GAS TURBINE AND METHOD OF CONTROLLING A GAS TURBINE AT PART-LOAD CONDITION

• US 20140182297A1
• Filed: 01/03/2013
• Published: 07/03/2014
• Est. Priority Date: 01/03/2013
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Terry, Jason Charles, Healy, Timothy Andrew, Pinson, Mark William, Jensen, Gregory Earl
• Application Number:
  US13/733,313
• Publication Number:
  US 20140182297A1
• Time in Patent Office: Days
• US Class Current: 60/773
• 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: F02C 9/48 Control of fuel supply conjointly with another control of the plant with nozzle section control F02K1/17

Abstract

A gas turbine includes a compressor section, a combustion section downstream from the compressor section, a turbine section downstream from the combustion section, and a controller. The controller controls the operation of the gas turbine at a reduced load, and is capable of querying a database including multiple sets of operational parameters for the gas turbine correlated with at least one measured output response at each set of operational parameters. One of the sets of operational parameters provides a desired gas turbine load that meets a target level for the output response. Related methods are also disclosed.

Claims

1. A method of operating a gas turbine at a reduced load, the method comprising:

operating a gas turbine at multiple sets of operational parameters;

measuring at least one output response of the gas turbine at each of the sets of operational parameters;

creating a database at least partially including correlations of each of the sets of operational parameters with the measured output response;

determining a desired reduced gas turbine load;

selecting a set of operational parameters from the database that provides the desired reduced gas turbine load and that meets a target level for the output response; and

further operating the gas turbine at the selected set of operational parameters.

2. The method of claim 1, further including the steps of:

measuring the output response during the further operation of the gas turbine;

comparing the measured output response to the target level for the output response; and

selecting an alternate set of operational parameters if the measured output response does not meet the target level.

3. The method of claim 2, further including, after the selecting an alternate set of operational parameters step, repeating the further operating step and the steps thereafter.

4. The method of claim 1, wherein the set of operational parameters includes one or more of the level of an inlet guide vane angle, an inlet bleed heat, a combustor fuel split, and a control curve.

5. The method of claim 1, wherein the output response includes one or more of a level of emissions, lean blowout, and combustor instability.

6. The method of claim 1, wherein the creating step includes generating partial derivatives relating the operational parameters to the measured output response.

7. The method of claim 1, further including adding to the database the measured output response at the set of operational parameters.

8. A method of operating a gas turbine at a reduced load, the method comprising:

determining a desired reduced gas turbine load;

consulting a database including multiple sets of operational parameters correlated with at least one measured output response at each set of operational parameters;

selecting a set of operational parameters from the database that corresponds to the reduced gas turbine load and that meets a target level for the output response; and

operating the gas turbine at the selected set of operational parameters.

9. The method of claim 8, further including the steps of:

measuring the output response during the operation of the gas turbine;

comparing the measured output response to the target level for the output response; and

selecting an alternate set of operational parameters if the measured output response does not meet the target level.

10. The method of claim 9, further including, after the selecting an alternate set of operational parameters step, repeating the operating step and the steps thereafter.

11. The method of claim 8, wherein the set of operational parameters includes one or more of the level of an inlet guide vane angle, an inlet bleed heat, a combustor fuel split, and a control curve.

12. The method of claim 8, wherein the output response includes one or more of a level of emissions, lean blowout, and combustor instability.

13. The method of claim 8, further including adding to the database the measured output response at the set of operational parameters.

14. The method of claim 8, wherein the database is created at least partially via operation of the gas turbine.

15. The method of claim 8, wherein the database is created at least partially via modeling.

16. A gas turbine including:

a compressor section;

a combustion section downstream from the compressor section;

a turbine section downstream from the combustion section; and

a controller for controlling the operation of the gas turbine at a reduced load, the controller capable of querying a database including multiple sets of operational parameters for the gas turbine correlated with at least one measured output response at each set of operational parameters, one of the sets of operational parameters providing a desired gas turbine load and that meets a target level for the output response.

17. The gas turbine of claim 16, wherein the set of operational parameters includes one or more of the level of an inlet guide vane angle, an inlet bleed heat, a combustor fuel split, and a control curve.

18. The gas turbine of claim 16, wherein the output response includes one or more of a level of emissions, lean blowout, and combustor instability.

19. The gas turbine of claim 16, further including at least one sensor in communication with the controller for sensing at least one output response.

20. The gas turbine of claim 19, wherein the controller adds to the database the sensed output response correlated with the set of operational parameters.

21. The gas turbine of claim 16, wherein the measured output responses are determined at least partially via operation of the gas turbine.

22. The gas turbine of claim 16, wherein the measured output responses are determined at least partially via modeling.