Combustor liner dilution opening

Patent metadata

Field	Value
Publication number	US-11268438-B2
Application number	US-201715705314-A
Country	US
Kind code	B2
Filing date	Sep 15, 2017
Priority date	Sep 15, 2017
Publication date	Mar 8, 2022
Grant date	Mar 8, 2022

Abstract

An apparatus and method for a combustor, the combustor including combustor liner having a plurality of dilution openings. The combustor receives a flow of fuel that is ignited and mixed with dilution air to form a flow of combustion gases. The flow of combustion gases travels through the combustor to a turbine section of an engine.

First claim

What is claimed is:

1. A combustor liner, the combustor liner comprising:
a wall having an outer surface and an inner surface and at least partially defining a combustion chamber about a longitudinal axis,
wherein the outer surface is radially outward of the inner surface relative to the longitudinal axis;
at least one dilution opening extending through the wall and defining an opening shape extending in an axial direction relative to the longitudinal axis; and
at least one backside device projection extending outward from the wall as one continuous piece along a portion of the opening shape and defining a projection wall extending out from the outer surface of the wall a wall height, and leaving a remaining portion of the opening shape free of the at least one backside device projection, to define at least a portion of a flow path that forms a dilution angle with the longitudinal axis;
wherein the projection wall includes a base connected at the outer surface, a tip opposite the base, and a first side positioned facing the dilution opening,
wherein the projection wall is configured to direct a flow of air into the dilution opening, wherein the base is disposed at a trailing edge of the dilution opening, and the projection wall is arranged such that the tip is disposed in an aft direction relative to the base, and
wherein a portion of the outer surface of the wall downstream of the trailing edge of the opening shape forms a backside angle with the first side of the projection wall along an entirety of the wall height that is an acute angle less than 90 degrees.

2. The combustor liner of claim 1 , wherein the opening shape is a keyhole shape.

3. The combustor liner of claim 1 , wherein the opening shape is an oval shape.

4. The combustor liner of claim 1 , wherein the opening shape is a tear drop shape.

5. The combustor liner of claim 1 , wherein the opening shape is a race track shape.

6. The combustor liner of claim 1 wherein the dilution angle is greater than or equal to 30 degrees.

7. The combustor liner of claim 2 , wherein the opening shape further comprises a leading edge and extends in the axial direction from the leading edge to the trailing edge.

8. The combustor liner of claim 7 , wherein the remaining portion of the dilution opening is located along the leading edge.

9. The combustor liner of claim 7 wherein the projection wall tapers from the trailing edge toward the leading edge such that the wall height at the leading edge is zero.

10. The combustor liner of claim 7 wherein the backside angle is equal to the dilution angle.

11. The combustor liner of claim 10 , wherein the dilution angle is greater than or equal to 30 degrees.

12. The combustor liner of claim 1 wherein the opening shape is one of an oval shape, tear drop shape, race track shape, or airfoil shape.

13. The combustor liner of claim 1 wherein the combustion chamber extends along the longitudinal axis from a dome assembly defining a dome height.

14. The combustor liner of claim 13 , wherein the flow path extends into the combustion chamber to a depth of at least 30% of the dome height.

15. The combustor liner of claim 13 , wherein the flow path extends into the combustion chamber to a depth of at least 70% of the dome height.

16. The combustor liner of claim 13 , wherein the flow path extends into the combustion chamber to a depth of 100% of the dome height.

Assignees

• Gen Electric

Inventors

• Vise Steven Clayton
• Danis Allen Michael
• Sekar Jayanth
• Naik Pradeep
• Vukanti Perumallu
• Johnson Arthur Wesley
• Cooper Clayton Stuart
• Sampath Karthikeyan

Classifications

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F23R3/06

  Arrangement of apertures along the flame tube · CPC title

• F23R3/16

  with devices inside the flame tube or the combustion chamber to influence the air or gas flow · CPC title

• F05D2270/082

  with as little NOx as possible · CPC title

• F05D2240/35

  Combustors or associated equipment · CPC title