System and method for detecting combustion hardware damage

• US 8,990,026 B2
• Filed: 01/03/2012
• Issued: 03/24/2015
• Est. Priority Date: 01/03/2012
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (GE Vernova, Inc.)
• Original Assignee: General Electric Company
• Inventors: Shaikh, Tauseef Ahmed, Iasillo, Robert Joseph, Jain, Praveen Babulal, Pg, KrishnaKumar, Radhakrishnan, Ajith Kizhuthrukovil, Soudary, Mallareddy
• Primary Examiner(s): Breene, John
• Assistant Examiner(s): Hagos, Eyob
• Application Number:
  US13/342,764
• Publication Number:
  US 20130173181A1
• Time in Patent Office: 1,176 Days
• Field of Search: 702/34
• US Class Current: 702/34
• CPC Class Codes: F23N 5/00 Systems for controlling combustion regulating fuel supply F23N1/00, regulating air supply or draught F23N3/00
• CPC Class Codes: F23N 5/16 using noise-sensitive detectors
• CPC Class Codes: F23N 5/242 using electronic means
• CPC Class Codes: G01M 5/0033 by determining damage, crack or wear
• CPC Class Codes: G01N 2291/2693 Rotor or turbine parts
• CPC Class Codes: G01N 29/046 using the echo of particles imparting on a surface; using acoustic emission of particles investigating concentration of particle suspensions G01N15/06; devices for measuring flow of solids in suspension G01F1/74
• CPC Class Codes: G01N 29/14 using acoustic emission techniques echo of particles G01N29/046; measuring mechanical vibrations or acoustic waves in solids in general G01H1/00

Abstract

A power generation plant including a plurality of combustor cans, one or more sensors configured to measure acoustic vibrations from the plurality of combustor cans, and a controller that includes a processor. The processor is programmed to identify a dominant tone of the measured acoustic vibrations, the dominant tone being a frequency where a highest amount of energy lies, determine, for each of the plurality of combustor cans, a frequency of the dominant tone at predefined time intervals, and determine a degradation status of at least one of the plurality of combustor cans based on the frequency of the dominant tone at each of the predefine time intervals for the at least one of the plurality of combustor cans.

Claims

1. A power generation plant comprising:

a plurality of combustor cans;

one or more sensors configured to measure acoustic vibration data from the plurality of combustor cans; and

a controller comprising a processor, the processor programmed to;

determine, for each of the plurality of combustor cans based on the acoustic vibration data, a frequency of a dominant tone at a plurality of predefined time intervals, the dominant tone being a frequency where a highest amount of energy lies;

identify, for each combustor can at each of the predefined time intervals, which of a plurality of sub frequency ranges the dominant tone falls within;

identify a dominant sub frequency range as one of the plurality of sub frequency ranges into which the greatest number of dominant tones falls for all combustor cans throughout the plurality of predefined time intervals; and

determine a degradation status of at least one of the plurality of combustor cans based on a number of the predefined time intervals for which the dominant tone of the at least one combustor can is not within the dominant sub frequency range.

2. A power generation plant in accordance with claim 1, wherein acoustic vibration data comprises combustion dynamics amplitude data.

3. A power generation plant in accordance with claim 2, wherein the processor is further programmed to perform a fast Fourier transform on the combustion dynamics amplitude data associated with each of the plurality of combustor cans to determine frequency data for each of the plurality of combustor cans.

4. A power generation plant in accordance with claim 1, wherein determining a degradation status of at least one of the plurality of combustor cans further comprises:

defining a frequency range based on the dominant tone; and

separating the defined frequency range into the plurality of sub frequency ranges.

5. A power generation plant in accordance with claim 1, wherein determining a degradation status of at least one of the plurality of combustor cans comprises:

identifying, as having combustor hardware damage, a combustor can of the plurality of combustor cans that has a greatest number of the predefined time intervals in which the dominant tone of the combustor can is not within the dominant sub frequency range.

6. A power generation plant in accordance with claim 5, wherein determining a degradation status of at least one of the plurality of combustor cans further comprises sending a signal indicative of combustor hardware damage for the identified combustor can.

7. A power generation plant in accordance with claim 5, wherein the combustor hardware damage is a crack enabling an increase in air flow leaning out a fuel to air ratio.

