Increased power in compressed-gas energy storage and recovery

• US 8,479,502 B2
• Filed: 01/10/2012
• Issued: 07/09/2013
• Est. Priority Date: 06/04/2009
• Status: Expired due to Fees

• Current Assignee: SustainX, Inc. (General Compression, Inc.)
• Original Assignee: SustainX, Inc. (General Compression, Inc.)
• Inventors: McBride, Troy O., Bollinger, Benjamin R.
• Primary Examiner(s): Lazo, Thomas E
• Application Number:
  US13/347,116
• Publication Number:
  US 20120137668A1
• Time in Patent Office: 546 Days
• Field of Search: 604/05, 604/07, 604/08, 604/10, 604/18, 604/59
• US Class Current: 60/410
• CPC Class Codes: F15B 1/00 Installations or systems with accumulators; Supply reservoir or sump assemblies
• CPC Class Codes: F15B 1/027 having accumulator charging devices
• CPC Class Codes: H02J 15/006 in the form of pneumatic energy, e.g. compressed air energy storage [CAES] accumulators for supplying fluid under pressure F15B1/04
• CPC Class Codes: Y02E 60/16 Mechanical energy storage, e.g. flywheels or pressurised fluids
• CPC Class Codes: Y10T 137/6416 With heating or cooling of the system

Abstract

In various embodiments, energy is stored or recovered via super-atmospheric compression and/or expansion of gas in conjunction with substantially adiabatic compression and/or expansion from or to atmospheric pressure.

Claims

1. A method for energy storage and recovery, the method comprising:

within a cylinder assembly, at least one of expanding or compressing gas between a first super-atmospheric pressure and a second super-atmospheric pressure larger than the first super-atmospheric pressure;

spraying heat-transfer fluid into the gas, the heat-transfer fluid exchanging heat with the gas during the at least one of expansion or compression to thermally condition the gas; and

at least one of (i) substantially adiabatically compressing gas from approximately atmospheric pressure to the first super-atmospheric pressure, or (ii) substantially adiabatically expanding gas from the first super-atmospheric pressure to approximately atmospheric pressure.

2. The method of claim 1, wherein the thermal conditioning renders the at least one of expansion or compression in the cylinder assembly substantially isothermal.

3. The method of claim 1, wherein the at least one of substantially adiabatically compressing gas or substantially adiabatically expanding gas is performed external to the cylinder assembly.

4. The method of claim 1, further comprising circulating the heat-transfer fluid between the cylinder assembly and a heat exchanger to maintain the heat-transfer fluid at a substantially constant temperature.

5. The method of claim 1, further comprising circulating gas from the cylinder assembly to an external heat exchanger and back to the cylinder assembly.

6. The method of claim 1, wherein energy stored during compression of gas originates from an intermittent renewable energy source of wind or solar energy, and gas is expanded to recover energy when the intermittent renewable energy source is nonfunctional.

7. The method of claim 1, wherein gas is substantially adiabatically compressed by a discrete blower and substantially adiabatically expanded by a discrete expander.

8. The method of claim 1, wherein gas is substantially adiabatically compressed and substantially adiabatically expanded by a bidirectional blower/expander.

9. The method of claim 1, further comprising supplying additional gas at the first super-atmospheric pressure to enable the at least one of substantially adiabatically compressing gas or substantially adiabatically expanding gas to be performed continuously at approximately constant power.

10. The method of claim 1, wherein gas is compressed within the cylinder assembly, and further comprising, thereafter, storing gas at approximately the second super-atmospheric pressure in a reservoir.

11. The method of claim 10, wherein the reservoir comprises a cavern.

12. The method of claim 10, wherein the reservoir comprises one or more pressure vessels.

13. The method of claim 1, wherein gas is expanded substantially adiabatically, and further comprising, thereafter, exhausting gas at approximately atmospheric pressure to atmosphere.

14. The method of claim 1, wherein the cylinder assembly comprises a movable boundary mechanism separating two chambers within the cylinder assembly, and further comprising at least one of (i) converting reciprocal motion of the boundary mechanism into rotary motion or (ii) converting rotary motion into reciprocal motion of the boundary mechanism.

