Swirler-ferrule assembly

Patent metadata

Field	Value
Publication number	US-2025035304-A1
Application number	US-202418913347-A
Country	US
Kind code	A1
Filing date	Oct 11, 2024
Priority date	Jun 24, 2021
Publication date	Jan 30, 2025
Grant date	—

Abstract

A swirler-ferrule assembly includes a radial swirler, a ferrule, a fuel nozzle, and a surface feature. The radial swirler includes a primary swirler vane having a primary air passage and a secondary swirler vane having a secondary air passage. The ferrule may be connected to the radial swirler. The surface feature may be located on the primary swirler vane and/or the ferrule. The surface feature may be configured to direct an air flow through the primary air passage away from a recirculation zone located upstream of the primary swirler vane. The surface feature has a trailing end and a distal end, and the fuel nozzle is axially aligned with the trailing end of the surface feature or is located axially downstream of the trailing end of the surface feature. The surface feature may have a plurality of grooves.

First claim

1 . A swirler-ferrule assembly comprising:
a radial swirler including:
(a) a primary swirler vane having a forward wall, an aft wall, and a primary air passage defined between the forward wall and the aft wall, wherein the forward wall defines a surface feature; and
(b) a secondary swirler vane having a secondary air passage;
a fuel nozzle configured to deliver fuel to a combustor; a ferrule connected to the radial swirler, the ferrule configured to center the fuel nozzle in the radial swirler; and the surface feature having a trailing end and a distal end and configured to direct an air flow through the primary air passage away from a recirculation zone located upstream of the primary swirler vane, wherein the fuel nozzle is located axially downstream of the trailing end of the surface feature.

2 . The swirler-ferrule assembly of claim 1 , wherein the surface feature is a ramp that is curved radially inward in an aft direction and axially in the aft direction from the trailing end of the surface feature to the distal end.

3 . The swirler-ferrule assembly of claim 2 , wherein the ferrule comprises a plurality of purge-air passages, each of the plurality of purge-air passages configured to intersect the surface feature between the trailing end and the distal end.

4 . The swirler-ferrule assembly of claim 2 , wherein the aft wall further comprises a lip having a venturi surface, the lip extending between the primary air passage and the secondary air passage, wherein the surface feature is configured to guide the air flow through the primary air passage toward the venturi surface.

5 . The swirler-ferrule assembly of claim 1 , wherein the surface feature is a ramp that is curved radially inward in a forward direction and axially in the forward direction from the trailing end to an intermediate point of the surface feature and is curved radially inward in an aft direction and axially in the aft direction from the intermediate point to the distal end.

6 . The swirler-ferrule assembly of claim 5 , wherein the ferrule comprises a plurality of purge-air passages, each of the plurality of purge-air passages configured to intersect the surface feature between the trailing end and the distal end.

7 . The swirler-ferrule assembly of claim 5 , wherein the intermediate point is axially forward of the trailing end and the distal end is axially aft of the intermediate point and axially forward of the trailing end.

8 . The swirler-ferrule assembly of claim 5 , wherein the aft wall further comprises a lip having a venturi surface, the lip extending between the primary air passage and the secondary air passage, wherein the surface feature is configured to guide the air flow through the primary air passage toward the venturi surface.

9 . The swirler-ferrule assembly of claim 1 , wherein the surface feature is a first lip, the first lip extending within the primary swirler vane and being curved radially inward in an aft direction and axially in the aft direction from the trailing end of the surface feature to the distal end of the surface feature, and wherein the primary swirler vane includes a ramp surface.

10 . The swirler-ferrule assembly of claim 9 , further comprising a second lip having a venturi surface, the second lip extending between the primary swirler vane and the secondary swirler vane, wherein the first lip divides the air flow through the primary swirler vane into a first air flow guided along the ramp surface of the primary swirler vane and a second air flow guided along the venturi surface.

11 . The swirler-ferrule assembly of claim 1 , wherein the surface feature is integral with the forward wall.

12 . The swirler-ferrule assembly of claim 1 , wherein the fuel nozzle is located axially downstream of the distal end of the surface feature.

13 . The swirler-ferrule assembly of claim 1 , wherein the fuel nozzle is located axially upstream of the distal end of the surface feature.

14 . The swirler-ferrule assembly of claim 1 , wherein the aft wall further comprises a lip having a venturi surface, the lip extending between the primary air passage and the secondary air passage, wherein the surface feature is configured to guide the air flow through the primary air passage toward the venturi surface.

15 . A swirler-ferrule assembly comprising:
a radial swirler including:
(a) a primary swirler vane having a forward wall, an aft wall, and a primary air passage defined between the forward wall and the aft wall, wherein the forward wall defines a surface feature; and
(b) a secondary swirler vane having a secondary air passage;
a fuel nozzle configured to deliver fuel to a combustor; a ferrule connected to the radial swirler, the ferrule configured to center the fuel nozzle in the radial swirler; and the surface feature having a trailing end and a distal end and configured to direct an air flow through the primary air passage away from a recirculation zone located upstream of the primary swirler vane, wherein the aft wall comprises a lip having a venturi surface, the lip extending between the primary air passage and the secondary air passage, wherein the surface feature is configured to guide the air flow through the primary air passage toward the venturi surface, and wherein the fuel nozzle is located axially downstream of the trailing end of the surface feature, and the fuel nozzle is located axially downstream of the distal end of the surface feature or axially upstream of the distal end of the surface feature.

16 . The swirler-ferrule assembly of claim 15 , wherein the surface feature is a ramp that is curved radially inward in an aft direction and axially in the aft direction from the trailing end of the surface feature to the distal end.

17 . The swirler-ferrule assembly of claim 15 , wherein the surface feature is a ramp that is curved radially inward in a forward direction and axially in the forward direction from the trailing end to an intermediate point of the surface feature and is curved radially inward in an aft direction and axially in the aft direction from the intermediate point to the distal end.

18 . The swirler-ferrule assembly of claim 17 , wherein the intermediate point is axially forward of the trailing end and the distal end is axially aft of the intermediate point and axially forward of the trailing end.

19 . The swirler-ferrule assembly of claim 15 , wherein the surface feature is a first lip and the lip having the venturi surface is a second lip, the first lip extending within the primary swirler vane and being curved radially inward in an aft direction and axially in the aft direction from the trailing end of the surface feature to the distal end of the surface feature, and wherein the primary swirler vane includes a ramp surface.

20 . The swirler-ferrule assembly of claim 15 , wherein the surface feature is integral with the forward wall.

Assignees

• Gen Electric

Inventors

• Vise Steven C
• Cooper Clayton S
• Benjamin Michael A
• Naik Pradeep
• Kim Kwanwoo
• Birmaher Shai
• Vukanti Perumallu
• Singh Saket
• Sampath Karthikeyan

Classifications

• B05B7/10

  producing a swirling discharge · CPC title

• B05B1/3421

  with channels emerging substantially tangentially in the swirl chamber · CPC title

• B05B15/555

  discharged by cleaning nozzles · CPC title

• B05B7/066

  with an inner liquid outlet surrounded by at least one annular gas outlet · CPC title

• B05B7/0458

  the gas and liquid flows being perpendicular just upstream the mixing chamber · CPC title