:

(A) evaluating one performance parameter of the engine under one performance condition to generate a first set of current engine data;

(B) comparing the first set of current engine data to a first set of prior engine data for the one performance condition of the one performance parameter to determine if there is an abnormality;

(C) if an abnormality is detected after comparing the first set of current engine data to the first set of prior engine data, evaluating the one performance parameter under at least two different performance conditions to generate a second set of current engine data;

(D) comparing the second set of current engine data to a second set of prior engine data for the at least two different performance conditions of the one performance parameter to determine if there is an abnormality;

(E) after comparing the second set of current engine data to the second set of prior engine data to determine if there is an abnormality;

(1) if an abnormality is detected, evaluating whether the abnormality is a fault unrelated to the performance of the engine;

(2) if an abnormality is not detected, evaluating the one performance parameter relative to at least one other engine performance parameter under at least one performance condition to generate a third set of current engine data;

(F) comparing the third set of current engine data to a third set of prior engine data for the at least one other engine performance parameter under at least one performance condition to determine if there is an abnormality;

(G) after comparing the third set of current engine data to the third set of prior engine data to determine if there is an abnormality;

(1) if an abnormality is detected, evaluating whether the abnormality is a fault unrelated to the performance of the engine;

(2) if an abnormality is not detected, evaluating whether the abnormality detected in step (C) is a fault related to performance of the engine.

7. The method of claim 6 wherein the one engine performance parameter in step (A) is exhaust gas temperature, specific fuel consumption, compressor rotor speed, fan rotor speed, engine air flow, cooling flow, bleed flow, leakage flow, thrust at rated power, compression pressure ratio, turbine pressure ratio, fan pressure ratio, engine pressure ration, turbine clearance control, compression temperature ratio, variable stator angle, variable bleed door position, vibration, oil consumption or acceleration time.

8. The method of claim 7 wherein the one engine performance parameter during step (A) is exhaust gas temperature or specific fuel consumption.

9. The method of claim 7 wherein the engine performance condition is an engine power level.

10. The method of claim 6 wherein step (B) comprises the steps of:

(1) plotting individual values for the first current engine data and the first prior engine data in order of earliest date collected to latest date collected to provide a data plot;

(2) running a statistical analysis on the data plot to determine the center line of the data plot and the statistical control limits below and above the center line.

11. The method of claim 10 wherein step (D) comprises the steps of:

(1) plotting each value of the second set of current and prior engine data at one power level relative to each value of the second set of current and prior engine data at a second power level to provide a second data plot;

(2) carrying out a regression analysis on the second data plot to obtain a center line for the second data plot and to obtain the difference above or below the center line of the second data plot for each value of the second set of current and prior engine data plotted in the second data plot; and

(3) plotting the differences obtained for each value of the second set of current and prior engine data in order from earliest date collected to latest date collected.

12. The method of claim 11 wherein step (E) (1) comprises the steps of:

(i) selecting a different second set of current engine data and a different second set of prior engine data;

(ii) comparing the different second set of current engine data to the different second set of prior engine data to determine if there is an abnormality; and

(iii) after comparing the different second set of current engine data to the different second set of prior engine data;

(a) if an abnormality is still detected, evaluating whether the abnormality is a fault unrelated to the performance of the engine;

(b) if an abnormality is not detected, proceeding to step (F).

13. A computerized system for evaluating whether faults detected during the testing of a gas turbine engine are related to engine performance problems or to problems unrelated to engine performance, the system comprising:

(A) a host computer;

(B) an analyzer workstation in communication with the host computer;

(C) a test cell for carrying out the evaluation of the engine and in communication with the host computer;

(D) software residing on the host computer for controlling access to prior engine data, for permitting electronic communication with the analyzer workstation and the test cell, and for processing data from at least one of the analyzer workstation and the test cell;

(E) software residing on the analyzer workstation for permitting electronic communication between the test cell, the host computer and the analyzer workstation and for transmitting data between at least the host computer and the analyzer workstation;

(F) software associated with the test cell for permitting electronic communication between the test cell, the host computer and the analyzer workstation and for transmitting data from the test cell to at least the host computer;

