Driven starter pump and start sequence

• US 9,410,449 B2
• Filed: 12/11/2013
• Issued: 08/09/2016
• Est. Priority Date: 11/29/2010
• Status: Active Grant

• Current Assignee: Echogen Power Systems, LLC
• Original Assignee: Echogen Power Systems, LLC
• Inventors: Held, Timothy James, Vermeersch, Michael, Xie, Tao
• Primary Examiner(s): Trieu, Thai Ba
• Assistant Examiner(s): Wan, Deming
• Application Number:
  US14/102,677
• Publication Number:
  US 20140096521A1
• Time in Patent Office: 972 Days
• Field of Search: 606/46, 606/45, 606/47
• US Class Current: 1/1
• CPC Class Codes: F01K 13/02 Controlling, e.g. stopping or starting
• CPC Class Codes: F01K 23/04 condensation heat from one cycle heating the fluid in another cycle
• CPC Class Codes: F01K 25/10 the vapours being cold, e.g. ammonia, carbon dioxide, ether
• CPC Class Codes: F01K 25/103 Carbon dioxide F01K25/065 takes precedence
• CPC Class Codes: F22B 35/086 operating at critical or supercritical pressure

Abstract

Aspects of the disclosure generally provide a heat engine system with a working fluid circuit and a method for starting a turbopump disposed in the working fluid circuit. The turbopump has a main pump and may be started and ramped-up using a starter pump arranged in parallel with the main pump of the turbopump. Once the turbopump reaches a self-sustaining speed of operation, a series of valves may be manipulated to deactivate the starter pump and direct additional working fluid to a power turbine for generating electrical power.

Claims

1. A method for starting a turbopump in a working fluid circuit, comprising:

circulating a working fluid in the working fluid circuit with a starter pump, the working fluid comprising carbon dioxide and the starter pump being in fluid communication with a first heat exchanger in thermal communication with a heat source;

transferring thermal energy to the working fluid from the heat source in the first heat exchanger;

expanding the working fluid in a drive turbine in fluid communication with the first heat exchanger, wherein the turbopump comprises the drive turbine operatively coupled to a main pump;

driving the main pump with the drive turbine;

diverting the working fluid discharged from the main pump into a first recirculation line disposed in the working fluid circuit, the first recirculation line having a first bypass valve arranged therein;

closing the first bypass valve as the turbopump reaches a self-sustaining speed of operation;

circulating the working fluid discharged from the main pump through the working fluid circuit;

deactivating the starter pump and opening a second bypass valve arranged in a second recirculation line disposed in the working fluid circuit; and

diverting the working fluid discharged from the starter pump into the second recirculation line.

2. The method of claim 1, wherein circulating the working fluid in the working fluid circuit with the starter pump is preceded by closing a shut-off valve to divert the working fluid around a power turbine arranged in the working fluid circuit.

3. The method of claim 2, further comprising:

opening the shut-off valve once the turbopump reaches the self-sustaining speed of operation, thereby directing the working fluid into the power turbine;

expanding the working fluid in the power turbine; and

driving a generator operatively coupled to the power turbine to generate electrical power.

4. The method of claim 2, further comprising:

opening the shut-off valve once the turbopump reaches the self-sustaining speed of operation;

directing the working fluid into a second heat exchanger fluidly coupled to the power turbine and in thermal communication with the heat source;

transferring additional thermal energy from the heat source to the working fluid in the second heat exchanger;

expanding the working fluid received from the second heat exchanger in the power turbine; and

driving a generator operatively coupled to the power turbine, whereby the generator is operable to generate electrical power.

5. The method of claim 2, further comprising:

opening the shut-off valve once the turbopump reaches the self-sustaining speed of operation;

directing the working fluid into a second heat exchanger in thermal communication with the heat source;

directing the working fluid from the second heat exchanger into a third heat exchanger fluidly coupled to the power turbine and in thermal communication with the heat source, wherein the first heat exchanger, the second heat exchanger, and the third heat exchanger are fluidly arranged in series with the heat source;

transferring additional thermal energy from the heat source to the working fluid in the third heat exchanger;

expanding the working fluid received from the third heat exchanger in the power turbine; and

driving a generator operatively coupled to the power turbine, whereby the generator is operable to generate electrical power.

20. The heat engine system of claim 1, further comprising:

a first bypass valve arranged in the first recirculation line; and

a second bypass valve arranged in the second recirculation line.

