IP Library Patent Application 16363220
Patent Application
App. No. 16/363,220

AFTERMARKET REPAIR PROCESS FOR A FUEL NOZZLE GUIDE HEAT SHIELD OF A GAS TURBINE ENGINE

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Quick Facts
Patent No.
US None
App. No.
16/363,220
Abstract

A method for repairing a fuel nozzle guide includes mechanically separating a heat shield of a damaged fuel nozzle guide from an inner portion of the fuel nozzle guide, manufacturing a replacement heat shield for the damaged fuel nozzle guide, and joining the replacement heat shield to the inner portion of the fuel nozzle guide.

Claims (30)

1 . A method for repairing a fuel nozzle guide comprising:

mechanically separating a heat shield of a damaged fuel nozzle guide from an inner portion of the fuel nozzle guide;

manufacturing a replacement heat shield of the damaged fuel nozzle guide; and

joining the replacement heat shield to the inner portion.

2 . The method of claim 1 , wherein manufacturing the replacement heat shield comprises additively manufacturing the replacement heat shield.

3 . The method of claim 1 , further comprising determining an set of actual dimensions of the heat shield and manufacturing the replacement heat shield according to the determined actual dimensions of the heat shield.

4 . The method of claim 1 , further comprising removing artifacts of the mechanical separation from the inner portion prior to joining the replacement heat shield to the inner portion.

5 . The method of claim 1 , wherein joining the replacement heat shield to the inner portion comprises fusing the replacement rim portion to the inner diameter portion.

6 . The method of claim 5 , wherein fusing the replacement heat shield to the inner portion provides a 100% penetration of the inner portion.

7 . The method of claim 6 , wherein fusing the replacement heat shield to the inner portion uses one of a plasma weld fusion, an electron beam weld fusion, a laser weld fusion, and a gas tungsten arc weld fusion.

8 . The method of claim 1 , further comprising repairing at least one crack in the inner portion prior to joining the replacement heat shield to the inner portion.

9 . The method of claim 1 , wherein manufacturing the replacement heat shield comprises creating a replacement heat shield having approximately identical dimensions to the heat shield.

10 . A fuel nozzle guide comprising:

a heat shield, wherein the heat shield is a ring defining an axis;

an inner portion fused to the heat shield and extending radially inward from and axially along the axis; and

wherein the heat shield is an additively manufactured replacement heat shield approximately identical to an original cast heat shield.

11 . The fuel nozzle guide of claim 10 , wherein a fusion between the inner portion and the heat shield extends along a full inner circumference of an inner diameter of the heat shield.

12 . The fuel nozzle guide of claim 11 , wherein the fusion provides a 100% penetration of the inner portion.

13 . The fuel nozzle guide of claim 12 , wherein the fusion is one of a plasma weld fusion, an electron beam weld fusion, a laser weld fusion, and a gas arc weld fusion.

14 . The fuel nozzle guide of claim 10 , wherein the heat shield further includes a plurality of cooling splines extending axially from a face of the heat shield.

15 . The fuel nozzle guide of claim 14 , wherein the plurality of cooling splines are distributed circumferentially evenly about the heat shield.

16 . The fuel nozzle guide of claim 14 , wherein each of the cooling splines in the plurality of cooling splines includes an axially outward corner defining a sharp corner angle.

17 . The fuel nozzle guide of claim 16 , wherein the sharp corner angle is in the range of 89 to 91 degrees.

18 . A repair process for a gas turbine engine comprising:

identifying a damaged fuel nozzle guide, wherein the damaged fuel nozzle guide is a cast single component;

mechanically separating a heat shield from a remainder of the damaged fuel nozzle guide;

additively manufacturing a replacement heat shield; and

fusing the replacement heat shield to the remainder of the damaged fuel nozzle guide, thereby repairing the damaged fuel nozzle guide.

19 . The repair process of claim 18 , wherein fusing the replacement heat shield to the remainder of the damaged fuel nozzle guide comprises applying a fusion process including a 100% penetration of a contact between the replacement heat shield and the remainder of the damaged fuel nozzle guide.

20 . The repair process of claim 18 , wherein additively manufacturing the replacement heat shield comprises determining an actual dimension of the remainder of the fuel nozzle guide, and additively manufacturing the replacement heat shield to match.

Assignments (4)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064402/0837 →
CORRECTIVE ASSIGNMENT TO CORRECT THE SPELLING ON THE ADDRESS 10 FARM SPRINGD ROAD FARMINGTONCONNECTICUT 06032 PREVIOUSLY RECORDED ON REEL 057190 FRAME 0719. ASSIGNOR(S) HEREBY CONFIRMS THE CORRECT SPELLING OF THE ADDRESS 10 FARM SPRINGS ROAD FARMINGTON CONNECTICUT 06032. Recorded Aug 19, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 057226/0390 →
CHANGE OF NAME Recorded Aug 16, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 057190/0719 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 15, 2019
From: RABINOVICH, ALBERT; ROSE, WILLIAM M.; BRINDLEY, WILLIAM J.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 048883/0237 →