초록 ▼

A method for determining an estimated operating parameter for a gas turbine including the steps of: determining an estimated operating parameter using an algorithm have an input from a sensor, wherein the algorithm includes a trim factor; determining a first trim factor based on a comparison of the

A method for determining an estimated operating parameter for a gas turbine including the steps of: determining an estimated operating parameter using an algorithm have an input from a sensor, wherein the algorithm includes a trim factor; determining a first trim factor based on a comparison of the first estimated operating parameter and the output of the sensor when a condition of the sensor is in a first mode, and during a subsequent determination of the estimated operating parameter, applying the first trim factor to subsequently determine the estimated operating condition if the condition of second sensor is in a second mode.

대표청구항 ▼

The invention claimed is: 1. A system for determining an estimated operating parameter for a gas turbine having an exhaust and a fuel controller comprising: a controller including a processor executing a combustion temperature scheduling algorithm and an emissions transfer function stored in electr

The invention claimed is: 1. A system for determining an estimated operating parameter for a gas turbine having an exhaust and a fuel controller comprising: a controller including a processor executing a combustion temperature scheduling algorithm and an emissions transfer function stored in electronic memory of the controller, wherein said scheduling algorithm outputs a temperature request signal applied to generate a fuel control command for said fuel controller and said scheduling algorithm receives as an input an emissions trim factor based on an estimated emission level generated by the emissions transfer function; an emission sensor measuring an emission level in the exhaust, wherein said sensor has an operating mode and a suspended mode, and an emissions trim factor switch selectively applying to the emissions transfer function a current emissions correction factor when said sensor is in the operating mode and a prior emissions correction factor when the sensor is in the suspended mode. 2. A system as in claim 1 wherein the emissions correction factor is a ratio of a prior estimated operating parameter and a current output of the sensor. 3. A system as in claim 1 wherein said emission sensor is a single sensor. 4. A system as in claim 1 wherein said emission sensor is healthy during the operating mode. 5. A system as in claim 1 wherein said emission sensor is placed in the suspended mode when said sensor is operating outside of a predetermined range. 6. A system as in claim 1 wherein said emission sensor is suspended during a period of steady state gas turbine operation and the estimated emission level is determined during said period of steady state gas turbine operation. 7. A system as in claim 1 wherein the emission sensor is a nitrogen oxide (NOx) emission sensor. 8. A system as in claim 1 wherein the prior emissions correction factor is a preceding prior emissions correction factor. 9. A system for determining an estimated operating parameter for a gas turbine comprising: a controller including a processor executing a gas turbine control scheduling algorithm and an emissions transfer function stored in electronic memory of the controller, wherein said scheduling algorithm outputs a turbine condition request signal applied to generate a control command for said gas turbine and said scheduling algorithm receives as an input an emissions trim factor based on an estimated emission level generated by the emissions transfer function; an emission sensor measuring an emission level in the exhaust, wherein said sensor has an operating mode and a suspended mode, and an emissions trim factor switch selectively applying to the emissions transfer function a current emissions correction factor when said sensor is in the operating mode and a prior emissions correction factor when the sensor is in the suspended mode. 10. A system as in claim 9 wherein the emissions correction factor is a ratio of a prior estimated operating parameter and a current output of the sensor. 11. A system as in claim 9 wherein said emission sensor is placed in the suspended mode when said sensor is operating outside of a predetermined range. 12. A system as in claim 9 wherein said emission sensor is suspended during a period of steady state gas turbine operation and the estimated emission level is determined during said period of steady state gas turbine operation. 13. A system as in claim 9 wherein the emission sensor is a nitrogen oxide (NOx) emission sensor. 14. A system as in claim 9 wherein the prior emissions correction factor is a preceding prior emissions correction factor. 15. A method for determining an estimated operating parameter for a gas turbine having an exhaust and a fuel controller wherein the controller includes a processor executing a combustion temperature scheduling algorithm and emissions transfer function stored in electronic memory of the controller, said method comprising: outputting a temperature request signal by the scheduling algorithm to generate a fuel control command for said fuel controller; receiving by the scheduling algorithm an emissions trim factor based on an estimated emission level generated by the emissions transfer function, wherein said emissions transfer function includes a emissions correction factor; measuring a emission level by an emission sensor in the exhaust, wherein said sensor has an operating mode and a suspended mode; using the emission level measured by the emission sensor to generate a current emissions correction factor; selectively switching the sensor between said modes, wherein the current emissions correction factor is selected when said sensor is in the operating mode and a prior emissions correction factor is selected when the sensor is in the suspended mode. 16. The method of claim 15 wherein the current emissions correction factor is a ratio of a prior estimated operating parameter and a current output of the sensor. 17. The method of claim 15 wherein said emission sensor is a single sensor and said sensor does not measure the emission level when in the suspended mode. 18. The method of claim 15 wherein said emission sensor is operating within a predetermined range of sensor outputs during the operating mode. 19. The method of claim 15 wherein said emission sensor is placed in the suspended mode while said sensor is operating outside of a predetermined range. 20. The method of claim 15 wherein said emission sensor is placed in the suspended mode during a period of steady state operation of the gas turbine.