6. A heat engine system, comprising:

a working fluid comprising carbon dioxide;

a working fluid circuit containing the working fluid and at least a portion of the working fluid circuit is configured to contain the working fluid in a supercritical state;

a turbopump comprising a main pump and a drive turbine operatively coupled together and hermetically-sealed within a casing, the main pump being configured to circulate the working fluid throughout the working fluid circuit;

a starter pump fluidly arranged in parallel with the main pump in the working fluid circuit;

a first check valve arranged in the working fluid circuit downstream of the main pump;

a power turbine fluidly coupled to both the main pump and the starter pump via the working fluid circuit;

a shut-off valve arranged in the working fluid circuit to divert the working fluid around the power turbine;

a condenser fluidly coupled to the working fluid circuit, disposed downstream of at least one recuperator and upstream of the main pump and the starter pump, and configured to remove thermal energy from the working fluid;

a first recirculation line disposed downstream of the main pump and upstream of the condenser within the working fluid circuit; and

a second recirculation line disposed downstream of the starter pump and upstream of the condenser within the working fluid circuit.

7. The heat engine system of claim 6, further comprising a second check valve arranged in the working fluid circuit downstream of the starter pump.

8. The heat engine system of claim 6, wherein the at least one recuperator comprises:

a first recuperator fluidly coupled to the power turbine via the working fluid circuit; and

a second recuperator fluidly coupled to the drive turbine via the working fluid circuit.

9. The heat engine system of claim 8, further comprising a third recuperator fluidly coupled to the second recuperator via the working fluid circuit, wherein the first recuperator, the second recuperator, and the third recuperator are fluidly arranged in series within the working fluid circuit.

10. The heat engine system of claim 6, further comprising a first heat exchanger, a second heat exchanger, and a third heat exchanger configured to be fluidly arranged in series and in thermal communication with a heat source and the first heat exchanger and the second heat exchanger are fluidly arranged in parallel within the working fluid circuit.

11. The heat engine system of claim 6, wherein the working fluid is in a supercritical state within working fluid circuit downstream from the power turbine and the drive turbine and upstream of the starter pump and the main pump.

12. A heat engine system, comprising:

a working fluid comprising carbon dioxide;

a working fluid circuit containing the working fluid and separating the working fluid into a first mass flow and a second mass flow, and at least a portion of the working fluid circuit is configured to contain the working fluid in a supercritical state;

a turbopump comprising a main pump and a drive turbine operatively coupled together and arranged within a casing, the main pump being configured to circulate the working fluid throughout the working fluid circuit and the drive turbine being configured to expand the working fluid;

a starter pump fluidly arranged in parallel with the main pump in the working fluid circuit;

a first heat exchanger in fluid communication with the main pump via the working fluid circuit and configured to be in thermal communication with a heat source, the first heat exchanger receiving the first mass flow and configured to transfer thermal energy from the heat source to the first mass flow;

a second heat exchanger in fluid communication with the main pump and the starter pump via the working fluid circuit and configured to be in thermal communication with the heat source, the second heat exchanger receiving the second mass flow and configured to transfer thermal energy from the heat source to the second mass flow;

a power turbine fluidly coupled to the first heat exchanger via the working fluid circuit and configured to expand the first mass flow;

a first recuperator fluidly coupled to the power turbine via the working fluid circuit and receiving the first mass flow discharged from the power turbine;

a condenser fluidly coupled to the working fluid circuit downstream of the first recuperator and upstream of the main pump and configured to remove thermal energy from the working fluid;

a first recirculation line disposed downstream of the main pump and upstream of the condenser within the working fluid circuit; and

a second recirculation line disposed downstream of the starter pump and upstream of the condenser within the working fluid circuit.

13. The heat engine system of claim 12, wherein the first heat exchanger and the second heat exchanger are configured to be fluidly arranged in series and in thermal communication with the heat source and the first heat exchanger and the second heat exchanger are fluidly arranged in parallel within the working fluid circuit.

14. The heat engine system of claim 12, wherein the first recuperator is configured to transfer residual thermal energy from the first mass flow to the second mass flow upstream of the drive turbine for the second mass flow.

15. The heat engine system of claim 12, wherein the first recuperator is configured to transfer residual thermal energy from the first mass flow discharged from the power turbine to the first mass flow directed to the first heat exchanger.

16. The heat engine system of claim 12, further comprising a second recuperator fluidly coupled to the drive turbine via the working fluid circuit and configured to receive the working fluid discharged from the drive turbine.

17. The heat engine system of claim 16, wherein the second recuperator is configured to transfer residual thermal energy from the second mass flow to a combination of the first and second mass flows.

18. The heat engine system of claim 16, wherein the second recuperator is configured to transfer residual thermal energy from the second mass flow discharged from the drive turbine to the second mass flow directed to the second heat exchanger.

19. The heat engine system of claim 12, wherein the working fluid is in a supercritical state within working fluid circuit downstream from the power turbine and the drive turbine and upstream of the starter pump and the main pump.