VALVE NETWORK AND METHOD FOR CONTROLLING PRESSURE WITHIN A SUPERCRITICAL WORKING FLUID CIRCUIT IN A HEAT ENGINE SYSTEM WITH A TURBOPUMP

• US 20170314420A1
• Filed: 10/28/2015
• Published: 11/02/2017
• Est. Priority Date: 11/03/2014
• Status: Active Grant

• Current Assignee: Echogen Power Systems, LLC
• Original Assignee: Echogen Power Systems, LLC
• Inventors: Bowan, Brett A., Vermeersch, Michael Louis
• Granted Patent: US 10,267,184 B2
• Time in Patent Office: Days
• CPC Class Codes: F01K 11/02 the engines being turbines
• CPC Class Codes: F01K 13/02 Controlling, e.g. stopping or starting
• CPC Class Codes: F01K 25/02 the fluid remaining in the liquid phase
• CPC Class Codes: F01K 25/103 Carbon dioxide F01K25/065 takes precedence
• 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: F04D 15/0011 by-pass valves
• CPC Class Codes: F04D 15/0072 Installation or systems with two or more pumps, wherein the flow path through the stages can be changed, e.g. series-parallel
• CPC Class Codes: F05D 2260/85 Starting

Abstract

Aspects of the invention generally provide a heat engine system and a method for activating a turbopump within the heat engine system during a start-up process. The heat engine system utilizes a working fluid circulated within a working fluid circuit for capturing thermal energy. In one exemplary aspect, a start-up process for a turbopump in the heat engine system is provided such that the turbopump achieves self-sustained operation in a supercritical Rankine cycle. Bypass and check valves of a start pump and the turbopump, a drive turbine throttle valve, and other valves, lines, or pumps within the working fluid circuit are controlled during the turbopump start-up process. A process control system may utilize advanced control techniques of the control sequence to provide a successful start-up process of the turbopump without over pressurizing the working fluid circuit or damaging the turbopump via low bearing pressure.

Claims

1. A heat engine system, comprising:

a working fluid circuit having a high pressure side and a low pressure side and containing a working fluid;

a heat exchanger fluidly coupled to and in thermal communication with the high pressure side of the working fluid circuit, configured to be fluidly coupled to and in thermal communication with a heat source stream, and configured to transfer thermal energy from the heat source stream to the working fluid within the high pressure side;

an expander fluidly coupled to the working fluid circuit, disposed between the high pressure side and the low pressure side, and configured to convert a pressure drop in the working fluid to mechanical energy;

a driveshaft coupled to the expander and configured to drive a device with the mechanical energy;

a start pump fluidly coupled to the working fluid circuit, disposed between the low pressure side and the high pressure side, and configured to circulate or pressurize the working fluid within the working fluid circuit;

a start pump bypass valve fluidly coupled to the working fluid circuit, disposed downstream of the start pump, and configured to control the flow of the working fluid flowing into the high pressure side from the start pump;

a turbopump fluidly coupled to the working fluid circuit, disposed between the low pressure side and the high pressure side, and configured to circulate or pressurize the working fluid within the working fluid circuit, wherein the turbopump contains a drive turbine coupled to and configured to drive a pump portion;

a turbopump bypass valve fluidly coupled to the working fluid circuit, disposed downstream of the pump portion of the turbopump, and configured to control the flow of the working fluid flowing into the high pressure side from the pump portion;

a drive turbine throttle valve fluidly coupled to the working fluid circuit, disposed upstream of the drive turbine, and configured to control the flow of the working fluid flowing into the drive turbine;

a recuperator fluidly coupled to the working fluid circuit and configured to transfer thermal energy from the working fluid within the low pressure side to the working fluid within the high pressure side;

a condenser in thermal communication with the working fluid circuit and configured to remove thermal energy from the working fluid in the low pressure side; and

a process control system operatively connected to the working fluid circuit and configured to adjust the turbopump bypass valve and the start pump bypass valve while providing a turbopump discharge pressure at a greater value than a start pump discharge pressure.

2. The heat engine system of claim 1, further comprising a control algorithm contained within the process control system.

3. The heat engine system of claim 2, wherein the control algorithm is configured to calculate and adjust valve positions for the turbopump bypass valve and the start pump bypass valve for providing the turbopump discharge pressure at the greater value than the start pump discharge pressure.

4. The heat engine system of claim 1, further comprising a turbopump check valve disposed downstream of an outlet of the pump portion of the turbopump, wherein the turbopump check valve is configured to adjust from a closed-position to an opened-position at a predetermined pressure.

5. The heat engine system of claim 4, further comprising a start pump check valve disposed downstream of an outlet of a pump portion of the start pump, wherein the start pump check valve is configured to adjust from an opened-position to a closed-position at the predetermined pressure.

