Method and filler material structure of high temperature braze repair for damages of base alloy components

Patent metadata

Field	Value
Publication number	US-2016279740-A1
Application number	US-201514669420-A
Country	US
Kind code	A1
Filing date	Mar 26, 2015
Priority date	Mar 26, 2015
Publication date	Sep 29, 2016
Grant date	—

Abstract

A method of braze repair of a base alloy component that includes a braze thermal cycle including a specially chosen peak braze temperature holding time segment and a purposely selected subsequent diffusion heat treatment segment. A multi-layer braze filler material structure used for the braze repair of a base alloy component including at least a first superalloy layer and a single mixture layer. The single mixture layer including at least a braze alloy and a second superalloy.

First claim

What is claimed is:

1 . A multi-layer braze filler material structure for the braze repair of a base alloy component comprising at least a first superalloy layer and a single mixture layer, wherein the single mixture layer comprises a braze alloy and a second superalloy.

2 . The multi-layer braze filler material structure of claim 1 , wherein the braze alloy material is a Nickel base braze alloy comprising at least one melting point depressing element.

3 . The multi-layer braze filler material structure of claim 1 , wherein the braze alloy material is a Cobalt base braze alloy comprising at least one melting point depressing element.

4 . The multi-layer braze filler material structure of claim 1 , wherein the braze alloy is non-eutectic.

5 . The multi-layer braze filler material structure of claim 1 , wherein the second superalloy material is a Nickel base superalloy compatible with both the braze alloy and the cast grade superalloy component.

6 . The multi-layer braze filler material structure of claim 1 , wherein the second superalloy material is a Cobalt base superalloy compatible with both the braze alloy and the cast grade superalloy component.

7 . The multi-layer braze filler material structure of claim 1 , wherein the mixture has a braze alloy to second superalloy mixing ratio range of approximately 95 braze alloy/5 second superalloy to approximately 60 braze alloy/40 second superalloy.

8 . The multi-layer braze filler material structure of claim 1 , wherein the multi-layer braze filler material structure comprises a double layer tape, wherein the single mixture layer is in direct contact with the base alloy component, and the first superalloy layer is on the exterior of the single mixture layer.

9 . A method of braze repair of a base alloy component comprising the steps of:
placing a multi-layer braze filler material structure on a braze repair site on the base alloy component, wherein the multi-layer braze filler material structure comprises at least a first superalloy layer and a single mixture layer, wherein the single mixture layer comprises a braze alloy and a second superalloy; placing the base alloy component and multi-layer braze filler material structure in a braze thermal cycle, wherein the braze thermal cycle comprises a peak braze temperature holding time segment, wherein a brazing peak temperature of the peak braze temperature holding time segment is held for a peak braze temperature holding time, and a subsequent diffusion heat treatment segment, wherein the base alloy component and multi-layer braze filler material structure is held at a braze homogenization diffusion temperature; and selecting the brazing peak temperature approximately within an upper half of a brazing temperature range of the braze alloy.

10 . The method of claim 9 , wherein the brazing peak temperature selected is approximately a high temperature limit of a brazing temperature range of the braze alloy.

11 . The method of claim 9 , wherein the braze peak temperature holding time is in a range of approximately two minutes to approximately thirty minutes at the brazing peak temperature.

12 . The method of claim 9 , wherein the braze homogenization diffusion temperature is within a melting range of the braze alloy.

13 . The method of claim 12 , wherein the braze homogenization diffusion temperature is approximately within a lower half of the melting range of the braze alloy.

14 . The method of claim 9 , wherein the braze alloy is non-eutectic.

15 . The method of claim 9 , wherein the single mixture has a braze alloy to second superalloy mixing ratio range of approximately 95 braze alloy/5 second superalloy to approximately 60 braze alloy/40 second superalloy.

16 . The method of claim 9 , wherein the multi-layer braze filler material structure comprises a double layer tape, wherein the single mixture layer is in direct contact with the base alloy component, and the first superalloy layer is on the exterior of the single mixture layer.

Assignees

• Siemens Energy Inc

Inventors

• Li Hang
• Ghunakikar Somesh J
• Lowe William J
• Garcia Mark A

Classifications

• B23K35/0238 Primary

  layered · CPC title

• B23K1/00

  Soldering, e.g. brazing, or unsoldering (B23K3/00 takes precedence) · CPC title

• B23K35/3033

  Ni as the principal constituent · CPC title

• B32B15/01

  all layers being exclusively metallic {(making layered metal workpieces by pressure cladding B23K20/22; making coatings with a metallic material characterised by its composition C23C30/00)} · CPC title

• B23K35/3046

  Co as the principal constituent · CPC title