15. The method of claim 1, wherein gas is compressed within the cylinder assembly, and further comprising, thereafter, (i) transferring the gas to a second cylinder assembly and (ii) compressing the gas within the second cylinder assembly from approximately the second super-atmospheric pressure to a third super-atmospheric pressure larger than the second super-atmospheric pressure.

16. The method of claim 1, wherein gas is expanded within the cylinder assembly, and further comprising, therebefore, (i) expanding the gas within a second cylinder assembly from a third super-atmospheric pressure larger than the second super-atmospheric pressure to approximately the second super-atmospheric pressure and (ii) transferring the gas to the cylinder assembly.

17. A method for energy storage and recovery, the method comprising:

substantially adiabatically compressing gas from approximately atmospheric pressure to a first super-atmospheric pressure;

within a cylinder assembly, compressing gas between the first super-atmospheric pressure and a second super-atmospheric pressure larger than the first super-atmospheric pressure;

thermally conditioning the gas during the compression within the cylinder assembly; and

thereafter, storing gas at a pressure approximately equal to or greater than the second super-atmospheric pressure in a reservoir.

18. The method of claim 17, wherein the thermal conditioning renders the compression in the cylinder assembly substantially isothermal.

19. The method of claim 17, wherein the substantially adiabatic compression is performed external to the cylinder assembly.

20. The method of claim 17, wherein thermally conditioning the gas comprises introducing a heat-transfer fluid within the cylinder assembly to exchange heat with the gas.

21. The method of claim 20, wherein introducing the heat-transfer fluid within the cylinder assembly comprises spraying the heat-transfer fluid into the gas.

22. The method of claim 20, further comprising circulating the heat-transfer fluid between the cylinder assembly and a heat exchanger to maintain the heat-transfer fluid at a substantially constant temperature.

23. The method of claim 17, wherein thermally conditioning the gas comprises circulating gas from the cylinder assembly to an external heat exchanger and back to the cylinder assembly.

24. The method of claim 17, wherein energy stored during compression of gas originates from an intermittent renewable energy source of wind or solar energy, and further comprising expanding gas to recover energy when the intermittent renewable energy source is nonfunctional.

25. The method of claim 17, wherein gas is substantially adiabatically compressed by a discrete blower.

26. The method of claim 17, wherein gas is substantially adiabatically compressed by a bidirectional blower/expander.

27. The method of claim 17, further comprising supplying additional gas at the first super-atmospheric pressure to enable the substantially adiabatic compression to be performed continuously at approximately constant power.

28. The method of claim 17, wherein the cylinder assembly comprises a movable boundary mechanism separating two chambers within the cylinder assembly, and further comprising at least one of (i) converting reciprocal motion of the boundary mechanism into rotary motion or (ii) converting rotary motion into reciprocal motion of the boundary mechanism.

29. The method of claim 17, wherein the reservoir comprises a cavern.

30. The method of claim 17, wherein the reservoir comprises one or more pressure vessels.

31. The method of claim 17, further comprising, after compression in the cylinder assembly, (i) transferring the gas to a second cylinder assembly and (ii) compressing the gas within the second cylinder assembly from approximately the second super-atmospheric pressure to a third super-atmospheric pressure larger than the second super-atmospheric pressure.

32. A method for energy storage and recovery, the method comprising:

substantially adiabatically compressing gas from approximately atmospheric pressure to a first super-atmospheric pressure;

within a cylinder assembly, compressing gas between the first super-atmospheric pressure and a second super-atmospheric pressure larger than the first super-atmospheric pressure;

thermally conditioning the gas during the compression within the cylinder assembly;

thereafter, transferring the gas to a second cylinder assembly; and

compressing the gas within the second cylinder assembly from approximately the second super-atmospheric pressure to a third super-atmospheric pressure larger than the second super-atmospheric pressure.

33. The method of claim 32, wherein the thermal conditioning renders the compression in the cylinder assembly substantially isothermal.

34. The method of claim 32, wherein the substantially adiabatic compression is performed external to the cylinder assembly.

