Cartridge tip for turbomachine combustor

Patent metadata

Field	Value
Publication number	US-11767978-B2
Application number	US-202117382458-A
Country	US
Kind code	B2
Filing date	Jul 22, 2021
Priority date	Jul 22, 2021
Publication date	Sep 26, 2023
Grant date	Sep 26, 2023

Abstract

A cartridge tip includes a main body having an outer annular wall and an inner core each extending between a respective upstream end and a respective downstream end. The inner core is radially spaced apart from the outer annular wall such that an annular air passage is defined at least partially between the outer annular wall and the inner core. A pilot fuel circuit extends between a pilot inlet defined in the upstream end of the inner core and a pilot outlet defined in a downstream end of the inner core. The pilot fuel circuit extends at least partially along an axial centerline of the cartridge tip. A main fuel circuit extends between a main inlet in the upstream end of the inner core and a plurality of main outlets circumferentially spaced apart from one another and disposed upstream from the from the pilot outlet.

First claim

What is claimed is:

1. A cartridge tip comprising:
a main body comprising an outer annular wall and an inner core each extending between a respective upstream end and a respective downstream end, the inner core radially spaced apart from the outer annular wall such that an annular air passage is defined at least partially between the outer annular wall and the inner core,
wherein one or more struts couple the outer annular wall to the inner core, an annular heat shield includes a first end coupled to the outer annular wall within the annular air passage downstream of the one or more struts, the annular heat shield extends axially from the first end to a free end within the annular air passage, a circumferential rib extends radially outward from the inner core and terminates within the annular air passage with the circumferential rib radially spaced apart from the annular heat shield within the annular air passage, wherein the circumferential rib is disposed downstream of the first end;
a pilot fuel circuit defined in the inner core of the main body, the pilot fuel circuit extending between a pilot inlet defined in the upstream end of the inner core and a pilot outlet defined in the downstream end of the inner core, wherein the pilot fuel circuit extends at least partially along an axial centerline of the cartridge tip, and wherein the pilot fuel circuit includes a pilot inlet portion extending from the pilot inlet; and
a main fuel circuit defined in the inner core of the main body, the main fuel circuit extending between a main inlet in the upstream end of the inner core and a plurality of main outlets circumferentially spaced apart from one another and disposed upstream from the pilot outlet, the main fuel circuit including an annular plenum surrounding the pilot inlet portion of the pilot fuel circuit.

2. The cartridge tip of claim 1 , wherein the main fuel circuit includes in a serial flow order a main inlet portion extending from the main inlet and having a first branch and a second branch, the annular plenum fluidly coupled to the first branch and the second branch of the main inlet portion, and a plurality of circumferentially spaced passages each extending from the annular plenum to a respective main outlet of the plurality of main outlets.

3. The cartridge tip of claim 1 , wherein the pilot fuel circuit includes in a serial flow order the pilot inlet portion extending from the pilot inlet, an annular portion, a plurality of tangential passages, and an aft plenum extending to the pilot outlet.

4. The cartridge tip of claim 3 , wherein each tangential passage of the plurality of tangential passages extends from the annular portion to the aft plenum, and wherein each of the tangential passages of the plurality of tangential passages extends at least partially tangentially from the aft plenum along a radial plane such that the plurality of tangential passages is operable to induce a swirling flow of fuel within the aft plenum upstream from the pilot outlet.

5. The cartridge tip of claim 1 , wherein the outer annular wall includes a cylindrical portion and a converging aft portion downstream from the cylindrical portion and upstream from an aft end of the outer annular wall.

6. The cartridge tip of claim 5 , wherein the annular air passage extends from an annular inlet to each of a first plurality of outlets, a second plurality of outlets, and a central outlet.

7. The cartridge tip of claim 6 , wherein the annular inlet is defined between the outer annular wall and the inner core at the respective upstream end of the inner core, wherein the first plurality of outlets is defined in the cylindrical portion of the outer annular wall, wherein the second plurality of outlets is at least partially defined in the converging aft portion of the outer annular wall downstream from the first plurality of outlets, and wherein the central outlet is defined in the converging aft portion of the outer annular wall downstream from the second plurality of outlets.

