Inverted cap igniter tube

Patent metadata

Field	Value
Publication number	US-9394830-B2
Application number	US-201314134024-A
Country	US
Kind code	B2
Filing date	Dec 19, 2013
Priority date	Mar 14, 2013
Publication date	Jul 19, 2016
Grant date	Jul 19, 2016

Abstract

An igniter tube assembly includes an igniter, an igniter tower with a radially extending portion, a ferrule with a radially extending portion, and a retainer with a radially extending portion. The ferrule and retainer capture the radially extending portion of the igniter tower and sealing surface provides an area for the ferrule to interface with the igniter tower. The igniter moves relative to the casing in which it is secured while a fluid seal between the igniter and ferrule controls air flow.

First claim

What is claimed is:

1. An igniter tube assembly comprising:
an igniter;
an igniter tower with a radially extending portion;
a ferrule with a radially extending portion; and
a retainer with a radially extending portion,
wherein the radially extending portion of the igniter tower is disposed between the radially extending portion of the retainer and the radially extending portion of the ferrule; and
wherein the igniter tower is formed of a first material and the ferrule is formed of a second material, and wherein the first material is a different material from the second material.

2. The igniter tube assembly as claimed in claim 1 , wherein the ferrule is secured to the retainer, the ferrule and retainer collectively retain the radially extending portion of the igniter tower.

3. The igniter tube assembly as claimed in claim 1 , wherein the ferrule is secured to the retainer by a weld.

4. The igniter tube assembly as claimed in claim 1 , wherein the igniter tower includes apertures for providing cooling air to the igniter.

5. The igniter tube assembly as claimed in claim 1 , further comprising a combustor wall, the igniter tower is secured to the combustor wall.

6. The igniter tube assembly as claimed in claim 1 , wherein the ferrule has a z-shaped configuration.

7. The igniter tube assembly as claimed in claim 1 , wherein the ferrule provides a seal about the igniter, thereby minimizing air flow between the ferrule and the igniter tower, while allowing relative movement between the igniter and a combustor wall.

8. The igniter tube assembly as claimed in claim 1 , wherein the second material is more resistant to friction-induced wear than the first material.

9. The igniter tube assembly as claimed in claim 1 , wherein the radially extending portion of the ferrule has an inner radius and an outer radius, each radius has a portion extending therefrom that includes a first longitudinal portion extending from the inner radius.

10. The igniter tube assembly as claimed in claim 9 , wherein the ferrule has a second longitudinal portion, and wherein the second longitudinal portion extends from the outer radius of the ferrule.

11. The igniter tube assembly as claimed in claim 10 , wherein the ferrule has a first face and a second face, and wherein the first longitudinal portion extends from the first face and the second longitudinal portion extends from the second face of the ferrule.

12. The igniter tube assembly as claimed in claim 1 , wherein the radial extending portion of the retainer has an inner radius and an outer radius, an annular portion extends from the outer radius of the retainer.

13. The igniter tube assembly as claimed in claim 1 , further comprising a seal positioned between the ferrule and the igniter.

14. An igniter tube assembly comprising:
an igniter tower with a radially extending portion;
a ferrule with a radially extending portion; and
a retainer with a radially extending portion;
wherein the radially extending portion of the igniter tower is disposed between the radially extending portion of the retainer and the radially extending portion of the ferrule; and
wherein the igniter tower is formed of a first material and the ferrule is formed of a second material, and wherein the first material is a different material from the second material.

15. The igniter tube assembly as claimed in claim 14 , wherein the ferrule is secured to the retainer and retains the radially extending portion of the igniter tower between the radially extending portion of the ferrule and the radially extending portion of the retainer.

16. The igniter tube assembly as claimed in claim 14 , further comprising an igniter.

17. The igniter tube assembly as claimed in claim 14 , further comprising a combustor shell, the igniter tower is secured to the combustor shell.

18. The igniter tube assembly as claimed in claim 14 , further comprising a combustor casing.

19. The igniter tube assembly as claimed in claim 14 , wherein the second material is more resistant to friction-induced wear than the first material.

20. A gas turbine engine having an igniter tube assembly, the igniter tube assembly comprising:
an igniter;
an igniter tower with an extended portion;
a ferrule with an extended portion; and
a retainer positioned below the ferrule, the retainer having an extended portion;
wherein the extended portion of the igniter tower is located between the extended portion of the retainer and the extended portion of the ferrule; and
wherein the igniter tower is formed of a first material and the ferrule is formed of a second material, and wherein the first material is a different material from the second material.

21. The gas turbine engine as claimed in claim 20 , wherein the second material is more resistant to friction-induced wear than the first material.

Assignees

• Rolls Royce Corp

Inventors

• Mccormick Kelly J

Classifications

• F02C7/264 Primary

  Ignition · CPC title

• F23R3/002 Primary

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title

• F23R3/60

  Support structures; Attaching or mounting means · CPC title

• F23D2207/00

  Ignition devices associated with burner · CPC title

• F23R2900/00012

  Details of sealing devices · CPC title