ADIABATIC COMPRESSED AIR ENERGY STORAGE SYSTEM WITH MULTI-STAGE THERMAL ENERGY STORAGE

• US 20110094231A1
• Filed: 10/28/2009
• Published: 04/28/2011
• Est. Priority Date: 10/28/2009
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Freund, Sebastian W.
• Application Number:
  US12/607,137
• Publication Number:
  US 20110094231A1
• Time in Patent Office: Days
• US Class Current: 60/727
• CPC Class Codes: F02C 1/02 the working fluid being an unheated pressurised gas
• 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: F05D 2260/211 by intercooling, e.g. during a compression cycle
• CPC Class Codes: Y02E 60/16 Mechanical energy storage, e.g. flywheels or pressurised fluids

Abstract

An ACAES system operable in a compression mode and an expansion mode of operation is disclosed and includes a compressor system configured to compress air supplied thereto and a turbine system configured to expand compressed air supplied thereto, with the compressor system including a compressor conduit and the turbine system including a turbine conduit. The ACAES system also includes a plurality of thermal energy storage (TES) units positioned on the compressor and turbine conduits and configured to remove thermal energy from compressed air passing through the compressor conduit and return thermal energy to air passing through the turbine conduit. The compressor conduit and the turbine conduit are arranged such that at least a portion of the plurality of TES units operate at a first pressure state during the compression mode of operation and at a second pressure state different from the first pressure state during the expansion mode of operation.

Claims

1. An adiabatic compressed air energy storage (ACAES) system operable in a compression mode to compress air and in an expansion mode to expand air, the 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 plurality of thermal energy storage (TES) units configured to remove thermal energy from compressed air passing through the compressor conduit and return thermal energy to air passing through the turbine conduit, each of the plurality of TES units being positioned on the compressor conduit along a length thereof between the air inlet and the air outlet of the compressor conduit and on the turbine conduit along a length thereof between the air inlet and the air outlet of the turbine conduit;

wherein the compressor conduit and the turbine conduit are arranged such that at least a portion of the plurality of TES units operate at a first pressure state during the compression mode of operation and at a second pressure state different from the first pressure state during the expansion mode of operation.

2. 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 TES units comprises a first TES unit positioned on the compressor conduit and the turbine conduit and a second TES unit positioned on the compressor conduit and the turbine conduit.

3. The ACAES system of claim 2 wherein the compressor conduit is arranged to pass air at a first pressure through the first TES unit and subsequently pass air at a second pressure through the second TES unit;

and

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

4. The ACAES system of claim 3 wherein the air at the first pressure comprises low pressure air and the air at the second pressure comprises high pressure air, such that the first TES unit receives low pressure air from the compressor conduit and high pressure air from the turbine conduit and such that the second TES unit receives high pressure air from the compressor conduit and low pressure air from the turbine conduit.

5. The ACAES system of claim 1 wherein:

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

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

the plurality of TES units comprises a first TES unit positioned on the compressor conduit and the turbine conduit, a second TES unit positioned on the compressor conduit and the turbine conduit, and a third TES unit positioned on the compressor conduit and the turbine conduit.

6. The ACAES system of claim 5 wherein the compressor conduit is arranged to pass air at a first pressure through the first TES unit, subsequently pass air at a second pressure through the second TES unit, and subsequently pass air at a third pressure through the third TES unit;

and

wherein the turbine conduit is arranged to pass air at the third pressure through the third TES unit, subsequently pass air at the second pressure through the first TES unit, and subsequently pass air at the first pressure through the second TES unit.

7. The ACAES system of claim 6 wherein the air at the first pressure comprises low pressure air, the air at the second pressure comprises intermediate pressure air, and the air at the third pressure comprises high pressure air, such that the first TES unit receives low pressure air from the compressor conduit and intermediate pressure air from the turbine conduit, such that the second TES unit receives intermediate pressure air from the compressor conduit and low pressure air from the turbine conduit, and such that the third TES unit receives high pressure air from the compressor conduit and high pressure air from the turbine conduit.

8. The ACAES system of claim 1 wherein each of the plurality of TES units comprises a plurality of TES subunits connected in parallel to both the compressor conduit and the turbine conduit.

