Flame monitoring of a gas turbine combustor using a characteristic spectral pattern from a dynamic pressure sensor in the combustor
US-9791150-B2 · Oct 17, 2017 · US
US9989423B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9989423-B2 |
| Application number | US-201514611639-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 2, 2015 |
| Priority date | Feb 2, 2015 |
| Publication date | Jun 5, 2018 |
| Grant date | Jun 5, 2018 |
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Systems and methods for measuring temperature in a gas turbine are disclosed. The method can include directing a first acoustic signal towards a gas path in a turbine; directing a second acoustic signal towards the gas path in the turbine; receiving the first acoustic signal and the second acoustic signal at a downstream gas path location; combining the first acoustic signal and the second acoustic signal to create a combined acoustic signal, where a portion of the first acoustic signal cancels out a portion of the second acoustic signal; and determining a temperature of the gas path based at least in part on the combined acoustic signal.
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What is claimed is: 1. A method for measuring temperature, the method comprising: directing a first acoustic signal towards a gas path in a turbine via a carrier waveguide; directing a second acoustic signal towards the gas path in the turbine via an interference waveguide, wherein the interference waveguide is longer than the carrier waveguide to create a phase shift between the first acoustic signal and the second acoustic signal; receiving the first acoustic signal and the second acoustic signal at a downstream gas path location; combining the first acoustic signal and the second acoustic signal to create a combined acoustic signal, wherein a portion of the first acoustic signal cancels out a portion of the second acoustic signal; and determining a temperature of the gas path based at least in part on a frequency corresponding to the portion of the first acoustic signal canceling out the portion of the second acoustic signal in the combined acoustic signal. 2. The method of claim 1 , wherein directing a first acoustic signal and a second acoustic signal towards a gas path in a turbine comprises: transmitting an input signal to a sound source; generating, via the sound source, an acoustic signal based at least in part on the input signal; transferring the acoustic signal from the sound source to a wave splitter via an input waveguide; splitting, via the wave splitter, the acoustic signal into the first acoustic signal and the second acoustic signal; directing the first acoustic signal via the carrier waveguide; and directing the second acoustic signal via the interference waveguide. 3. The method of claim 2 , wherein the acoustic signal comprises an acoustic spectrum. 4. The method of claim 2 , wherein a controller is coupled to the sound source, and wherein the controller is configured to generate the input signal. 5. The method of claim 2 , wherein the sound source comprises at least one of: (i) a speaker, (ii) a solenoid air valve, (iii) a siren, (iv) a shaker drive diaphragm, or (v) an air horn. 6. The method of claim 1 , wherein the temperature of the gas path comprises at least one of: (i) an exhaust temperature of a gas turbine, (ii) a temperature within a hot gas path of a gas turbine, or (iii) an actual firing temperature of a gas turbine, or any other temperature that is desired to measure. 7. The method of claim 1 , wherein combining the first acoustic signal and the second acoustic signal to create a combined acoustic signal comprises: combining the first acoustic signal and the second acoustic signal via a wave adder; directing the combined acoustic signal from the wave adder to a microphone via an output waveguide, wherein the microphone is coupled to an analog-to-digital converter; generating, via the microphone, an electrical wave based on the combined acoustic signal; generating, via the microphone, an analog signal based on the electrical wave; and converting, via the analog-to-digital converter, the analog signal into a digital signal. 8. The method of claim 7 , wherein determining, via a controller, a temperature of the gas path based at least in part on a frequency corresponding to the portion of the first acoustic signal that cancels out the portion of the second acoustic signal in the combined acoustic signal comprises: identifying, via the controller, some signal minima in the digital signal corresponding to the portion of the first acoustic signal that cancels out a portion of the second acoustic signal; selecting, via the controller, the frequency associated with the signal minima, wherein the frequency is associated with a temperature; and determining, via the controller, the temperature of the gas path based at least in part on the selected frequency. 9. The method of claim 1 , wherein the temperature of the gas path is an average temperature across the carrier waveguide. 10. The method of claim 1 , wherein the carrier waveguide and the interference waveguide are disposed between a wave splitter and a wave adder. 11. A gas turbine temperature measurement system comprising: a measurement device comprising: a sound source configured to output an acoustic signal; a wave splitter configured to split the acoustic signal into a first acoustic signal and a second acoustic signal; a carrier waveguide configured to direct the first acoustic signal towards a gas path; an interference waveguide configured to direct the second acoustic signal towards the gas path, wherein the interference waveguide is longer than the carrier waveguide to create a phase shift between the first acoustic signal and the second acoustic signal; a wave adder configured to combine the first acoustic signal and the second acoustic signal to create a combined acoustic signal, wherein a portion of the first acoustic signal cancels out a portion of the second acoustic signal; at least one memory operable to store computer-executable instructions; and at least one controller configured to access the at least one memory and execute the computer-executable instructions to: generate an input signal; and determine a temperature of the gas path based at least in part on a frequency corresponding to the portion of the first acoustic signal that cancels out the portion of the second acoustic signal in the combined acoustic signal. 12. The system of claim 11 , wherein the acoustic signal comprises an acoustic spectrum. 13. The system of claim 11 , wherein the sound source comprises at least one of: (i) a speaker, (ii) a solenoid air valve, (iii) a siren, (iv) a shaker drive diaphragm, or (v) an air horn. 14. The system of claim 11 , wherein the temperature of the gas path comprises at least one of: (i) an exhaust temperature of a gas turbine, (ii) a temperature within a hot gas path of a gas turbine, or (iii) an actual firing temperature of a gas turbine, or any other temperature that is desired to measure. 15. The system of claim 11 , wherein the at least one controller is coupled to the sound source and further configured to transmit the input signal to the sound source. 16. The system of claim 11 , further comprising a microphone configured to: generate an electrical wave based on measuring the combined acoustic signal; and generate an analog signal based on the electrical wave. 17. The system of claim 16 , further comprising an analog-to-digital converter to convert the analog signal into a digital signal. 18. The system of claim 17 , wherein the at least one controller configured to access the at least one memory and execute the computer-executable instructions to determine a temperature of the gas path based at least in part on a frequency corresponding to the portion of the first acoustic signal that cancels out the portion of the second acoustic signal in the combined acoustic signal comprises: identifying some signal minima in the digital signal, wherein the signal minima corresponds to the portion of the first acoustic signal canceled out by a portion of the second acoustic signal; selecting the frequency associated with the signal minima, wherein the frequency is associated with a temperature; and determining the temperature of the gas path based at least in part on the selected frequency. 19. The system of claim 11 , wherein the carrier waveguide and the interference waveguide are disposed between the wave splitter and the wave adder. 20. A non-transitory computer-readable medium comprising computer-readable instructions operable to: direct, via at least one carrier waveguide
using measurement of acoustic effects · CPC title
Physics · mapped topic
for measuring temperature of moving fluids or granular materials capable of flow · CPC title
of moving gases · CPC title
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