Method for reconditioning fuel nozzle assemblies

Patent metadata

Field	Value
Publication number	US-10364982-B2
Application number	US-201615354030-A
Country	US
Kind code	B2
Filing date	Nov 17, 2016
Priority date	Nov 19, 2015
Publication date	Jul 30, 2019
Grant date	Jul 30, 2019

Abstract

A method of reconditioning and fabricating turbine components is provided. In one embodiment, the method is performed on a fuel nozzle assembly of a gas turbine, and comprises providing a pre-assembled fuel nozzle assembly having a base, a body extending from the base to a fuel nozzle tip, an inner assembly, and an outer assembly. The method further comprises removing at least a portion of the fuel nozzle tip and the inner assembly, coupling and joining a replacement inner assembly to the base, and coupling and joining a replacement fuel nozzle tip to the replacement inner assembly and to the outer assembly to provide a reconditioned fuel nozzle.

First claim

We claim:

1. A method for reconditioning fuel nozzle assemblies, the method comprising:
providing a fuel nozzle assembly comprising:
a base; and
a body extending from the base to a fuel nozzle tip, the body comprising an inner channel defined at least partially by an inner channel wall and an outer channel defined at least partially by an outer channel wall, the inner channel wall and the outer channel wall each brazed to the base,
wherein the fuel nozzle tip comprises an end cover that is brazed to the inner channel wall and coupled to the outer channel wall;
decoupling at least a portion of the fuel nozzle tip from the inner channel wall and the outer channel wall;
removing material from the base to provide an access opening to the inner channel through the base;
decoupling at least a portion of the inner channel wall from the base via the access opening;
removing the decoupled portion of the inner channel wall from the body;
providing a replacement inner channel wall that is welded to a replacement fuel nozzle tip;
welding the replacement inner channel wall to the base through the access opening;
sealing the access opening after welding the replacement inner channel wall to the base; and
coupling the replacement fuel nozzle tip to the outer channel wall.

2. The method of claim 1 , wherein the replacement fuel nozzle tip further comprises an insert and a replacement end cover that are beam welded to each other.

3. The method of claim 2 , further comprising beam welding the insert to a cavity wall of the replacement end cover.

4. The method of claim 3 , wherein the insert further comprises a shoulder extending from an outer surface of the insert, and wherein the shoulder is beam welded to the cavity wall of the replacement end cover.

5. The method of claim 2 , further comprising beam welding a distal end of the replacement inner channel wall to the insert and beam welding a distal end of the outer channel wall to the replacement end cover.

6. The method of claim 5 , wherein the distal end of the inner channel wall is offset axially from the distal end of the outer channel wall.

7. The method of claim 1 , wherein removing material from the base results in a portion of the inner channel wall remaining coupled to the base after the decoupled portion of the inner channel wall is removed from the body.

Assignees

• Ansaldo Energia Switzerland AG

Inventors

• Marchal Darius N
• McGhee Michael

Classifications

• F23R2900/00016

  Retrofitting in general, e.g. to respect new regulations on pollution · CPC title

• F23R3/286

  having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title

• B23P2700/13

  Parts of turbine combustion chambers · CPC title

• B23P6/005

  using only replacement pieces of a particular form · CPC title

• B23K26/282

  of tube sections · CPC title