Carbon dioxide power cycle

• US 4,498,289 A
• Filed: 12/27/1982
• Issued: 02/12/1985
• Est. Priority Date: 12/27/1982
• Status: Expired due to Fees

• Current Assignee: Ian Osgerby
• Original Assignee: Ian Osgerby
• Inventors: Osgerby, Ian
• Primary Examiner(s): Ostrager, Allen M.
• Application Number:
  US06/453,724
• Time in Patent Office: 778 Days
• Field of Search: 60/39.52, 60/39.17, 60/39.04, 60/647, 60/651, 60/671, 60/650, 60/682
• US Class Current: 60/39.52
• CPC Class Codes: F01K 25/103 Carbon dioxide F01K25/065 takes precedence
• CPC Class Codes: F02C 1/005 being recirculated
• CPC Class Codes: F02C 1/08 Semi-closed cycles
• CPC Class Codes: F02C 3/34 with recycling of part of the working fluid, i.e. semi-closed cycles with combustion products in the closed part of the cycle
• CPC Class Codes: F02C 6/003 Gas-turbine plants with heaters between turbine stages
• CPC Class Codes: Y02E 20/32 Direct CO2 mitigation
• CPC Class Codes: Y02E 20/34 Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Abstract

An improved direct fired power system generating and employing a combustion gas which includes carbon dioxide or a working fluid including a combustion chamber (20) for burning a mixture which includes oxygen, carbonaceous fuel and recycled carbon dioxide working fluid at a first pressure of above 1100 PSI thereby providing a combustion gas which includes carbon dioxide and water at substantially the first pressure and above 31° C. A first turbine (16) allows the gas to expand therethrough to generate power and reduce the combustion gas pressure to a second pressure below 1100 PSI while maintaining gas temperature above 31° C. A second burner (20) heats the combustion gas to a higher temperature and a second turbine (21) allows the gas to expand therethrough to generate power and reduce the pressure to a third pressure while maintaining gas temperature above 31° C. A heat exchanger (26) includes ducts (28), (30) in heat exchange relationship. Duct (30) conducts recycled carbon dioxide working fluid at substantially the first pressure therethrough and to the combustion chamber. Duct (28) conducts combustion gas from turbine (21) therethrough to transfer heat to the recycled carbon dioxide working fluid to condense at least a portion of the water in the combustion gas but maintain the carbon dioxide thereof in a gaseous phase. Condensed water is separated from the gas. A condensor (33) cools the gas to a first temperature above 31° C. and a compressor (42) compresses the gas to a fourth pressure of at least 1100 psi but below the first pressure. A second condensor (44) cools the gas to a second temperature below the first temperature but above 31° C. and a second compressor (24) compresses the gas to substantially the first pressure to provide recycled carbon dioxide working fluid which is delivered to heat exchanger (26).

Claims

1. An improved direct fired power system generating and employing a combustion gas which includes carbon dioxide as a working fluid comprising:

means defining a combustion chamber for burning a mixture which includes oxygen, a carbonaceous fuel and recycled carbon dioxide working fluid at a supercritical first pressure, thereby providing a combustion gas which includes carbon dioxide and water at substantially said first pressure, and a supercritical temperature,

means defining a first turbine for receiving combustion gas from said combustion chamber and allowing said gas to expand therethrough to generate power and reduce the pressure of said combustion gas to a second pressure while maintaining a supercritical state,

means for receiving said combustion gas from said first turbine and heating said gas at said second pressure to a higher temperature

means defining a second turbine for receiving combustion gas from said means for heating and allowing said gas to expand therethrough to generate power and further reduce the pressure on said combustion gas to a third pressure while maintaining a supercritical state,

means defining a heat exchanger having first and second ducts in heat exchange relationship, said first duct receiving combustion gas from said second turbine and conducting said gas therethrough, said second duct conducting recycled carbon dioxide working fluid at substantilly said first pressure and a temperature below that of said combustion gas in said first duct therethrough and having an output connected to said combustion chamber for providing at least a portion of said recycled carbon dioxide thereto, for enabling said combustion gas to transfer heat to said recycled carbon dioxide to condense at least a portion of the water in said combustion gas, but maintain the carbon dioxide thereof in a supercritical state,

means for separating the condensed water from the remainder of said combustion gas

first cooling means connected to the output of said first duct of said heat exchanger for receiving combustion gas therefrom and cooling said combustion gas to a supercritical first temperature,

first compression means for receiving said combustion gas from said first cooling means and compressing said combustion gas to a fourth pressure below said first pressure,

second cooling means for receiving said combustion gas from said first compression means and cooling said combustion gas to a second temperature at essentially the liquid/gas interface of said combuston gas and,

second compression means for receiving said combustion gas from said second cooling means and compressing said gas to substantially said first pressure to thereby provide said recycled carbon dioxide working fluid, said second compression means being connected to the input of said second duct of said heat exchanger for providing said recycled carbon dioxide thereto.

