Weld forced crack and braze repair for superalloys

Patent metadata

Field	Value
Publication number	US-10279416-B2
Application number	US-201615070324-A
Country	US
Kind code	B2
Filing date	Mar 15, 2016
Priority date	Mar 15, 2016
Publication date	May 7, 2019
Grant date	May 7, 2019

Abstract

A method of repairing an oxidized defect in a superalloy article includes removing substantially all of the oxidized defect to form a cleaned out portion of the superalloy article; filling a portion of the cleaned out portion with a weld by fusion welding; cracking the weld; and filling the cracked weld and a remaining portion of the cleaned out portion with a braze material.

First claim

What is claimed is:

1. A method of repairing an oxidized defect in a superalloy article, the method comprising:
removing substantially all of the oxidized defect to form a cleaned out portion of the superalloy article;
filling a portion of the cleaned out portion with a weld by fusion welding;
cracking the weld; and
filling the cracked weld and a remaining portion of the cleaned out portion with a braze material; wherein cracking the weld comprises dropping a temperature of the weld at a rate sufficient to cause cracking during the welding; and wherein cracking the weld comprises quenching the weld.

2. The method of claim 1 , wherein removing substantially all of the oxidized defect to form the cleaned out portion includes vacuum furnace cleaning.

3. The method of claim 2 , wherein the vacuum furnace cleaning includes fluoride ion cleaning.

4. The method of claim 1 , wherein removing substantially all of the oxidized defect to form the cleaned out portion includes mechanical cleaning.

5. The method of claim 4 , wherein the mechanical cleaning comprises grinding.

6. The method of claim 1 , wherein removing substantially all of the oxidized defect to form the cleaned out portion includes chemical cleaning.

7. The method of claim 6 , wherein the chemical cleaning includes etching.

8. The method of claim 1 , wherein filling the portion of the cleaned out portion with the weld comprises filling the portion with weld material that is the same as the superalloy article.

9. The method of claim 1 , wherein cracking the weld comprises cracking the weld after the weld is formed.

10. The method of claim 1 , wherein cracking the weld comprises inputting heat while forming the weld.

11. A method of repairing an oxidized defect in a superalloy article, the method comprising:
removing substantially all of the oxidized defect to form a cleaned out portion of the superalloy article;
filling a portion of the cleaned out portion with a weld by fusion welding;
cracking the weld; and
filling the cracked weld and a remaining portion of the cleaned out portion with a braze material, wherein cracking the weld comprises inputting heat while forming the weld by induction heating.

12. The method of claim 1 , further comprising:
covering the weld with the braze material.

13. The method of claim 1 , further comprising:
heat treating the braze filled weld.

14. The method of claim 1 , wherein fusion welding comprises Metal Inert Gas (MIG) welding or Gas Tungsten Arc Welding (GTAW).

15. The method of claim 14 , wherein fusion welding comprises Tungsten Inert Gas (TIG) welding.

16. The method of claim 1 , wherein the braze material comprises a combination of high melt material and low melt material.

17. A method repairing an oxidized defect in a Ni-based superalloy article including Al and Ti, the method comprising:
removing substantially all of the oxidized defect to form a cleaned out portion of the superalloy article, wherein removing substantially all of the oxidized defect includes vacuum cleaning, mechanical cleaning, and/or chemical cleaning;
filling a portion of the cleaned out portion with a weld by fusion welding;
cracking the weld by restraining the weld;
filling the cracked weld and a remaining portion of the cleaned out portion with a braze material;
covering the weld with the braze material; and
heat treating the braze filled and covered weld.

18. The method of claim 17 , wherein the Ni-based superalloy comprises greater than about 3% Al and less than about 6% Ti.

19. The method of claim 17 , wherein filling the weld by fusion welding comprises Metal Inert Gas (MIG) welding or Gas Tungsten Arc Welding (GTAW).

Assignees

• Gen Electric

Inventors

• Whims Lawrence James
• Lambert John Christopher
• Eminoglu Cem Murat
• Shubert Gary Charles
• Klimczuk Piotr Artur
• Gaik Adam

Classifications

• B23K9/0026

  specially adapted for particular articles or work · CPC title

• F01D5/005

  Repairing methods or devices · CPC title

• B23K2101/001

  Turbines · CPC title

• B23K28/02

  Combined welding or cutting procedures or apparatus · CPC title

• B23P6/045

  of turbine components, e.g. moving or stationary blades, rotors, etc. · CPC title