Internally-mounted torch igniters with removable igniter heads

Patent metadata

Field	Value
Publication number	US-11680528-B2
Application number	US-202017127236-A
Country	US
Kind code	B2
Filing date	Dec 18, 2020
Priority date	Dec 18, 2020
Publication date	Jun 20, 2023
Grant date	Jun 20, 2023

Abstract

A torch igniter for a combustor of a gas turbine engine includes an igniter body and an igniter head. The igniter body is disposed within a high-pressure case of a gas turbine engine and extends primarily along a first axis, and includes an annular wall and an outlet wall. The annular wall surrounds the first axis and defines a radial extent of a combustion chamber therewithin. The outlet wall is disposed at a downstream end of the annular wall, defines a downstream extent of the combustion chamber, and includes an outlet fluidly communicating between the combustion chamber and an interior of the combustor. The igniter head is removably attached to the igniter body at an upstream end of the annular wall, wherein the igniter head defines an upstream extent of the combustion chamber, and includes an ignition source and a fuel injector.

First claim

The invention claimed is:

1. A torch igniter for a combustor of a gas turbine engine, the torch igniter comprising:
an igniter body disposed within a high-pressure case of the gas turbine engine and extending primarily along a first axis, the igniter body comprising:
an annular wall surrounding the first axis and defining a radial extent of a combustion chamber therewithin; and
an outlet wall disposed at a downstream end of the annular wall, and defining a downstream extent of the combustion chamber, the outlet wall including an outlet fluidly communicating between the combustion chamber and an interior of the combustor;

an igniter head removably attached to the igniter body at an upstream end of the annular wall, wherein the igniter head defines an upstream extent of the combustion chamber, and comprises:
an ignition source extending at least partially into the combustion chamber; and
a fuel injector configured to inject fuel into the combustion chamber with an orientation impinging on the ignition source
wherein the igniter head extends through the high-pressure case and at least partially outside of the high-pressure case.

2. The torch igniter of claim 1 , wherein the igniter head further comprises a cap defining the upstream extent of the combustion chamber.

3. The torch igniter of claim 1 , further comprising an aperture in a wall of the high-pressure case through which the igniter head extends.

4. The torch igniter of claim 3 , further comprising a flange extending from an exterior of the annular wall, wherein the flange is configured to create a seal with an inner surface of the high-pressure case and the seal is configured to prevent air flow through the aperture.

5. The torch igniter of claim 4 , wherein a pressure of air of the high-pressure case presses the flange against the inner surface of the high-pressure case to create the seal.

6. The torch igniter of claim 4 , wherein the flange extends transverse to the axis.

7. The torch igniter of claim 4 , further comprising a second flange extending from an exterior of the igniter head, wherein the second flange is configured to create a second seal with an outer surface of the high pressure case and the second seal is configured to prevent flow out of the high-pressure case.

8. The torch igniter of claim 7 , wherein the second seal is formed by a sealing structure disposed in a groove of the second flange adjacent to the exterior of the outer surface of the high-pressure case.

9. The torch igniter of claim 7 , wherein the second flange extends transverse to the axis.

10. The torch igniter of claim 1 , further comprising a first cooling air passage formed within the annular wall, wherein the first cooling air passage surrounds the combustion chamber and is configured to cool an interior surface of the annular wall.

11. The torch igniter of claim 10 , further comprising a second cooling air passage formed within the igniter head, wherein the second cooling air passage is directly fluidly connected to the first cooling air passage.

12. The torch igniter of claim 11 , further comprising an air inlet disposed in the igniter head and directly fluidly connected to the second cooling air passage, wherein:
the air inlet is configured to intake a flow of air from a compressed air source, to flow a first portion of the flow of air to the fuel injector, and to flow a second portion of the flow of air to the second air cooling passage;
the fuel injector is configured to atomize an injected fuel with the first portion of the flow of air; and
the second cooling air passage is configured to channel the second portion of the flow of air to the first cooling air passage.

13. The torch igniter of claim 11 , further comprising an air inlet disposed in the igniter body and directly fluidly connected to the first cooling air passage, wherein:
the air inlet is configured to intake a flow of compressed air from inside the high-pressure case;
the first cooling air passage is configured to channel the flow of air to the second cooling air passage;
the second cooling air passage is configured to channel the flow of air to the fuel injector; and
the fuel injector is configured to atomize an injected fuel with the flow of air.

14. The torch igniter of claim 11 , further comprising:
an air inlet disposed in the igniter body and directly fluidly connected to the first cooling air passage; and
an aperture extending through the cap, wherein the aperture directly fluidly connects the second cooling air passage to the combustion chamber, wherein:
the first cooling air passage is configured to channel the flow of air to the second cooling air passage; and
the second cooling air passage is configured to channel the flow of air into the combustion chamber through the aperture.

15. The torch igniter of claim 1 , wherein the igniter head is removably attached by a screw attachment.

16. The torch igniter of claim 15 , wherein the screw attachment forms a seal between the igniter head and the igniter body.

17. The torch igniter of claim 1 , wherein at least one of the igniter head and the igniter body is formed as a single monolithic piece.

18. The torch igniter of claim 1 , wherein the igniter body further comprises a receiving structure disposed at the upstream extent of the combustion chamber and the receiving structure is configured to receive the igniter head.

19. The torch igniter of claim 18 , wherein the receiving structure is configured to create a seal between the igniter head and the igniter body.

20. A torch igniter for a combustor of a gas turbine engine, the torch igniter comprising:
an igniter body disposed within a high-pressure case of the gas turbine engine and extending primarily along a first axis, the igniter body comprising:
an annular wall surrounding the first axis and defining a radial extent of a combustion chamber therewithin; and
an outlet wall disposed at a downstream end of the annular wall, and defining a downstream extent of the combustion chamber, the outlet wall including an outlet fluidly communicating between the combustion chamber and an interior of the combustor;

an igniter head removably attached to the igniter body at an upstream end of the annular wall, wherein the igniter head defines an upstream extent of the combustion chamber, and comprises:
an ignition source extending at least partially into the combustion chamber; and
a fuel injector configured to inject fuel into the combustion chamber with an orientation impinging on the ignition source; and

a first cooling air passage formed within the annular wall, wherein the first cooling air passage surrounds the combustion chamber and is configured to cool an interior surface of the annular wall;
a second cooling air passage formed within the igniter head, wherein the second cooling air passage is directly fluidly connected to the first cooling air passage; and
an air inlet disposed in the igniter body and directly fluidly connected to the first cooling air passage, wherein:
the air inlet is configured to intake a flow of compressed air from inside the high-pressure case;
the first cooling air passage is configured to channel the flow of air to the second cooling air passage;
the second cooling air passage is configured to channel the flow of air to the fuel injector; and
the fuel injector is configured to atomize an injected fuel with the flow of air.

Assignees

• Delavan Inc

Inventors

• Ryon Jason
• Prociw Lev Alexander
• Myers Steve
• Tibbs Andy M
• Williams Brandon P

Classifications

• F05D2240/55

  Seals · CPC title

• F02C7/18

  the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title

• F23R2900/03044

  Impingement cooled combustion chamber walls or subassemblies · CPC title

• F05D2260/201

  by impingement of a fluid · CPC title

• F02C7/22

  Fuel supply systems · CPC title