MEMS emissions sensor system for a turbine engine

• US 20080282770A1
• Filed: 05/18/2007
• Published: 11/20/2008
• Est. Priority Date: 05/18/2007
• Status: Active Grant

• Current Assignee: Siemens Energy Incorporated (Siemens AG)
• Original Assignee: Siemens Power Generation, Inc.
• Inventors: Bunce, Richard H.
• Granted Patent: US 7,578,177 B2
• Time in Patent Office: Days
• US Class Current: 73/23.31
• CPC Class Codes: F02C 9/00 Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants controlling air intakes F02C7/057; controlling turbines F01D; controlling compressors F04D27/00; controlling in general G05
• CPC Class Codes: G01N 1/2247 Sampling from a flowing stream of gas
• CPC Class Codes: G01N 1/26 with provision for intake from several spaces

Abstract

Aspects of the invention are directed to the use of microelectromechanical systems (MEMS) based emissions sensors in a turbine engine system to measure one or more emissions values associated with a gas flow in the system. The emissions value can be, for example, the temperature of a gas flow and/or the amount of a particular compound, such as carbon monoxide, in the gas flow. Due to their small size, a plurality of MEMS emissions sensors can readily be incorporated at various locations in a turbine engine system. For example, the MEMS emissions sensors can be operatively positioned in an exhaust stack, downstream of the last row of blades in the turbine section, or in the leading edge of a turbine vane. The MEMS sensors can be operatively connected to a data acquisition system, which can statistically analyze the emissions values measured by the MEMS sensors.

Claims

1. An emissions measurement system comprising:

a turbine engine;

a gas flow in the turbine engine; and

a plurality of MEMS emissions sensors operatively positioned within the turbine engine, wherein each of the MEMS emissions sensors measures an emissions value of the gas flow.

2. The system of claim 1 wherein the emissions value is at least one of the amount of carbon monoxide in the gas flow or the temperature of the gas flow.

3. The system of claim 1 wherein the MEMS emissions sensors are adapted to withstand at least about 800 degrees Fahrenheit.

4. The system of claim 1 wherein the turbine engine includes a row of rotating blades, wherein the plurality of MEMS emissions sensors are operatively positioned proximate the row of rotating blades.

5. The system of claim 1 wherein the turbine engine includes a row of stationary vanes, each vane having a leading edge, wherein the plurality of MEMS emissions sensors are attached to at least one of the stationary vanes proximate the leading edge.

6. The system of claim 1 further including a data acquisition system operatively connected to the plurality of MEMS emissions sensors, wherein the data acquisition system receives emissions values measured by the plurality of MEMS emissions sensors.

7. The system of claim 6 wherein the data acquisition system is programmed with a statistical algorithm, wherein the data acquisition system statistically analyzes the emissions values measured by the plurality of MEMS emissions sensors.

8. The system of claim 7 wherein the data acquisition system is programmed to filter the emissions values based on at least one filter criteria, whereby measured emission values outside of the filter criteria are disregarded.

9. An emissions measurement system comprising:

a turbine engine;

an exhaust stack having a flow passage, wherein the flow passage receives an exhaust gas from the turbine engine; and

a plurality of MEMS emissions sensors operatively positioned within the flow passage, wherein each of the plurality of MEMS emissions sensors measures an emissions value of the exhaust gas.

10. The system of claim 9 wherein the emissions value is at least one of the amount of carbon monoxide in the exhaust gas or the temperature of the exhaust gas.

11. The system of claim 9 wherein a maximum of about 100 MEMS emissions sensors are provided per square millimeter.

12. The system of claim 9 further including a data acquisition system operatively connected to the plurality of MEMS emissions sensors, wherein the data acquisition system receives emissions values measured by the plurality of MEMS emissions sensors.

13. The system of claim 12 wherein the data acquisition system is programmed with a statistical algorithm, wherein the data acquisition system statistically analyzes the emissions values measured by the plurality of MEMS emissions sensors.

14. The system of claim 13 wherein the data acquisition system is programmed to filter the emissions values based on at least one filter criteria, whereby measured emission values outside of the filter criteria are disregarded.

15. A method of measuring turbine engine emissions comprising the steps of:

operating a turbine engine system, wherein the turbine engine system includes a gas traveling along a gas flow path;

operatively positioning a plurality of MEMS emissions sensors within the gas flow path; and

measuring an emissions value of the gas flow with each of the plurality of MEMS emissions sensors.

16. The method of claim 15 further including the step of statistically analyzing the measured emissions values.

17. The method of claim 16 wherein the statistically analyzing step includes performing at least one of the following statistical analyses:

average, root mean square, Student'"'"'s T or Monte Carlo.

18. The method of claim 17 further including the step of filtering the measured emissions values based on at least one filter criteria, wherein measured emissions values outside of the at least one filter criteria are disregarded.

19. The method of claim 18 wherein the filter criteria is at least one of a reasonableness filter, an accuracy filter or a consistency filter.

20. The method of claim 15 wherein the emissions value is at least one of the amount of carbon monoxide in the gas or the temperature of the gas.