Power generation system having compressor creating excess air flow and turbo-expander to increase turbine exhaust gas mass flow

Patent metadata

Field	Value
Publication number	US-9828887-B2
Application number	US-201514662805-A
Country	US
Kind code	B2
Filing date	Mar 19, 2015
Priority date	Mar 19, 2015
Publication date	Nov 28, 2017
Grant date	Nov 28, 2017

Abstract

A power generation system may include: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied. The first integral compressor has a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A turbo-expander may be operatively coupled to the second gas turbine system. Control valves may control flow of the excess air flow from the first gas turbine system to at least one of the second gas turbine system and the turbo-expander, and flow of a discharge of the turbo-expander to an exhaust of at least one of the first turbine component and the second turbine component.

First claim

What is claimed is:

1. A power generation system, comprising:
a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of at least one of the first combustor and the first turbine component, creating an excess air flow,
a second gas turbine system including, a second turbine component, a second compressor and a second combustor to which air from the second compressor and fuel are supplied, the second combustor arranged to supply hot combustion gases to the second turbine component;
a turbo-expander operatively coupled to the second gas turbine system;
a first control valve system controlling flow of the excess air flow along an excess air flow path from the first gas turbine system to the second gas turbine system and the turbo-expander; and
a second control valve system combining a flow of a discharge of the turbo-expander directly with an exhaust of the first turbine component and the second turbine component to increase a gas mass flow of the exhaust of at least one of the first turbine component and the second turbine component;
wherein the exhaust of at least one of the first turbine component and the second turbine component is supplied to at least one steam generator for powering a steam turbine system.

2. The power generation system of claim 1 , wherein the excess air flow is supplied to a discharge of the second compressor by the first control valve system.

3. The power generation system of claim 1 , wherein the excess air flow is supplied to the second combustor by the first control valve system.

4. The power generation system of claim 1 , wherein the excess air flow is supplied to a turbine nozzle cooling inlet of the second turbine component by the first control valve system.

5. The power generation system of claim 1 , wherein the first control valve system controls flow of the excess air flow to at least one of a discharge of the second compressor, the second combustor and a turbine nozzle cooling inlet of the second turbine component.

6. The power generation system of claim 5 , wherein the first control valve system includes a first valve controlling a first portion of the excess air flow to the discharge of the second compressor, a second valve controlling a second portion of the excess air flow to the second combustor, and a third valve controlling a third portion of the flow of the excess air flow to the turbine nozzle cooling inlets of the second turbine component.

7. The power generation system of claim 6 , further comprising at least one sensor for measuring a flow rate of at least a portion of the excess air flow, each of the at least one sensor operably coupled to the first control valve system.

8. The power generation system of claim 1 , wherein the second control valve system includes a first valve controlling a first portion of the discharge of the turbo-expander to the exhaust of the first turbine component and a second valve controlling a second portion of the discharge of the turbo-expander to the exhaust of the second turbine component.

9. The power generation system of claim 1 , wherein the second gas turbine system further includes a rotating shaft coupling the second compressor, the second turbine component, a starter motor and the turbo-expander.

10. The power generation system of claim 1 , wherein the first gas turbine system further includes a rotating shaft coupling the first integral compressor, the first turbine component, and a load commutated inverter (LCI) motor.

11. A power generation system, comprising:
a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of at least one of the first combustor and the first turbine component, creating an excess air flow;
a second gas turbine system including a second turbine component, a second compressor and a second combustor to which air from the second compressor and fuel are supplied, the second combustor arranged to supply hot combustion gases to the second turbine component;
a turbo-expander operatively coupled to the second gas turbine system;
a first control valve system controlling flow of the excess air flow along an excess air flow path from the first gas turbine system to the second gas turbine system and the turbo-expander; and
a second control valve system combining a flow of a discharge of the turbo-expander directly with an exhaust of the first turbine component and the second turbine component to increase a gas mass flow of the exhaust of at least one of the first turbine component and the second turbine component, wherein the second control valve system includes a first valve controlling a first portion of the discharge of the turbo-expander to the exhaust of the first turbine component and a second valve controlling a second portion of the discharge of the turbo-expander to the exhaust of the second turbine component, wherein the exhaust of at least one of the first turbine component and the second turbine component is supplied to at least one steam generator for powering a steam turbine system,
wherein the second gas turbine system further includes a rotating shaft coupling the second compressor, the second turbine component, a starter motor and the turbo-expander.

12. The power generation system of claim 11 , wherein the first control valve system controls flow of the excess air flow to at least one of a discharge of the second compressor, the second combustor and a turbine nozzle cooling inlet of the second turbine component.

13. The power generation system of claim 12 , wherein the first control valve system includes a first valve controlling a first portion of the excess air flow to the discharge of the second compressor, a second valve controlling a second portion of the excess air flow to the second combustor, and a third valve controlling a third portion of the flow of the excess air flow to the turbine nozzle cooling inlets of the second turbine component.

14. The power generation system of claim 11 , wherein the first gas turbine system further includes a rotating shaft coupling the first integral compressor, the first turbine component, and a load commutated inverter (LCI) motor.

Assignees

• Gen Electric

Inventors

• Ekanayake Sanji
• Davis Dale Joel
• Kim Kihyung
• Scipio Alston Ilford
• Tong Leslie Yung Min

Classifications

• F02C6/08

  the gas being bled from the gas-turbine compressor · CPC title

• F01K23/10 Primary

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

• F05D2220/72

  a steam turbine · CPC title

• F02C3/13 Primary

  having variable working fluid interconnections between turbines or compressors or stages of different rotors {(controlling flow ratio between different flows of multi-flow jet-propulsion plant, e.g. ducted fan F02K3/075)} · 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