Gas turbine swirl detection

Patent metadata

Field	Value
Publication number	US-11204303-B2
Application number	US-201916451941-A
Country	US
Kind code	B2
Filing date	Jun 25, 2019
Priority date	Jun 25, 2019
Publication date	Dec 21, 2021
Grant date	Dec 21, 2021

Abstract

A non-transitory computer readable medium with instructions stored thereon, the instructions executable by one or more processors for calculating base swirl in a gas turbine; and calculating relative swirl in the gas turbine. Also, a method for gas turbine maintenance, comprising identifying a combustor in need of repair or replacement within a gas turbine; and repairing or replacing the combustor; wherein said identifying comprises calculating base swirl of the gas turbine and calculating relative swirl of the gas turbine in order to associate a gas path from a thermocouple to the combustor in need of repair or replacement.

First claim

The invention claimed is:

1. A non-transitory computer readable medium with instructions stored thereon,
wherein the instructions are executable by one or more processors configured to perform calculating base swirl and relative swirl in a gas turbine;
wherein calculating relative swirl comprises calculating the difference between the base swirl and a reference swirl retrieved from a reference database;
wherein calculating base swirl comprises calculating (a) unsteady pressure amplitude as a function of angular position within the gas turbine and (b) mean-subtracted exhaust temperature as a function of angular position within the gas turbine; and
wherein a reference database is updated in real time with base swirl data as a function of gas turbine load.

2. The non-transitory computer readable medium of claim 1 , wherein calculating base swirl comprises calculating (a) unsteady pressure amplitude as a function of angular position within the gas turbine and/or (b) mean-subtracted exhaust temperature as a function of angular position within the gas turbine.

3. The non-transitory computer readable medium of claim 1 , wherein calculating base swirl comprises determining an average angular offset between an unsteady pressure amplitude as a function of an angular position within the gas turbine and a mean-subtracted exhaust temperature as a function of angular position within the gas turbine, wherein the average angular offset is a function of a gas turbine load.

4. The non-transitory computer readable medium of claim 1 , wherein calculating base swirl comprises measuring a pressure amplitude within the gas turbine and fitting the pressure amplitude to the expression A*e{circumflex over ( )}(i*Θ d ), wherein A is a constant coefficient, i is the square root of negative one, e is Euler's number, and Θ d is the angular phase of the measured pressure amplitude.

5. The non-transitory computer readable medium of claim 1 , wherein the reference swirl is selected on the basis of a turbine load, wherein the reference swirl comprises a mean-subtracted exhaust temperature pattern for a plurality of samples.

6. A gas turbine system comprising:
a computer system comprising at least one processor coupled to memory and the computer readable medium of claim 1 ; and
at least one gas turbine comprising at least one thermocouple and at least one pressure sensor, wherein the computer system is configured to receive real time data input from the at least one thermocouple, wherein the computer system is configured to receive real time data input from the at least one pressure sensor.

7. The non-transitory computer readable medium of claim 1 , wherein calculating base swirl comprises measuring a mean-subtracted gas path temperature within the gas turbine and fitting the mean-subtracted gas path temperature to the expression B*e{circumflex over ( )}(i*Θ t ), wherein B is a constant coefficient, i is the square root of negative one, e is Euler's number, and Θ t is the angular phase of the measured mean-subtracted gas path temperature.

8. The non-transitory computer readable medium of claim 7 , wherein calculating base swirl further comprises measuring a pressure amplitude within the gas turbine and fitting the pressure amplitude to the expression A*e{circumflex over ( )}(i*Θ d ), wherein A is a constant coefficient, i is the square root of negative one, e is Euler's number, and Θ d is the angular phase of the measured pressure amplitude, wherein calculating base swirl comprises calculating a second swirl, wherein said second swirl is 2*π*(Θ t −Θ d ).

9. The non-transitory computer readable medium of claim 8 , wherein calculating base swirl further comprises determining an average angular offset between an unsteady pressure amplitude as a function of an angular position within the gas turbine and a mean-subtracted exhaust temperature as a function of angular position within the gas turbine, and wherein the average angular offset is cross correlated with the second swirl.

10. A method for gas turbine maintenance, comprising:
identifying a combustor in need of repair or replacement within a gas turbine; and
repairing or replacing the combustor;
wherein said identifying comprises calculating base swirl of the gas turbine and calculating relative swirl of the gas turbine in order to identify a gas path from a thermocouple to the combustor in need of repair or replacement, wherein calculating relative swirl comprises calculating the difference between the base swirl and a reference swirl retrieved from a reference database; wherein a reference database is updated in real time with base swirl data as a function of gas turbine load.

11. The method of claim 10 , wherein calculating base swirl comprises calculating (a) unsteady pressure amplitude as a function of angular position within the gas turbine and/or (b) mean-subtracted exhaust temperature as a function of angular position within the gas turbine.

12. The method of claim 10 , wherein calculating base swirl comprises calculating (a) unsteady pressure amplitude as a function of angular position within the gas turbine and (b) mean-subtracted exhaust temperature as a function of angular position within the gas turbine.

13. The method of claim 10 , wherein calculating base swirl comprises determining an average angular offset between an unsteady pressure amplitude as a function of angular position within the gas turbine and a mean-subtracted exhaust temperature as a function of angular position within the gas turbine, wherein the average angular offset is a function of gas turbine load.

14. The method of claim 10 , wherein calculating base swirl comprises measuring a pressure amplitude within the gas turbine and fitting the pressure amplitude to the expression A*e{circumflex over ( )}(i*Θ d ), wherein A is a constant coefficient, i is the square root of negative one, e is Euler's number, and Θ d is the angular phase of the measured pressure amplitude.

15. The method of claim 10 , wherein the reference swirl is selected on the basis of turbine load, wherein the reference swirl comprises a mean-subtracted exhaust temperature pattern for a plurality of samples, wherein the plurality of samples are gas path temperatures measured by a thermocouple, wherein the relative swirl is equal to a cross-correlation shift, wherein the cross-correlation shift is a phase shift that gives the highest correlation coefficient between the base swirl and reference swirl.

16. The method of claim 10 , wherein calculating base swirl comprises measuring a mean-subtracted gas path temperature within the gas turbine and fitting the mean-subtracted gas path temperature to the expression B*e{circumflex over ( )}(i*Θ t ), wherein B is a constant coefficient, i is the square root of negative one, e is Euler's number, and Θ t is the angular phase of the measured mean-subtracted gas path temperature.

17. The method of claim 16 , wherein calculating base swirl further comprises measuring a pressure amplitude within the gas turbine and fitting the pressure amplitude to the expression A*e{circumflex over ( )}(i*Θ d ), wherein A is a constant coefficient, i is the square root of negative one, e is Euler's number, and Θ d is the angular phase of the measured pressure amplitude, wherein calculating base swirl comprises calculating a second swirl, wherein said second swirl is 2*π*(Θ t −Θ d ).

18. The method of claim 17 , wherein calculating base swirl further comprises determining an average angular offset between an unsteady pressure amplitude as a function of angular position within t

Assignees

• Electric Power Res Institute Inc

Inventors

• Angello Leonard Charles
• Emerson Benjamin
• Lieuwen Timothy Charles
• Noble David Robert

Classifications

• F05D2230/80

  Repairing, retrofitting or upgrading methods · CPC title

• F05D2230/72

  Maintenance · CPC title

• F05D2260/80

  Diagnostics · CPC title

• F23R2900/00013

  Reducing thermo-acoustic vibrations by active means · CPC title

• F05D2240/35

  Combustors or associated equipment · CPC title