Systems and methods for controlling compressor extraction cooling

1. A method for controlling compressor extraction cooling in a gas turbine comprising a compressor and a turbine section, the method comprising:

providing a plurality of different cooling mediums;

extracting air from a compressor associated with a gas turbine;

injecting the different cooling mediums into the compressor extraction air, wherein the compressor extraction air is cooled by the cooling mediums prior to or during introduction to the turbine section;

determining, after injection of the different cooling mediums, an expected temperature of the compressor extraction air and a measured temperature of the compressor extraction air;

adjusting, based at least in part on a temperature difference between the expected temperature and the measured temperature, respective amounts of the cooling mediums injected into the compressor extraction air; and

selectively controlling at least one of the compressor extraction air or the cooling mediums based at least in part on a characteristic associated with the gas turbine.

2. The method of claim 1 , wherein the characteristic comprises at least one of: a downstream pressure in the turbine section, a downstream air temperature in the turbine section, a downstream metal temperature of a portion of the turbine section, ambient temperature, an air flow measurement associated with the compressor extraction air, a pressure measurement associated with the compressor extraction air, a temperature measurement associated with the compressor extraction air, a cooling medium flow measurement, a cooling medium temperature, a cooling medium pressure, or any combination thereof.

3. The method of claim 1 , wherein selectively controlling at least one of the compressor extraction air or the cooling medium based at least in part on a characteristic associated with the gas turbine comprises at least one of the following: controlling the amount of each cooling medium introduced to the compressor extraction air, controlling the temperature of each cooling medium introduced to the compressor extraction air, controlling the pressure of each cooling medium introduced to the compressor extraction air, controlling the amount of compressor extraction air introduced to the turbine section, controlling the temperature of compressor extraction air introduced to the turbine section, controlling the pressure of compressor extraction air introduced to the turbine section, or any combination thereof.

4. The method of claim 1 , wherein selectively controlling at least one of the compressor extraction air or the cooling mediums based at least in part on a characteristic associated with the gas turbine is facilitated by at least one of the following: an open-type loop control, an active-type control, a closed-type loop control, or a passive-type control.

5. The method of claim 1 , wherein selectively controlling at least one of the compressor extraction air or the cooling mediums based at least in part on a characteristic associated with the gas turbine is facilitated by an open-type loop controller comprising a table with one or more predefined target characteristics associated with the gas turbine.

6. The method of claim 1 , further comprising:

mounting one or more distribution devices to the gas turbine, wherein the one or more distribution devices can distribute at least a portion of the cooling mediums prior to or during introduction of the cooling mediums to the compressor extraction air.

7. The method of claim 1 , wherein providing the plurality of different cooling mediums comprises providing one or more distribution devices operable to distribute at least a portion of the cooling mediums prior to or during introduction of the cooling mediums to the compressor extraction air.

8. The method of claim 1 , wherein introducing the cooling mediums to the compressor extraction air comprises distributing at least a portion of the cooling mediums and introducing at least the distributed portion of the cooling mediums to the compressor extraction air.

9. The method of claim 1 , wherein selectively controlling at least one of the compressor extraction air or the cooling mediums based at least in part on a characteristic associated with the gas turbine is facilitated by at least one processor.

10. A system for controlling cooling of compressor extraction air in a gas turbine comprising a compressor and a turbine section, the system comprising:

one or more storage devices operable to store a plurality of different cooling mediums; one or more distribution devices operable to:

receive the different cooling mediums from the one or more storage devices; and inject at least a portion of the different cooling mediums prior to or during introduction of the cooling mediums into the compressor extraction air, wherein the compressor extraction air is cooled by the cooling mediums prior to introduction to the turbine section;

one or more control devices operable to:

determine, after injection of the different cooling mediums, an expected temperature of the compressor extraction air and a measured temperature of the compressor extraction air;

adjust, based at least in part on a temperature difference between the expected temperature and the measured temperature, respective amounts of the cooling mediums injected into the compressor extraction air; and

selectively control at least one of the compressor extraction air or the cooling mediums based at least in part on a characteristic associated with the gas turbine.

