Method of tight crack braze repair using acoustics

Patent metadata

Field	Value
Publication number	US-10500663-B2
Application number	US-201615252887-A
Country	US
Kind code	B2
Filing date	Aug 31, 2016
Priority date	Aug 31, 2016
Publication date	Dec 10, 2019
Grant date	Dec 10, 2019

Abstract

A method for braze repair of tight cracks in a superalloy component is provided. The method includes directing energy, e.g., from an acoustic energy source, towards surfaces of the tight crack to break up one or more contaminants, corrosion products, or oxides at the surface. The directed energy may cause opposed walls of the tight crack to vibrate to break up the oxides, and to generate a modest heat for allowing infiltration of the tight crack with a braze material. The braze material is then melted at a melt temperature of the braze material but below the melt temperature of the component. The braze material is then solidified to repair the tight crack.

First claim

I claim:

1. A method comprising:
vibrating opposed side walls of a crack in a superalloy component to produce relative movement between the side walls and rubbing between the side walls to break up contaminants;
applying a braze material to a surface of the component proximate to the crack;
working the braze material into the crack to fill the crack; and
heating at least opposed surfaces of the crack to a melt temperature of the braze material but below a melt temperature of the superalloy component.

2. The method of claim 1 further comprising:
solidifying the braze material on the superalloy component.

3. The method of claim 2 , wherein the braze material is solidified via cooling the superalloy component in a uniform manner.

4. The method of claim 2 further comprising:
grinding, polishing, or machining any excess braze material from the superalloy component.

5. The method of claim 4 further comprising:
inspecting the superalloy component prior to grinding, polishing, or machining any excess braze material.

6. The method of claim 1 , wherein the opposed walls are vibrated via an energy source directed towards at least one of the opposed surfaces of the crack.

7. The method of claim 6 , wherein the energy sources is an acoustic energy source.

8. The method of claim 6 , wherein the energy source creates a heat energy to work the braze material into the crack.

9. The method of claim 1 , wherein the braze material is a fine material sized to infiltrate the crack and comprises a powdered superalloy and a melting point suppressant.

10. A method for braze repair of a superalloy component comprising:
directing acoustic energy towards a first surface of a crack in the component to break up one or more contaminants, corrosion products, or oxides at the surface and to produce relative movement and rubbing between the first surface and a second surface of the crack opposite the first surface;
vibrating one of the first surface and the second surface of the crack to generate heat and relative motion for infiltrating the crack with a braze material;
melting the braze material at a melt temperature below the melt temperature of the component;
solidifying the braze material to repair the crack with the braze material.

11. The method of claim 10 further comprising the step of cosmetically cleaning the component prior to directing the acoustic energy.

12. The method of claim 10 , wherein the component is submerged in the braze material prior to directing the acoustic energy.

13. The method of claim 10 , wherein the braze material is solidified by cooling the component in a uniform manner.

14. The method of claim 10 further comprising:
inspecting the component for cracks after solidifying the braze material; and
grinding, polishing, or machining any excess braze material from the component upon determining that no cracks are present.

15. The method of claim 10 , wherein the acoustic energy is directed to opposed surfaces of the crack to break up one or more contaminants, corrosion products, or oxides at the opposed surfaces.

16. The method of claim 10 , wherein the braze material is a fine material sized to infiltrate the crack and comprises a powdered superalloy and a melting point suppressant.

17. The method of claim 10 , wherein the relative motion smooths the opposed walls to enhance wetting and infiltration of the crack.

Assignees

• Siemens Energy Inc

Inventors

• Bruck Gerald J

Classifications

• B23K1/002

  Soldering by means of induction heating · CPC title

• B23K1/206

  Cleaning · CPC title

• B23K1/0004

  Resistance soldering · CPC title

• B23K1/06 Primary

  making use of vibrations, e.g. supersonic vibrations · CPC title

• B23K1/0018

  Brazing of turbine parts · CPC title