Brazing titanium aluminum alloy components

Patent metadata

Field	Value
Publication number	US-2017197270-A1
Application number	US-201615370635-A
Country	US
Kind code	A1
Filing date	Dec 6, 2016
Priority date	Jan 8, 2016
Publication date	Jul 13, 2017
Grant date	—

Abstract

In some examples, the disclosure describes a technique that includes covering a joint surface of a first part including a titanium aluminum (TiAl) alloy with a braze material including aluminum, where covering the joint surface includes at least one of electroplating the braze material on the joint surface, hot dipping the braze material on the joint surface, or positioning a foil of the braze material adjacent to the joint surface, positioning a second part including a titanium alloy in contact with the first part to define a joint region, where the joint region includes the braze material interposed between the second part and the joint surface of the first part, and heating the joint region to at least partially melt the braze material to form a braze joint connecting the first part to the second part.

First claim

What is claimed is:

1 . A method comprising:
covering a joint surface of a first part comprising a titanium aluminum (TiAl) alloy with a braze material comprising aluminum, wherein covering the joint surface comprises at least one of electroplating the braze material on the joint surface, hot dipping the braze material on the joint surface, or positioning a foil of the braze material adjacent to the joint surface; positioning a second part comprising a titanium alloy in contact with the first part to define a joint region, wherein the joint region comprises the braze material interposed between the second part and the joint surface of the first part; and heating the joint region to at least partially melt the braze material to form a braze joint connecting the first part to the second part.

2 . The method of claim 1 , wherein the second part comprises a Tim alloy.

3 . The method of claim 1 , wherein coating the braze material comprises electroplating the braze material on the joint surface of the first part.

4 . The method of claim 1 , wherein the braze material comprises at least about 99% by weight elemental aluminum.

5 . The method of claim 1 , further comprising depositing a titanium-based powder on the braze material after coating the braze material on the joint surface of the first part, wherein the joint region comprises the titanium-based powder interposed between the braze material and the second part.

6 . The method of claim 5 , wherein the titanium-based powder comprises titanium hydride.

7 . The method of claim 1 , wherein the braze joint comprises a TiAl alloy.

8 . The method of claim 7 , wherein the braze joint comprises about 40 atomic percent (at. %) to about 60 at. % titanium and about 39 at. % to about 60 at. % aluminum.

9 . The method of claim 1 , wherein the first part comprises about 46 at. % to about 56 at. % titanium and about 39 at. % to about 49 at. % aluminum.

10 . The method of claim 1 , wherein heating the joint region comprises:
heating the joint region in a vacuum furnace to melt the braze material, or locally heating the braze material using at least one of a laser or a plasma arc torch to at least partially melt the braze material.

11 . The method of claim 1 , further comprising masking a portion of the first part to define the joint surface prior to coating the braze material on the joint surface.

12 . An assembly comprising:
a first part comprising a TiAl alloy and a layer of a braze material on a joint surface of the first part, wherein the braze material comprises at least 99% by weight aluminum; a second part comprising a TiAl alloy, wherein the first part and second part contact one another to define a joint region, wherein the joint region comprises the layer of the braze material interposed between the second part and the joint surface of the first part; and a heat source configured to heat at least the braze material in the joint region to at least partially melt the layer of braze material.

13 . The assembly of claim 12 , wherein the first part and the second part comprise about 46 at. % to about 56 at. % titanium and about 39 at. % to about 49 at. % aluminum.

14 . The assembly of claim 12 , further comprising a titanium-based powder deposited on the layer of the braze material, wherein the joint region comprises the titanium-based powder interposed between the braze material and the second part.

15 . The assembly of claim 14 , wherein the titanium-based powder comprises titanium hydride.

16 . The assembly of 14 , wherein the titanium-based powder comprises at least one of niobium or molybdenum based powder.

17 . The assembly of claim 12 , wherein the layer of the braze material comprises a solid layer of the braze material that defines a thickness of about 20 to about 200 microns.

18 . The assembly of claim 12 , wherein the second part comprises a second layer of braze material comprising at least about 99% by weight aluminum on a second joint surface of the second part.

19 . A method comprising:
electroplating a braze material comprising aluminum on a joint surface of a first part comprising a titanium aluminum (TiAl) alloy; positioning a second part in contact with the first part to define a joint region, wherein the joint region comprises the braze material interposed between the second part and the joint surface of the first part; and heating the joint region to at least partially melt the braze material and to form a braze joint that joins the first part to the second part.

20 . The method of claim 19 , further comprising:
depositing a titanium-based powder on the braze material prior to heating the joint region; wherein joint region comprises the titanium-based powder interposed between the braze material and the second part.

Assignees

• Rolls Royce Corp

Inventors

• Shuck Quinlan Yee
• Bader Jacque Sue

Classifications

• C25D3/44

  Aluminium · CPC title

• B23K1/19

  taking account of the properties of the materials to be soldered · CPC title

• B23K1/0018

  Brazing of turbine parts · CPC title

• B23K1/08

  Soldering by means of dipping in molten solder · CPC title

• C22C14/00

  Alloys based on titanium · CPC title