Method and apparatus for detecting combustion instability in continuous combustion systems

• US 6,993,960 B2
• Filed: 04/10/2003
• Issued: 02/07/2006
• Est. Priority Date: 12/26/2002
• Status: Active Grant

• Current Assignee: Woodward Governor Company
• Original Assignee: Woodward Governor Company
• Inventors: Benson, Kelly J.
• Primary Examiner(s): MCCALL, ERIC SCOTT
• Application Number:
  US10/411,167
• Publication Number:
  US 20040123653A1
• Time in Patent Office: 1,034 Days
• Field of Search: 73/350.8, 731/173, 731/16, 731/172, 731/181, 73/350.1, 73/350.3, 73/350.6, 73/350.7
• US Class Current: 73/112.01
• CPC Class Codes: F05B 2260/80 Diagnostics
• CPC Class Codes: F23D 2900/00015 Pilot burners specially adapted for low load or transient conditions, e.g. for increasing stability
• CPC Class Codes: F23N 1/022 using electronic means
• CPC Class Codes: F23N 2229/12 with flame rectification current detecting means
• CPC Class Codes: F23N 2241/20 Gas turbines
• CPC Class Codes: F23N 5/123 using electronic means
• CPC Class Codes: F23N 5/242 using electronic means
• CPC Class Codes: F23R 2900/00013 Reducing thermo-acoustic vibrations by active means
• CPC Class Codes: F23R 3/286 having fuel-air premixing devices F23R3/30 takes precedence
• CPC Class Codes: F23R 3/343 Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion ignition in gas-turbine plants F02C7/264; pilot flame igniters F23Q9/00
• CPC Class Codes: G01L 23/225 circuit arrangements therefor

Abstract

An apparatus and method to sense the onset of combustion stability is presented. An electrode is positioned in a turbine combustion chamber such that the electrode is exposed to gases in the combustion chamber. The electrode may be integrated with an igniter. A control module applies a voltage potential to the electrode and detects a combustion ionization signal and determines if there is an oscillation in the combustion ionization signal indicative of the occurrence of combustion stability or the onset of combustion instability. The control module broadcasts a notice if the parameters indicate the combustion process is at the onset of combustion instability or broadcasts an alarm signal if the parameters indicate the combustion process is instable. Combustion parameters are adjusted to drive the combustion process towards stability.

Claims

1. A system for detecting combustion instability in a continuous combustion system having a combustion region comprising:

at least one retractable igniter having at least one electrode, the at least one retractable igniter positioned at a location such that the at least one electrode is exposed to gases in the combustion region; and

a controller coupled to the at least one electrode, the controller capable of receiving from the at least one electrode a combustion ionization signal and detecting an oscillation in the combustion ionization signal indicative of the occurrence of combustion instability, wherein the controller is adapted to monitor a temperature of the at least one retractable igniter and actively position the at least one retractable igniter to take ion measurements and retract the at least one retractable igniter if the temperature is above a threshold.

2. The system of claim 1 wherein the controller is adapted to position the retractable igniter to keep the retractable igniter exposed to gases in the combustion region and below a temperature threshold.

3. The system of claim 1 wherein the controller is further adapted to retract the at least one retractable igniter if the temperature is rapidly approaching the threshold.

4. The system of claim 1 wherein the controller is adapted to excite the at least one electrode to create an electric field from the at least one electrode to a ground of the combustion region.

5. A system for detecting combustion instability in an afterburner having a combustion region comprising:

at least one electrode positioned in the combustion region at a location such that the at least one electrode is exposed to gases in the combustion region;

a control module coupled to the at least one electrode, the control module adapted to excite the at least one electrode to create an electric field from the at least one electrode to a ground of the combustion region and receive from the at least one electrode a combustion ionization signal, the control module further adapted to detect an oscillation in the combustion ionization signal indicative of the occurrence of combustion instability; and

wherein the at least one electrode is positioned in an igniter of the afterburner.

6. The system of claim 5 wherein the control module is adapted to perform a method for detecting combustion instability in the afterburner, the method comprising the steps of:

receiving an ion current signal from the electrode indicative of ion current flowing through the electrode that is exposed to combustion gases in the combustion region of the afterburner;

determining if parameters of the ion current signal indicate the combustion process is one of at the onset of combustion instability or is unstable; and

sending a signal to an engine controller if the parameters of the ion current signal indicate the combustion process is one of at the onset of combustion instability or is unstable.

7. A method for detecting combustion instability in a lean premix gas turbine having an electrode positioned in the combustion chamber at a location such that the electrode is exposed to combustion gases containing free ions in the combustion chamber, the method comprising the steps of:

applying a voltage to the electrode during the combustion process;

determining parameters of a current flowing between the electrode and at least one wall of the combustion chamber;

determining if the parameters indicate the combustion process is one of at the onset of combustion instability or is unstable; and

adjusting at least one combustion system parameter if the parameters indicate the combustion process is one of at the onset of combustion instability or is unstable, wherein the step determining if the parameters indicate the combustion process is one of at the onset of combustion instability or is unstable comprises determining that the combustion process is at the onset of combustion instability if an oscillation frequency is within a predetermined frequency range and an oscillation magnitude corresponds to a first threshold.

8. The method of claim 7 wherein the first threshold corresponds to ±

1 psi.

