Lean blowout precursor detection for gas turbines
A method for detecting blowout precursors in at least one gas turbine combustor comprising: receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in part on the wavelet analysis. Provided also is a system and a non-transitory computer readable medium configured to perform the method.
1. A method for detecting blowout precursors in at least one gas turbine combustor, comprising receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using a simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in part on the wavelet analysis, wherein said determining the existence of a blowout precursor comprises determining an increase in amplitude of time dependent spectral content in at least one predefined band of high frequency dynamics.
2. The method of claim 1 , wherein the band of high frequency dynamics is predefined based on an identification of bands of high frequency dynamics that appeared for the combustor approximately one second before a previous blowout event.
3. The method of claim 1 , wherein performing the wavelet analysis comprises determining the dominant frequencies of oscillation of an acoustic data signal as a function of time to calculate a wavelet coefficient.
4. The method of claim 3 , further comprising using a windowed root-mean-square calculation to process the wavelet coefficient to determine the amplitude of the wavelet coefficient, and determining the existence of a blowout precursor based on an increased amplitude of the wavelet coefficient oscillation.
5. A system for acoustic detection of blowout precursors in at least one gas turbine combustor comprising an acoustic measuring device in communication with the combustor, wherein the acoustic measuring device generates signals indicative of acoustic combustion dynamics in the combustor in real time; and a blowout precursor monitoring unit that receives the acoustic signals and performs a simplified Mexican Hat wavelet transform analysis to detect the existence of a blowout precursor, wherein the blowout precursor monitoring unit detects the existence of a blowout precursor by determining an increase in amplitude of time dependent spectral content in at least one predefined band of high frequency dynamics.
6. The system as in claim 5 , further comprising a combustion controller configured to control at least one parameter of the operation of the combustor based at least in part on detection of a blowout precursor by the blowout precursor monitoring unit.
7. The system as in claim 6 , wherein the combustion controller is configured to generate at least one control signal upon detection of a blowout precursor to adjust a fuel-air ratio of fuel and air supplied to the combustor associated with the blowout precursor.
8. The system of claim 5 , wherein the at least one band of high frequency dynamics is predefined based on an identification of bands of high frequency dynamics that appeared for the combustor approximately one second before a previous blowout event.
9. The system of claim 5 , wherein the blowout precursor monitoring unit performs the wavelet analysis by determining the dominant frequencies of oscillation of the acoustic signal as a function of time to calculate a wavelet coefficient.
10. The system of claim 9 , wherein the blowout precursor monitoring unit uses a windowed root-mean-square calculation to process the wavelet coefficient to determine the amplitude of the wavelet coefficient, and detects the existence of a blowout precursor based on an increased amplitude of the wavelet coefficient oscillation.
11. The system of claim 5 , wherein the blowout precursor monitoring unit, upon detection of a blowout precursor, sends an alarm signal to an electronic device and/or sends a signal indicating the detection of the blowout precursor to a combustion controller.
12. A non-transitory computer-readable storage medium on which is encoded executable program code for performing a method for detecting blowout precursors in at least one gas turbine combustor comprising, receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using a simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in part on the wavelet analysis, wherein said determining the existence of a blowout precursor comprises determining an increase in amplitude of time dependent spectral content in at least one predefined band of high frequency dynamics.
13. The non-transitory computer readable medium of claim 12 , wherein the band of high frequency dynamics is predefined based on an identification of bands of high frequency dynamics that appeared for the combustor approximately one second before a previous blowout event.
14. The non-transitory computer readable medium of claim 12 , wherein performing the wavelet analysis comprises determining the dominant frequencies of oscillation of an acoustic data signal as a function of time to calculate a wavelet coefficient.
15. The non-transitory computer readable medium of claim 14 , wherein the method further comprises using a windowed root-mean-square calculation to process the wavelet coefficient to determine the amplitude of the wavelet coefficient, and determining the existence of a blowout precursor based on an increased amplitude of the wavelet coefficient oscillation.
16. A method for detecting blowout precursors in at least one gas turbine combustor, comprising receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using a simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in part on the wavelet analysis, wherein performing the wavelet analysis comprises determining the dominant frequencies of oscillation of an acoustic data signal as a function of time to calculate a wavelet coefficient.
17. A system for acoustic detection of blowout precursors in at least one gas turbine combustor comprising an acoustic measuring device in communication with the combustor, wherein the acoustic measuring device generates signals indicative of acoustic combustion dynamics in the combustor in real time; and a blowout precursor monitoring unit that receives the acoustic signals and performs a simplified Mexican Hat wavelet transform analysis to detect the existence of a blowout precursor, wherein the blowout precursor monitoring unit performs the wavelet analysis by determining the dominant frequencies of oscillation of the acoustic signal as a function of time to calculate a wavelet coefficient.
18. A non-transitory computer-readable storage medium on which is encoded executable program code for performing a method for detecting blowout precursors in at least one gas turbine combustor comprising, receiving combustion dynamics acoustic data measured by an acoustic measuring device associated with the combustor in real time; performing wavelet analysis on the acoustic data using a simplified Mexican Hat wavelet transform analysis; and determining the existence of a blowout precursor based at least in part on the wavelet analysis, wherein performing the wavelet analysis comprises determining the dominant frequencies of oscillation of an acoustic data signal as a function of time to calculate a wavelet coefficient.