(G) the system being capable of allowing the analyzer to;

(1) compare a first set of current engine data to a first set of prior engine data for one performance parameter of the engine under one performance condition to determine if there is an abnormality;

(2) if an abnormality is detected after comparing the first set of current engine data to the first set of prior engine data, compare a second set of current engine data to a second set of prior engine data for at least two different performance conditions to determine if there is an abnormality;

(3) after comparing the second set of current engine data to the second set of prior engine data to determine if there is an abnormality;

(a) if an abnormality is detected, evaluate whether the abnormality is a fault unrelated to the performance of the engine;

(b) if an abnormality is not detected, compare a third set of current engine data to a third set of prior engine data for at least one other engine performance parameter under at least one performance condition to determine if there is an abnormality

14. The system of claim 14 which is further capable of allowing the analyzer to:

(4) after comparing the third set of current engine data to the third set of prior engine data to determine if there is an abnormality;

(a) if an abnormality is detected, evaluate whether the abnormality is a fault unrelated to the performance of the engine;

(b) if an abnormality is not detected, evaluate whether the abnormality detected in (1) is a fault related to performance of the engine.

15. The system of claim 14 wherein the one engine performance parameter in (G) (1) is exhaust gas temperature, specific fuel consumption, compressor rotor speed, fan rotor speed, engine air flow, cooling flow, bleed flow, leakage flow, thrust at rated power, compression pressure ratio, turbine pressure ratio, fan pressure ratio, engine pressure ration, turbine clearance control, compression temperature ratio, variable stator angle, variable bleed door position, vibration, oil consumption or acceleration or time.

16. The system of claim 15 wherein the one engine performance parameter during (G) (1) is exhaust gas temperature or specific fuel consumption.

17. The system of claim 15 wherein the engine performance condition is an engine power level.

18. A computerized system for evaluating whether faults detected during the testing of a gas turbine engine are related to engine performance problems or to problems unrelated to engine performance, the system comprising:

(A) a host computer;

(B) an analyzer workstation in communication with the host computer;

(C) a test cell for carrying out the evaluation of the engine and in communication with the host computer;

(D) software residing on the host computer for controlling access to prior engine data, for permitting electronic communication with the analyzer workstation and the test cell, and for processing data from at least one of the analyzer workstation and the test cell;

(E) software residing on the analyzer workstation for permitting electronic communication between the test cell, the host computer and the analyzer workstation and for transmitting data between at least the host computer and the analyzer workstation;

(F) software associated with the test cell for permitting electronic communication between the test cell, the host computer and the analyzer workstation and for transmitting data from the test cell to at least the host computer;

(G) the system being capable of allowing the analyzer to;

(1) evaluate one performance parameter of the engine under one performance condition to generate a first set of current engine data;

(2) compare the first set of current engine data to a first set of prior engine data for the one performance condition of the one performance parameter to determine if there is an abnormality;

(3) if an abnormality is detected after comparing the first set of current engine data to the first set of prior engine data, evaluate the one performance parameter under at least two different performance conditions to generate a second set of current engine data;

(4) compare the second set of current engine data to a second set of prior engine data for the at least two different performance conditions of the one performance parameter to determine if there is an abnormality;

(5) after comparing the second set of current engine data to the second set of prior engine data to determine if there is an abnormality;

(a) if an abnormality is detected, evaluate whether the abnormality is a fault unrelated to the performance of the engine;

(b) if an abnormality is not detected, evaluating the one performance parameter relative to at least one other engine performance parameter under at least one performance condition to generate a third set of current engine data;

(6) comparing the third set of current engine data to a third set of prior engine data for the at least one other engine performance parameter under at least one performance condition to determine if there is an abnormality;

(7) after comparing the third set of current engine data to the third set of prior engine data to determine if there is an abnormality;

(a) if an abnormality is detected, evaluating whether the abnormality is a fault unrelated to the performance of the engine;

(b) if an abnormality is not detected, evaluating whether the abnormality detected in step (2) is a fault related to the performance of the engine.