8. A power generation plant in accordance with claim 1, wherein the processor is further programmed to determine whether the gas turbine is running at a steady state;

and

if the gas turbine is running at a steady state, the processor is configured to receive the measured acoustic vibration data corresponding to each of the plurality of combustor cans.

9. A method for monitoring gas turbine combustor hardware, the method comprising:

obtaining, by a controller from sensors coupled to the gas turbine combustor hardware, acoustic vibration data corresponding to each of a plurality of combustor cans;

determining, by the controller for each of the plurality of combustor cans based on the acoustic vibration data, a frequency of a dominant tone at a plurality of predefined time intervals, the dominant tone being a frequency where a highest amount of energy lies;

identifying, by the controller for each combustor can at each of the predefined time intervals, which of a plurality of sub frequency ranges the dominant tone falls within;

identifying, by the controller, a dominant sub frequency range as one of the plurality of sub frequency ranges into which the greatest number of dominant tones falls for all combustor cans throughout the plurality of predefined time intervals; and

determining, by the controller, a degradation status of at least one of the plurality of combustor cans based on a number of the predefined time intervals for which the dominant tone of the at least one combustor can is not within the dominant sub frequency range.

10. A method in accordance with claim 9, wherein acoustic vibration data comprises combustion dynamics amplitude data.

11. A method in accordance with claim 10, further comprising performing, by the controller, a fast Fourier transform on the combustion dynamics amplitude data associated with each of the plurality of combustor cans to determine frequency data for each of the plurality of combustor cans.

12. A method in accordance with claim 9, wherein determining a degradation status of at least one of the plurality of combustor cans further comprises:

defining a frequency range based on the dominant tone; and

separating the defined frequency range into the plurality of sub frequency ranges.

13. A method in accordance with claim 9, wherein determining a dominant sub frequency range determining a degradation status of at least one of the plurality of combustor cans comprises:

identifying by the controller, as having combustor hardware damage, a combustor can of the plurality of combustor cans that has a greatest number of the predefined time intervals in which the dominant tone of the combustor can is not within the dominant sub frequency range.

14. A method in accordance with claim 13, wherein determining a degradation status of at least one of the plurality of combustor cans further comprises sending a signal indicative of combustor hardware damage for the identified combustor can.

15. A method in accordance with claim 13, wherein the combustor hardware damage is a crack enabling an increase in air flow leaning out a fuel to air ratio.

16. A method in accordance with claim 9, further comprising determining, by the controller, whether the gas turbine is running at a steady state;

and

if the gas turbine is running at a steady state, accessing, by the controller, the acoustic vibration data corresponding to each of the plurality of combustor cans.

17. A system for monitoring gas turbine combustor hardware, the system comprising:

a combustor comprising a plurality of combustor cans;

one or more sensors configured to measure combustion dynamics amplitude data from acoustic vibrations corresponding to each of the plurality of combustor cans; and

a controller comprising a processor, the processor programmed to;

determine frequency data from the measured combustion dynamics amplitude data;

determine, for each of the plurality of combustor cans based on the frequency data, a frequency of a dominant tone at a plurality of predefined time intervals, the dominant tone being a frequency where a highest amount of energy lies;

identify, for each combustor can at each of the predefined time intervals, which of a plurality of sub frequency ranges the dominant tone falls within;

identify a dominant sub frequency range as one of the plurality of sub frequency ranges into which the greatest number of dominant tones falls for all combustor cans throughout the plurality of predefined time intervals; and

determine a degradation status of at least one of the plurality of combustor cans based on a number of predefined time intervals for which the dominant tone of the at least one combustor can is not within the dominant sub frequency range.

18. A system in accordance with claim 17, wherein determining a degradation status of at least one of the plurality of combustor cans comprises;

defining a frequency range based on the dominant tone; and

separating the defined frequency range into the plurality of sub frequency ranges.

19. A system in accordance with claim 17, wherein determining a degradation status of at least one of the plurality of combustor cans comprises:

identifying, as having combustor hardware damage, a combustor can of the plurality of combustor cans that has a greatest number of predefined time intervals for which the dominant tone of the combustor can is not within the dominant sub frequency range.

20. A system in accordance with claim 19, further comprising an alarm configured to activate in response to a signal received from the processor, the signal indicative of combustor hardware damage for the identified combustor can.