COOLING SYSTEM FOR AN ENERGY STORAGE SYSTEM AND METHOD OF OPERATING THE SAME

• US 20160160864A1
• Filed: 12/05/2014
• Published: 06/09/2016
• Est. Priority Date: 12/05/2014
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Freund, Sebastian Walter, Becquin, Guillaume, Bieber, Mathilde
• Application Number:
  US14/561,528
• Publication Number:
  US 20160160864A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F02C 1/04 the working fluid being heated indirectly in a fluidised-bed combustor F02C3/205
• CPC Class Codes: F02C 6/16 for storing compressed air
• CPC Class Codes: F02C 7/12 Cooling of plants of component parts, see the relevant subclasses, e.g. F01D; cooling of engines in general F01P
• CPC Class Codes: F02C 7/141 of working fluid
• CPC Class Codes: F02C 7/143 before or between the compressor stages
• CPC Class Codes: F04D 25/08 the working fluid being air, e.g. for ventilation
• CPC Class Codes: F04D 25/16 Combinations of two or more pumps ; Producing two or more separate gas flows
• CPC Class Codes: F05D 2260/42 Storage of energy
• CPC Class Codes: F25B 1/00 Compression machines, plants or systems with non-reversible cycle F25B3/00, F25B5/00, F25B6/00, F25B7/00, F25B9/00 take precedence
• CPC Class Codes: F25B 15/02 without inert gas F25B15/004, F25B15/006, F25B15/008, F25B15/12, F25B15/14, F25B15/16 take precedence
• CPC Class Codes: F25B 27/02 using waste heat, e.g. from internal-combustion engines
• CPC Class Codes: Y02A 30/274 using waste energy, e.g. from internal combustion engine
• CPC Class Codes: Y02E 60/16 Mechanical energy storage, e.g. flywheels or pressurised fluids

Abstract

An energy storage system includes an intercooler coupled to an axial compressor and a multi-stage radial compressor including a first stage radial compressor and a second stage radial compressor, coupled to the intercooler. The energy storage system further includes a thermal energy storage unit coupled to the multi-stage radial compressor and an air storage unit coupled to the thermal energy storage unit. The energy storage system also includes a turbine coupled to the thermal energy storage unit and a cooling system coupled to the axial compressor and configured to cool air fed to the axial compressor.

Claims

1. An energy storage system comprising:

an axial compressor;

an intercooler coupled to the axial compressor;

a multi-stage radial compressor comprising a first stage radial compressor and a second stage radial compressor, coupled to the intercooler;

a thermal energy storage unit coupled to the multi-stage radial compressor;

an air storage unit coupled to the thermal energy storage unit;

a turbine coupled to the thermal energy storage unit; and

a cooling system coupled to the axial compressor and configured to cool air fed to the axial compressor.

2. The energy storage system of claim 1, wherein the cooling system comprises a vapor compression cycle comprising an evaporator configured to feed the air in heat exchange relationship with a refrigerant to the cool the air fed to the axial compressor.

3. The energy storage system of claim 1, further comprising a separator coupled to the cooling system and the axial compressor and configured to remove a condensate from a cooled air fed to the axial compressor.

4. The energy storage system of claim 1, wherein the cooling system comprises a vapor absorption cycle comprising:

a heat exchanger configured to feed the air in heat exchange relationship with a refrigerant to the cool the air fed to the axial compressor; and

a heat source selected from at least one of the intercooler, the second stage radial compressor, the thermal energy storage unit, and an after-cooler coupled to the thermal energy storage unit and the air storage unit,

a generation unit coupled to the heat source and configured to feed a fluid from the heat source in heat exchange relationship with the refrigerant to boil the refrigerant.

5. The energy storage system of claim 4, wherein the heat source comprises the intercooler, wherein the fluid comprises compressed air fed from the axial compressor.

6. The energy storage system of claim 4, wherein the heat source comprises the second stage radial compressor, wherein the fluid comprises a cooling medium fed from the second stage radial compressor.

7. The energy storage system of claim 4, wherein the heat source comprises the thermal energy storage unit, wherein the fluid comprises a cooling medium fed from the thermal energy storage unit.

8. The energy storage system of claim 4, wherein the heat source comprises the after-cooler, wherein the fluid comprises a cooling medium fed from the after-cooler.

9. The energy storage system of claim 4, further comprising a recuperator coupled to the thermal energy storage unit, the air storage unit, and the turbine.

10. The energy storage system of claim 9, wherein the recuperator is configured to feed an exhaust gas from the turbine in heat exchange relationship with cooled compressed air fed from the air storage unit to the thermal energy storage unit to preheat the cooled compressed air.

11. The energy storage system of claim 1, wherein the cooling system further comprises a water source for spraying water to cool the air fed to the axial compressor.

12. A method for operating an energy storage system;

cooling air fed to an axial compressor via a cooling system;

feeding a first compressed air from the axial compressor to a multi-stage radial compressor comprising a first stage radial compressor and a second stage radial compressor, via an intercooler;

feeding a second compressed air from the multi-stage radial compressor to a thermal energy storage unit;

storing a thermal energy from the second compressed air in the thermal energy storage unit;

feeding a cooled compressed air from the thermal energy storage unit to an air storage unit;

feeding the cooled compressed air from the air storage unit to the thermal energy storage unit to heat the cooled compressed air using the stored thermal energy; and

feeding a heated compressed air from the thermal energy storage unit to a turbine to expand the heated compressed air and generate an electric power via a generator.

13. The method of claim 12, wherein feeding air via a cooling system comprises feeding the air in heat exchange relationship with a refrigerant via an evaporator of a vapor compression cycle to the cool the air fed to the axial compressor.

14. The method of claim 12, further comprising removing a condensate from a cooled air fed to the axial compressor via a separator.

15. The method of claim 12, wherein feeding air via a cooling system comprises feeding the air in heat exchange relationship with a refrigerant to the cool the air fed to the axial compressor and feeding a fluid from a heat source in heat exchange relationship with the refrigerant to boil the refrigerant;

wherein the heat source is selected from at least one of the intercooler, the second stage radial compressor, the thermal energy storage unit, and an after-cooler coupled to the thermal energy storage unit and the air storage unit.

16. The method of claim 15, wherein the fluid comprises the first compressed air fed from the axial compressor and the heat source comprises the intercooler.

17. The method of claim 15, wherein the fluid comprises a cooling medium fed from the second stage radial compressor and the heat source comprises the second stage radial compressor.

18. The method of claim 15, wherein the fluid comprises a cooling medium fed from the thermal energy storage unit and the heat source comprises the thermal energy storage unit.

19. The method of claim 15, wherein the fluid comprises a cooling medium fed from the after-cooler and the heat source comprises the after-cooler.

20. The method of claim 12, further comprising preheating the cooled compressed air fed from the air storage unit to the thermal energy storage unit by feeding an exhaust gas from the turbine in heat exchange relationship with the cooled compressed air via a recuperator.

21. The method of claim 12, wherein cooling air comprises spraying water from a water source to cool the air fed to the axial compressor.