Combustion turbine engine combustor basket igniter port alignment verification tool and method for validating igniter alignment

Patent metadata

Field	Value
Publication number	US-9651261-B2
Application number	US-201414314109-A
Country	US
Kind code	B2
Filing date	Jun 25, 2014
Priority date	Jun 25, 2014
Publication date	May 16, 2017
Grant date	May 16, 2017

Abstract

A combustion turbine engine combustor igniter port alignment and dimensional verification tool is insertable in guide tube and igniter boss portions of the igniter port. The tool has concentrically nested outer and inner sleeves, having respective circumferential profiles that are separately slidably insertable within corresponding igniter port guide tube and igniter boss portions that have inner circumferential profiles in conformance with minimal dimension specifications. Concentric alignment of the guide tube and igniter boss is validated by inserting the nested outer and inner sleeves into the igniter port. The verification tool is capable of validating igniter port alignment and dimensions before the combustor is installed in a combustion turbine engine.

First claim

What is claimed is:

1. An igniter port alignment verification tool for a combustion turbine combustor basket of the type having:
outer and inner combustor shrouds nested along a combustor centerline axis;
an igniter port coupled to the inner and outer combustor shrouds at a port angle defined by an igniter port centerline axis and the combustor centerline axis, the igniter port including a tubular guide tube and a tubular igniter boss that are concentrically aligned along the igniter port centerline axis;
the guide tube having a proximal guide tube axial end that is coupled to and outwardly projects from the outer shroud, a guide tube axial length, and a guide tube inner circumferential profile having a first minimum dimension specification;
the igniter boss having a proximal boss axial end that is coupled to and projecting outwardly from the inner shroud, a distal boss axial end proximal the guide tube proximal end, an igniter boss axial length, and an igniter boss inner circumferential profile having a second minimum dimension specification;

said igniter alignment tool comprising:
an outer sleeve, having a first distal end defining a first outer circumferential profile that is adapted for slidable insertion into a first minimum dimension guide tube inner circumferential profile, the outer sleeve first circumferential profile continuous at least along its axial length that corresponds to the axial length of the guide tube; and
an inner sleeve, having a second distal end defining a second outer circumferential profile that is adapted for slidable insertion into a second minimum dimension igniter boss inner circumferential profile;

the inner sleeve slidably retained in nested concentric alignment within the outer sleeve, with the combined nested sleeves slidably insertable within concentrically aligned guide tube and igniter boss respective first and second inner circumferential profiles.

2. The tool of claim 1 , the outer sleeve first distal end angled for circumferential abutment proximal a corresponding distal boss axial end of an igniter boss when said outer sleeve is inserted into a guide tube having an inner circumferential profile meeting the first minimum dimension specification.

3. The tool of claim 1 , the outer sleeve first distal end angled for circumferential abutment proximal a corresponding distal boss axial end of an igniter boss when said outer sleeve is inserted into a guide tube having an inner circumferential profile meeting the first minimum dimension specification.

4. The tool of claim 1 , further comprising a protractor contacting the inner and/or outer sleeve, for measuring the port angle.

5. The tool of claim 4 , the inner and/or outer sleeve having a flat surface for contacting the protractor.

6. The tool of claim 5 , the protractor comprising an electronic protractor.

7. An igniter port alignment verification tool for a combustion turbine combustor basket of the type having:
outer and inner combustor shrouds nested along a combustor centerline axis;
an igniter port coupled to the inner and outer combustor shrouds at a port angle defined by an igniter port centerline axis and the combustor centerline axis, the igniter port including a tubular guide tube and a tubular igniter boss that are concentrically aligned along the igniter port centerline axis;
the guide tube having a proximal guide tube axial end that is coupled to and outwardly projects from the outer shroud, a guide tube axial length, and a guide tube inner circumferential profile having a first minimum dimension specification;
the igniter boss having a proximal boss axial end that is coupled to and projecting outwardly from the inner shroud, a distal boss axial end proximal the guide tube proximal end, an igniter boss axial length, and an igniter boss inner circumferential profile having a second minimum dimension specification;

said igniter alignment tool comprising:
an outer sleeve, having a first distal end defining a first outer circumferential profile that is adapted for slidable insertion into a first minimum dimension guide tube inner circumferential profile; and
an inner sleeve, having a second distal end defining a second outer circumferential profile that is adapted for slidable insertion into a second minimum dimension igniter boss inner circumferential profile, the inner sleeve second circumferential profile continuous at least along its axial length that corresponds to the axial length of the igniter boss;

the inner sleeve slidably retained in nested concentric alignment within the outer sleeve, with the combined nested sleeves slidably insertable within concentrically aligned guide tube and igniter boss respective first and second inner circumferential profiles.

8. A method for validating igniter port alignment and/or inner circumferential profile minimal dimension specification conformity for a combustion turbine combustor basket of the type having:
outer and inner combustor shrouds nested along a combustor centerline axis;
the igniter port coupled to the inner and outer combustor shrouds at a port angle defined by an igniter port centerline axis and the combustor centerline axis, the igniter port including a tubular guide tube and a tubular igniter boss that are concentrically aligned along the igniter port centerline axis;
the guide tube having a proximal guide tube axial end that is coupled to and outwardly projects from the outer shroud and a guide tube inner circumferential profile having a first minimum dimension specification;
the igniter boss having a proximal boss axial end that is coupled to and projecting outwardly from the inner shroud, a distal boss axial end proximal the guide tube proximal end and an igniter boss inner circumferential profile having a second minimum dimension specification;

said method comprising:
providing an alignment tool including an outer sleeve, having a first distal end defining a first outer circumferential profile that is adapted for slidable insertion into a first minimum dimension guide tube inner circumferential profile; and an inner sleeve, having a second distal end defining a second outer circumferential profile that is adapted for slidable insertion into a second minimum dimension igniter boss inner circumferential profile; the inner sleeve slidably retained in nested concentric alignment within the outer sleeve;
inserting the outer sleeve first distal end into the guide tube, validating guide tube conformity with the first minimum dimension specification if said first distal end passes through said guide tube; and/or
inserting the inner sleeve second distal end into the igniter boss, validating igniter boss conformity with the second minimum dimension specification if said second distal end passes through said igniter boss; and/or
inserting the combined nested sleeves into the igniter port, validating alignment of the guide tube and igniter boss if the respective inner and outer sleeves are received in their corresponding respective guide tube and igniter boss.

9. The method of claim 8 , comprising performing all three insertions of the outer and inner sleeve respective distal ends and the nested sleeves into the igniter port.

10. The method of claim 9 performed on a combustor basket prior to its installation within a combustion turbine.

11. The method of claim 10 , further comprising conforming either or both of the guide tube inner circumferential profile to the first minimum dimension specification or the igniter boss inner circumferential profile to the second minimum dimension specification.

12. The method of claim 10 , further comprising concentrically aligning the ignite

Assignees

• Siemens Energy Inc

Inventors

• Sullivan Peter C
• Olejarski Michael J

Classifications

• F23R3/60 Primary

  Support structures; Attaching or mounting means · CPC title

• B33Y50/02

  for controlling or regulating additive manufacturing processes · CPC title

• F23R2900/00017

  Assembling combustion chamber liners or subparts · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title

• B29C67/0088

  Operations & Transport · mapped topic