Fuel nozzle and swirler

Patent metadata

Field	Value
Publication number	US-12085281-B2
Application number	US-202318350205-A
Country	US
Kind code	B2
Filing date	Jul 11, 2023
Priority date	Dec 21, 2021
Publication date	Sep 10, 2024
Grant date	Sep 10, 2024

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.

First claim

What is claimed is:

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.

Assignees

• Gen Electric

Inventors

• 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

Classifications

• F23R3/38

  comprising rotary fuel injection means · CPC title

• F23R3/28 Primary

  characterised by the fuel supply (burners F23D) · CPC title

• F23R3/286

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

• F23D2209/10

  Flame flashback · CPC title

• F23D14/82

  Preventing flashback or blowback · CPC title