ADIABATIC COMPRESSED AIR ENERGY STORAGE SYSTEM WITH LIQUID THERMAL ENERGY STORAGE

• US 20110100010A1
• Filed: 10/30/2009
• Published: 05/05/2011
• Est. Priority Date: 10/30/2009
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Finkenrath, Matthias, Freund, Sebastian W., Gonzalez Salazar, Miguel Angel, Hoffmann, Stephanie Marie-Noelle, Botero, Cristina, Belloni, Clarissa S.K.
• Application Number:
  US12/609,449
• Publication Number:
  US 20110100010A1
• Time in Patent Office: Days
• US Class Current: 60/659
• CPC Class Codes: F02C 1/005 being recirculated
• CPC Class Codes: F02C 6/16 for storing compressed air
• CPC Class Codes: F02C 6/18 using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants using waste heat as source of energy for refrigeration plants F25B27/02; using the waste heat of a gasturbine for steam generation or in a steam cycle see F01K23/10
• CPC Class Codes: F02C 7/10 by means of regenerative heat-exchangers
• CPC Class Codes: F05D 2220/60 making use of surplus or waste energy
• CPC Class Codes: Y02E 60/16 Mechanical energy storage, e.g. flywheels or pressurised fluids

Abstract

An adiabatic compressed air energy storage (ACAES) system includes a compressor system, an air storage unit, and a turbine system. The ACAES system further includes a thermal energy storage (TES) system that includes a container, a plurality of heat exchangers, a liquid TES medium conduit system fluidly coupling the container to the plurality of heat exchangers, and a liquid TES medium stored within the container. The TES system also includes a plurality of pumps coupled to the liquid TES medium conduit system and configured to transport the liquid TES medium between the plurality of heat exchangers and the container, and a thermal separation system positioned within the container configured to thermally isolate a first portion of the liquid TES medium at a lower temperature from a second portion of the liquid TES medium at a higher temperature.

Claims

1. An adiabatic compressed air energy storage (ACAES) system comprising:

a compressor system configured to compress air supplied thereto, the compressor system comprising;

a plurality of compressors; and

a compressor conduit fluidly connecting the plurality of compressors together and having an air inlet and an air outlet;

an air storage unit connected to the air outlet of the compressor conduit and configured to store compressed air received from the compressor system;

a turbine system configured to expand compressed air supplied thereto from the air storage unit, the turbine system comprising;

a plurality of turbines; and

a turbine conduit fluidly connecting the plurality of turbines together and having an air inlet and an air outlet; and

a thermal energy storage (TES) system configured to remove thermal energy from compressed air passing through the compressor conduit and to return thermal energy to air passing through the turbine conduit, the TES system comprising;

a container;

a plurality of heat exchangers;

a liquid TES medium conduit system fluidly coupling the container to the plurality of heat exchangers;

a liquid TES medium stored within the container;

a plurality of pumps coupled to the liquid TES medium conduit system and configured to transport the liquid TES medium between the plurality of heat exchangers and the container; and

a thermal separation system positioned within the container configured to thermally isolate a first portion of the liquid TES medium at a lower temperature from a second portion of the liquid TES medium at a higher temperature.

2. The ACAES system of claim 1 wherein the thermal separation system comprises a floating separator piston configured to vary its position within the container according to the amount of liquid TES medium at the first temperature within the container.

3. The ACAES system of claim 1 wherein the thermal separation system comprises a medium positioned at a fixed location within the container.

4. The ACAES system of claim 3 wherein the thermal separation system comprises one of concrete, rocks, bricks, and metal.

5. The ACAES system of claim 1 wherein the liquid TES medium conduit system fluidly couples the plurality of heat exchangers together in a parallel mode.

6. The ACAES system of claim 1 further comprising:

a first pump fluidly coupled to the liquid TES medium conduit system and configured to convey a quantity of the liquid TES medium within the container and on a first side of the thermal separation system to the plurality of heat exchangers; and

a second pump fluidly coupled to the liquid TES medium conduit system and configured to convey a quantity of the liquid TES medium within the container and on a second side of the thermal separation system to the plurality of heat exchangers.

7. The ACAES system of claim 1 wherein:

the plurality of compressors comprises a low pressure compressor and a high pressure compressor;

the plurality of turbines comprises a low pressure turbine and a high pressure turbine; and

the plurality of heat exchangers comprises;

a first heat exchanger connected to the compressor conduit between the low pressure compressor and the high pressure compressor and connected to the turbine conduit between the low pressure turbine and the high pressure turbine; and

a second heat exchanger connected to the compressor conduit between the high pressure compressor and the air storage unit and connected to the turbine conduit between the high pressure turbine and the air storage unit.

8. The ACAES system of claim 7 wherein the compressor conduit is arranged to pass air at a first pressure through the first heat exchanger and to subsequently pass air at a second pressure through the second heat exchanger;

and

wherein the turbine conduit is arranged to pass air at the second pressure through the second heat exchanger and to subsequently pass air at the first pressure through the first heat exchanger.

9. The ACAES system of claim 8 wherein the air at the first pressure comprises low pressure air and the air at the second pressure comprises high pressure air.

