Method and apparatus for detecting combustion instability in continuous combustion systems

• US 7,204,133 B2
• Filed: 08/31/2005
• Issued: 04/17/2007
• Est. Priority Date: 12/26/2002
• Status: Expired due to Term

• Current Assignee: Woodward Governor Company
• Original Assignee: Woodward Governor Company
• Inventors: Van Dyne, Ed, Tozzi, Luigi P., Benson, Kelly J., Barrett, Jeff B.
• Primary Examiner(s): MCCALL, ERIC SCOTT
• Application Number:
  US11/216,317
• Publication Number:
  US 20060000260A1
• Time in Patent Office: 594 Days
• Field of Search: 73/350.1, 73/350.3, 73/350.6, 73/350.7, 73/350.8, 731/16, 731/172, 731/173, 731/181
• 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 in the continuous combustion system 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.

2. The system of claim 1 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.

3. The system of claim 2 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 position the retractable igniter to keep the retractable igniter exposed to gases in the combustion region and below a temperature threshold.

5. 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.

6. 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, the at least one retractable igniter being retractable during operation of the continuous combustion system; 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.

7. The system of claim 6 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.

8. The system of claim 7 wherein the controller is further adapted to retract the at least one retractable igniter if the temperature is rapidly approaching the threshold.

9. The system of claim 6 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.

10. The system of claim 6 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.

11. A method for detecting combustion instability in a lean premix gas turbine having a combustion chamber and 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 of the lean premix gas turbine;

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

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.

12. The method of claim 11 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.

13. The method of claim 12 wherein the first threshold corresponds to±

1 psi.

14. The method of claim 12 wherein the predetermined frequency range is approximately±

50 Hz of a critical frequency of the gas turbine.

15. The method of claim 12 wherein the predetermined frequency range is between approximately 10 Hz and approximately 10 kHz.

16. The method of claim 12 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.