IP Library › Granted Patent US 12,085,281
Granted Patent B2
US 12,085,281 · App. 18/350,205 · Granted Sep 10, 2024

Fuel nozzle and swirler

Inventors: Perumallu Vukanti (Bengaluru, IN); Pradeep Naik (Bengaluru, IN); Clayton S. Cooper (Evendale, OH); Michael A. Benjamin (Cincinnati, OH); Michael T. Bucaro (Arvada, CO); Manampathy G. Giridharan (Evendale, OH); Steven C. Vise (West Chester, OH); Ajoy Patra (Bengaluru, IN); Saket Singh (Bengaluru, IN); R Narasimha Chiranthan (Bengaluru, IN)
Assignee: General Electric Company
F23R3/14F23R3/286
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Quick Facts
Patent No.
US 12,085,281
App. No.
18/350,205
Granted
Sep 10, 2024
Kind
B2
Abstract

An engine can utilize a combustor to combust fuel to drive the engine. A fuel nozzle assembly can supply fuel to the combustor for combustion or ignition of the fuel. The fuel nozzle assembly can include a swirler and a fuel nozzle to supply a mixture of fuel and air for combustion, which can supply a primary fuel supply and a secondary fuel supply. Increasing efficiency and reducing emission require the use of alternative fuels, which combust at higher temperatures or burn at faster burn speeds than traditional fuels, requiring improved fuel introduction without the occurrence of flame holding or flashback.

Claims (32)

1. A fuel nozzle assembly comprising:

a fuel nozzle including an outer wall encasing a fuel passage and defining a longitudinal axis;

a swirler circumscribing the fuel nozzle defining a swirler air passage; and

a fuel nozzle wall passage provided within the outer wall and exhausting at a first outlet, and the fuel nozzle wall passage exhausting to the fuel passage at a second outlet.

2. The fuel nozzle assembly of claim 1 wherein the fuel nozzle wall passage circumscribes the fuel passage.

3. The fuel nozzle assembly of claim 1 wherein the first outlet exhausts to the swirler air passage.

4. The fuel nozzle assembly of claim 1 further comprising a splitter extending from the swirler.

5. The fuel nozzle assembly of claim 4 wherein the first outlet is positioned forward of the splitter relative to the longitudinal axis.

6. The fuel nozzle assembly of claim 1 wherein the first outlet is arranged tangentially, relative to the longitudinal axis, to impart a swirl to fuel exhausted from the first outlet.

7. A fuel nozzle assembly for a gas turbine engine, the fuel nozzle assembly comprising:

a fuel nozzle including an outer wall encasing a fuel passage and defining a longitudinal axis;

a cap provided in the fuel passage;

a swirler circumscribing the fuel nozzle defining a swirler air passage; and

a fuel nozzle wall passage provided within the outer wall and exhausting at a first outlet;

wherein the first outlet exhausts to the fuel passage aft of the cap relative to the longitudinal axis.

8. The fuel nozzle assembly of claim 7 wherein the swirler includes a splitter separating the swirler air passage into a radially inner passage and a radially outer passage, and wherein the first outlet exhausts to the radially inner passage.

9. The fuel nozzle assembly of claim 7 wherein the fuel nozzle wall passage circumscribes the fuel passage.

10. The fuel nozzle assembly of claim 7 further comprising a splitter extending from the swirler.

11. The fuel nozzle assembly of claim 7 wherein the fuel nozzle wall passage includes a second outlet exhausting to the swirler air passage.

12. The fuel nozzle assembly of claim 7 wherein the first outlet is arranged tangentially, relative to the longitudinal axis, to impart a swirl to fuel exhausted from the first outlet.

13. A fuel nozzle assembly comprising:

a fuel nozzle including an outer wall encasing a fuel passage and defining a longitudinal axis;

a swirler circumscribing the fuel nozzle defining a swirler air passage; and

a fuel nozzle wall passage provided within the outer wall and exhausting at a first outlet;

wherein the first outlet is arranged tangentially, relative to the longitudinal axis, to impart a swirl to fuel exhausted from the first outlet.

14. The fuel nozzle assembly of claim 13 wherein the fuel nozzle wall passage circumscribes the fuel passage.

15. The fuel nozzle assembly of claim 13 wherein the first outlet exhausts to the swirler air passage.

16. The fuel nozzle assembly of claim 13 further comprising a splitter extending from the swirler.

17. The fuel nozzle assembly of claim 16 wherein the first outlet is positioned forward of the splitter relative to the longitudinal axis.

18. The fuel nozzle assembly of claim 13 wherein the fuel nozzle wall passage includes a second outlet exhausting to the fuel passage.

19. The fuel nozzle assembly of claim 13 further comprising a cap provided in the fuel passage.

20. The fuel nozzle assembly of claim 19 wherein the first outlet is positioned aft of the cap.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 11, 2023
From: VUKANTI, PERUMALLU; NAIK, PRADEEP; COOPER, CLAYTON S.; BENJAMIN, MICHAEL A.; BUCARO, MICHAEL T.; GIRIDHARAN, MANAMPATHY G.; VISE, STEVEN C.; PATRA, AJOY; SINGH, SAKET; CHIRANTHAN, R. NARASIMHA
To: GENERAL ELECTRIC COMPANY
Reel/Frame 064213/0188 →
Priority Claims (1)
IN 202111059707 · Dec 21, 2021 · national
Continuity (2)
Continuation 17682373 · Feb 28, 2022
Related Publication 20230366551A1 · Nov 16, 2023
Cited By (1)
US 12,492,819