Model-less combustion dynamics autotune

Patent metadata

Field	Value
Publication number	US-10830443-B2
Application number	US-201615391450-A
Country	US
Kind code	B2
Filing date	Dec 27, 2016
Priority date	Nov 30, 2016
Publication date	Nov 10, 2020
Grant date	Nov 10, 2020

Abstract

This disclosure relates to systems and methods for tuning combustion dynamics in a combustor. In one embodiment of the disclosure, a method includes providing, via at least one sensor, combustion dynamics amplitude data associated with a combustor. Method may allow monitoring, by an equipment controller communicatively coupled to the at least one sensor, the combustion dynamics amplitude data. The method may allow detecting at least one change in acoustic pressure amplitude associated with combustion in the combustor. In response to detecting the change in the acoustic pressure amplitude, the method proceeds with determining a fuel split change to at least two fuel circuits configured to supply fuel to the combustor, and applying the fuel split change to the combustor.

First claim

What is claimed is:

1. A system for tuning of combustion dynamics, the system comprising:
a combustor;
a primary fuel circuit in communication with the combustor;
a secondary fuel circuit in communication with the combustor;
at least one combustion dynamics amplitude data sensor associated with the combustor configured to convert combustion dynamics amplitude data into at least one electrical signal;
at least one nitrogen oxide emission sensor associated with the combustor;
a split control; and
an equipment controller communicatively coupled to the at least one combustion dynamics amplitude data sensor and the at least one nitrogen oxide emission sensor,
wherein the equipment controller is configured to:
determine target nitrogen oxide emissions via a target emissions module, wherein the target nitrogen oxide emissions is based at least in part on a load, a measured nitrogen oxide emission via the at least one nitrogen oxide emission sensor, and a cycle of a turbine in communication with the combustor;
receive the at least one electrical signal from the at least one combustion dynamics amplitude data sensor;
analyze an exhaust temperature of the combustor;
analyze the measured nitrogen oxide emission associated with combustion in the combustor;
analyze predicted nitrogen oxide emissions via a predicted emissions module, wherein the predicted emissions module is configured to predict the predicted nitrogen oxide emissions based at least in part on the exhaust temperature;
analyze the at least one electrical signal to detect at least one change in an acoustic pressure amplitude associated with combustion in the combustor, wherein detection of the at least one change in the acoustic pressure amplitude includes:
dividing the at least one electrical signal into a set of several ranges of frequencies,
determining predefined dynamics amplitude threshold levels within each frequency ranges in the set of several ranges of frequencies, wherein the predefined dynamics amplitude threshold levels include a low amplitude level, a lower acceptable amplitude level, a higher acceptable amplitude level, a high amplitude level, a significantly high amplitude level, and a highest amplitude level, and
determining that the acoustic pressure amplitude exceeds a predefined dynamics amplitude threshold levels for at least one vibrational frequency band within each of the frequency ranges in the set of several ranges of frequencies;

select predefined splits based on each of the predefined dynamics amplitude threshold levels in each of the frequency ranges in the set of several ranges of frequencies, wherein the predefined splits include a direction and a value of split change that should be used when the acoustic pressure amplitude reaches one of the predefined dynamics amplitude threshold levels: a predefined increase at the low amplitude level, no split change at the lower acceptable amplitude level, no split change at the higher acceptable amplitude level, a small predefined decrease at the high amplitude level, a medium predefined decrease at the significantly high amplitude level, and a large predefined decrease at the highest amplitude level;
determine a fuel split change in response to the at least one change in the acoustic pressure amplitude, the predicted nitrogen oxide emissions, and the target nitrogen oxide emission, the fuel split change being a change of the ratio of flow between the primary fuel circuit and the secondary fuel circuit, wherein determining the fuel split change is based on one of the predefined splits; and
apply the fuel split change to the split control, and

wherein the split control is configured to provide the fuel split change between the primary fuel circuit and the secondary fuel circuit.

2. The system of claim 1 , wherein the set of several ranges of frequencies includes a range of frequencies from a low range of frequencies to a high range of frequencies.

3. The system of claim 1 , wherein the predefined dynamics amplitude threshold levels are based on at least one of the following: a type of the combustor, acoustics inside the combustor, and a geometrical shape of the combustor.

4. The system of claim 1 , wherein the at least one nitrogen oxide emission sensor is coupled to the equipment controller, and wherein the equipment controller is further configured to:
determine that the measured nitrogen oxide emission exceeds a predefined emissions threshold; and
based on determining the measured nitrogen oxide emission exceeds the predefined emissions threshold, adjust control parameters of the combustor to correct the measured nitrogen oxide emission.

5. The system of claim 1 , wherein the fuel split change is provided by the split control incrementally for a period of time until the at least one change in the acoustic pressure amplitude in the combustor is eliminated.

6. The system of claim 5 , wherein the equipment controller is further configured to:
determine that the combustion dynamics amplitude are within predefined allowable limits;
in response to determining:
increment the fuel split change to reduce the combustion dynamics amplitude level;
provide the fuel split change to an emissions algorithm configured to control the measured nitrogen oxide emission of the combustor to allow the emission algorithm maintain the measured nitrogen oxide emission within acceptable emissions limits.

7. The system of claim 5 , wherein the period is determined based on conditions of a site and needs and variability of a machine, the site and the machine being associated with the combustor.

8. A method for tuning of combustion dynamics in a combustor, the method comprising:
providing, via at least one combustion dynamics amplitude data sensor, combustion dynamics amplitude data associated with the combustor in a form of at least one electrical signal;
providing, via at least one nitrogen oxide emission sensor, nitrogen oxide emission data associated with the combustor;
determining predicted nitrogen oxide emissions via a predicted emissions module, wherein the predicted emissions module is configured to predict the predicted nitrogen oxide emissions based at least in part on exhaust temperature;
determining target emissions via a target emissions module, wherein the target emissions is based at least in part on a load, a measured emission via the at least one nitrogen oxide emission sensor, and a cycle of a turbine in communication with the combustor;
monitoring, by an equipment controller communicatively coupled to the at least one combustion dynamics amplitude data sensor, the at least one electrical signal to detect at least one change in an acoustic pressure amplitude associated with combustion in the combustor, wherein detection of the at least one change in the acoustic pressure amplitude includes:
dividing the at least one electrical signal into a set of several ranges of frequencies,
determining predefined dynamics amplitude threshold levels within each frequency ranges in the set of several ranges of frequencies, wherein the predefined dynamics amplitude threshold levels include a low amplitude level, a lower acceptable amplitude level, a higher acceptable amplitude level, a high amplitude level, a significantly high amplitude level, and a highest amplitude level, and
determining that the acoustic pressure amplitude exceeds a predefined dynamics amplitude threshold levels for at least one vibrational frequency band within each of the frequency ranges in the set of several ranges of frequencies;

selecting predefined splits based on each of the predefined dynamics amplitude threshold levels in each of the frequency ranges in the set of several ranges of frequencies, wherein the predefined splits include a dir

Assignees

• Gen Electric

Inventors

• Arthanari Akilezkrishnamurthy
• Lal Mihir
• Harper James
• Dean Douglas Edward
• Kulkarni Abhijit Prabhakar

Classifications

• F02C9/34

  Joint control of separate flows to main and auxiliary burners · CPC title

• F23R3/34 Primary

  Feeding into different combustion zones · CPC title

• F02C7/00 Primary

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · 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

• F02C9/26

  Control of fuel supply (F02C9/48 takes precedence; fuel valves F02C7/232) · CPC title