35. The method of claim 32, wherein thermally conditioning the gas comprises introducing a heat-transfer fluid within the cylinder assembly to exchange heat with the gas.

36. The method of claim 35, wherein introducing the heat-transfer fluid within the cylinder assembly comprises spraying the heat-transfer fluid into the gas.

37. The method of claim 35, further comprising circulating the heat-transfer fluid between the cylinder assembly and a heat exchanger to maintain the heat-transfer fluid at a substantially constant temperature.

38. The method of claim 32, wherein thermally conditioning the gas comprises circulating gas from the cylinder assembly to an external heat exchanger and back to the cylinder assembly.

39. The method of claim 32, wherein energy stored during compression of gas originates from an intermittent renewable energy source of wind or solar energy, and further comprising expanding gas to recover energy when the intermittent renewable energy source is nonfunctional.

40. The method of claim 32, wherein gas is substantially adiabatically compressed by a discrete blower.

41. The method of claim 32, wherein gas is substantially adiabatically compressed by a bidirectional blower/expander.

42. The method of claim 32, further comprising supplying additional gas at the first super-atmospheric pressure to enable the substantially adiabatic compression to be performed continuously at approximately constant power.

43. The method of claim 32, wherein the cylinder assembly comprises a movable boundary mechanism separating two chambers within the cylinder assembly, and further comprising at least one of (i) converting reciprocal motion of the boundary mechanism into rotary motion or (ii) converting rotary motion into reciprocal motion of the boundary mechanism.

44. The method of claim 32, further comprising storing gas at a pressure approximately equal to or greater than the second super-atmospheric pressure in a cavern.

45. The method of claim 32, further comprising storing gas at a pressure approximately equal to or greater than the second super-atmospheric pressure in one or more pressure vessels.

46. A method for energy storage and recovery, the method comprising:

within a cylinder assembly, expanding gas between a first super-atmospheric pressure and a second super-atmospheric pressure larger than the first super-atmospheric pressure;

thermally conditioning the gas during the expansion within the cylinder assembly;

substantially adiabatically expanding gas from the first super-atmospheric pressure to approximately atmospheric pressure; and

prior to expanding gas within the cylinder assembly, (i) expanding the gas within a second cylinder assembly from a third super-atmospheric pressure larger than the second super-atmospheric pressure to approximately the second super-atmospheric pressure and (ii) transferring the gas to the cylinder assembly.

47. The method of claim 46, wherein the thermal conditioning renders the expansion in the cylinder assembly substantially isothermal.

48. The method of claim 46, wherein the substantially adiabatic expansion is performed external to the cylinder assembly.

49. The method of claim 46, wherein thermally conditioning the gas comprises introducing a heat-transfer fluid within the cylinder assembly to exchange heat with the gas.

50. The method of claim 49, wherein introducing the heat-transfer fluid within the cylinder assembly comprises spraying the heat-transfer fluid into the gas.

51. The method of claim 49, further comprising circulating the heat-transfer fluid between the cylinder assembly and a heat exchanger to maintain the heat-transfer fluid at a substantially constant temperature.

52. The method of claim 46, wherein thermally conditioning the gas comprises circulating gas from the cylinder assembly to an external heat exchanger and back to the cylinder assembly.

53. The method of claim 46, further comprising compressing gas to store energy originating from an intermittent renewable energy source of wind or solar energy, wherein gas is expanded to recover energy when the intermittent renewable energy source is nonfunctional.

54. The method of claim 46, wherein gas substantially adiabatically expanded by a discrete expander.

55. The method of claim 46, wherein gas is substantially adiabatically expanded by a bidirectional blower/expander.

56. The method of claim 46, further comprising supplying additional gas at the first super-atmospheric pressure to enable the substantially adiabatic expansion to be performed continuously at approximately constant power.

57. The method of claim 46, further comprising exhausting gas at approximately atmospheric pressure to atmosphere.

58. The method of claim 46, wherein the cylinder assembly comprises a movable boundary mechanism separating two chambers within the cylinder assembly, and further comprising at least one of (i) converting reciprocal motion of the boundary mechanism into rotary motion or (ii) converting rotary motion into reciprocal motion of the boundary mechanism.