Fuel nozzle with discrete jet inner air swirler

Patent metadata

Field	Value
Publication number	US-9284933-B2
Application number	US-201313782969-A
Country	US
Kind code	B2
Filing date	Mar 1, 2013
Priority date	Mar 1, 2013
Publication date	Mar 15, 2016
Grant date	Mar 15, 2016

Abstract

A fuel nozzle includes an axial fuel circuit having a converging front surface with an axial fuel outlet formed therein, an air swirler surrounding the axial fuel circuit and having a converging front wall, a swirl chamber bounded by the converging front surface of the axial fuel circuit and the converging front wall of the air swirler, and an air cap surrounding the air swirler, such that an air circuit is defined between the air cap and the air swirler. A plurality of circumferentially disposed discrete jet passages extend through the converging front wall of the air swirler for directing atomizing air from the air circuit to the swirl chamber.

First claim

What is claimed is:

1. A fuel nozzle comprising:
a) an axial fuel circuit having a converging front surface with an axial fuel outlet formed therein;
b) an air swirler surrounding the axial fuel circuit and having a converging front wall;
c) a swirl chamber bounded by the converging front surface of the axial fuel circuit and the converging front wall of the air swirler;
d) an air cap surrounding the air swirler, such that an air circuit is defined between the air cap and the air swirler, wherein circumferentially spaced apart axial air vanes are arranged within the air circuit; and
e) a plurality of circumferentially disposed discrete jet passages extending through the converging front wall of the air swirler for directing atomizing air from the air circuit to the swirl chamber.

2. A fuel nozzle as recited in claim 1 , wherein the converging front wall of the air swirler defines a converging circumferential inner surface that forms a boundary of the swirl chamber.

3. A fuel nozzle as recited in claim 1 , wherein the converging front wall of the air swirler defines a diverging circumferential inner surface that forms a boundary of the swirl chamber.

4. A fuel nozzle as recited in claim 1 , wherein the converging front wall of the air swirler defines an axial circumferential inner surface that forms a boundary of the swirl chamber.

5. A fuel nozzle as recited in claim 1 , wherein the discrete jet passages are disposed between the axial air vanes.

6. A fuel nozzle as recited in claim 1 , wherein the air cap is a converging air cap.

7. A fuel nozzle comprising:
a) an axial fuel circuit having a converging front surface with an axial fuel outlet formed therein;
b) an inner air swirler surrounding the axial fuel circuit and having a converging front wall;
c) a swirl chamber bounded by the converging front surface of the axial fuel circuit and the converging front wall of the inner air swirler;
d) an outer air swirler surrounding the inner air swirler, such that an inner air circuit is defined between the inner and outer air swirlers;
e) an air cap surrounding the outer air swirler, such that an outer air circuit is defined between the outer air swirler and the air cap; and
f) a plurality of circumferentially spaced apart discrete jet passages extending through the converging front wall of the inner air swirler for directing inner atomizing air from the inner air circuit to the swirl chamber.

8. A fuel nozzle as recited in claim 7 , wherein the converging front wall of the inner air swirler defines a converging circumferential inner surface that forms a boundary of the swirl chamber.

9. A fuel nozzle as recited in claim 7 , wherein the converging front wall of the inner air swirler defines a diverging circumferential inner surface that forms a boundary of the swirl chamber.

10. A fuel nozzle as recited in claim 7 , wherein the converging front wall of the air swirler defines an axial circumferential inner surface that forms a boundary of the swirl chamber.

11. A fuel nozzle as recited in claim 7 , wherein a plurality of circumferentially spaced apart axial air vanes are arranged within the inner air circuit.

12. A fuel nozzle as recited in claim 11 , wherein the discrete jet passages are disposed between the axial air vanes.

13. A fuel nozzle as recited in claim 7 , wherein a plurality of circumferentially spaced apart axial air vanes are arranged within the outer air circuit.

14. A fuel nozzle as recited in claim 7 , wherein the outer air swirler is a converging outer air swirler.

15. A fuel nozzle as recited in claim 7 , wherein the air cap is a converging air cap.

16. A fuel nozzle comprising:
a) an axial fuel circuit having a converging front surface with an axial fuel outlet formed therein;
b) an air swirler surrounding the axial fuel circuit and having a converging front wall that defines a converging circumferential inner surface;
c) a swirl chamber bounded by the converging front surface of the axial fuel circuit and the converging circumferential inner surface of the converging front wall of the air swirler;
d) a converging air cap surrounding the air swirler, such that an air circuit is defined between the air cap and the air swirler for directing outer wiping air through the fuel nozzle, wherein circumferentially spaced apart axial air vanes are arranged within the air circuit; and
e) a plurality of circumferentially spaced apart discrete jet passages extending through the converging front wall of the air swirler for directing atomizing air from the air circuit to the swirl chamber.

17. A fuel nozzle as recited in claim 16 , wherein the discrete jet passages are disposed between the axial air vanes.

Assignees

• Delavan Inc

Inventors

• Myers Steven Jay

Classifications

• F23D11/386

  Nozzle cleaning · CPC title

• F23R3/14 Primary

  by using swirl vanes · CPC title

• F23D2900/00002

  Cleaning burner parts, e.g. burner tips · CPC title

• F02M61/162 Primary

  Means to impart a whirling motion to fuel upstream or near discharging orifices · CPC title

• F23D11/105

  at least one of the fluids being submitted to a swirling motion · CPC title