6. The heat engine system of claim 5, wherein the predetermined pressure is about 2,200 psig or greater.

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

an inventory supply line fluidly coupled to the low pressure side of the working fluid circuit and configured to transfer the working fluid into the working fluid circuit;

an inventory supply valve fluidly coupled to the inventory supply line and configured to control the flow of the working fluid flowing through the inventory supply line; and

a transfer pump fluidly coupled to the inventory supply line, configured to pressurize the inventory supply line, and configured to flow the working fluid through the inventory supply line and into the working fluid circuit.

8. The heat engine system of claim 7, wherein the inventory supply line, the inventory supply valve, and the transfer pump are components within a mass management system fluidly coupled to the low pressure side of the working fluid circuit.

9. The heat engine system of claim 8, wherein the mass management system further comprises a mass control tank fluidly coupled to the low pressure side by the inventory supply line and configured to receive, store, and dispense the working fluid.

10. The heat engine system of claim 7, wherein the process control system is configured to pressurize a section of the inventory supply line with the transfer pump and configured to adjust the inventory supply valve and the drive turbine throttle valve for transferring the working fluid into the drive turbine.

11. The heat engine system of claim 1, wherein at least a portion of the working fluid circuit contains the working fluid in a supercritical state and the working fluid comprises carbon dioxide.

12. The heat engine system of claim 1, wherein the expander is a power turbine and the driveshaft is coupled to a power device configured to convert the mechanical energy into electrical energy, the power device is selected from a generator, an alternator, a motor, derivatives thereof, or combinations thereof.

13. A method for activating a turbopump within a heat engine system during a start-up process, comprising:

circulating a working fluid within a working fluid circuit, wherein the working fluid circuit has a high pressure side and a low pressure side;

transferring thermal energy from a heat source stream to the working fluid by at least one heat exchanger fluidly coupled to and in thermal communication with the high pressure side of the working fluid circuit;

pressurizing a section of an inventory supply line with a transfer pump while maintaining an inventory supply valve in a closed-position, wherein the inventory supply line is fluidly coupled to and between a storage tank and the working fluid circuit;

flowing the working fluid from the high pressure side into a drive turbine of the turbopump, wherein the working fluid has an inlet pressure measured near an inlet of the drive turbine;

flowing the working fluid from a pump portion of the turbopump into the high pressure side, wherein the working fluid as a turbopump discharge pressure measured near an outlet of the pump portion of the turbopump;

detecting a desirable pressure within the section of the inventory supply line and detecting the turbopump discharge pressure equal to or greater than the inlet pressure;

adjusting the inventory supply valve to an opened-position, providing a drive turbine throttle valve in an opened-position, and flowing the working fluid through the inventory supply line, through the working fluid circuit, and into the drive turbine, wherein the drive turbine throttle valve is fluidly coupled to the working fluid circuit upstream of the drive turbine; and

increasing the turbopump discharge pressure during an acceleration process of the turbopump by;

switching a process controller for a turbopump bypass valve from an automatic mode setting to a manual mode setting;

switching a process controller for a start pump bypass valve from an automatic mode setting to a manual mode setting;

monitoring the turbopump discharge pressure via a process control system operatively connected to the working fluid circuit;

detecting an undesirable value of the turbopump discharge pressure via the process control system, wherein the undesirable value is less than a predetermined threshold value of the turbopump discharge pressure;

adjusting the turbopump bypass valve and the start pump bypass valve with the process control system to increase the turbopump discharge pressure;

detecting a desirable value of the turbopump discharge pressure via the process control system, wherein the desirable value is equal to or greater than the predetermined threshold value of the turbopump discharge pressure; and

switching the process controllers for the turbopump bypass valve and start pump bypass valve from the manual mode settings to the automatic mode settings.

14. The method of claim 13, further comprising circulating the working fluid within the working fluid circuit by a start pump prior to adjusting the inventory supply valve to the opened-position.

15. The method of claim 14, wherein the turbopump discharge pressure is greater than a start pump discharge pressure.

16. The method of claim 15, further comprising opening a turbopump check valve and closing a start pump check valve, wherein the turbopump check valve is fluidly coupled to the working fluid circuit downstream of the pump portion of the turbopump and the start pump check valve is fluidly coupled to the working fluid circuit downstream of a pump portion of the start pump.

17. The method of claim 13, further comprising activating adaptive tuning on the process controller of the turbopump bypass valve to change response properties for maintaining a specified setpoint.

18. The method of claim 13, further comprising flowing the working fluid through a power turbine and converting the thermal energy into mechanical energy.

19. The method of claim 18, further comprising converting the mechanical energy into electrical energy by a power generator or alternator coupled to the power turbine.

20. The method of claim 13, wherein at least a portion of the working fluid is in a supercritical state and the storage tank is a mass control tank.