8. The cartridge tip of claim 1 , wherein the one or more struts include a first strut and a second strut diametrically opposed to one another, and wherein the first strut and the second strut are each disposed in the annular air passage immediately downstream from an annular inlet.

9. The cartridge tip of claim 1 , wherein the cartridge tip is integrally formed.

10. The cartridge tip of claim 1 , wherein the annular air passage is disposed radially outward from both the pilot fuel circuit and the main fuel circuit.

11. The cartridge tip of claim 1 , wherein a downstream-flowing portion of the annular air passage is disposed between the annular heat shield and the inner core, and wherein an upstream-flowing portion of the annular air passage is disposed between the annular heat shield and the outer annular wall.

12. The cartridge tip of claim 11 , wherein the circumferential rib terminates within the downstream-flowing portion of the annular air passage, wherein the circumferential rib is disposed closer to the first end of the annular heat shield than the free end of the annular heat shield, and wherein the circumferential rib has a frustoconical cross-sectional shape.

13. A combustor comprising:
an end cover;
a combustion liner defining a combustion chamber;
a plurality of fuel nozzles extending between the end cover and the combustion liner; and
at least one liquid fuel cartridge extending through a fuel nozzle of the plurality of fuel nozzles to a cartridge tip, the cartridge tip comprising:
a main body comprising an outer annular wall and an inner core each extending between a respective upstream end and a respective downstream end, the inner core radially spaced apart from the outer annular wall such that an annular air passage is defined at least partially between the outer annular wall and the inner core,
wherein one or more struts couple the outer annular wall to the inner core, an annular heat shield includes a first end coupled to the outer annular wall within the annular air passage downstream of the one or more struts, the annular heat shield extends axially from the first end to a free end within the annular air passage, a circumferential rib extends radially outward from the inner core and terminates within the annular air passage with the circumferential rib radially spaced apart from the annular heat shield within the annular air passage, wherein the circumferential rib is disposed downstream of the first end;
a pilot fuel circuit defined in the inner core of the main body, the pilot fuel circuit extending between a pilot inlet defined in the upstream end of the inner core and a pilot outlet defined in the downstream end of the inner core, wherein the pilot fuel circuit extends at least partially along an axial centerline of the cartridge tip, and wherein the pilot fuel circuit includes a pilot inlet portion extending from the pilot inlet; and
a main fuel circuit defined in the inner core of the main body, the main fuel circuit extending between a main inlet in the upstream end of the inner core and a plurality of main outlets circumferentially spaced apart from one another and disposed upstream from the pilot outlet, the main fuel circuit including an annular plenum surrounding the pilot inlet portion of the pilot fuel circuit.

14. The combustor of claim 13 , wherein the main fuel circuit includes in a serial flow order a main inlet portion extending from the main inlet and having a first branch and a second branch, the annular plenum fluidly coupled to the first branch and the second branch of the main inlet portion, and a plurality of circumferentially spaced passages each exte

Assignees

• Gen Electric

Inventors

• Morgan Dana
• Stoia Lucas John
• Exley Elizabeth Leigh
• Bobba Mohan Krishna
• Mane Netaji Haribhau
• Pourcho John Bryan

Classifications

• F23R3/343 Primary

  Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion (ignition in gas-turbine plants F02C7/264; pilot flame igniters F23Q9/00) · CPC title

• F02C7/24

  Heat or noise insulation (air intakes having provisions for noise suppression F02C7/045; turbine exhaust heads, chambers, or the like F01D25/30; silencing nozzles of jet-propulsion plants F02K1/00) · CPC title

• F05D2260/231

  Preventing heat transfer · CPC title

• F23C1/08

  liquid and gaseous fuel · CPC title

• F23D11/38

  Nozzles; Cleaning devices therefor · CPC title