Combined cycle power plant thermal energy conservation

Patent metadata

Field	Value
Publication number	US-9945266-B2
Application number	US-201514820739-A
Country	US
Kind code	B2
Filing date	Aug 7, 2015
Priority date	Aug 28, 2014
Publication date	Apr 17, 2018
Grant date	Apr 17, 2018

Abstract

A combined cycle power plant includes a gas turbine having a primary flow passage, a heat recovery steam generator having a heat exchanger disposed downstream from the primary flow passage, an exhaust stack in fluid communication with the primary flow passage and disposed downstream from the heat recovery steam generator and a reversible turning gear coupled to a rotor shaft of the gas turbine. The reversible turning gear counter rotates the rotor shaft during turning gear counter rotation operation of the gas turbine and reverses flow of combustion exhaust gas from the exhaust stack through the heat exchanger and back into the primary flow passage of the gas turbine, thereby conserving thermal energy stored in the heat recovery steam generator. A method for conserving thermal energy of a combined cycle power plant during counter rotation turning gear operation of the gas turbine is also disclosed.

First claim

What is claimed is:

1. A combined cycle power plant, comprising:
a gas turbine having a primary flow passage defined therein and a rotor shaft;
a heat recovery steam generator having a heat exchanger disposed downstream from the primary flow passage;
an exhaust stack in fluid communication with the primary flow passage and disposed downstream from the heat recovery steam generator; and
a reversible turning gear coupled to the rotor shaft of the gas turbine, wherein the reversible turning gear counter rotates the rotor shaft during turning gear counter rotation operation of the gas turbine and reverses flow of combustion exhaust gas from the exhaust stack through the heat exchanger and back into the primary flow passage of the gas turbine.

2. The combined cycle power plant as in claim 1 , wherein the primary flow passage is at least partially defined by one or more of an exhaust duct, a turbine, a compressor discharge casing, a compressor and an inlet.

3. The combined cycle power plant as in claim 1 , wherein the exhaust stack includes a hatch, wherein the hatch at least partially seals an exhaust gas from the gas turbine within the exhaust stack.

4. The combined cycle power plant as in claim 1 , wherein the gas turbine includes a bleed air outlet in fluid communication with the primary flow passage, wherein the bleed air outlet is fluidly coupled to the exhaust stack.

5. The combined cycle power plant as in claim 4 , wherein the bleed air outlet is positioned along an inlet section of the gas turbine.

6. The combined cycle power plant as in claim 4 , wherein the bleed air outlet is positioned along a compressor of the gas turbine.

7. The combined cycle power plant as in claim 4 , wherein the bleed air outlet is positioned along an outer casing of a combustion section of the gas turbine.

8. The combined cycle power plant as in claim 4 , wherein the bleed air outlet is positioned along a turbine of the gas turbine.

9. The combined cycle power plant as in claim 4 , wherein the bleed air outlet is positioned along an exhaust duct of the gas turbine.

10. The combined cycle power plant as in claim 4 , further comprising a blower fluidly coupled to the bleed air outlet and the exhaust stack, wherein the blower provides for fluid communication between the primary flow passage and the exhaust stack.

11. A method for conserving thermal energy of a combined cycle power plant during turning gear operation, the combined cycle power plant including a gas turbine having a rotor shaft, a heat recovery steam generator downstream from an exhaust outlet of the gas turbine and an exhaust stack downstream from the heat recovery steam generator, the method comprising:
routing combustion exhaust gas from the gas turbine through the heat recovery steam generator and into the exhaust stack during fired operation of the gas turbine, wherein the rotor shaft rotates in a regular rotational direction;
shutting down the combustion section of the gas turbine;
counter rotating the rotor shaft of the gas turbine via a turning gear, wherein counter rotation of the rotor shaft draws the combustion exhaust gas from the exhaust stack in a reverse flow direction, back through the heat recovery steam generator and through a primary flow passage of the gas turbine.

12. The method as in claim 11 , further comprising measuring temperature of the combustion exhaust gas within a section of the gas turbine.

13. The method as in claim 12 , further comprising stopping the counter rotation of the rotor shaft and resuming regular rotation of the rotor shaft when a measured temperature within a section of the gas turbine is above a predefined limit.

14. The method as in claim 13 , wherein the predefined temperature limit is within a range of 125 to 250 degrees Fahrenheit at the compressor inlet.

15. The method as claim 11 , further comprising energizing a blower during counter rotation turning gear operation, wherein the blower is fluidly coupled to a bleed air outlet and wherein the bleed air outlet is in fluid communication with the primary flow passage.

16. The method as in claim 15 , further comprising routing at least a portion of the combustion exhaust gas from the primary flow passage through the bleed air outlet and into the exhaust stack via the blower.

17. The method as in claim 11 , further comprising at least partially sealing the exhaust stack from atmosphere during counter rotation turning gear operation of the gas turbine.

18. The method as in claim 11 , further comprising routing at least a portion of the combustion exhaust gas from the primary flow passage of the gas turbine back into the exhaust stack during counter rotation turning gear operation of the gas turbine.

19. A method for conserving thermal energy of a combined cycle power plant, the combined cycle power plant including a gas turbine having a rotor shaft, a heat recovery steam generator downstream from an exhaust outlet of the gas turbine and an exhaust stack downstream from the heat recovery steam generator, the method comprising:
routing combustion exhaust gas from the gas turbine through the heat recovery steam generator and into the exhaust stack during fired operation of the gas turbine;
shutting down the combustion section of the gas turbine;
counter rotating a rotor shaft of the gas turbine via a reversible turning gear, wherein counter rotation of the rotor shaft draws the combustion exhaust gas from the exhaust stack in a reverse flow direction, back through the heat recovery steam generator and through a primary flow passage of the gas turbine;
measuring a temperature of the combustion exhaust gas exiting an inlet section of the gas turbine; and
comparing the measured combustion exhaust gas temperature to a predefined maximum compressor inlet temperature, wherein if the measured temperature is below the predefined maximum compressor inlet temperature, continue counter rotation of the rotor shaft, if the temperature is above the predefined maximum compressor inlet temperature discontinue counter rotation of the rotor shaft.

Assignees

• Gen Electric

Inventors

• Ekanayake Sanji
• Mestroni Julio Enrique
• Scipio Alston I

Classifications

• F01K23/10 Primary

  with exhaust fluid of one cycle heating the fluid in another cycle (F01K17/025 takes precedence) · CPC title

• F02C7/00

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title

• F01D25/34

  Turning or inching gear · CPC title

• F02C7/12

  Cooling of plants (of component parts, see the relevant subclasses, e.g. F01D; cooling of engines in general F01P) · CPC title

• Y02E20/16

  Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT] · CPC title