System and method for high efficiency power generation using a nitrogen gas working fluid

Patent metadata

Field	Value
Publication number	US-9410481-B2
Application number	US-201113235746-A
Country	US
Kind code	B2
Filing date	Sep 19, 2011
Priority date	Sep 21, 2010
Publication date	Aug 9, 2016
Grant date	Aug 9, 2016

Abstract

A method of power production using a high pressure/low pressure ratio Brayton Power cycle with predominantly N 2 mixed with CO 2 and H 2 O combustion products as the working fluid is provided. The high pressure can be in the range 80 bar to 500 bar. The pressure ratio can be in the range 1.5 to 10. The natural gas fuel can be burned in a first high pressure combustor with a near stoichiometric quantity of pressurized preheated air and the net combustion gas can be mixed with a heated high pressure recycle N 2 +CO 2 +H 2 O stream which moderates the mixed gas temperature to the value required for the maximum inlet temperature to a first power turbine producing shaft power.

First claim

The invention claimed is:

1. A power production system, comprising:
a first combustor configured to combust a first fuel stream and a first air stream in the presence of a first recycle stream to produce a first combustion stream;
a first turbine configured to expand the first combustion stream;
a first heat exchanger configured to receive at least a portion of a first discharge stream from the first turbine,
wherein the first heat exchanger is configured to employ the portion of the first discharge stream to heat the first air stream and at least a portion of the first recycle stream that is produced from the first discharge stream;

a second combustor configured to combust a second fuel stream and a second air stream in the presence of a second recycle stream that is produced from the first discharge stream to produce a second combustion stream;
a second turbine configured to expand the second combustion stream; and
a second heat exchanger configured to heat the second air stream and the second recycle stream,
wherein the first turbine is positioned upstream of the first heat exchanger and the first heat exchanger is positioned upstream of the second turbine in terms of a flow of the first discharge stream.

2. The power production system of claim 1 , wherein the second heat exchanger is configured to employ a second discharge stream from the second turbine to heat the second air stream and the second recycle stream.

3. The power production system of claim 1 , wherein the second heat exchanger is further configured to heat a second portion of the first recycle stream.

4. The power production system of claim 1 , further comprising a third combustor configured to combust a third fuel stream and a third air stream in the presence of a second discharge stream received from the second turbine to produce a third combustion stream; and
a third turbine configured to expand the third combustion stream.

5. The power production system of claim 4 , wherein the second heat exchanger is configured to employ a third discharge stream from the third turbine to heat the second air stream and the second recycle stream.

6. The power production system of claim 5 , wherein the second heat exchanger is further configured to heat the third air stream.

7. The power production system of claim 5 , wherein the second heat exchanger is further configured to heat a second portion of the first recycle stream.

8. The power production system of claim 1 , further comprising a recycle compressor configured to compress the first recycle stream.

9. The power production system of claim 1 , wherein a second portion of the first discharge stream is directed to the second combustor.

10. The power production system of claim 1 , further comprising a scrubber configured to receive a cooled discharge stream from the second heat exchanger.

11. The power production system of claim 10 , wherein the scrubber comprises a CO 2 adsorption system.

12. The power production system of claim 1 , further comprising an air compressor system configured to compress a feed air stream to produce the first air stream and the second air stream.

13. The power production system of claim 12 , wherein the air compressor system comprises a first air compressor configured to compress the first air stream and a second air compressor configured to compress the second air stream.

14. The power production system of claim 13 , wherein the second air compressor is further configured to compress the first air stream before the first air compressor compresses the first air stream.

15. The power production system of claim 13 , wherein the air compressor system is configured to control a flow rate of the first air stream and a flow rate of the second air stream to result in substantially stoichiometric combustion in the first combustor and the second combustor.

16. The power production system of claim 15 , wherein the air compressor system is configured to control the flow rate of the first air stream and the flow rate of the second air stream to result in up to about 5% excess O 2 in the combustion in the first combustor and the second combustor.

17. The power production system of claim 1 , wherein the first fuel stream and the second fuel stream comprise a compressed hydrocarbon gas.

18. The power production system of claim 17 , wherein the compressed hydrocarbon gas comprises methane.

19. The power production system of claim 1 , wherein the first air stream and the second air stream comprise compressed ambient air.

20. The power production system of claim 1 , wherein the first recycle stream and the second recycle stream are greater than 50% N 2 on a molar basis.

21. The power production system of claim 1 , further comprising a separator configured to remove a liquid stream from the portion of the first discharge stream directed through the first heat exchanger.

22. The power production system of claim 1 , wherein the power production system is configured to operate with a net electrical generation efficiency on a lower heating value basis of at least about 60% when operating with a turbine temperature from about 1,300° C. to about 1,500° C.

23. A power production system, comprising:
an air supply configured to supply a first air stream;
a fuel supply configured to supply a first fuel stream,
a first combustor configured to combust the first fuel stream and the air stream in the presence of a first recycle stream to produce a first combustion stream that is greater than 50% N2 on a molar basis,
wherein the air supply and the fuel supply are configured to supply the first air stream and the first fuel stream in a ratio configured to result in substantially stoichiometric combustion in the first combustor with up to about 5% excess 02;
a first turbine configured to expand the first combustion stream;
a first heat exchanger configured to receive at least a portion of a discharge stream from the first turbine,
wherein the first heat exchanger is configured to employ the portion of the discharge stream to heat the first air stream and at least a portion of the first recycle stream that is produced from the discharge stream;
a second combustor configured to combust a second fuel stream and a second air stream in the presence of a second recycle stream that is produced from the discharge stream to produce a second combustion stream;
a second turbine configured to expand the second combustion stream; and
a second heat exchanger configured to heat the second air stream and the second recycle stream.

Assignees

• Palmer Miles
• Allam Rodney John
• Fetvedt Jeremy Eron
• 8 Rivers Capital Llc

Inventors

• Palmer Miles
• Allam Rodney John
• Fetvedt Jeremy Eron

Classifications

• F02C6/003

  Gas-turbine plants with heaters between turbine stages · CPC title

• F02C9/48

  Control of fuel supply conjointly with another control of the plant (with nozzle section control F02K1/17) · CPC title

• F02C7/10

  by means of regenerative heat-exchangers · CPC title

• F01N3/0857

  Carbon oxides · CPC title

• F05D2240/40

  Use of a multiplicity of similar components · CPC title