SYSTEM AND METHOD FOR GAS TURBINE POWER AUGMENTATION

• US 20110173947A1
• Filed: 01/19/2010
• Published: 07/21/2011
• Est. Priority Date: 01/19/2010
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: ZHANG, HUA, AMMANN, LISA KAMDAR, TOMEY, JAMES PATRICK, KIPPEL, BRADLY AARON, ZHANG, JIANMIN
• Application Number:
  US12/689,544
• Publication Number:
  US 20110173947A1
• Time in Patent Office: Days
• US Class Current: 60/39.83
• CPC Class Codes: F02C 7/185 Cooling means for reducing the temperature of the cooling air or gas
• CPC Class Codes: Y10T 137/0645 With condition responsive control means

Abstract

A gas turbine power augmentation system and method are provided. The system includes a chiller, a controller, a heat exchanger, and a gas turbine inlet air flow. The chiller may be operable to chill a coolant flow using energy from a heat source. The controller may be operably connected to the chiller and configured to regulate operation of the chiller in relation to at least one environmental condition. The heat exchanger may be in fluid communication with the chiller and configured to allow the coolant flow to pass through the heat exchanger. The gas turbine inlet air flow may be directed through the heat exchanger before entering a gas turbine inlet, allowing the air flow to interact with the coolant flow, thereby cooling the air flow.

Claims

1. A gas turbine power augmentation system comprising:

a chiller, the chiller operable to chill a coolant flow using energy from a heat source;

a controller operably connected to the chiller and configured to regulate operation of the chiller in relation to at least one environmental condition, wherein regulating operation of the chiller comprises operating the chiller to chill the coolant flow when the environmental condition is at a first environmental condition level and not operating the chiller to chill the coolant flow when the environmental condition is at a second environmental condition level;

a heat exchanger in fluid communication with the chiller and configured to allow the coolant flow to pass through the heat exchanger; and

a gas turbine inlet air flow, wherein the air flow is directed through the heat exchanger before entering a gas turbine inlet, allowing the air flow to interact with the coolant flow, thereby cooling the air flow.

2. The gas turbine power augmentation system of claim 1, wherein the environmental condition is the ambient relative humidity of air upstream of the heat exchanger.

3. The gas turbine power augmentation system of claim 1, wherein the first environmental condition level is an ambient relative humidity of air upstream of the heat exchanger at or above 50%, and the second environmental condition level is an ambient relative humidity of air upstream of the heat exchanger below 50%.

4. The gas turbine power augmentation system of claim 1, wherein the environmental condition is the temperature of air downstream of the heat exchanger.

5. The gas turbine power augmentation system of claim 1, wherein regulation of the operation of the chiller by the controller in relation to at least one environmental condition can be overridden to manage at least one operating condition.

6. The gas turbine power augmentation system of claim 5, wherein the operating condition is grid stability.

7. The gas turbine power augmentation system of claim 1, wherein the air flow is cooled primarily through sensible cooling when the environmental condition is at the first environmental condition level and cooled primarily through latent cooling when the environmental condition is at the second environmental condition level.

8. The gas turbine power augmentation system of claim 1, wherein the chiller is an absorption chiller.

9. The gas turbine power augmentation system of claim 1, wherein the heat exchanger is a direct-contact heat exchanger.

10. The gas turbine power augmentation system of claim 1, wherein the heat source is one of gas turbine exhaust, heat recovery steam generator water, heat recovery steam generator steam, steam turbine sealing steam, waste hot water, or generator cooling water.

11. A gas turbine power augmentation system comprising:

an absorption chiller, the absorption chiller operable to chill a coolant flow using energy from a heat source;

a direct-contact heat exchanger, the direct-contact heat exchanger in fluid communication with the absorption chiller and configured to allow the coolant flow to pass through the direct-contact heat exchanger;

a controller operably connected to the absorption chiller, the controller configured to monitor the ambient relative humidity of air upstream of the direct-contact heat exchanger, to operate the absorption chiller to chill the coolant flow when the ambient relative humidity is at or above a fixed ambient relative humidity level, and to not operate the absorption chiller to chill the coolant flow when the ambient relative humidity is below the fixed ambient relative humidity level; and

a gas turbine inlet air flow, wherein the air flow is directed through the heat exchanger before entering a gas turbine inlet, allowing the air flow to interact with the coolant flow, thereby cooling the air flow,

wherein the air flow is cooled primarily through sensible cooling when the ambient relative humidity is at or above the fixed ambient relative humidity level and cooled primarily through latent cooling when the ambient relative humidity is below the fixed ambient relative humidity level.

12. The gas turbine power augmentation system of claim 11, wherein the fixed ambient relative humidity level is 50%.

13. The gas turbine power augmentation system of claim 11, wherein the heat source is one of gas turbine exhaust, heat recovery steam generator water, heat recovery steam generator steam, steam turbine sealing steam, waste hot water, or generator cooling water.

14. A method for augmenting gas turbine power comprising:

measuring at least one environmental condition;

regulating operation of a chiller in relation to the at least one environmental condition, wherein operation of the chiller chills a coolant flow using energy from a heat source, and wherein regulating operation of the chiller comprises operating the chiller to chill the coolant flow when the environmental condition is at a first environmental condition level and not operating the chiller to chill the coolant flow when the environmental condition is at a second environmental condition level; and

communicating the coolant flow through a heat exchanger, wherein the heat exchanger is configured to allow a gas turbine inlet air flow passing through the heat exchanger to interact with the coolant flow, thereby cooling the air flow before the air flow enters a gas turbine inlet.

15. The method for augmenting gas turbine power of claim 14, wherein the environmental condition is the ambient relative humidity of air upstream of the heat exchanger.

16. The method for augmenting gas turbine power of claim 14, wherein the first environmental condition level is an ambient relative humidity of air upstream of the heat exchanger at or above 50%, and the second environmental condition is an ambient relative humidity of air upstream of the heat exchanger below 50%.

17. The method for augmenting gas turbine power of claim 14, wherein the environmental condition is the temperature of air downstream of the heat exchanger.

18. The method for augmenting gas turbine power of claim 14, wherein the chiller is an absorption chiller.

19. The method for augmenting gas turbine power of claim 14, wherein the heat exchanger is a direct-contact heat exchanger.

20. The method for augmenting gas turbine power of claim 14, wherein the heat source is one of gas turbine exhaust, heat recovery steam generator water, heat recovery steam generator steam, steam turbine sealing steam, waste hot water, or generator cooling water.