2. System in accordance with claim 1 wherein said first means for cooling includes a condensor having a first duct connected between said first duct of said heat exchanger and said first compression means for conducting combustion gas therethrough and a second duct in heat transfer relationship with said first duct for conducting a cooling fluid therethrough.

3. System in accordance with claim 1 wherein said second cooling means includes a condensor having a first duct connected between said first compression means and second compression means for conducting combustion gas therethrough and a second duct in heat transfer relationship with said first duct for conducting a cooling fluid therethrough.

4. System in accordance with claim 1 further including means for drawing carbon dioxide from said system for ancillary use.

5. System in accordance with claim 1 wherein said means for drawing carbon dioxide is located between said first cooling means and said first compression means.

6. System in accordance with claim 4 wherein said means for drawing carbon dioxide is located between said second compression means and said heat exchanger to provide supercritical carbon dioxide product.

7. System in accordance with claim 1 wherein one or more noble gases are mixed with the oxygen in said combustion chamber and thereby present in said combustion gas and further including means for drawing said noble gases from said combustion gas for ancillary use thereof.

8. System in accordance with claim 1 wherein said means for separating condensed water from said combustion product are connected to said first duct of said heat exchanger.

9. System in accordance with claim 2 wherein said means for separating are connected to said first duct of said first condensor.

10. System in accordance with claim 1 wherein said second compression means includes a pump.

11. System in accordance with claim 10 wherein at least a portion of power generated by either of said first or second turbines is used to operate said pump.

12. System in accordance with claim 1 further including air separation means for separating at least nitrogen from an air supply to provide oxygen for burning in said combustion chamber.

13. System in accordance with claim 1 wherein said second cooling means cools said combustion gas to no lower than 27°

C.

14. A method for enhancing the efficiency of a power cycle which generates and employs a combustion gas including carbon dioxide as a working fluid comprising:

introducing a mixture which includes oxygen, carbonaceous fuel and recycled carbon dioxide gas at a supercritical first pressure into a combustion chamber and burning said mixture to provide a combustion gas which includes carbon dioxide and water at substantially said first pressure and a supercritical temperature,

allowing said combustion gas to expand through a first turbine to generate power and reduce the pressure of said combustion gas to a second pressure while maintaining a supercritical state,

heating said combustion gas at substantially said second pressure to a higher temperature,

allowing said reheated combustion gas to expand through a second turbine to generate power and further reduce the pressure of said combustion gas to a third pressure while maintaining a supercritical state,

passing said combustion gas in heat exchange relationship with recycled carbon dioxide working fluid at said first pressure and a temperature lower than said combustion gas whereby heat is transferred from said combustion gas to said recycled carbon dioxide to condense at least a portion of the water in said combustion gas but maintain the carbon dioxide therein in a supercritical state,

cooling said combustion gas to a first temperature,

compressing said combustion gas to a fourth pressure below said first pressure,

cooling said combustion gas to a second temperature at essentially the liquid/gas interface of said combustion gas,

compressing said combustion gas to substantially said first pressure to provide said recycled carbon dioxide working fluid and

separating condensed water from said combustion gas following either the heat exchange or cooling to a first temperature steps.

15. Method in accordance with claim 14 futher including drawing carbon dioxide from said system for ancillary use.

16. Method in accordance with claim 14 further including removing one or more noble gases from the combustion gases.

17. Method in accordance with claim 14 including mixing additional recycled carbon dioxide working fluid with said combustion gas prior to heating said combustion gas.

18. Method in accordance with claim 14 further including separating at least nitrogen from an air supply to provide oxygen for burning in said combustion chamber.

19. Method in accordance with claim 14 wherein said combustion gas is cooled to no lower than 27°

C. in the cooling to a second temperature step.