10. The ACAES system of claim 7 further comprising an intercooler connected to the compressor conduit between the first heat exchanger and the high pressure compressor.

11. The ACAES system of claim 1 further comprising:

a drive shaft coupleable to the compressor system and coupleable to the turbine system, the drive shaft configured to transfer rotational power to the compressor system and configured to receive rotational power from the turbine system; and

a motor-generator unit coupled to the drive shaft and configured to;

receive electrical energy from an external energy source and generate and transfer rotational power to the drive shaft; and

receive rotational power from the drive shaft and generate electrical energy in response thereto.

12. A method for adiabatic compressed air energy storage (ACAES) comprising:

supplying air to a compressor system, the compressor system including a plurality of compressor units fluidly connected by a compressor conduit;

compressing the air in the compressor system during a compression stage;

storing the compressed air in a compressed air storage unit;

supplying the compressed air from the compressed air storage unit to a turbine system, the turbine system including a plurality of turbine units fluidly connected by a turbine conduit;

expanding the air in the turbine system during an expansion stage; and

during each of the compression stage and the expansion stage, passing the air through a liquid thermal energy storage (TES) system coupled to each of the compressor conduit and the turbine conduit, the liquid TES system comprising;

a liquid storage volume;

a plurality of heat exchangers fluidly coupled to the liquid storage volume; and

a thermal separation unit configured to thermally isolate a liquid in the liquid storage volume on a first side of the thermal separation unit from a liquid in the liquid storage volume on a second side of the thermal separation unit.

13. The method of claim 12 further comprising:

pumping the liquid in the liquid storage volume on the first side of the thermal separation unit through the plurality of heat exchangers in a parallel mode during the compression stage to remove heat from the air passing through the compressor conduit; and

pumping the liquid in the liquid storage volume on the second side of the thermal separation unit through the plurality of heat exchangers in a parallel mode during the expansion stage to add heat to the air passing through the turbine conduit.

14. The method of claim 12 wherein passing the air through the plurality of TES units comprises:

passing the air through a first heat exchanger of the plurality of heat exchangers and subsequently passing the air through a second heat exchanger of the plurality of heat exchangers when passing the air through the compressor conduit such that low pressure air passes through the first heat exchanger and high pressure air passes through the second heat exchanger; and

passing the air through the second heat exchanger and subsequently passing the air through the first heat exchanger when passing the air through the turbine conduit such that high pressure air passes through the second heat exchanger and low pressure air passes through the first heat exchanger.

15. An adiabatic compressed air energy storage (ACAES) system comprising:

a compressor system configured to compress air supplied thereto, the compressor system comprising;

a plurality of compressors; and

a compressor conduit connecting the plurality of compressors and having an air inlet and an air outlet;

an air storage unit connected to the air outlet of the compressor conduit and configured to store compressed air received from the compressor system;

a turbine system configured to expand compressed air supplied thereto from the air storage unit, the turbine system comprising;

a plurality of turbines; and

a turbine conduit connecting the plurality of turbines and having an air inlet and an air outlet; and

a liquid thermal energy storage (TES) system comprising a TES liquid configured to remove thermal energy from compressed air passing through the compressor conduit and to return thermal energy to air passing through the turbine conduit, the liquid TES system further comprising;

a storage volume configured to store the TES liquid;

a plurality of heat exchangers fluidly coupled to the storage volume; and

a thermal separator positioned within the container and configured to thermally separate a hot volume of the TES liquid from a cold volume of the TES liquid within the storage volume.

16. The ACAES system of claim 15 wherein the thermal separator comprises a floating piston configured to float on the amount of the cold volume of the TES liquid within the container.

17. The ACAES system of claim 15 wherein the thermal separator comprises a fixed position medium within the container comprising one of concrete, rocks, bricks, and metal.

18. The ACAES system of claim 15 wherein the TES system further comprises a TES conduit system fluidly coupling the plurality of heat exchangers to the storage volume, wherein the TES conduit system further couples the plurality of heat exchangers together in a parallel mode.

19. The ACAES system of claim 18 wherein the TES conduit system further comprises:

a first pump configured to convey a quantity of the hot volume of the TES liquid from the container to the plurality of heat exchangers; and

a second pump configured to convey a quantity of the cold volume of the TES liquid from the container to the plurality of heat exchangers.

20. The ACAES system of claim 15 wherein:

the plurality of compressors comprises a low pressure compressor and a high pressure compressor;

the plurality of turbines comprises a low pressure turbine and a high pressure turbine;

the plurality of heat exchangers comprises;

a first heat exchanger fluidly coupled to the compressor conduit between the low pressure compressor and the high pressure compressor and fluidly coupled to the turbine conduit between the low pressure turbine and the high pressure turbine;

a second heat exchanger fluidly coupled to the compressor conduit between the high pressure compressor and the air storage unit and fluidly coupled to the turbine conduit between the high pressure turbine and the air storage unit;

the compressor conduit is arranged to pass air at a first pressure through the first heat exchanger and to subsequently pass air at a second pressure through the second heat exchanger; and

the turbine conduit is arranged to pass air at the second pressure through the second heat exchanger and to subsequently pass air at the first pressure through the first heat exchanger.