Dual-fuel fuel nozzle with gas and liquid fuel capability

Patent metadata

Field	Value
Publication number	US-10955141-B2
Application number	US-201715626387-A
Country	US
Kind code	B2
Filing date	Jun 19, 2017
Priority date	Jun 19, 2017
Publication date	Mar 23, 2021
Grant date	Mar 23, 2021

Abstract

The present disclosure is directed to a fuel nozzle including a center body having a tube shape and a ring manifold disposed at an aft end of the center body. The fuel nozzle also includes an inner tube extending axially through the ring manifold and disposed within the center body. The inner tube is in fluid communication with a diluent supply. The fuel nozzle further includes a fuel tube extending helically around a portion of the inner tube. The fuel tube fluidly couples a fuel plenum of the ring manifold to a liquid fuel supply. Furthermore, the fuel nozzle includes a plurality of fuel injectors circumferentially spaced within an outer band of the ring manifold and in fluid communication with the fuel plenum. Each fuel injector is oriented to direct atomized liquid fuel radially outward from the center body. The ring manifold and the inner tube are thermally decoupled.

First claim

What is claimed is:

1. A fuel nozzle, comprising:
a center body having a tube shape;
a ring manifold disposed at an aft end of the center body;
an inner tube extending axially through the ring manifold and disposed within the center body, the inner tube being in fluid communication with a diluent supply, the inner tube and the ring manifold at least partially defining a gas plenum within the center body;
an outer sleeve connected to the ring manifold and extending axially from the ring manifold to an aft end;
a nozzle body disposed within the outer sleeve, the nozzle body comprising an aft face that is disposed axially inward from the aft end of the outer sleeve, wherein an aft end of the inner tube is disposed within the outer sleeve and spaced apart from the nozzle body such that an axial gap is defined therebetween;
a fuel tube extending helically around a portion of the inner tube, the fuel tube fluidly coupling a fuel plenum of the ring manifold to a liquid fuel supply;
a plurality of fuel injectors circumferentially spaced within an outer band of the ring manifold and in fluid communication with the fuel plenum, each fuel injector of the plurality of fuel injectors being oriented to direct a flow of atomized liquid fuel radially outward from the center body;
a flexible seal disposed within the outer sleeve and circumferentially surrounding a portion of the inner tube, wherein the flexible seal extends between an aft side wall of the ring manifold and the aft end of the inner tube;
a fluid chamber, defined collectively by the aft side wall of the ring manifold, the outer sleeve, the flexible seal, and the nozzle body, that receives a diluent from the inner tube; and

wherein the ring manifold is unrestrained relative to the inner tube.

2. The fuel nozzle of claim 1 , wherein one or more fuel injectors of the plurality of fuel injectors is removably inserted into the ring manifold.

3. The fuel nozzle as in claim 1 , further comprising a plurality of turning vanes that extends radially outward from the center body, each turning vane including at least one fuel port, wherein a gas fuel plenum is in fluid communication with a gas fuel supply and each fuel port is in fluid communication with the gas fuel plenum.

4. The fuel nozzle as in claim 1 , wherein an aft end of the fuel tube is connected to a forward side wall of the ring manifold.

5. The fuel nozzle of claim 1 , wherein the nozzle body is disposed downstream from the aft end of the inner tube, wherein the nozzle body defines a plurality of apertures.

6. The fuel nozzle as in claim 5 , wherein the plurality of apertures is in fluid communication with the fluid chamber.

7. The fuel nozzle as in claim 1 , wherein the flexible seal is axially spaced apart from both the nozzle body and radially spaced apart from the outer sleeve such that the fluid chamber surrounds the flexible seal within the outer sleeve.

8. The fuel nozzle as in claim 7 , wherein the flexible seal is a bellows.

9. A combustor, comprising:
an end cover; and
a center fuel nozzle disposed along an axial centerline of the end cover, the center fuel nozzle comprising:
a center body having a tube shape;
a ring manifold disposed at an aft end of the center body;
an inner tube extending axially through the ring manifold and disposed within the center body, the inner tube being in fluid communication with a diluent supply, the inner tube and the ring manifold at least partially defining a gas plenum within the center body;
an outer sleeve connected to the ring manifold and extending axially from the ring manifold to an aft end;
a nozzle body disposed within the outer sleeve, the nozzle body comprising an aft face that is disposed axially inward from the aft end of the outer sleeve, wherein an aft end of the inner tube is disposed within the outer sleeve and spaced apart from the nozzle body such that an axial gap is defined therebetween;
a fuel tube extending helically around a portion of the inner tube, the fuel tube fluidly coupling a fuel plenum of the ring manifold to a liquid fuel supply;
a plurality of fuel injectors circumferentially spaced within an outer band of the ring manifold and in fluid communication with the fuel plenum, each fuel injector of the plurality of fuel injectors being oriented to direct a flow of atomized liquid fuel radially outward from the center body; a flexible seal disposed within the outer sleeve and circumferentially surrounding a portion of the inner tube, wherein the flexible seal extends between an aft side wall of the ring manifold and the aft end of the inner tube;
a fluid chamber defined collectively by the aft side wall of the ring manifold, the outer sleeve, the flexible seal, and the nozzle body, that receives a diluent from the inner tube; and
wherein the ring manifold is unrestrained relative to the inner tube.

10. The combustor of claim 9 , wherein one or more fuel injectors of the plurality of fuel injectors are removably inserted into the ring manifold.

11. The combustor as in claim 9 , further comprising a plurality of turning vanes that extends radially outward from the center body, each turning vane including at least one fuel port, wherein a gas fuel plenum is in fluid communication with a gas fuel supply and each fuel port is in fluid communication with the gas fuel plenum.

12. The combustor as in claim 9 , wherein an aft end of the fuel tube is connected to a forward side wall of the ring manifold.

13. The combustor of claim 9 , wherein the nozzle body is disposed within the outer sleeve downstream from the aft end of the inner tube, and wherein the nozzle body defines a plurality of apertures.

14. The fuel nozzle as in claim 1 , wherein the inner tube axially terminates at the aft end of the inner tube, wherein the aft end of the inner tube extends radially outward from an outer surface of the inner tube, and wherein the flexible seal extends axially between the aft end of the inner tube and the aft side wall of the ring manifold such that the flexible seal is radially spaced apart from the outer surface of the inner tube.

15. The fuel nozzle as in claim 1 , wherein the fluid chamber is only in fluid communication with the inner tube and the nozzle body.

16. The fuel nozzle as in claim 1 , wherein the fluid chamber is defined only by the aft side wall of the ring manifold, the outer sleeve, the flexible seal, and the nozzle body.

Assignees

• Gen Electric

Inventors

• Graham Kaitlin Marie
• Johnson Thomas Edward
• Myers Geoffrey David

Classifications

• F23D17/002

  gaseous or liquid fuel · CPC title

• F23R3/283

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title

• F23R3/286

  having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title

• F23R3/38 Primary

  comprising rotary fuel injection means · CPC title

• F23R3/36 Primary

  Supply of different fuels · CPC title