METHODS FOR INCREASING CARBON DIOXIDE CONTENT IN GAS TURBINE EXHAUST AND SYSTEMS FOR ACHIEVING THE SAME

• US 20100180565A1
• Filed: 01/16/2009
• Published: 07/22/2010
• Est. Priority Date: 01/16/2009
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Draper, Samuel David
• Application Number:
  US12/355,246
• Publication Number:
  US 20100180565A1
• Time in Patent Office: Days
• US Class Current: 60/39.520
• CPC Class Codes: F02C 1/007 combination of cycles
• CPC Class Codes: F02C 1/08 Semi-closed cycles
• CPC Class Codes: F02C 3/22 the fuel or oxidant being gaseous at standard temperature and pressure F02C3/28 takes precedence
• CPC Class Codes: Y02E 20/16 Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

Abstract

Disclosed herein is a system comprising a first compressor; the compressor being operative to compress air; a turbine; the turbine being disposed downstream of the first compressor; the turbine being operative to combust a hydrocarbon fuel along with compressed air from the first compressor to produce an exhaust gas stream; and a second compressor; the second compressor being disposed downstream of the turbine; the second compressor being operative to compress the exhaust gas stream and to recycle the compressed exhaust gas stream to the turbine. Disclosed herein is a method comprising compressing air in a first compressor; combusting the air along with a hydrocarbon fuel in a turbine; generating an exhaust gas stream from the turbine; compressing the exhaust gas stream in a second compressor; recirculating the compressed exhaust gas stream to the turbine; separating carbon dioxide from the exhaust gas stream; and storing the carbon dioxide.

Claims

1. A method comprising:

compressing air in a first compressor;

combusting the air along with a hydrocarbon fuel in a turbine;

generating an exhaust gas stream from the turbine;

separating the exhaust gas stream into a first portion and a second portion;

separating carbon dioxide from the first portion;

compressing the second portion in a second compressor; and

recirculating the compressed second portion to the turbine.

2. The method of claim 1, wherein an amount of carbon dioxide in the exhaust gas stream is increased from about 3 to about 18 volume percent of the total volume of the exhaust gas stream from the turbine.

3. The method of claim 1, wherein an amount of carbon dioxide in the exhaust gas stream is increased from about 5 to about 14 volume percent of the total volume of the exhaust gas stream from the turbine.

4. The method of claim 1, wherein the ratio of air to the exhaust gas stream supplied to the turbine is up to about 0.25:

1.

5. The method of claim 1, wherein an oxygen content in the exhaust gas stream is less than or equal to about 12 volume percent, based on the total volume of the exhaust gas stream from the turbine.

6. The method of claim 1, wherein an oxygen content in the exhaust gas stream is less than or equal to about 2 volume percent, based on the total volume of the exhaust gas stream from the turbine.

7. The method of claim 5, wherein the first portion is about 40 to about 80 volume percent while the second portion is about 20 to about 60 volume percent, based on the total volume of the exhaust gas stream from the turbine.

8. The method of claim 5, wherein the first portion is about 45 to about 65 volume percent while the second portion is about 35 to about 55 volume percent, based on the total volume of the exhaust gas stream from the turbine.

9. The method of claim 1, further comprising storing the carbon dioxide in a tank.

10. The method of claim 1, further comprising storing the carbon dioxide in an underground geologic formation.

11. A system that uses the method of claim 1.

12. A system comprising:

a first compressor;

the compressor being operative to compress air;

a turbine;

the turbine being disposed downstream of the first compressor;

the turbine being operative to combust a hydrocarbon fuel along with compressed air from the first compressor to produce an exhaust gas stream; and

a second compressor;

the second compressor being disposed downstream of the turbine;

the second compressor being operative to compress the exhaust gas stream and to recycle the compressed exhaust gas stream to the turbine.

13. The system of claim 12, further comprising a combustion system;

the combustion system being operative to combust the compressed air and the hydrocarbon fuel.

14. The system of claim 13, further comprising a carbon dioxide separation system;

the carbon dioxide separation system being effect to extract carbon dioxide from the exhaust stream.

15. The system of claim 12, further comprising a flow divider;

the flow divider being operative to divide the exhaust gas stream into a first portion and a second portion;

the first portion being discharged to a carbon dioxide separator while the second portion is recirculated to the second compressor.

16. The system of claim 12, wherein the system is operative to facilitate recycling of the exhaust gas stream till an amount of oxygen is reduced to less than or equal to about 2 volume percent, based on the volume of the exhaust gas stream.

17. A system comprising:

a first compressor;

the compressor being operative to compress air;

a combustion system;

the combustion system being downstream of the first compressor;

a turbine;

the turbine being disposed downstream of the first compressor;

the turbine being operative to combust a hydrocarbon fuel along with compressed air from the first compressor to produce an exhaust gas stream; and

a second compressor;

the second compressor being disposed downstream of the turbine;

the second compressor being operative to compress the exhaust gas stream and to recycle the compressed exhaust gas stream to the turbine;

the system providing a means to facilitate recycling of the exhaust gas stream till an amount of oxygen is reduced to less than or equal to about 12 volume percent, based on the volume of the exhaust gas stream.

18. The system of claim 17, further comprising a carbon dioxide separation system;

the carbon dioxide separation system being effective to extract carbon dioxide from the exhaust stream.

19. The system of claim 17, further comprising a flow divider;

the flow divider being operative to divide the exhaust gas stream into a first portion and a second portion;

the first portion being discharged to a carbon dioxide separator while the second portion is recirculated to the second compressor.

20. The system of claim 19, further comprising a sequestration system where carbon dioxide is sequestered.