Indirectly determining exhaust gas parameters

Patent metadata

Field	Value
Publication number	US-9927348-B2
Application number	US-201514948750-A
Country	US
Kind code	B2
Filing date	Nov 23, 2015
Priority date	Nov 23, 2015
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

Abstract

Various embodiments include a system having: a computing device configured to monitor a gas turbine (GT) by: determining a moisture content and/or an oxygen content of inlet air entering the inlet of the GT compressor section; determining a corresponding one of the moisture content and/or the oxygen content of exhaust gas from the GT turbine section; calculating a flow rate of the exhaust gas from the turbine section and a flow rate of the inlet air entering the inlet of the compressor section based upon the moisture content and/or the oxygen content of the inlet air and the exhaust gas; and calculating a temperature of the exhaust gas and an energy of the exhaust gas from the turbine section based upon the flow rate of the exhaust gas from the turbine and the flow rate of the inlet air entering the inlet of the compressor section.

First claim

We claim:

1. A system comprising:
at least one computing device configured to monitor a gas turbine (GT) having a compressor section with an inlet, a combustor section fluidly connected with the compressor section, and a turbine section fluidly connected with the combustor section, by performing actions including:
determining at least one of a moisture content or an oxygen content of inlet air entering the inlet of the compressor section;
determining a corresponding one of the at least one of the moisture content or the oxygen content of exhaust gas from the turbine section;
calculating a flow rate of the exhaust gas from the turbine section and a flow rate of the inlet air entering the inlet of the compressor section based upon the at least one of the moisture content or the oxygen content of the inlet air and the exhaust gas; and
calculating a temperature of the exhaust gas and an energy of the exhaust gas from the turbine section based upon the flow rate of the exhaust gas from the turbine and the flow rate of the inlet air entering the inlet of the compressor section.

2. The system of claim 1 , wherein the at least one computing device is further configured to compare the parameters (flow/energy/temperature) of the exhaust gas with a threshold range of exhaust gas parameter values.

3. The system of claim 2 , wherein the at least one computing device is further configured to modify at least one operating parameter of the GT in response to the parameter values of the exhaust gas deviating from the threshold ranges.

4. The system of claim 3 , wherein the modifying of the operating parameter of the GT includes modifying a firing temperature of the combustor section.

5. The system of claim 3 , wherein the threshold ranges includes approximately a +/−0.5 percent deviation to approximately a +/−1 percent deviation from a design exhaust energy value, or approximately a +/−5 degree Celsius deviation to approximately a +/−20 degree Celsius deviation from a design exhaust temperature value.

6. The system of claim 1 , wherein the determining of the at least one of the moisture content or the oxygen content of the inlet air and the determining of the corresponding one of the at least one of the moisture content or the oxygen content of exhaust gas from the turbine section includes measuring the at least one of the moisture content or the oxygen content of the inlet air and the corresponding one of the at least one of the moisture content or the oxygen content of exhaust gas from the turbine section using a set of sensors.

7. The system of claim 1 , wherein both the moisture content and the oxygen content of the inlet air and the exhaust gas are determined, wherein the moisture content and the oxygen content are independent variables.

8. A computer program product comprising program code, which when executed by at least one computing device, causes the at least one computing device to monitor a gas turbine (GT) having a compressor section with an inlet, a combustor section fluidly connected with the compressor section, and a turbine section fluidly connected with the combustor section, by performing actions including:
determining at least one of a moisture content or an oxygen content of inlet air entering the inlet of the compressor section;
determining a corresponding one of the at least one of the moisture content or the oxygen content of exhaust gas from the turbine section;
calculating a flow rate of the exhaust gas from the turbine section and a flow rate of the inlet air entering the inlet of the compressor section based upon the at least one of the moisture content or the oxygen content of the inlet air and the exhaust gas; and
calculating a temperature of the exhaust gas and an energy of the exhaust gas from the turbine section based upon the flow rate of the exhaust gas from the turbine and the flow rate of the inlet air entering the inlet of the compressor section.

9. The computer program product of claim 8 , wherein the program code causes the at least one computing device to further compare the parameters (flow/energy/temperature) of the exhaust gas with threshold ranges of exhaust parameter values.

10. The computer program product of claim 9 , wherein the program code causes the at least one computing device to further modify an operating parameter of the GT in response to the parameters of the exhaust gas deviating from the threshold ranges.

11. The computer program product of claim 10 , wherein the modifying of the operating parameter of the GT includes modifying a firing temperature of the combustor section.

12. The computer program product of claim 10 , wherein the threshold range includes approximately a +/−0.5 percent deviation to approximately a +/−1 percent deviation from a design exhaust energy value, or approximately a +/−5 degree Celsius deviation to approximately a +/−20 degree Celsius deviation from a design exhaust temperature value.

13. The computer program product of claim 8 , wherein the determining of the at least one of the moisture content or the oxygen content of the inlet air and the determining of the corresponding one of the at least one of the moisture content or the oxygen content of exhaust gas from the turbine section includes measuring the at least one of the moisture content or the oxygen content of the inlet air and the corresponding one of the at least one of the moisture content or the oxygen content of exhaust gas from the turbine section using a set of sensors.

14. The computer program product of claim 8 , wherein both the moisture content and the oxygen content of the inlet air and the exhaust gas are determined, wherein the moisture content and the oxygen content are independent variables.

15. A system comprising:
a gas turbine (GT) having a compressor section with an inlet, a combustor section fluidly connected with the compressor section, and a turbine section fluidly connected with the combustor section; and
at least one computing device coupled with the GT, the at least one computing device configured to perform actions including:
determining at least one of a moisture content or an oxygen content of inlet air entering the inlet of the compressor section;
determining a corresponding one of the at least one of the moisture content or the oxygen content of exhaust gas from the turbine section;
calculating a flow rate of the exhaust gas from the turbine section and a flow rate of the inlet air entering the inlet of the compressor section based upon the at least one of the moisture content or the oxygen content of the inlet air and the exhaust gas; and
calculating a temperature of the exhaust gas and an energy of the exhaust gas from the turbine section based upon the flow rate of the exhaust gas from the turbine and the flow rate of the inlet air entering the inlet of the compressor section.

16. The system of claim 15 , wherein the at least one computing device is further configured to compare the energy of the exhaust gas with a threshold range of exhaust energy values.

17. The system of claim 16 , wherein the at least one computing device is further configured to modify an operating parameter of the GT in response to the energy of the exhaust gas deviating from the threshold range.

18. The system of claim 17 , wherein the modifying of the operating parameter of the GT includes modifying a firing temperature of the combustor section.

19. The system of claim 17 , wherein the threshold range includes approximately a +/−0.5 percent deviation to approximately a +/−1 percent deviation from a de

Assignees

• Gen Electric

Inventors

• Zhang Daili
• Dinu Constantin

Classifications

• F05D2270/303

  Temperature · CPC title

• F05D2270/301

  Pressure · CPC title

• G01M15/14 Primary

  Testing gas-turbine engines or jet-propulsion engines · CPC title

• G01K13/02

  for measuring temperature of moving fluids or granular materials capable of flow · CPC title

• F05D2270/313

  Air temperature · CPC title