High efficiency power production methods, assemblies, and systems

Patent metadata

Field	Value
Publication number	US-11459896-B2
Application number	US-202117149245-A
Country	US
Kind code	B2
Filing date	Jan 14, 2021
Priority date	Sep 21, 2010
Publication date	Oct 4, 2022
Grant date	Oct 4, 2022

Abstract

The present disclosure provides methods, assemblies, and systems for power production that can allow for increased efficiency and lower cost components arising from the control, reduction, or elimination of turbine blade mechanical erosion by particulates or chemical erosion by gases in a combustion product flow. The methods, assemblies, and systems can include the use of turbine blades that operate with a blade velocity that is significantly reduced in relation to conventional turbines used in typical power production systems. The methods and systems also can make use of a recycled circulating fluid for transpiration protection of the turbine and/or other components. Further, recycled circulating fluid may be employed to provide cleaning materials to the turbine.

First claim

The invention claimed is:

1. A power generation system comprising:
a combustor configured for providing a combustion product stream;
a turbine assembly comprising a casing defining an inlet in fluid communication with the combustor and an outlet for release of a turbine discharge stream, the casing including therein a rotor and a plurality of blades extending radially outwardly from the rotor, the turbine assembly having a ratio of a length of the turbine assembly to an average diameter of the blades, said ratio being 3.5 to 7, the length of the turbine assembly being defined as a distance substantially between a blade of the plurality of blades that is immediately adjacent the inlet and a blade of the plurality of blades that is immediately adjacent the outlet; and
a power generator in connection with the turbine assembly.

2. The power generation system of claim 1 , wherein a blade height of the plurality of blades is less than 0.275 m.

3. The power generation system of claim 1 , wherein the turbine assembly comprises less than 2,000 of the plurality of blades.

4. The power generation system of claim 1 , wherein the length of the turbine assembly is less than 11 meters.

5. The power generation system of claim 1 , wherein the length of the turbine assembly is 6 meters to 10 meters.

6. The power generation system of claim 1 , wherein the average diameter of the blades is 0.25 meters to 3 meters.

7. The power generation system of claim 1 , further comprising one or more components configured for processing the turbine discharge stream to provide a purified stream.

8. The power generation system of claim 7 , wherein the one or more components configured for processing the turbine discharge stream are effective to form a stream of purified carbon dioxide.

9. The power generation system of claim 1 , further comprising at least one heat exchange configured to receive the turbine discharge stream and remove heat therefrom to produce an unprocessed recycle stream.

10. The power generation system of claim 9 , further comprising at least one reactor configured to receive the unprocessed recycle stream, remove impurities therefrom, and provide a purified recycle stream.

11. The power generation system of claim 10 , further comprising one or more pressurization unit selected from the group of compressors, pumps, and combinations thereof, configured to pressurize the purified recycle stream.

12. A method of power generation comprising:
combusting a fuel with oxygen in a combustor to form a combustion product stream;
expanding the combustion product stream in a turbine assembly comprising a casing defining an inlet for receiving the combustion product stream and an outlet for release of a turbine discharge stream, the casing including therein a rotor and a plurality of blades extending radially outwardly from the rotor, the turbine assembly having a ratio of a length of the turbine assembly to an average diameter of the blades, said ratio being 3.5 to 7, the length of the turbine assembly being defined as a distance substantially between a blade of the plurality of blades that is immediately adjacent the inlet and a blade of the plurality of blades that is immediately adjacent the outlet;
generating power with a generator in connection with the turbine assembly; and
processing the turbine discharge stream to provide a purified stream.

13. The method of claim 12 , wherein the processing comprises:
removing heat from the turbine discharge stream in at least one heat exchanger to provide a cooled stream; and
passing the cooled stream through a separation unit to provide the purified stream.

14. The method of claim 13 , further comprising pressurizing the purified stream in one or more pressurization units selected from the group of compressors, pumps, and combinations thereof.

15. The method of claim 14 , wherein after said pressurizing, at least a portion of the purified stream is recycled to the combustor.

16. The method of claim 14 , wherein the purified stream comprises carbon dioxide.

17. The method of claim 12 , wherein combusting the fuel with the oxygen in the combustor is carried out in the presence of pressurized carbon dioxide.

18. The method of claim 17 , wherein the pressurized carbon dioxide is at a pressure of at least 7.5 Mpa.

Assignees

• 8 Rivers Capital Llc

Inventors

• Palmer Miles R
• Fetvedt Jeremy Eron
• Allam Rodney John

Classifications

• F01D5/085 Primary

  cooling fluid circulating inside the rotor · CPC title

• F01D25/14

  Casings modified therefor (double casings F01D25/26) · CPC title

• F05D2230/22

  by sintering · CPC title

• F01D5/183 Primary

  Blade walls being porous · CPC title

• F05D2260/95

  Preventing corrosion · CPC title