9. The method of claim 7 wherein the predetermined frequency range is approximately ±

50 Hz of a critical frequency of the gas turbine.

10. The method of claim 7 wherein the predetermined frequency range is between approximately 10 Hz and approximately 10 kHz.

11. The method of claim 7 wherein the step of determining if the parameters indicate the combustion process is one of at the onset of combustion instability or is unstable comprises determining that the combustion process is unstable if an oscillation frequency is within the audible frequency range and an oscillation magnitude corresponds to at least a second threshold.

12. A method of maintaining combustion stability of a combustion process in a combustion system having a fuel nozzle and a combustion chamber, the method comprising the steps of:

placing an ion sensor in the combustion chamber such that the ion sensor is exposed to combustion gases, the ion sensor having at least one electrode proximate the fuel nozzle and at least one electrode on an outer wall of the combustion chamber;

applying a voltage between the at least one electrode proximate the fuel nozzle and the at least one electrode on the outer wall of the combustion chamber;

receiving an ion signal from the ion sensor;

determining an oscillation frequency and an oscillation magnitude from the ion signal; and

adjusting at least one parameter if the oscillation frequency and oscillation magnitude are indicative of one of an onset of combustion instability and combustion instability to drive the combustion process towards stability.

13. The method of claim 12 wherein the step of adjusting the at least one parameter includes adjusting a combustion system parameter.

14. The method of claim 12 further comprising the step of determining if the oscillation frequency and oscillation magnitude are indicative of one of an onset of combustion instability and combustion instability.

15. A method of maintaining combustion stability of a combustion process in a combustion system having a fuel nozzle and a combustion chamber, the method comprising the steps of:

placing an ion sensor in the combustion chamber such that the ion sensor is exposed to combustion gases;

receiving an ion signal from the ion sensor;

determining an oscillation frequency and an oscillation magnitude from the ion signal; and

adjusting at least one combustion system parameter if the oscillation frequency and oscillation magnitude are indicative of one of an onset of combustion instability and combustion instability to drive the combustion process towards stability; and

wherein the step of adjusting a combustion system parameter includes adjusting one of enriching the air/fuel ratio and adjusting the flow nozzle geometry of the fuel nozzle.

16. A method of maintaining combustion stability of a combustion process in a combustion system having a fuel nozzle and a combustion chamber, the method comprising the steps of:

placing an ion sensor in the combustion chamber such that the ion sensor is exposed to combustion gases;

receiving an ion signal from the ion sensor;

determining an oscillation frequency and an oscillation magnitude from the ion signal; and

adjusting at least one parameter if the oscillation frequency and oscillation magnitude are indicative of one of an onset of combustion instability and combustion instability to drive the combustion process towards stability,

wherein the step of determining if the oscillation frequency and oscillation magnitude are indicative of one of the onset of combustion instability and combustion instability includes determining that the oscillation frequency and oscillation magnitude are indicative of the onset of combustion instability if the oscillation frequency is within a predetermined frequency range and the oscillation magnitude corresponds to a first threshold.

17. The method of claim 16 wherein the predetermined frequency range is approximately ±

50 Hz from a critical frequency of the combustion system.

18. A method of maintaining combustion stability of a combustion process in a combustion system having a fuel nozzle and a combustion chamber, the method comprising the steps of:

placing an ion sensor in the combustion chamber such that the ion sensor is exposed to combustion gases;

receiving an ion signal from the ion sensor;

determining an oscillation frequency and an oscillation magnitude from the ion signal; and

adjusting at least one parameter if the oscillation frequency and oscillation magnitude are indicative of one of an onset of combustion instability and combustion instability to drive the combustion process towards stability,

wherein the step of determining if the oscillation frequency and oscillation magnitude are indicative of one of the onset of combustion instability and combustion instability includes determining that the oscillation frequency and oscillation magnitude are indicative of combustion instability if the oscillation frequency is within a predetermined frequency range and the oscillation magnitude corresponds to a second threshold.

19. The method of claim 18 wherein the predetermined frequency range is approximately ±

50 Hz from a critical frequency of the combustion system.

20. A system for detecting combustion instability of a combustion process in a combustion system having a fuel nozzle and a combustion chamber comprising:

an electronic module in communication with an ion sensor, the electronic module receiving an ion signal from the ion sensor and determining an oscillation frequency and an oscillation magnitude of the ion signal and adjusting at least one combustion parameter if the oscillation frequency and oscillation magnitude are indicative of one of an onset of combustion instability and combustion instability to drive the combustion process towards stability.

21. The system of claim 20 further comprising an ion sensor placed in the combustion chamber such that the ion sensor is exposed to combustion gases, the ion sensor in communication with the electronic module.

22. The system of claim 21 wherein the ion sensor is a retractable igniter and the electronic module monitors a temperature of the retractable igniter and actively positions the retractable igniter to take ion measurements and retracts the retractable igniter if the temperature is above a threshold.

23. The system of claim 20 further comprising a trim valve in series with the fuel nozzle and wherein the at least one parameter is the air/fuel ratio of the combustion chamber, the electronic module enriching the air/fuel ratio if the oscillation frequency and oscillation magnitude are indicative of one of an onset of combustion instability and combustion instability to drive the combustion process towards stability.

24. The system of claim 20 wherein the at least one parameter is the flow nozzle geometry of the fuel nozzle.