Nozzle system and method for starting and operating gas turbines on low-Btu fuels

Patent metadata

Field	Value
Publication number	US-9771869-B2
Application number	US-201414154692-A
Country	US
Kind code	B2
Filing date	Jan 14, 2014
Priority date	Mar 25, 2013
Publication date	Sep 26, 2017
Grant date	Sep 26, 2017

Abstract

A fuel nozzle system for enabling a gas turbine to start and operate on low-Btu fuel includes a primary tip having primary fuel orifices and a primary fuel passage in fluid communication with the primary fuel orifices, and a fuel circuit capable of controlling flow rates of a first and second low-Btu fuel gases flowing into the fuel nozzle. The system is capable of operating at an ignition status, in which at least the first low-Btu fuel gas is fed to the primary fuel orifices and ignited to start the gas turbine, and a baseload status, in which at least the second low-Btu fuel gas is fired at baseload. The low-Btu fuel gas ignited at the ignition status has a content of the first low-Btu fuel gas higher than that of the low-Btu fuel gas fired at the baseload status. Methods for using the system are also provided.

First claim

The invention claimed is:

1. A fuel nozzle system for enabling a gas turbine to start and operate on low-Btu fuel, comprising:
a fuel nozzle, said fuel nozzle comprising;
a primary tip comprising a plurality of primary fuel orifices; and
a primary fuel passage in fluid communication with the primary fuel orifices;

a fuel circuit capable of controlling flow rates of a first low-Btu fuel gas and a second low-Btu fuel gas flowing into the fuel nozzle; and
wherein the fuel nozzle system is capable of operating at:
an ignition status, in which a first fuel composition comprising at least the first low-Btu fuel gas is fed to the primary fuel orifices and ignited to start the gas turbine;
a baseload status, in which a second fuel composition comprising at least the second low-Btu fuel gas is fired to operate the gas turbine; and

wherein the fuel circuit is configured to separately control flow rates of the first low-Btu fuel gas and the second low-Btu fuel gas such that the the first fuel composition ignited at the ignition status has a content of the first low-Btu fuel gas higher than that of the second fuel composition fired at the baseload status;
wherein the first low-Btu fuel gas comprises a first combination of one or more of syngas, blast furnace gas and coke oven gas;
wherein the second low-Btu fuel gas comprises a second combination of one or more of syngas, blast furnace gas and coke oven gas; and
wherein the first combination is different than the second combination.

2. The fuel nozzle system of claim 1 , wherein
the fuel nozzle further comprises:
a secondary tip comprising a plurality of secondary fuel orifices; and
a secondary fuel passage in fluid communication with the secondary fuel orifices; and

the fuel circuit is configured to separately control compositions of fuel split between the primary and secondary passages such that at least the second low-Btu fuel gas is fed to the secondary fuel orifices for firing during the baseload status.

3. The fuel nozzle system of claim 2 , wherein the fuel nozzle system is configured such that compressed air flows to the secondary fuel orifices for purging during the ignition status, and at least one of the first or second low-Btu fuel gas flows to the primary fuel orifices for firing during the baseload status.

4. The fuel nozzle system of claim 2 , wherein the fuel nozzle system is configured such that compressed air flows to the secondary fuel orifices for purging during the ignition status, and compressed air flows to the primary fuel orifices for purging during the baseload status.

5. The fuel nozzle system of claim 2 , wherein the fuel nozzle system is configured such that at least one of the first or second low-Btu fuel gas flows to the secondary fuel orifices for ignition during the ignition status, and compressed air flows to the primary fuel orifices for purging during the baseload status.

6. The fuel nozzle system of claim 2 , wherein the fuel nozzle system is configured to have at least one of the first or second low-Btu fuel gas flowing to the secondary fuel orifices for ignition during the ignition status, and having at least one of the first or second low-Btu fuel gas flowing to the primary fuel orifices for firing during the baseload status.

7. The fuel nozzle system of claim 2 , wherein the primary fuel orifices in the primary tip are located downstream of the secondary fuel orifices in the secondary tip.

8. The fuel nozzle system of claim 2 , wherein a diameter of the primary fuel orifice is less than ⅓ of that of the secondary fuel orifice.

