System and method for thermal control in a gas turbine engine

• US 9,003,764 B2
• Filed: 12/16/2011
• Issued: 04/14/2015
• Est. Priority Date: 12/16/2011
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (GE Vernova, Inc.)
• Original Assignee: General Electric Company
• Inventors: Thacker, Pradeep Stanley, Avagliano, Aaron John
• Primary Examiner(s): SUNG, GERALD LUTHER
• Application Number:
  US13/329,203
• Publication Number:
  US 20130152598A1
• Time in Patent Office: 1,215 Days
• Field of Search: 60/391.82, 60/395, 60/391.7, 60/395.2, 122/7.R, 122/7.B
• US Class Current: 60/39.52
• CPC Class Codes: F02C 1/007 combination of cycles
• CPC Class Codes: F02C 1/06 using reheated exhaust gas F02C1/08 takes precedence
• CPC Class Codes: F02C 6/00 Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
• CPC Class Codes: F02C 6/003 Gas-turbine plants with heaters between turbine stages
• CPC Class Codes: F02C 6/04 Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output F02C6/18 takes precedence ; for a fluidised-bed combustor F02C3/205
• CPC Class Codes: Y02E 20/14 Combined heat and power generation [CHP]
• CPC Class Codes: Y02E 20/16 Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

Abstract

A system includes a gas turbine engine that includes a compressor section configured to generate compressed air and a combustor coupled to the compressor section. The combustor is configured to combust a first mixture comprising the compressed air and a first fuel to generate a first combustion gas. The gas turbine engine also includes a turbine section coupled to the combustor. The turbine section is configured to expand the first combustion gas to generate an exhaust gas. The gas turbine engine also includes a boiler coupled to the turbine section. The boiler is configured to combust a second mixture comprising a portion of the first combustion gas and a second fuel to generate a second combustion gas that is routed to the turbine section. In addition, the boiler generates a first steam from heat exchange with the second combustion gas.

Claims

1. A system, comprising:

a gas turbine engine, comprising;

a compressor section configured to generate compressed air;

a combustor coupled to the compressor section, wherein the combustor is configured to combust a first mixture comprising the compressed air and a first fuel to generate a first combustion gas;

a turbine section coupled to the combustor, wherein the turbine section is configured to expand the first combustion gas to generate an exhaust gas; and

a boiler coupled to the turbine section, wherein the boiler is configured to combust a second mixture comprising a portion of the first combustion gas and a second fuel to generate a second combustion gas that is routed into the turbine section at a gas return location downstream from the combustor, and wherein the boiler generates a first steam from heat exchange with the second combustion gas.

2. The system of claim 1, wherein a temperature of the exhaust gas is greater than approximately 575 degrees Celsius.

3. The system of claim 1, comprising a steam power plant coupled to the turbine section.

4. The system of claim 1, wherein the steam power plant comprises:

a heat recovery steam generator (HRSG) coupled to the turbine section, wherein the HRSG is configured to generate a second steam from heat exchange with the exhaust gas; and

a steam turbine coupled to the HRSG, wherein the steam turbine is configured to drive a load using at least the first steam, or the second steam, or a combination thereof.

5. The system of claim 4, wherein the HRSG is configured to receive the first steam.

6. The system of claim 1, wherein the compressor section comprises a plurality of compressor stages and the turbine section comprises a plurality of turbine stages.

7. The system of claim 6, wherein the boiler is fluidly coupled to a first turbine stage of the plurality of turbine stages, or a second turbine stage of the plurality of turbine stages, or both the first and second turbine stages of the plurality of turbine stages at one or more locations downstream from the combustor.

8. The system of claim 6, comprising an intercooler coupled to a first compressor stage and a second compressor stage of the plurality of compressor stages, wherein the intercooler is configured to cool a first compressed air generated by the first compressor stage.

9. The system of claim 1, comprising a plurality of boilers fluidly coupled to the turbine section at one or more locations downstream from the combustor.

10. The system of claim 1, comprising a plurality of gas turbine engines fluidly coupled to the boiler at one or more locations downstream from the combustor.

11. The system of claim 1, wherein the compressor section comprises:

a first compressor configured to generate an air flow;

an intercooler coupled to the first compressor, wherein the intercooler is configured to cool the air flow; and

a second compressor coupled to the intercooler, wherein the second compressor is configured to compress the air flow to generate the compressed air.

12. The system of claim 1, comprising a controller configured to control the boiler to increase a temperature of the exhaust gas.

13. A system, comprising:

a turbine controller configured to control a reheater to increase a temperature of an exhaust gas generated by a combustor of a turbine engine having a turbine coupled to the reheater, wherein the reheater is configured to combust a mixture comprising a first combustion gas and a fuel to generate a second combustion gas that is routed into the turbine at a gas return location downstream from the combustor to be expanded in the turbine, and wherein the reheater generates steam from heat exchange with the second combustion gas.

14. The system of claim 13, wherein the reheater comprises:

a reheat combustor configured to combust the first combustion gas and the fuel to generate the second combustion gas,

a superheater heat exchanger configured to generate a superheated steam from heat exchange with the second combustion gas,

a reheater heat exchanger configured to generate a reheated steam from heat exchange with the second combustion gas, and

a boiler heat exchanger configured to generate steam from heat exchange with the second combustion gas.

15. The system of claim 14, wherein the reheater comprises a plurality of combustors.

16. The system of claim 13, wherein the mixture comprises compressed air from a compressor section coupled to the turbine.

21. The system of claim 13, comprising the reheater coupled to the turbine controller.

22. The system of claim 13, wherein the reheater is separate from a heat recovery steam generator (HRSG) coupled to the turbine engine.

17. A method, comprising:

compressing air in a compressor section of a turbine engine to generate compressed air;

combusting a first mixture comprising the compressed air and a first fuel in a combustor of the turbine engine downstream from the compressor section to generate a first combustion gas;

expanding the first combustion gas in a turbine section of the turbine engine downstream from the combustor to generate an exhaust gas;

combusting a second mixture comprising a portion of the first combustion gas and a second fuel in a boiler fluidly coupled to the turbine section downstream from the combustor to generate a second combustion gas;

routing the second combustion gas into the turbine section at a gas return location downstream from the combustor; and

generating a first steam in the boiler by exchanging heat from the second combustion gas to a boiler feedwater.

18. The method of claim 17, comprising generating a superheated steam in the boiler by exchanging heat from the second combustion gas to an inlet steam.

19. The method of claim 17, comprising generating a second steam in a heat recovery steam generator (HRSG) from heat exchange with the exhaust gas.

20. The method of claim 17, wherein the turbine section comprises a plurality of turbine stages, wherein the boiler is fluidly coupled to a first turbine stage of the plurality of turbine stages, or a second turbine stage of the plurality of turbine stages, or both the first and second turbine stages of the plurality of turbine stages at one or more locations downstream from the combustor.

23. A system, comprising:

a gas turbine engine, comprising;

a compressor section configured to generate compressed air;

a combustor coupled to the compressor section, wherein the combustor is configured to combust a first mixture comprising the compressed air and a first fuel to generate a first combustion gas;

a turbine section coupled to the combustor, wherein the turbine section is configured to expand the first combustion gas to generate an exhaust gas; and

a boiler coupled to the turbine section, wherein the boiler is configured to combust a second mixture comprising a portion of the first combustion gas and a second fuel to generate a second combustion gas that is routed to the turbine section, and wherein the boiler generates a first steam from heat exchange with the second combustion gas; and

a heat recovery steam generator (HRSG) coupled to the turbine section, wherein the HRSG is configured to generate a second steam from heat exchange with the exhaust gas.