Nozzle assembly for a dual-fuel fuel nozzle

Patent metadata

Field	Value
Publication number	US-10612784-B2
Application number	US-201715626461-A
Country	US
Kind code	B2
Filing date	Jun 19, 2017
Priority date	Jun 19, 2017
Publication date	Apr 7, 2020
Grant date	Apr 7, 2020

Abstract

The present disclosure is directed to a nozzle assembly including a header manifold and a ring manifold, which defines a liquid fuel plenum, spaced from the header manifold. An outer sleeve connects to the ring manifold, and a nozzle body connects to the outer sleeve. The ring manifold, the outer sleeve, and the nozzle body define a fluid chamber. An inner fuel tube extends from the header manifold to the nozzle body. A portion of the inner fuel tube extends helically about an axial centerline of the nozzle assembly between the ring manifold and the nozzle body. A first fuel tube extends helically around a portion of the inner fuel tube. The first fuel tube fluidly couples the liquid fuel plenum to the header manifold. A second fuel tube extends helically around a portion of the inner fuel tube and fluidly couples the liquid fuel plenum to the header manifold.

First claim

What is claimed is:

1. A nozzle assembly, comprising:
a fuel manifold upstream of a downstream end of an end cover;
a ring manifold axially spaced from the fuel manifold, the ring manifold defining a liquid fuel plenum;
an outer sleeve connected to an aft side wall of the ring manifold;
a nozzle body connected to an aft end of the outer sleeve, wherein the ring manifold, the outer sleeve, and the nozzle body define a fluid chamber;
an inner fuel tube extending axially from the fuel manifold through the end cover and the ring manifold to the nozzle body, a radial gap defined between the ring manifold and the inner fuel tube, the radial gap extending axially from a forward side wall of the ring manifold to the aft side wall of the ring manifold, wherein a portion of the inner fuel tube extends helically about an axial centerline of the nozzle assembly between the aft side wall of the ring manifold and the nozzle body;
a first fuel tube extending axially from the fuel manifold through the end cover to the ring manifold, the first fuel tube further extending helically around a portion of the inner fuel tube and connected to the ring manifold radially outward of the radial gap, wherein the first fuel tube fluidly couples the liquid fuel plenum of the ring manifold to the fuel manifold to supply liquid fuel to at least one injector in the ring manifold; and
a second fuel tube extending axially from the fuel manifold to the ring manifold, the second fuel tube further extending helically around a portion of the inner fuel tube, wherein the second fuel tube fluidly couples the liquid fuel plenum of the ring manifold to the fuel manifold.

2. The nozzle assembly as in claim 1 , further comprising an axially oriented fuel injector mounted in an opening of the nozzle body, wherein the axially oriented fuel injector is fluidly coupled to the inner fuel tube.

3. The nozzle assembly as in claim 2 , wherein the axially oriented fuel injector is removably mounted within the opening of the nozzle body.

4. The nozzle assembly as in claim 1 , further comprising a plurality of radially oriented fuel injectors circumferentially spaced along an outer band of the ring manifold, wherein the plurality of radially oriented fuel injectors is in fluid communication with the liquid fuel plenum.

5. The nozzle assembly as in claim 4 , wherein each of the radially oriented fuel injectors of the plurality of radially oriented fuel injectors is removably mounted in a respective opening defined in the ring manifold.

6. The nozzle assembly as in claim 4 , further comprising a plurality of turning vanes positioned upstream of the plurality of radially oriented fuel injectors.

7. The nozzle assembly as in claim 1 , further comprising a tube support member coupled to the inner fuel tube, the first fuel tube and the second fuel tube.

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

9. The nozzle assembly as in claim 8 , wherein an aft end of the second fuel tube is connected to the forward side wall of the ring manifold.

10. The nozzle assembly as in claim 1 , wherein the inner fuel tube is axially unrestrained by the ring manifold.

11. The nozzle assembly as in claim 1 , wherein the first fuel tube and the second fuel tube are radially outward of the axial centerline of the nozzle assembly.

12. The nozzle assembly as in claim 1 , wherein coils of the first fuel tube and the second fuel tube are wound together with identical spacing and numbers of turns.

13. A dual-fuel fuel nozzle assembly, comprising:
a center body having a tube shape;
a gas fuel plenum defined within the center body; and
a nozzle assembly breach loaded through an end of the center body, wherein the nozzle assembly comprises:
a fuel manifold upstream of a downstream end of an end cover;
a ring manifold axially spaced from the fuel manifold, the ring manifold defining a liquid fuel plenum;
an outer sleeve connected to an aft side wall of the ring manifold;
a nozzle body connected to an aft end of the outer sleeve, wherein the ring manifold, the outer sleeve, and the nozzle body define a fluid chamber;
an inner fuel tube extending axially from the fuel manifold through the end cover and the ring manifold to the nozzle body, a radial gap defined between the ring manifold and the inner fuel tube, the radial gap extending axially from a forward side wall of the ring manifold to the aft side wall of the ring manifold, wherein a portion of the inner fuel tube extends helically about an axial centerline of the nozzle assembly between the aft side wall of the ring manifold and the nozzle body;
a first fuel tube extending axially from the fuel manifold through the end cover to the ring manifold, the first fuel tube further extending helically around a portion of the inner fuel tube and connected to the ring manifold radially outward of the radial gap, wherein the first fuel tube fluidly couples the liquid fuel plenum of the ring manifold to the fuel manifold to supply liquid fuel to at least one injector in the ring manifold; and
a second fuel tube extending axially from the fuel manifold to the ring manifold, the second fuel tube further extending helically around a portion of the inner fuel tube, wherein the second fuel tube fluidly couples the liquid fuel plenum of the ring manifold to the fuel manifold.

14. The dual-fuel fuel nozzle assembly as in claim 13 , wherein the nozzle assembly further comprises an axially oriented fuel injector mounted in an opening of the nozzle body, wherein the axially oriented fuel injector is fluidly coupled to the inner fuel tube.

15. The dual-fuel fuel nozzle assembly as in claim 14 , wherein the axially oriented fuel injector is removably mounted within the opening of the nozzle body.

16. The dual-fuel fuel nozzle assembly as in claim 13 , wherein the nozzle assembly further comprises a plurality of radially oriented fuel injectors circumferentially spaced along an outer band of the ring manifold; wherein the plurality of radially oriented fuel injectors is in fluid communication with the liquid fuel plenum; and wherein each of the radially oriented fuel injectors of the plurality of radially oriented fuel injectors is removably mounted in a respective opening defined in the ring manifold.

17. The dual-fuel fuel nozzle assembly as in claim 16 , further comprising a plurality of turning vanes positioned upstream of the plurality of radially oriented fuel injectors.

18. The dual-fuel fuel nozzle assembly as in claim 13 , wherein the inner fuel tube is axially unrestrained by the ring manifold.

19. The dual-fuel fuel nozzle assembly as in claim 13 , wherein the first fuel tube and the second fuel tube are radially outward of the axial centerline of the center body; and wherein an aft end of the first fuel tube and an aft end of the second fuel tube are connected to a forward side wall of the ring manifold.

20. The dual-fuel fuel nozzle assembly as in claim 13 , wherein coils of the first fuel tube and the second fuel tube are wound together with identical spacing and numbers of turns.

Assignees

• Gen Electric

Inventors

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

Classifications

• F23R3/36 Primary

  Supply of different fuels · CPC title

• F02C7/222

  Fuel flow conduits, e.g. manifolds · CPC title

• F23R3/283

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

• F23D17/002

  gaseous or liquid fuel · CPC title

• F23R3/38 Primary

  comprising rotary fuel injection means · CPC title