Control of System with Gas Based Cycle

• US 20150211386A1
• Filed: 03/11/2013
• Published: 07/30/2015
• Est. Priority Date: 04/30/2012
• Status: Active Grant

• Current Assignee: Energy Technologies Institute LLP
• Original Assignee: Isentropic, Ltd.
• Inventors: Howes, Jonathan Sebastian, Macnaghten, James, Hunt, Rowland Geoffrey
• Granted Patent: US 9,915,177 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F01K 3/02 Use of accumulators and specific engine types; Control thereof
• CPC Class Codes: F01K 3/12 having two or more accumulators
• CPC Class Codes: F01K 7/00 Steam engine plants characterised by the use of specific types of engine F01K3/02 takes precedence; Plants or engines characterised by their use of special steam systems, cycles or processes reciprocating-piston engines using uniflow principle F01B17/04; Control means specially adapted for such systems, cycles or processes; Use of withdrawn or exhaust steam for feed-water heating
• CPC Class Codes: F01K 7/16 the engines being only of turbine type the engines using steam of critical or overcritical pressure F01K7/32; the engines being of extraction or non-condensing type F01K7/34
• CPC Class Codes: F01K 7/36 the engines being of positive-displacement type

Abstract

System (2) for carrying out a gas based thermodynamic cycle in which a gas is compressed in at least one compressor (8) in one part of the cycle and is expanded in at least one expander (10) operating simultaneously in an upstream or downstream part of the cycle, wherein the change in absolute internal power with gas mass flow rate differs as between the compressor and the expander and wherein the system comprises a control system configured to make selective adjustments so as individually to control, either directly or indirectly, the respective gas mass flow rates through each of the compressor and expander. The system may be an energy storage system including a pumped heat energy storage system configured to provide independent graduated control of system pressure and output power by selective adjustment of the respective gas mass flow rates through each half-engine.

Claims

1. A system for carrying out a gas based thermodynamic cycle, the system comprising:

at least one compressor configured to compress a gas in one part of the cycle;

at least one expander configured to operate simultaneously to expand the gas in an upstream or downstream part of the cycle, wherein a change in absolute internal power with gas mass flow rate differs as between the compressor and the expander; and

a control system configured to make selective adjustments so as individually to control, either directly or indirectly, respective gas mass flow rates through each of the compressor and the expander so as to provide independent control of first and second system variables.

3. A system according to claim 1, wherein the control system is further configured so as to provide independent graduated control of the first and second system variables.

4. A system according to claim 3, wherein the the first and second system variables are a power variable and a pressure or pressure related variable.

5. A system according to claim 3, wherein the control system is configured to increase or decrease the first system variable whilst maintaining the second system variable constant.

7. A system according to claim 1, configured as an energy storage system, the energy storage system comprising:

a first stage comprising;

a hot half-engine operable as the at least one compressor during a charging mode and as the at least one expander during a discharging mode and, wherein the hot half-engine comprises at least one single reversible machine or respective machines to implement compression and expansion functions; and

a first heat store configured to receive and store thermal energy from gas compressed by the hot half-engine in the charging mode, and configured to transfer thermal energy to the gas compressed by the cold half-engine in the discharging mode; and

a second stage comprising;

a cold half-engine operable as the at least one expander to receive gas from the first heat store during the charging mode, operable as the at least one compressor driving gas into the first heat store during the discharging mode, and comprising a single reversible machine or respective machines to implement compression and expansion functions; and

a second heat store configured to transfer thermal energy to gas expanded by the cold half-engine during the charging mode, and configured to receive and store thermal energy from gas expanded by the hot half-engine during the discharging mode.

8. A system according to claim 7, wherein the system is configured to use an external power input during the charging mode and to generate an external power output during the discharging mode,

wherein the control system is further configured to provide independent graduated control of a pressure or pressure related variable associated with the system and independent graduated control of the external power input or output of the system by selective adjustment of a gas flow rate through the hot half-engine and a gas flow rate through the cold half-engine.

9. A system according to claim 7, wherein the control system is further configured to implement an algorithm using an external power input or output and a system internal condition as input, wherein the algorithm calculates respective mass flow rates of the hot and cold half-engines as output.