11. The system of claim 10 , wherein the characteristic comprises at least one of: a downstream pressure in the turbine section, a downstream air temperature in the turbine section, a downstream metal temperature of a portion of the turbine section, ambient temperature, an air flow measurement associated with the compressor extraction air, a pressure measurement associated with the compressor extraction air, a temperature measurement associated with the compressor extraction air, a cooling medium flow measurement, a cooling medium temperature, a cooling medium pressure, or any combination thereof.

12. The system of claim 10 , wherein selectively controlling at least one of the compressor extraction air or the different cooling mediums based at least in part on a characteristic associated with the gas turbine comprises at least one of the following: controlling the amount of each of the cooling mediums introduced to the compressor extraction air, controlling the temperature each of the cooling mediums introduced to the compressor extraction air, controlling the pressure each of the cooling mediums introduced to the compressor extraction air, controlling the amount of compressor extraction air introduced to the turbine section, controlling the temperature of compressor extraction air introduced to the turbine section, controlling the pressure of compressor extraction air introduced to the turbine section, or any combination thereof.

13. The system of claim 10 , wherein the one or more control devices can implement at least one of the following: an open-type loop control, an active-type control, a closed-type loop control, or a passive-type control.

14. The system of claim 10 , wherein the one or more control devices comprises an open-type loop controller comprising a table with one or more predefined target characteristics associated with the gas turbine.

15. A gas turbine comprising:

a turbine section;

a compressor, wherein air is extracted from at least one portion of the compressor for introduction into the turbine section;

one or more storage devices operable to store a plurality of different cooling mediums;

and

one or more distribution devices operable to:

receive the different cooling mediums from the one or more storage devices; and

inject at least a portion of the different cooling mediums prior to or during introduction of the cooling mediums into the air extracted from the at least one portion of the compressor, wherein the air is cooled by the cooling mediums prior to introduction to the turbine section; and

one or more control devices operable to:

determine, after injection of the different cooling mediums, an expected temperature of the compressor extraction air and a measured temperature of the compressor extraction air;

adjust, based at least in part on a temperature difference between the expected temperature and the measured temperature, respective amounts of the cooling mediums injected into the compressor extraction air; and

selectively control at least one of the compressor extraction air or the cooling mediums based at least in part on a characteristic associated with the gas turbine.

16. The gas turbine of claim 15 , wherein the characteristic comprises at least one of: a downstream pressure in the turbine section, a downstream air temperature in the turbine section, a downstream metal temperature of a portion of the turbine section, ambient temperature, an air flow measurement associated with the compressor extraction air, a pressure measurement associated with the compressor extraction air, a temperature measurement associated with the compressor extraction air, a cooling medium flow measurement, a cooling medium temperature, a cooling medium pressure, or any combination thereof.

17. The gas turbine of claim 15 , wherein selectively controlling at least one of the compressor extraction air or the cooling mediums based at least in part on a characteristic associated with the gas turbine comprises at least one of the following:

controlling the amount of each of the cooling mediums introduced to the compressor extraction air, controlling the temperature each of the cooling mediums introduced to the compressor extraction air, controlling the pressure each of the cooling mediums introduced to the compressor extraction air, controlling the amount of compressor extraction air introduced to the turbine section, controlling the temperature of compressor extraction air introduced to the turbine section, controlling the pressure of compressor extraction air introduced to the turbine section, or any combination thereof.

18. The gas turbine of claim 15 , wherein the one or more control devices can implement at least one of the following: an open-type loop control, an active-type control, a closed-type loop control, or a passive-type control.

19. The gas turbine of claim 15 , wherein the one or more control devices comprises an open-type loop controller comprising a table with one or more predefined target characteristics associated with the gas turbine.

20. The gas turbine of claim 15 , wherein the one or more control devices comprise at least one of the following: a processor, a software program, or a hardware component.