SYSTEMS, METHODS, AND APPARATUS FOR DETECTING FAILURE IN GAS TURBINE HARDWARE

• US 20110257864A1
• Filed: 04/15/2010
• Published: 10/20/2011
• Est. Priority Date: 04/15/2010
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Intile, John Charles, Carey, Bradley Steven, Peczka, Daniel Joseph, John, Justin V., Nirmalan, Nirm Velumylum, Szepek, Scott William
• Granted Patent: US 8,818,684 B2
• Time in Patent Office: Days
• US Class Current: 701/100
• CPC Class Codes: F01D 21/00 Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
• 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 2260/80 Diagnostics

Abstract

Certain embodiments of the invention may include systems, methods, and apparatus for detecting failure in gas turbine hardware. According to an example embodiment of the invention, a method for detecting a failure in a gas turbine is provided. The method can include monitoring a parameter associated with the turbine, wherein the monitored parameter comprises at least one turbine bucket temperature, detecting an event associated with operation of the turbine, wherein the event is based at least in part on the monitored parameter, and initiating shutdown of the turbine upon detection of the event wherein the monitored parameter is above a predetermined value for at least a predetermined time duration.

Claims

1. A method for detecting a failure in a gas turbine comprising:

monitoring a parameter associated with the turbine, wherein the monitored parameter comprises at least one turbine bucket temperature;

detecting an event associated with operation of the turbine, wherein the event is based at least in part on the monitored parameter; and

initiating shutdown of the turbine upon detection of the event wherein the monitored parameter is above a predetermined value for at least a predetermined time duration.

2. The method of claim 1, wherein the monitored parameter associated with the turbine combustor further comprises at least one of:

bucket emissivity, acoustical energy, or exhaust NOx level.

3. The method of claim 1, wherein initiating shutdown is performed upon detection of the event after fuel flow or airflow associated with the turbine has initialized or stabilized.

4. The method of claim 1, wherein monitoring a parameter associated with the turbine comprises determining a moving average of the parameter over at least one time duration.

5. The method of claim 1, wherein an event comprises a turbine bucket temperature increase of greater than about 5 degrees Fahrenheit over less than about 10 minutes

6. The method of claim 1, wherein an event comprises an exhaust NOx increase of greater than about 2 ppm over less than about 10 minutes

7. The method of claim 1, wherein initiating shutdown of the turbine occurs when an event has been detected and a difference between the current monitored parameter and a stored past monitored parameter is sustained above about 25% of a limit associated with the event for greater than about 1 minute.

8. A system for detecting failure comprising:

a gas turbine;

at least one sensor for measuring a parameter associated with the turbine, wherein the measured parameter comprises at least one turbine bucket temperature;

at least one processor configured to;

receive and monitor the measured parameter from the at least one sensor;

detect an event associated with operation of the turbine, wherein the event is based at least in part on the monitored parameter; and

initiate shutdown of the turbine upon detection of the event wherein the monitored parameter is above a predetermined value for at least a predetermined time duration.

9. The system of claim 8, wherein the at least one sensor is further operable to measure one or more of bucket emissivity, acoustical energy, or exhaust NOx level.

10. The system of claim 8, wherein the at least one processor is further configured to initiate shutdown upon detection of the event after fuel flow or airflow associated with the turbine has initialized or stabilized.

11. The system of claim 8, wherein the at least one processor is configured for receiving and monitoring from the at least one sensor, the measured parameter associated with the turbine, wherein monitoring comprises determining a moving average of the measured parameter over at least one time duration.

12. The system of claim 8, wherein an event comprises a turbine bucket temperature increase of greater than about 5 degrees Fahrenheit over less than about 10 minutes

13. The system of claim 8, wherein an event comprises an exhaust NOx increase of greater than about 2 ppm over less than about 10 minutes

14. The system of claim 8, wherein initiating shutdown of the turbine occurs when an event has been detected and a difference between the current monitored parameter and a stored past monitored parameter is sustained above about 25% of a limit associated with the event for greater than about 1 minute.

15. An apparatus for detecting failure in a turbine comprising:

at least one processor configured to;

receive and monitor a measured parameter from at least one sensor, wherein the measured parameter comprises at least one turbine bucket temperature;

detect an event associated with operation of the turbine, wherein the event is based at least in part on the monitored parameter; and

initiate shutdown of the turbine upon detection of the event wherein the monitored parameter is above a predetermined value for at least a predetermined time duration.

16. The apparatus of claim 15, wherein the at least one processor is configured to receive and monitor a measured parameter from the at least one sensor, wherein the measured parameter further comprises one or more of:

bucket emissivity, acoustical energy, or exhaust NOx level.

17. The apparatus of claim 15, wherein the at least one processor is further configured to initiate shutdown upon detection of the event after fuel flow or airflow associated with the turbine has initialized or stabilized.

18. The apparatus of claim 15, wherein the at least one processor is configured for receiving and monitoring from the at least one sensor, the measured parameter associated with the turbine, wherein monitoring comprises determining a moving average of the measured parameter over at least one time duration.

19. The apparatus of claim 15, wherein the at least one processor is further configured to detect an event associated with the operation of the turbine, wherein an event comprises a turbine bucket temperature increase of greater than about 5 degrees Fahrenheit or an exhaust NOx increase of greater than about 2 ppm over less than about 10 minutes.

20. The apparatus of claim 15, wherein initiating shutdown of the turbine occurs when an event has been detected and a difference between the current monitored parameter and a stored past monitored parameter is sustained above about 25% of a limit associated with the event for greater than about 1 minute.