19. The system of claim 18 wherein the one engine performance parameter in (G) (1) is exhaust gas temperature, specific fuel consumption, compressor rotor speed, fan rotor speed, engine air flow, cooling flow, bleed flow, leakage flow, thrust at rated power, compression pressure ratio, turbine pressure ratio, fan pressure ratio, engine pressure ration, turbine clearance control, compression temperature ratio, variable stator angle, variable bleed door position, vibration, oil consumption or acceleration time.

20. The system of claim 19 wherein the one engine performance parameter during (G) (1) is exhaust gas temperature or specific fuel consumption.

21. The system of claim 19 wherein the engine performance condition is an engine power level.

22. The system of claim 18 wherein the analyzer during (G) (2):

(a) plots individual values for the first current engine data and the first prior engine data in order of earliest date collected to latest date collected to provide a data plot;

(b) runs a statistical analysis on the data plot to determine the center line of the data plot and the statistical control limits below and above the center line.

23. The system of claim 22 wherein the analyzer during (G) (4):

(a) plots each value of the second set of current and prior engine data at one power level relative to each value of the second set of current and prior engine data at a second power level to provide a second data plot;

(b) carrys out a regression analysis on the second data plot to obtain a center line for the second data plot and to obtain the difference above or below the center line of the second data plot for each value of the second set of current and prior engine data plotted in the second data plot; and

(c) plots the differences obtained for each value of the second set of current and prior engine data in order from earliest date collected to latest date collected.

24. The system of claim 23 wherein the analyzer during (G) (5) (a):

(i) selects a different second set of current engine data and a different second set of prior engine data;

(ii) compares the different second set of current engine data to the different second set of prior engine data to determine if there is an abnormality; and

(iii) after comparing the different second set of current engine data to the different second set of prior engine data;

(a) if an abnormality is still detected, evaluates whether the abnormality is a fault unrelated to the performance of the engine;

(b) if an abnormality is not detected, proceeds to (G) (6).

25. Software for use in a computerized system for evaluating whether faults detected during the testing of a gas turbine engine are related to engine performance problems or to problems unrelated to engine performance, the system including a server, an analyzer computer in communication with the server, and a test cell for carrying out the evaluation of the engine and in communication with the server;

the software comprising;

(A) a server software component that can reside on the server that is capable of controlling access to prior engine data, permitting electronic communication between the analyzer computer and the test cell, and processing data from at least one of the analyzer computer and the test cell;

(B) an analyzer software component that can reside on the analyzer computer and is capable of permitting electronic communication between the test cell, the server and the analyzer computer and transmitting data between at least the server and the analyzer computer;

(C) a test cell software component that can be associated with the test cell and is capable of permitting electronic communication between the test cell, the server and the analyzer computer and transmitting data to at least the server;

(D) the software when used with the system being capable of allowing the analyzer to;

(1) compare a first set of current engine data to a first set of prior engine data for the one performance condition of the one performance parameter to determine if there is an abnormality;

(2) if an abnormality is detected after comparing the first set of current engine data to the first set of prior engine data, a second set of current engine data to a second set of prior engine data for the at least two different performance conditions of the one performance parameter to determine if there is an abnormality;

(3) after comparing the second set of current engine data to the second set of prior engine data to determine if there is an abnormality;

(a) if an abnormality is detected, evaluate whether the abnormality is a fault unrelated to the performance of the engine;

(c) if an abnormality is not detected, evaluate the one performance parameter relative to at least one other engine performance parameter under at least one performance condition to generate a third set of current engine data.

26. The software of claim 25 which is further capable of allowing the analyzer to:

(4) after comparing the third set of current engine data to the third set of prior engine data to determine if there is an abnormality;

(a) if an abnormality is detected, evaluate whether the abnormality is a fault unrelated to the performance of the engine;

(b) if an abnormality is not detected, evaluating whether the abnormality detected in step (2) is a fault related to performance of the engine.

