System and method for mixing tempering air with flue gas for hot SCR catalyst

Patent metadata

Field	Value
Publication number	US-10092878-B2
Application number	US-201615060161-A
Country	US
Kind code	B2
Filing date	Mar 3, 2016
Priority date	Mar 3, 2016
Publication date	Oct 9, 2018
Grant date	Oct 9, 2018

Abstract

A simple-cycle gas turbine system includes an injection system including a plurality of injection tubes that may inject a fluid into a duct of an exhaust processing system that may process exhaust gas generated by a gas turbine engine. The exhaust processing system includes a selective catalytic reduction (SCR) system that may reduce a level of nitrogen oxides (NO x ) within the exhaust gas; and a mixing system positioned adjacent to the plurality of injection tubes and within the exhaust processing system. The mixing system includes a mixing module having a plurality of turbulators that may swirl the fluid, or the exhaust gas, or both, in a first swirl direction to encourage turbulent flow along an axis of the exhaust processing system and thereby facilitate mixing between the fluid and the exhaust gas.

First claim

The invention claimed is:

1. A simple-cycle gas turbine system comprising:
an injection system comprising a plurality of injection tubes configured to inject a fluid into a duct of an exhaust processing system configured to process exhaust gas generated by a gas turbine engine, wherein the exhaust processing system comprises a selective catalytic reduction (SCR) system disposed within an exhaust duct of the exhaust processing system and configured to reduce a level of nitrogen oxides (NO x ) within the exhaust gas; and
a mixing system positioned adjacent to the plurality of injection tubes and within the exhaust processing system, wherein the mixing system comprises a mixing module having a grid comprising a plurality of rotary turbulators configured to swirl the fluid, or the exhaust gas, or both, in a first swirl direction to encourage turbulent flow along an axis of the exhaust processing system and thereby facilitate mixing between the fluid and the exhaust gas, wherein the mixing module is disposed within a transition duct of the exhaust processing system positioned between the gas turbine engine and the exhaust duct such that each rotary turbulator of the plurality of rotary turbulators is arranged at a different position relative to another rotary turbulator along a dimension of the grid, wherein the dimension is crosswise to the axis, and wherein each rotary turbulator of the plurality of rotary turbulators comprises a shaft configured to rotate the respective rotary turbulator about the axis.

2. The system of claim 1 , wherein the mixing module is a first mixing module and the plurality of rotary turbulators is a first plurality of rotary turbulators, and wherein the mixing system comprises a second mixing module positioned downstream of the first mixing module and having a second plurality of rotary turbulators configured to swirl the fluid, the exhaust gas, or both, in a second swirl direction within the exhaust processing system.

3. The system of claim 2 , wherein the first and second swirl directions are the same.

4. The system of claim 2 , wherein the first and second swirl directions are different.

5. The system of claim 2 , wherein the first plurality of rotary turbulators and the second plurality of rotary turbulators are aligned along a longitudinal axis of the exhaust processing system.

6. The system of claim 2 , wherein the first plurality of rotary turbulators and the second plurality of rotary turbulators are arranged in a staggered configuration along a longitudinal axis of the exhaust processing system.

7. The system of claim 2 , wherein the first mixing module, the second mixing module, or both are disposed between injection tubes of the plurality of injection tubes.

8. The system of claim 1 , wherein each rotary turbulator of the plurality of rotary turbulators comprises a plurality of fins radially extending from a center of the rotary turbulator, and wherein a fin of the plurality of fins is configured to rotate about a longitudinal axis of the exhaust processing system in the first swirl direction.

9. The system of claim 1 , wherein the mixing module comprises a plurality of corrugated packing plates configured to swirl the air, the exhaust gas, or both at least in the first swirl direction.

