Power generation system exhaust cooling

Patent metadata

Field	Value
Publication number	US-9840953-B2
Application number	US-201514753080-A
Country	US
Kind code	B2
Filing date	Jun 29, 2015
Priority date	Jun 29, 2015
Publication date	Dec 12, 2017
Grant date	Dec 12, 2017

Abstract

A system for reducing a temperature of an exhaust gas stream of a gas turbine system according to an embodiment includes: a compressor component of a gas turbine system; an airflow generation system for attachment to a rotatable shaft of the gas turbine system, the airflow generation system and the compressor component drawing in an excess flow of air through an air intake section; a mixing area for receiving an exhaust gas stream produced by the gas turbine system; an air extraction system for: extracting at least a portion of the excess flow of air generated by the airflow generation system and the compressor component to provide bypass air; and diverting the bypass air into the mixing area to reduce a temperature of the exhaust gas stream; and a fluid injection system for injecting an atomized fluid into the mixing area to reduce a temperature of the exhaust gas stream.

First claim

What is claimed is:

1. A system for reducing a temperature of an exhaust gas stream of a gas turbine system, comprising:
a compressor component of a gas turbine system;
an airflow generation system for attachment to a rotatable shaft of the gas turbine system, the airflow generation system and the compressor component drawing in an excess flow of air through an air intake section;
a mixing area for receiving an exhaust gas stream produced by the gas turbine system;
an air extraction system for extracting at least a portion of the excess flow of air generated by the airflow generation system and the compressor component to provide bypass air, and for diverting the bypass air into the mixing area to reduce a temperature of the exhaust gas stream; and
a fluid injection system for injecting an atomized fluid into the mixing area to reduce a temperature of the exhaust gas stream; further comprising an exhaust processing system, including: a carbon monoxide (CO) removal system and a selective catalytic reduction (SCR) system for processing the reduced temperature exhaust gas stream; and where the mixing area is disposed upstream of the exhaust processing system; and further including injecting the atomized fluid into a second mixing area disposed between the (CO) removal system and the selective catalytic reduction (SCR) system.

2. The system of claim 1 , wherein the excess flow of air generated by the airflow generation system and the compressor component is about 10% to about 40% greater than a flow rate capacity of at least one of a combustor component and a turbine component of the gas turbine system.

3. The system of claim 1 , wherein the compressor component of the gas turbine system includes at least one oversized compressor stage, and wherein the airflow generation system comprises a fan.

4. The system of claim 1 , wherein the atomized fluid comprises water.

5. The system of claim 1 , wherein the atomized fluid comprises a water and ammonia solution.

6. The system of claim 1 , wherein the air extraction system comprises:
a bypass duct for diverting the bypass air around the gas turbine system into the mixing area to reduce the temperature of the exhaust gas stream; or
an enclosure surrounding the gas turbine system and forming an air passage, the bypass air flowing through the air passage and around the gas turbine system into the mixing area to reduce a temperature of the exhaust gas stream.

7. The system of claim 1 , wherein the air extraction system is configured to divert a portion of the excess flow of air into the compressor component to supercharge the gas turbine system.

8. A turbomachine system, comprising:
a gas turbine system including a compressor component, a combustor component, and a turbine component, wherein the compressor component of the gas turbine system includes at least one oversized compressor stage;
a shaft driven by the turbine component;
a fan coupled to the shaft upstream of the gas turbine system, the fan and the at least one oversized compressor stage of the compressor component drawing in an excess flow of air through an air intake section;
a mixing area for receiving an exhaust gas stream produced by the gas turbine system;
an air extraction system for: extracting at least a portion of the excess flow of air generated by the fan and the at least one oversized compressor stage of the compressor component to provide bypass air; and diverting the bypass air into the mixing area to reduce a temperature of the exhaust gas stream;
a fluid injection system for injecting an atomized fluid into the mixing area to reduce a temperature of the exhaust gas stream;

and
an exhaust processing system for processing the reduced temperature exhaust gas stream; wherein the exhaust processing system comprises a carbon monoxide (CO) removal system and a selective catalytic reduction (SCR) system; and the mixing area is disposed upstream of the exhaust processing system; and further including injecting the atomized fluid into a second mixing area disposed between the (CO) removal system and the selective catalytic reduction (SCR) system.

9. The turbomachine system of claim 8 , wherein the excess flow of air generated by the fan and the at least one oversized compressor stage of the compressor component is about 10% to about 40% greater than a flow rate capacity of at least one of the combustor component and the turbine component of the gas turbine system.

10. The turbomachine system of claim 8 , wherein the atomized fluid comprises water.

11. The turbomachine system of claim 8 , wherein the atomized fluid comprises a water and ammonia solution.

12. A power generation system, comprising:
a gas turbine system including a compressor component, a combustor component, and a turbine component, wherein the compressor component of the gas turbine system includes at least one oversized compressor stage;
a shaft driven by the turbine component;
an electrical generator coupled to the shaft for generating electricity;
a fan coupled to the shaft upstream of the gas turbine system, the fan and the at least one oversized compressor stage of the compressor component drawing in an excess flow of air through an air intake section;
a mixing area for receiving an exhaust gas stream produced by the gas turbine system;
an air extraction system for: extracting at least a portion of the excess flow of air generated by the fan and the at least one oversized compressor stage of the compressor component to provide bypass air; and diverting the bypass air into the mixing area to reduce a temperature of the exhaust gas stream;
a fluid injection system for injecting an atomized fluid into the mixing area to reduce a temperature of the exhaust gas stream; and
an exhaust processing system for processing the reduced temperature exhaust gas stream; wherein the exhaust processing system comprises a carbon monoxide (CO) removal system and a selective catalytic reduction (SCR) system; and the mixing area is disposed upstream of the exhaust processing system; and further including injecting the atomized fluid into a second mixing area disposed between the (CO) removal system and the selective catalytic reduction (SCR) system.

13. The power generation system of claim 12 , wherein the excess flow of air generated by the fan and the at least one oversized compressor stage of the compressor component is about 10% to about 40% greater than a flow rate capacity of at least one of the combustor component and the turbine component of the gas turbine system.

14. The power generation system of claim 12 , wherein the atomized fluid comprises water or a water and ammonia solution.

Assignees

• Gen Electric

Inventors

• Kulkarni Parag Prakash
• Davis Jr Lewis Berkley
• Reed Robert Joseph

Classifications

• F05D2270/082

  with as little NOx as possible · CPC title

• F05D2260/606

  Bypassing the fluid · CPC title

• F05D2260/212

  by water injection · CPC title

• F05D2250/80

  Size or power range of the machines · CPC title

• F02C9/18

  by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages {(F02C3/113 takes precedence)} · CPC title