Igniter for a gas turbine

Patent metadata

Field	Value
Publication number	US-9739204-B2
Application number	US-201313890368-A
Country	US
Kind code	B2
Filing date	May 9, 2013
Priority date	May 9, 2013
Publication date	Aug 22, 2017
Grant date	Aug 22, 2017

Abstract

A gas turbine igniter includes an igniter rod disposed within a guide tube configured for travel between a hot-end region and a cold-end region and a cap connected to the guide tube, the cap defining an access passageway for the igniter rod. An attachment structure is provided for reducing the moment loading at the cold end of the igniter rod. The attachment structure has threaded outer surface configured to engage in a threaded connection with a threaded inner surface of the cap in an end portion of the cap that is proximate to the cold-end region, whereby the attachment structure is attachable to the end portion of the cap via the threaded connection. An inner surface of the attachment structure forms a guide surface for the igniter rod, at a reduced radial clearance with the igniter rod in comparison to the cap, proximate to the cold-end region.

First claim

The invention claimed is:

1. A gas turbine igniter, comprising:
an igniter rod configured for travel between a hot-end region and a cold-end region within a guide tube,
a cap connected to the guide tube, the cap defining an access passageway for the igniter rod,
a bushing attachable to an end portion of the cap that is proximate to the cold-end region, the bushing having an inner surface and an outer surface,
wherein an outer surface of the bushing is threaded to engage with a threaded inner surface of the cap in said end portion of the cap,
wherein a bearing is attached to the inner surface of the bushing, and
wherein the inner surface of the bearing defines a guided path for the igniter rod within the cap proximate to the cold-end region.

2. The gas turbine igniter according to claim 1 , wherein the bushing is formed as split bushing having first and second bushing parts, and the bearing is formed as a split bearing having first and second bearing parts that are respectively attached to the inner surfaces of the first and second busing parts.

3. The gas turbine igniter according to claim 1 , wherein the bearing is formed from bronze.

4. The gas turbine igniter according to claim 1 , wherein the bearing is glued to the inner surface of the bushing.

5. A retrofit structure for a gas turbine igniter, the igniter comprising an igniter rod disposed within a guide tube and configured for travel between a hot-end region and a cold-end region, and a cap connected to the guide tube, the cap defining an access passageway for the igniter rod, the retrofit structure comprising:
a bushing comprising a threaded outer surface configured to engage in a threaded connection with a threaded inner surface of the cap in an end portion of the cap that is proximate to the cold-end region, such that the retrofit structure is attachable to said end portion of the cap via said threaded connection, and
a bearing attached to an inner surface of the bushing, the bearing comprising an inner surface forming a guide surface for the igniter rod, at a reduced radial clearance with the igniter rod in comparison to the cap, proximate to the cold-end region.

6. The retrofit structure according to claim 5 , wherein the bushing is formed as split bushing having first and second bushing parts, and the bearing is formed as a split bearing having first and second bearing parts that are respectively attached to the inner surfaces of the first and second busing parts.

7. The retrofit structure according to claim 6 , wherein the bearing is formed of bronze.

8. A retrofit method for reducing moment loading at a cold-end of a gas turbine igniter, the igniter comprising an igniter rod disposed within a guide tube and configured for travel between a hot-end region and a cold-end region, and a cap connected to the guide tube, the cap defining an access passageway for the igniter rod, the retrofit method comprising:
forming an internal threading on an inner surface of the cap at an end portion of the cap that is proximate to the cold-end region, and
attaching the retrofit structure of claim 5 to the end portion of the cap that is proximate to the cold-end region via a threaded connection between the threaded outer surface of the retrofit structure and the threaded inner surface of the cap,
wherein the inner surface of the retrofit structure forms a guide surface for the igniter rod, at a reduced radial clearance with the igniter rod in comparison to the cap, proximate to the cold-end region.

9. The method according to claim 8 , further comprising a machining operation to increase an inner diameter of the cap prior to forming the internal threading.

Assignees

• Bird Derek A
• Siemens Energy Inc

Inventors

• Bird Derek A

Classifications

• F02C7/266 Primary

  Electric (sparking plugs H01T) · CPC title

• F05D2260/941

  particularly aimed at mechanical or thermal stress reduction · CPC title

• Y10T29/49716

  Converting · CPC title

• F05D2260/99

  Ignition, e.g. ignition by warming up of fuel or oxidizer in a resonant acoustic cavity · CPC title