10. The system of claim 9 , wherein the corrugated packing plates are perforated.

11. The system of claim 1 , wherein the injection system is configured to inject cooling air as the fluid into the transition duct, wherein the transition duct is fluidly coupled to a turbine of the gas turbine engine, and wherein the mixing module is configured to encourage turbulent flow of the exhaust gas and the cooling fluid along the axis of the exhaust processing system and thereby facilitate mixing and heat exchange between the cooling air and the exhaust gas.

12. The system of claim 1 , wherein the injection system is configured to inject a reductant as the fluid into the exhaust duct containing a catalyst of the SCR system, wherein a second mixing module of the mixing system is disposed within the exhaust duct, and wherein the second mixing module is configured to encourage turbulent flow of the exhaust gas and the reductant along the axis of the exhaust processing system and thereby facilitate mixing between the reductant and the exhaust gas.

13. A simple cycle heavy-duty gas turbine system, comprising:
a mixing system disposed in an exhaust processing system of the simple cycle heavy-duty gas turbine system, wherein the mixing system comprises:
a first mixing module comprising a first grid having a first plurality of rotary turbulators configured to swirl cooling air, an exhaust stream generated by a heavy-duty gas turbine engine of the simple cycle heavy-duty gas turbine system, or both, in a first swirl direction; and
a second mixing module comprising a second grid having a second plurality of rotary turbulators configured to swirl the cooling air, the exhaust stream, or both, in a second swirl direction, wherein the first mixing module, the second mixing module, or both are disposed within a transition duct of the exhaust processing system such that each rotary turbulator of the first and second plurality of rotary turbulators is arranged at a different position relative to another rotary turbulator along a dimension of the respective grid, wherein the dimension is crosswise to a flow direction through the exhaust processing system, and wherein each rotary turbulator of the first and second plurality of rotary turbulators comprises a shaft configured to rotate the rotary turbulator about a longitudinal axis of the exhaust processing system.

14. The system of claim 13 , wherein the mixing system is positioned adjacent to an air injection system, wherein the air injection system comprises a plurality of air injection tubes configured to supply the cooling air to the transition section.

15. The system of claim 14 , wherein the first mixing module, the second mixing module, or both, are disposed between air injection tubes of the plurality of air injection tubes.

16. The system of claim 13 , wherein the first and second swirl directions are the same.

17. The system of claim 13 , wherein the first and second swirl directions are different.

18. The system of claim 13 , wherein the first plurality of rotary turbulators and the second plurality of rotary turbulators are aligned along a longitudinal axis of the exhaust processing system.

19. The system of claim 13 , wherein the first plurality of rotary turbulators and the second plurality of rotary turbulators are arranged in a staggered configuration along a longitudinal axis of the exhaust processing system.

20. A method of processing exhaust gas in a simple cycle gas turbine system, comprising:
flowing an exhaust stream from a gas turbine engine and into a transition section of an exhaust processing system;
injecting cooling air into a flow of the exhaust stream in the transition section using an air injection system comprising a plurality of air injection tubes configured to inject the cooling air;
swirling the exhaust stream, or the cooling air, or both, in the transition section of the exhaust processing system using a mixing system having an array of mixing modules, wherein each mixing module of the array of mixing modules comprises a grid having a plurality of rotary turbulators configured to swirl the exhaust stream, the cooling air, or both in a first direction, a second direction, or both, and wherein swirling the exhaust gas, the air, or both mixes and facilitate

Assignees

• Gen Electric

Inventors

• Zhang Hua
• Merchant Laxmikant
• Kippel Bradly Aaron
• Ponyavin Valery Ivanovich

Classifications

• B01D53/9418 Primary

  for removing nitrogen oxides by selective catalytic reduction [SCR] using a reducing agent in a lean exhaust gas · CPC title

• B01D53/8631

  Processes characterised by a specific device · CPC title

• F01D25/305 Primary

  with fluid, e.g. liquid injection · CPC title

• B01D2258/0283

  Flue gases · CPC title

• F05D2260/2212

  by creating turbulence · CPC title