27. The software of claim 26 that is stored and installable from one or more nonvolatile electronic storage media.

28. The software of claim 27 wherein the electronic media are floppy disks or CD ROM disks.

29. The software of claim 26 which has instructions provided or associated therewith for how to use the software with the system, how to install the software on the system, or how to use with and install the software on the system.

30. Software for use in a computerized system for evaluating whether faults detected during the testing of a gas turbine engine are related to engine performance problems or to problems unrelated to engine performance, the system including a server, an analyzer computer in communication with the server, and a test cell for carrying out the evaluation of the engine and in communication with the server;

the software comprising;

(A) a server software component that can reside on the server that is capable of controlling access to prior engine data, permitting electronic communication between the analyzer computer and the test cell, and processing data from at least one of the analyzer computer and the test cell;

(B) an analyzer software component that can reside on the analyzer computer and is capable of permitting electronic communication between the test cell, the server and the analyzer computer and transmitting data between at least the server and the analyzer computer;

(C) a test cell software component that can be associated with the test cell and is capable of permitting electronic communication between the test cell, the server and the analyzer computer and transmitting data to at least the server;

(D) the software when used with the system being capable of allowing the analyzer to;

(1) evaluate one performance parameter of the engine under one performance condition to generate a first set of current engine data;

(2) compare the first set of current engine data to a first set of prior engine data for the one performance condition of the one performance parameter to determine if there is an abnormality;

(1) if an abnormality is detected after comparing the first set of current engine data to the first set of prior engine data, evaluate the one performance parameter under at least two different performance conditions to generate a second set of current engine data;

(2) compare the second set of current engine data to a second set of prior engine data for the at least two different performance conditions of the one performance parameter to determine if there is an abnormality;

(3) after comparing the second set of current engine data to the second set of prior engine data to determine if there is an abnormality;

(a) if an abnormality is detected, evaluate whether the abnormality is a fault unrelated to the performance of the engine;

(b) if an abnormality is not detected, evaluate the one performance parameter relative to at least one other engine performance parameter under at least one performance condition to generate a third set of current engine data;

(4) comparing the third set of current engine data to a third set of prior engine data for the at least one other engine performance parameter under at least one performance condition to determine if there is an abnormality;

(5) after comparing the third set of current engine data to the third set of prior engine data to determine if there is an abnormality;

(c) if an abnormality is detected, evaluating whether the abnormality is a fault unrelated to the performance of the engine;

(d) if an abnormality is not detected, evaluating whether the abnormality detected in step (3) is a fault related to performance of the engine.

31. The software of claim 30 that is stored and installable from one or more nonvolatile electronic storage media.

32. The software of claim 31 wherein the electronic media are floppy disks or CD ROM disks.

33. The software of claim 30 which has instructions provided or associated therewith for how to use the software with the system, how to install the software on the system, or how to use with and install the software on the system.

34. The software of claim 30 which is capable of allowing the analyzer during (D) (2) to:

(a) plot individual values for the first current engine data and the first prior engine data in order of earliest date collected to latest date collected to provide a data plot;

(b) run a statistical analysis on the data plot to determine the center line of the data plot and the statistical control limits below and above the center line.

35. The software of claim 34 which is capable of allowing the analyzer during (D) (4) to:

(a) plot each value of the second set of current and prior engine data at one power level relative to each value of the second set of current and prior engine data at a second power level to provide a second data plot;

(b) carry out a regression analysis on the second data plot to obtain a center line for the second data plot and to obtain the difference above or below the center line of the second data plot for each value of the second set of current and prior engine data plotted in the second data plot; and

(c) plot the differences obtained for each value of the second set of current and prior engine data in order from earliest date collected to latest date collected.

36. The software of claim 35 which is capable of allowing the analyzer during (D) (5) (a) to:

(i) select a different second set of current engine data and a different second set of prior engine data;

(ii) compare the different second set of current engine data to the different second set of prior engine data to determine if there is an abnormality; and

(iii) after comparing the different second set of current engine data to the different second set of prior engine data;

(a) if an abnormality is still detected, evaluate whether the abnormality is a fault unrelated to the performance of the engine;

(b) if an abnormality is not detected, proceed to (D) (6).