9. The fuel nozzle system of claim 1 , wherein:
the fuel nozzle further comprises a secondary tip comprising a plurality of secondary fuel orifices in fluid communication with the primary fuel orifices; and
the fuel nozzle system is configured such that:
at least the first low-Btu fuel gas flows to both the primary and secondary fuel orifices for ignition during the ignition status; and
at least the second low-Btu fuel gas flows to both the primary and secondary fuel orifices for firing and/or purging during the baseload status.

10. The fuel nozzle system of claim 9 , wherein the primary fuel orifices in the primary tip are located downstream of the secondary fuel orifices in the secondary tip.

11. The fuel nozzle system of claim 9 , wherein a diameter of the primary fuel orifice is less than ⅓ of that of the secondary fuel orifice.

12. The fuel nozzle system of claim 1 , wherein the fuel nozzle system is configured to have the at least the second low-Btu fuel gas flowing to the primary fuel orifices for firing during the baseload status.

13. A method for starting and operating a gas turbine on low-Btu fuels using a fuel nozzle comprising:
providing a first low-Btu fuel source capable of providing a first low-Btu fuel gas;
providing a second low-Btu fuel source capable of providing a second low-Btu fuel gas having a heating value lower than that of the first low-Btu fuel gas;
providing a fuel nozzle comprising:
a primary tip comprising a plurality of primary fuel orifices, and
a primary fuel passage in fluid communication with the primary fuel orifices;

providing a fuel circuit for separately controlling flow rates of the first low-Btu fuel gas and the second low-Btu fuel gas flowing into the fuel nozzle;
operating the fuel nozzle in an ignition status, comprising:
igniting a first fuel composition comprising at least the first low-Btu fuel gas at the primary fuel orifices to start the gas turbine; and

operating the fuel nozzle in a baseload status, comprising:
firing a second fuel composition comprising at least the second low-Btu fuel gas to operate the gas turbine;

wherein the first fuel composition ignited at the ignition status has a content of the first low-Btu fuel gas higher than that of the second fuel composition fired at the baseload status;
wherein the first low-Btu fuel gas comprises a first combination of one or more of syngas, blast furnace gas and coke oven gas;
wherein the second low-Btu fuel gas comprises a second combination of one or more of syngas, blast furnace gas and coke oven gas; and
wherein the first combination is different than the second combination.

14. The method of claim 13 , wherein:
providing the fuel nozzle further comprises providing a secondary tip comprising a plurality of secondary fuel orifices and a secondary fuel passage in fluid communication with the secondary fuel orifices; and
operating the fuel nozzle in a baseload status comprises firing the second low-Btu fuel gas or second combination of the first and second low-Btu fuel gases at the secondary fuel orifices.

15. The method of claim 14 , wherein:
operating the fuel nozzle in an ignition status further comprises feeding compressed air to the secondary fuel orifices for purging; and
operating the fuel nozzle in a baseload status further comprises firing at least one of the first and second low-Btu fuel gases at the primary fuel orifices.

16. The method of claim 14 , wherein:
operating the fuel nozzle in an ignition status further comprises feeding compressed air to the secondary fuel orifices for purging; and
operating the fuel nozzle in a baseload status further comprises feeding compressed air to the primary fuel orifices for purging.

17. The method of claim 14 , wherein:
operating the fuel nozzle in an ignition status further comprises igniting at least one of the first or second low-Btu fuel gas at the secondary fuel orifices; and
operating the fuel nozzle in a baseload status further comprises feeding compress

Assignees

• Gen Electric

Inventors

• Li Suhui
• Haynes Joel Meier
• Yu Ping
• Chen Wei
• Leach David
• Lipinski John Joseph
• Cardenas Jr Manuel Moises
• Wu Wenjie
• Zhang Qingguo

Classifications

• F23R3/36

  Supply of different fuels · CPC title

• F02C7/264 Primary

  Ignition · CPC title

• F02C3/22

  the fuel or oxidant being gaseous at standard temperature and pressure (F02C3/28 takes precedence) · CPC title

• F02C3/20

  using a special fuel, oxidant, or dilution fluid to generate the combustion products · CPC title

• F02C9/40

  specially adapted to the use of a special fuel or a plurality of fuels · CPC title