Power generation system and method with partially recuperated flow path

• US 10,385,735 B2
• Filed: 04/24/2017
• Issued: 08/20/2019
• Est. Priority Date: 02/26/2014
• Status: Active Grant

• Current Assignee: Peregrine Turbine Technologies LLC
• Original Assignee: Peregrine Turbine Technologies LLC
• Inventors: Stapp, David Scott
• Primary Examiner(s): Nguyen, Hoang M
• Application Number:
  US15/495,349
• Publication Number:
  US 20170226901A1
• Time in Patent Office: 848 Days
• Field of Search: 60772, 60 39181, 60 39183, 60650, 60655, 60651, 60682
• 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 19/04 in combination with cooling or heating
• CPC Class Codes: F01K 23/02 the engine cycles being thermally coupled
• CPC Class Codes: F01K 25/103 Carbon dioxide F01K25/065 takes precedence
• CPC Class Codes: F01K 3/18 having heaters having both steam accumulator and heater F01K3/14; steam heaters per se F22
• 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: F02C 1/007 combination of cycles
• CPC Class Codes: F02C 1/04 the working fluid being heated indirectly in a fluidised-bed combustor F02C3/205
• CPC Class Codes: F02C 1/10 Closed cycles
• CPC Class Codes: F02C 6/04 Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output F02C6/18 takes precedence ; for a fluidised-bed combustor F02C3/205
• CPC Class Codes: F22B 3/08 at critical or supercritical pressure values
• CPC Class Codes: Y02E 20/14 Combined heat and power generation [CHP]

Abstract

The present disclosure relates to a power generation system and related methods that use supercritical fluids, whereby a portion of the supercritical fluid is recuperated.

Claims

1. A system configured to generate power, comprising:

an air breathing cycle configured to heat air flowing along the air breathing cycle;

a supercritical fluid cycle including a supercritical fluid compressor configured to receive and compress a supercritical fluid, a supercritical fluid turbine configured to receive and expand the supercritical fluid, at least one recuperating heat exchanger, a first valve configured to direct at least a portion of the compressed supercritical fluid discharged from the supercritical fluid compressor to the at least one recuperating heat exchanger, and a second valve configured to direct at least a portion of the expanded supercritical fluid discharged from the supercritical fluid turbine to the at least one recuperating heat exchanger;

one or more controllers in electronic communication with the first valve and the second valve, the one or more controllers configured to operate the first valve and the second valve so as to direct the flow of the supercritical fluid through the supercritical fluid cycle; and

a plurality of cross cycle heat exchangers arranged so that supercritical fluid from the supercritical fluid cycle and air from the air breathing cycle passes therethrough but does not intermix.

2. The system of claim 1, wherein the first valve is further configured to split the compressed supercritical fluid discharged from the supercritical fluid compressor into first and second discharge streams of compressed supercritical fluid, such that a) the first discharge stream of compressed supercritical fluid is directed to the at least one recuperating heat exchanger, and b) the second discharge stream of compressed supercritical fluid is directed to at least one cross cycle heat exchanger, and

the second valve is further configured to direct the expanded supercritical fluid discharged from the supercritical fluid turbine into first and second discharge streams of expanded supercritical fluid, such that a) the first discharge stream of expanded supercritical fluid is directed to the at least one recuperating heat exchanger, and b) the second discharge stream of expanded supercritical fluid is directed to at least one different cross cycle heat exchanger.

3. The system of claim 2, wherein the one or more controllers operates the first valve to direct between 55% to 75% of the compressed supercritical fluid discharged from the supercritical fluid compressor into the first discharge stream of compressed supercritical fluid.

4. The system of claim 2, wherein the one or more controllers operates the first valve to direct about 67% of the compressed supercritical fluid discharged from the supercritical fluid compressor into the first discharge stream of compressed supercritical fluid.

5. The system of claim 2, wherein the one or more controllers operates the second valve to direct between 70% to 90% of the expanded supercritical fluid discharged from the supercritical fluid turbine into the first discharge stream of expanded supercritical fluid.

6. The system of claim 2, wherein the one or more controllers operates the second valve to direct about 80% of the expanded supercritical fluid discharged from the supercritical fluid turbine into the first discharge stream of expanded supercritical fluid.

7. The system of claim 1, further comprising:

an eddy current torque coupling; and

a third valve, the third valve configured to direct at least a portion of the compressed supercritical fluid discharged from the supercritical fluid compressor to the eddy current torque coupling,

wherein the one or more controllers is an electronic communication with the third valve, and the one or more controllers is configured to operate the third valve so as to direct the flow of the supercritical fluid through the supercritical fluid cycle.

8. The system of claim 2, further comprising:

an eddy current torque coupling; and

a third valve, the third valve configured to split the second discharge stream of compressed supercritical fluid into third and fourth discharge streams of compressed supercritical fluid, such that a) the third discharge stream of compressed supercritical fluid is directed to the eddy current torque coupling, and b) the fourth discharge stream of compressed supercritical fluid is directed to the at least one cross cycle heat exchanger,

wherein the one or more controllers is an electronic communication with the third valve, and the one or more controllers is configured to operate the third valve so as to direct at least a portion of the second discharge stream of compressed supercritical fluid into the third discharge stream of compressed supercritical fluid and to direct the balance of the second discharge stream of compressed supercritical fluid into the fourth discharge stream of compressed supercritical fluid.

9. The system of claim 8, further comprising:

an eddy current torque coupling discharge stream; and

first and second temperature sensors, the first and second temperature sensors in electronic communication with the one or more controllers, wherein the first temperature sensor is configured to measure a temperature of the fourth discharge stream of compressed supercritical fluid, and the second temperature sensor is configured to measure a temperature of the eddy current torque coupling discharge stream,

wherein the one or more controllers are further configured to operate the third valve in response to the temperature of the fourth discharge stream and the temperature of the eddy current torque coupling discharge stream.

10. The system of claim 1, wherein the supercritical fluid is carbon dioxide.