System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system

Patent metadata

Field	Value
Publication number	US-10683801-B2
Application number	US-201715456957-A
Country	US
Kind code	B2
Filing date	Mar 13, 2017
Priority date	Nov 2, 2012
Publication date	Jun 16, 2020
Grant date	Jun 16, 2020

Abstract

A system includes a gas turbine system having a turbine combustor, a turbine driven by combustion products from the turbine combustor, and an exhaust gas compressor driven by the turbine. The exhaust gas compressor is configured to compress and supply an exhaust gas to the turbine combustor. The gas turbine system also has an exhaust gas recirculation (EGR) system. The EGR system is configured to recirculate the exhaust gas along an exhaust recirculation path from the turbine to the exhaust gas compressor. The system further includes a main oxidant compression system having one or more oxidant compressors. The one or more oxidant compressors are separate from the exhaust gas compressor, and the one or more oxidant compressors are configured to supply all compressed oxidant utilized by the turbine combustor in generating the combustion products.

First claim

The invention claimed is:

1. A system, comprising:
a gas turbine system, comprising:
a turbine combustor;
a turbine driven by combustion products from the turbine combustor; and
an exhaust gas compressor driven by the turbine, wherein the exhaust gas compressor is configured to compress and supply an exhaust gas to the turbine combustor;

an exhaust gas recirculation (EGR) system, wherein the EGR system is configured to recirculate the exhaust gas along an exhaust recirculation path from the turbine to the exhaust gas compressor;
a main oxidant compression system configured to supply compressed oxidant to the gas turbine system, and the main oxidant compression system comprises:
a first oxidant compressor coupled to a shaft of the gas turbine system, such that the first oxidant compressor is at least partially driven by the gas turbine system; and
a second oxidant compressor;

an electrical generator coupled to the shaft of the gas turbine system;
a drive coupled to the second oxidant compressor, wherein the drive comprises a steam turbine or an electric motor; and
a gearbox coupling the drive to the second oxidant compressor, wherein the gearbox is configured to enable the second oxidant compressor to operate at a speed different from an operating speed of the drive.

2. The system of claim 1 , wherein the first oxidant compressor and the second oxidant compressor are configured to operate in a series configuration of compression.

3. The system of claim 2 , wherein the first oxidant compressor is a low pressure oxidant compressor and the second oxidant compressor is a high pressure oxidant compressor.

4. The system of claim 1 , wherein the drive coupled to the second oxidant compressor comprises the steam turbine.

5. The system of claim 4 , wherein the EGR system comprises a heat recovery steam generator configured to receive a stream of water to generate steam via a heat exchange relationship with the exhaust gas.

6. The system of claim 5 , wherein the heat recovery generator is configured to supply the steam to the steam turbine, and wherein the steam turbine is configured to drive the second oxidant compressor via electric power generated from the steam.

7. The system of claim 1 , wherein the drive is the electric motor, and wherein the electric motor receives electric power from the generator to drive the second oxidant compressor.

8. The system of claim 1 , wherein the gearbox comprises a parallel shaft gearbox having input and output shafts that are generally parallel with one another, or wherein the gearbox comprises an epicyclic gearbox having input and output shafts in line with one another.

9. The system of claim 1 , comprising a stoichiometric combustion system having the turbine combustor configured to combust a fuel/oxidant mixture in a combustion equivalence ratio of between 0.95 and 1.05 fuel to oxygen in the oxidant.

10. A system, comprising:
a gas turbine system, comprising:
a turbine combustor;
a turbine driven by combustion products from the turbine combustor; and
an exhaust gas compressor driven by the turbine, wherein the exhaust gas compressor is configured to compress and supply an exhaust gas to the turbine combustor;

an exhaust gas recirculation (EGR) system, wherein the EGR system is configured to recirculate the exhaust gas along an exhaust recirculation path from the turbine to the exhaust gas compressor; and
a main oxidant compression system configured to supply compressed oxidant to the gas turbine system, and the main oxidant compression system comprises:
a first oxidant compressor coupled to a shaft of the turbine of the gas turbine system in series, such that the first oxidant compressor is at least partially driven by the gas turbine system;
a second oxidant compressor coupled to the shaft of the turbine of the gas turbine system in series between the first oxidant compressor and the gas turbine, such that the second oxidant compressor is at least partially driven by the gas turbine system; and
a gearbox coupled to the shaft of the turbine of the gas turbine system between the first oxidant compressor and the second oxidant compressor, wherein the gearbox is configured to enable the first oxidant compressor to operate at a speed different from the second oxidant compressor.

11. The system of claim 10 , wherein the first oxidant compressor receives compressed oxidant from the second oxidant compressor.

12. The system of claim 11 , wherein the first oxidant compressor is a high pressure oxidant compressor and the second oxidant compressor is a low pressure oxidant compressor.

13. The system of claim 11 , wherein the first oxidant compressor is a centrifugal compressor and the second oxidant compressor is an axial flow compressor.

14. The system of claim 10 , comprising a stoichiometric combustion system having the turbine combustor configured to combust a fuel/oxidant mixture in a combustion equivalence ratio of between 0.95 and 1.05 fuel to oxygen in the oxidant.

15. The system of claim 10 , wherein the gearbox comprises a speed-increasing gearbox.

16. A system, comprising:
a gas turbine system, comprising:
a turbine combustor;
a turbine driven by combustion products from the turbine combustor; and
an exhaust gas compressor driven by the turbine, wherein the exhaust gas compressor is configured to compress and supply an exhaust gas to the turbine combustor;

an exhaust gas recirculation (EGR) system, wherein the EGR system is configured to recirculate the exhaust gas along an exhaust recirculation path from the turbine to the exhaust gas compressor;
a main oxidant compression system configured to supply compressed oxidant to the gas turbine system, and the main oxidant compression system comprises:
a first oxidant compressor coupled to a shaft of the gas turbine system, such that the first oxidant compressor is at least partially driven by the gas turbine system; and
a second oxidant compressor configured to receive partially compressed oxidant from the first oxidant compressor to supply compressed oxidant to the gas turbine system; and

a steam turbine coupled to the second oxidant compressor and configured to at least partially drive the second oxidant compressor, wherein the steam turbine is coupled to the second oxidant compressor via a gearbox, and wherein the gearbox is configured to enable the second oxidant compressor to operate at a speed different from an operating speed of the steam turbine.

17. The system of claim 16 , wherein the first oxidant compressor is an axial flow compressor and the second oxidant compressor is an axial flow compressor.

18. The system of claim 16 , wherein the gas turbine system comprises a heat recovery steam generator configured to receive a stream of water to generate steam via a heat exchange relationship with the exhaust gas.

19. The system of claim 18 , wherein the heat recovery generator is configured to supply the steam to the steam turbine, and wherein the steam turbine is configured to at least partially drive the second oxidant compressor via electric power generated from the steam.

20. The system of claim 16 , wherein the first oxidant compressor is a low pressure oxidant compressor and the second oxidant compressor is a high pressure oxidant compressor.

Assignees

• Gen Electric
• Exxonmobil Upstream Res Co

Inventors

• Huntington Richard A
• Mittricker Franklin F
• Starcher Loren K
• Dhanuka Sulabh K
• O'Dea Dennis M
• Draper Samuel D
• Hansen Christian M
• Denman Todd
• West James A

Classifications

• Y02E20/16

  Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT] · CPC title

• F02C6/10

  supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant · CPC title

• F02C3/04

  having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) · CPC title

• F02C3/107 Primary

  with two or more rotors connected by power transmission · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title