Controlled organic rankine cycle system for recovery and conversion of thermal energy

• US 8,528,333 B2
• Filed: 03/03/2008
• Issued: 09/10/2013
• Est. Priority Date: 03/02/2007
• Status: Active Grant

• Current Assignee: Victor Juchymenko
• Original Assignee: Victor Juchymenko
• Inventors: Juchymenko, Victor
• Primary Examiner(s): NGUYEN, HOANG M
• Application Number:
  US12/529,539
• Publication Number:
  US 20100018207A1
• Time in Patent Office: 2,017 Days
• Field of Search: 606/14, 606/16, 606/18, 606/51, 606/71, 606/60, 606/64, 606/66, 606/68, 606/76
• US Class Current: 60/618
• CPC Class Codes: F01K 23/02 the engine cycles being thermally coupled
• CPC Class Codes: F01K 23/065 the combustion taking place in an internal combustion piston engine, e.g. a diesel engine
• CPC Class Codes: F01K 25/10 the vapours being cold, e.g. ammonia, carbon dioxide, ether

Abstract

A system for controlled recovery of thermal energy and conversion to mechanical energy. The system collects thermal energy from a reciprocating engine, specifically from engine jacket fluid and/or engine exhaust and uses this thermal energy to generate a secondary power source by evaporating an organic propellant and using the gaseous propellant to drive an expander in production of mechanical energy. A monitoring module senses ambient and system conditions such as temperature, pressure, and flow of organic propellant at one or more locations; and a control module regulates system parameters based on monitored information to optimize secondary power output. A tertiary, or back-up power source may also be present. The system may be used to meet on-site power demands using primary, secondary, and tertiary power.

Claims

1. A system for controlled recovery of thermal energy from a natural gas compression module powered by a reciprocating engine, the natural gas compression module comprising one or more compression stages for compressing natural gas flowing within a pipeline and conversion of said thermal energy to mechanical energy, the system comprising:

a. a natural gas compression module and a reciprocating engine operable to provide a primary power source and a one or more sources of thermal energy;

b. a circulating pump, at least one propellant heat exchanger, an expander, and a condenser, arranged to operate an organic Rankine cycle in which thermal energy is collected from the engine and from the natural gas compression module and is transferred to a liquid organic propellant in the at least one propellant heat exchanger to evaporate the propellant, which gaseous propellant then drives the expander in production of mechanical energy to create a secondary power source, for use in powering at least one system parasitic load with spent propellant from the expander condensed back into liquid form by the condenser for reuse within the organic Rankine cycle;

c. a sensor for measuring at least one of;

temperature;

pressure; and

flow of organic propellant within the Rankine cycle;

d. and a control module for regulating operation of the Rankine cycle based on said sensor measurements, to optimize power generation by the secondary power source.

2. The system as in claim 1, wherein thermal energy is collected from the reciprocating engine by circulation of fluid about an engine jacket of the reciprocating engine, which thermal energy is transferred from the jacket fluid to the organic propellant at the propellant heat exchanger.

3. The system as in claim 2, wherein the control module regulates the flow of jacket fluid between the engine and the heat exchanger to control the amount of thermal energy collected from the engine for use within the organic Rankine cycle.

4. The system as in claim 2, further comprising a jacket fluid diverter valve for directing engine jacket water to the engine jacket fluid heat exchanger or to an engine radiator.

5. The system as in claim 2, further comprising a second propellant heat exchanger, wherein additional thermal energy is collected from the reciprocating engine by circulation of thermal fluid about a thermal fluid heat exchanger within the engine exhaust system, with said additional thermal energy transferred to the organic propellant at the second propellant heat exchanger.

6. The system as in claim 5, wherein the thermal fluid comprises water, glycol, a mineral based thermal oil or a synthetic based thermal oil.

7. The system as in claim 5, further comprising an exhaust diverter valve for venting engine exhaust gas to atmosphere, wherein the control module regulates operation of the exhaust diverter valve to regulate the amount of thermal energy from the exhaust that is transferred to the thermal fluid for use within the organic Rankine cycle.