11. A system according to claim 7, wherein the control system is further configured to maintain a pressure of the first store or a pressure of the second store within an optimum range, or, at an optimum value.

12. A system according to claim 7, wherein the control system is further configured to maintain an output temperature of the hot half-engine within an optimum range, or, at an optimum value.

14. A system according to claim 7, wherein the control system is further configured to increase or decrease external power input or output whilst maintaining a pressure variable constant by increasing or decreasing the respective mass flow rates through the hot and cold half-engines by the same amount.

15. A system according to claim 7, wherein the control system is further configured to control a pressure variable whilst maintaining external power input or output constant by changing the mass flow rates through the hot and cold half-engines by selected differing amounts that do not affect the external power input or output.

16. A system according to claim 1, wherein one or both of the at least one compressor and at least one expander comprise multiple compressor/expander stages and the control system is further configured to control mass flow rates differentially between individual stages of the compressor/expander stages in order to maintain inter-stage pressures at desired values.

17. A system according to claim 1, wherein one or both of the at least one compressor and at least one expander comprises a positive displacement device, the positive displacement device comprising a reciprocating valved device through which internal power and mass flow rate is controlled by selective alteration of valve timings.

19. A system according to claim 17, wherein the valved device is a reciprocating piston assembly comprising a working volume respectively connected via a high pressure valve to a high pressure region and via a low pressure valve to a low pressure region.

20. A system according to claim 19, wherein the valved device is configured such that both the high pressure valve and the low pressure valve open on pressure equalisation, and the control system is further configured only to control the timing of valve closure events of the high pressure valve and the low pressure valve.

27. A storage system according to claim 20, wherein the control system is further configured to mechanically determine the timing of valve closure events based on an external power input or output and on at least one system internal condition.

28. A storage system according to claim 20, wherein the control system is further configured to electronically determine the timing of valve closure events based on an external power input or output and on at least one system internal condition.

29. A storage system according to claim 20, wherein the control system is further configured to determine valve timing adjustments for an external power input or output, or to determine pressure modification based on parametric inputs, the parametric inputs comprising at least one current system internal condition and at least one current system external condition.

66. A system according to claim 7, wherein one or both of the hot half-engine and the cold half-engine comprises a positive displacement device, the positive displacement device comprising a reciprocating valved device through which internal power and mass flow rate are controlled by selective alteration of valve timings.

2. (canceled)

6. (canceled)

10. (canceled)

13. (canceled)

18. (canceled)

21-26. -26. (canceled)

30-65. -65. (canceled)

67. A method of implementing a gas based thermodynamic cycle with an energy storage system, wherein the energy storage system comprises a first stage comprising a hot half-engine and a first heat store, and a second stage comprising a cold half-engine and a second heat store, wherein the energy storage system uses an external power input during a charging mode, and the energy storage system generates an external power output during a discharging mode, the method comprising:

operating the hot half-engine and cold half-engine simultaneously;

compressing a gas using the hot half-engine of the first stage as a compressor during the charging mode and expanding the gas using the hot half-engine as an expander during the discharging mode, the hot half-engine comprising a single reversible machine or respective machines for the compression function and the expansion function;

receiving and storing, in the first heat store of the first stage, thermal energy from gas compressed by the hot half-engine in the charging mode;

transferring, in the first heat store, thermal energy to gas compressed by the cold half-engine in the discharging mode;

using the cold half-engine of the second stage as an expander to receive and expand gas coming from the first heat store during the charging mode, and using the cold half-engine as a compressor to compress and drive the gas into the first heat store during the discharging mode, the cold-half engine comprising a single reversible machine or respective machines for the expansion function and the compression function;

transferring, in the second heat store of the second stage, thermal energy to gas expanded by the cold half-engine during the charging mode;

receiving and storing, in the second heat store, thermal energy from gas expanded by the hot half-engine during the discharging mode; and

selectively adjusting, with a control system of the energy storage system, respective gas mass flow rates through the simultaneously operating hot half-engine and the cold half-engine to provide independent graduated control of a pressure or a pressure related variable associated with the energy storage system and independent graduated control of the external power input or output of the energy storage system.