9. The ACAES system of claim 1 wherein the plurality of TES units are arranged along the compressor conduit and the turbine conduit to cool the air subsequent to each stage of compression and to heat the air prior to each stage of expansion, respectively.

10. The ACAES system of claim 1 wherein each of the plurality of TES units operates in a temperature range of 200°

to 360°

Celsius.

11. 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 plurality of thermal energy storage (TES) units connected to each of the compressor conduit and the turbine conduit, the plurality of TES units spaced intermittently among the plurality of compressor units and the plurality of turbine units, to cool and heat the air as it passes through the respective compressor conduit and the turbine conduit;

wherein the air is routed through the plurality of TES units such that at least a portion of the plurality of TES units operate at a first pressure state during the compression stage and at a second pressure state different from the first pressure state during the expansion stage.

12. The method of claim 11 wherein passing the air through the plurality of TES units comprises:

passing the air through a first TES unit and subsequently passing the air through a second TES unit when passing the air through the compressor conduit such that low pressure air passes through the first TES unit and high pressure air passes through the second TES unit; and

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

13. The method of claim 11 wherein passing the air through the plurality of TES units comprises:

passing the air through a first TES unit, subsequently passing the air through a second TES unit, and subsequently passing the air through a third TES unit when passing the air through the compressor conduit, such that low pressure air passes through the first TES unit, intermediate pressure air passes through the second TES unit, and high pressure air passes through the third TES unit; and

passing the air through the third TES unit, subsequently passing the air through the first TES unit, and subsequently passing the air through the second TES unit when passing the air through the turbine conduit, such that high pressure air passes through the third TES unit, intermediate pressure air passes through the first TES unit, and low pressure air passes through the second TES unit.

14. The method of claim 11 wherein compressing the air comprises compressing the air in one of a two-stage compressor system and a three-stage compressor system;

and

wherein expanding the air comprises expanding the air in one of a two-stage turbine system and a three-stage turbine system.

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 compression path 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 compression path 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

an expansion path connecting the plurality of turbines and having an air inlet and an air outlet; and

a multi-stage thermal energy storage (TES) system configured to cool air passing through the compression path during a charging stage and heat air passing through the expansion path during a discharging stage, the multi-stage TES system comprising a plurality of TES units each configured to operate in a different pressure state;

wherein the compression path and the expansion path are routed such that at least a portion of the plurality of TES units operate at a first pressure state during the charging stage and at a second pressure state different from the first pressure state during the discharging stage.

16. The ACAES system of claim 15 wherein the multi-stage TES system comprises:

a first TES unit connected to each of the compression path and the expansion path; and

a second TES unit connected to each of the compression path and the expansion path;

wherein the first TES unit operates at a low pressure state during the charging stage and at a high pressure state during the discharging stage, and wherein the second TES unit operates at a high pressure state during the charging stage and at a low pressure state during the discharging stage.

17. The ACAES system of claim 16 wherein the compression path is routed to pass low pressure air through the first TES unit and subsequently pass high pressure air through the second TES unit;

and

wherein the expansion path is routed to pass high pressure air through the first TES unit and subsequently pass low pressure air through the second TES unit.

18. The ACAES system of claim 15 wherein the multi-stage TES system comprises:

a first TES unit connected to each of the compression path and the expansion path;

a second TES unit connected to each of the compression path and the expansion path; and

a third TES unit connected to each of the compression path and the expansion path;

wherein the first TES unit operates at a low pressure state during the charging stage and at an intermediate pressure state during the discharging stage, wherein the second TES unit operates at an intermediate pressure state during the charging stage and at a low pressure state during the discharging stage, and wherein the third TES unit operates at a high pressure state during the charging stage and at a high pressure state during the discharging stage.

19. The ACAES system of claim 18 wherein the compression path is routed to pass low pressure air through the first TES unit, pass intermediate pressure air through the second TES unit, and pass high pressure air through the third TES unit;

and

wherein the expansion path is routed to pass high pressure air through the third TES unit, pass intermediate pressure air through the first TES unit, and pass low pressure air through the second TES unit.

20. The ACAES system of claim 15 wherein each of the plurality of TES units comprises a plurality of TES subunits connected in parallel to both the compression path and the expansion path.