8. The system as in claim 1 wherein the sensor is an ambient air temperature sensor.

9. The system as in claim 1, wherein the control module comprises a processor for processing sensor measurements to determine the physical state of the organic propellant.

10. The system as in claim 1, wherein the control module compares sensor measurements to previously simulated performance schemes stored in the control module, and sends an adjustment signal to at least one system component.

11. The system as in claim 10, wherein the adjustment signal results in a reallocation of system power.

12. The system as in claim 10, wherein the adjustment signal effects a change in;

rate of heat transfer from the engine to the organic propellant;

rate of condensation of propellant;

volume of organic propellant;

flow rate of organic propellant;

or propellant pressure within the system.

13. The system as in claim 1, further comprising a power hub for receiving secondary power and supplying electric power to system components.

14. The system as in claim 1, wherein the condenser is located proximal to a jacket fluid radiator and wherein the control system operates an electric fan for blowing air across the radiator and condenser simultaneously.

15. The system as in claim 1, further comprising an air cooled radiator for cooling engine jacket fluid, whereby engine jacket fluid within the radiator is cooled by blowing ambient air across the radiator with a fan, and wherein the control module modulates the speed of the fan based on the temperature of the jacket water, such that the jacket water is cooled prior to its return to the engine.

16. The system as in claim 1 wherein the natural gas compression module further comprises a boost compressor powered with secondary power generated by the expander.

17. The system as in claim 16, wherein the secondary power is provided as mechanical shaft horsepower or electric power.

18. The system as in claim 1, wherein the natural gas compression module further comprises a cooling module to remove heat from the natural gas after at least one stage of compression.

19. The system as in claim 18, wherein the cooling module transfers thermal energy from the natural gas to the organic propellant.

20. The system as in claim 18, wherein the natural gas cooling module comprises a fan for blowing air across natural gas conduits, and wherein the fan is powered with secondary power generated by the expander.

21. The system as in claim 20, wherein the series of natural gas conduits are located proximal to the organic propellant condenser, and wherein the control system operates an electric fan for blowing air across the conduits and the condenser simultaneously.

22. The system as in claim 20, wherein the series of natural gas conduits are located proximal to an engine radiator, and wherein the control system operates an electric fan for blowing air across the radiator and conduits simultaneously.

23. The system as in claim 20, wherein the series of conduits are located proximal to the organic propellant condenser and an engine jacket fluid radiator, such that the fan simultaneously blows air across the gas cooling conduits, the condenser, and the radiator.

24. The system as in claim 1, wherein the expander is a screw expander.

25. The system as in claim 24, wherein rotational speed of the screw expander is adjusted using a throttle valve, which throttle valve is monitored and regulated by a speed control module.

26. The system as in claim 1, further comprising a recuperator for recovering thermal energy from organic propellant exiting the expander.

27. The system as in claim 1, further comprising a tertiary power source for providing supplementary power when primary and secondary power outputs are insufficient to meet local Power demands.

28. The system as in claim 1, wherein the control module regulates operation of the Rankine cycle through communication with at least one variable frequency drive or relay.

32. The system as in claim 1, wherein the secondary power source produces electric power for use in powering the parasitic load.

33. The system as in claim 1, wherein the sensor is located at the expander or condenser.

34. The system as in claim 1, further comprising a tertiary power source for providing supplementary power to the power hub.

29. A system for providing power at a remote site comprising:

a reciprocating engine operable to provide a primary power output and one or more sources of thermal energy;

a natural gas compression module powered by said reciprocating engine;

an organic Rankine cycle for collecting thermal energy from the reciprocating engine and converting said thermal energy to secondary power output;

a control module for regulating operating conditions of the engine and organic Rankine cycle to maximize secondary power output;

a tertiary power source; and

a power hub for receiving a combination of primary, secondary, and tertiary power and for supplying power to the site on demand.

30. The system as in claim 29, wherein the tertiary power source is grid power.

31. The system as in claim 29, wherein the tertiary power source is a generator.