Systems and methods for controlling mode transfers of a combustor

Patent metadata

Field	Value
Publication number	US-9810156-B2
Application number	US-201213718588-A
Country	US
Kind code	B2
Filing date	Dec 18, 2012
Priority date	Dec 18, 2012
Publication date	Nov 7, 2017
Grant date	Nov 7, 2017

Abstract

Systems and methods for controlling mode transfers of a turbine combustor are provided. According to one embodiment, a system may include a controller to control a combustor, and a processor communicatively coupled to the controller. The processor may be configured to receive current operating conditions, target operating limits, and combustor transfer functions. The combustor transfer functions may be evaluated to estimate operating limits associated with one or more combustion modes under the current operating conditions. The estimated operating limits associated with the one or more combustor modes may be compared to the target operating limits, and, based on the comparison, at least one of the combustion modes may be selected. The combustor may then be selectively transferred to the selected combustion mode.

First claim

What is claimed is:

1. A method for controlling mode transfers of a combustor, the method comprising:
receiving, by a processor, one or more current operating conditions associated with a current combustion mode;
receiving, by the processor, one or more target operating limits;
receiving, by the processor, one or more combustor transfer functions;
evaluating, by the processor, the one or more combustor transfer functions to estimate one or more operating limits associated with the current combustion mode and one or more operating limits associated with a plurality of combustion modes under the one or more current operating conditions to obtain one or more estimated operating limits associated with the current combustion mode and one or more estimated operating limits associated with the plurality of combustion modes, wherein the current combustion mode is not included in the plurality of combustion modes;
comparing, by the processor, the one or more estimated operating limits associated with the current combustion mode and the one or more estimated operating limits associated with the plurality of combustion modes to the one or more target operating limits to determine similarity of the one or more estimated operating limits associated with the current combustion mode and the one or more estimated operating limits associated with the plurality of combustion modes to the one or more target operating limits;
based on the comparing, scoring the current combustion mode and each of the plurality of combustion modes to determine a combustion mode with a desired performance for the one or more current operating conditions, wherein the combustion mode with the desired performance has a highest similarity of one or more estimated operating limits associated with the combustion mode with the desired performance to the one or more target operating limits;
based at least in part on the scoring, selecting, by the processor, from the current combustion mode and the plurality of combustion modes, the combustion mode with the desired performance for the one or more current operating conditions;
determining that the combustion mode with the desired performance selected from the current combustion mode and the plurality of combustion modes includes one of the plurality of combustion modes;
based on the determining that the combustion mode with the desired performance includes one of the plurality of combustion modes, determining whether one or more differences between the one or more estimated operating limits associated with the combustion mode with the desired performance and the one or more estimated operating limits associated with the current combustion mode exceed one or more predetermined threshold values; and
when the one or more differences exceed the one or more predetermined threshold values, transferring the combustor to the combustion mode with the desired performance.

2. The method of claim 1 , wherein the combustor comprises a Dry Low Nitrogen Oxide (DLN) combustor.

3. The method of claim 1 , wherein the one or more current operating conditions comprise one or more of a loading rate and an ambient temperature.

4. The method of claim 1 , wherein the one or more target operating limits comprise one or more of an emission, a combustion instability, a lean blowout boundary, combustor dynamics, a fuel supply pressure, and a temperature.

5. The method of claim 1 , wherein the one or more current operating conditions comprise one or more of a real-time calculated machine condition and a measured machine operating condition.

6. The method of claim 1 , wherein the one or more combustor transfer functions comprise an objective function providing a real-time score of a combustion mode based on the one or more estimated operating limits associated with the combustion mode.

7. The method of claim 6 , further comprising reevaluating, by the processor, the one or more combustor transfer functions under the one or more current operating conditions.

8. A system for controlling mode transfers of a combustor, the system comprising:
a controller configured to control the combustor; and
a processor communicatively coupled to the controller and configured to:
receive one or more current operating conditions associated with a current combustion mode;
receive one or more target operating limits;
receive one or more combustor transfer functions;
evaluate the one or more combustor transfer functions to estimate one or more operating limits associated with the current combustion mode and one or more operating limits associated with a plurality of combustion modes under the one or more current operating conditions to obtain one or more estimated operating limits associated with the current combustion mode and one or more estimated operating limits associated with the plurality of combustion modes, wherein the current combustion mode is not included in the plurality of combustion modes;
compare the one or more estimated operating limits associated with the current combustion mode and the one or more estimated operating limits associated with the plurality of combustion modes to the one or more target operating limits to determine similarity of the one or more estimated operating limits associated with the current combustion mode and the one or more estimated operating limits associated with the plurality of combustion modes to the one or more target operating limits;
score the current combustion mode and each of the plurality of combustion modes to determine a combustion mode with a desired performance for the one or more current operating conditions, wherein the combustion mode with the desired performance has a highest similarity of one or more estimated operating limits associated with the combustion mode with the desired performance to the one or more target operating limits;
select, from the current combustion mode and the plurality of combustion modes, the combustion mode with the desired performance for the one or more current operating conditions;
determine that the combustion mode with the desired performance selected from the current combustion mode and the plurality of combustion modes includes one of the plurality of combustion modes;
determine whether one or more differences between the one or more estimated operating limits associated with the combustion mode with the desired performance and the one or more estimated operating limits associated with the current combustion mode exceed one or more predetermined threshold values; and
when the one or more differences exceed the one or more predetermined threshold values, transfer the combustor to the combustion mode with the desired performance.

9. The system of claim 8 , wherein the combustor comprises a Dry Low Nitrogen Oxide (DLN) combustor.

10. The system of claim 8 , wherein the one or more current operating conditions comprise one or more of a loading rate and an ambient temperature.

11. The system of claim 8 , wherein the one or more operating limits comprise one or more of an emission, a combustion instability, a lean blowout boundary, combustor dynamics, a fuel supply pressure, and a temperature.

12. The system of claim 8 , wherein the one or more operating conditions comprise one or more of a real-time calculated machine condition and a measured machine operating condition.

13. The system of claim 8 , wherein the one or more combustor transfer functions comprise an objective function providing a real-time score of a combustion mode based on the one or more estimated operating limits associated with the combustion mode.

14. The system of claim 13 , wherein the processor is further con

Assignees

• Gen Electric

Inventors

• Terry Jason Charles
• Healy Timothy Andrew

Classifications

• F23N2241/20

  Gas turbines · CPC title

• F23N5/203 Primary

  using electronic means · CPC title

• F02C9/28

  Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) · CPC title

• F02C9/00 Primary

  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 title

• F23N2041/20

  Mechanical Engineering · mapped topic