Process for producing intermetallic wear-resistant layer for titanium materials

Patent metadata

Field	Value
Publication number	US-9561556-B2
Application number	US-201414461516-A
Country	US
Kind code	B2
Filing date	Aug 18, 2014
Priority date	Aug 19, 2013
Publication date	Feb 7, 2017
Grant date	Feb 7, 2017

Abstract

Disclosed is a process for producing a wear-resistant layer, in particular on components of gas turbines or aero engines. The process comprises providing a component with a titanium material on at least part of a surface on which the wear-resistant layer is to be produced, applying a solder formed from a cobalt base material to the titanium material, soldering the solder to the titanium material by applying heat and producing at least one diffusion zone between solder and titanium material which comprises intermetallic phases.

First claim

What is claimed is:

1. A process for producing a wear-resistant layer on a component, wherein the process comprises:
providing a component which comprises a titanium material on at least part of a surface of the component on which the wear-resistant layer is to be produced,
contacting the titanium material with a solder in the form of a paste or semifinished product formed from a cobalt base material,
soldering the solder to the titanium material by applying heat to thereby produce one or more diffusion zones between solder and titanium material, which one or more diffusion zones comprise one or more intermetallic phases and form the wear-resistant layer, the soldering being carried out at a temperature of from about 1100° C. to about 1200° C.

2. The process of claim 1 , wherein the component is a component of a gas turbine or of an aero engine.

3. The process of claim 1 , wherein the process further comprises removing excess solder present on top of the one or more diffusion zones, whereby the wear-resistant layer is present on the surface of the correspondingly treated component.

4. The process of claim 1 , wherein the solder comprises hard phase particles.

5. The process of claim 4 , wherein the hard phase particles comprise ceramic and/or intermetallic phases.

6. The process of claim 1 , wherein the solder is employed in the form of a paste.

7. The process of claim 1 , wherein the solder is employed in the form of a semifinished product.

8. The process of claim 7 , wherein the semifinished product is a solder tape.

9. The process of claim 1 , wherein in addition to cobalt the solder comprises one or more elements selected from chromium, molybdenum, iron, nickel, tungsten, tantalum, titanium, zirconium, and silicon.

10. The process of claim 1 , wherein the titanium material comprises titanium as main constituent and one or more elements selected from molybdenum, niobium, aluminum, boron, silicon.

11. The process of claim 1 , wherein soldering is carried out at a temperature of from about 1100° C. to about 1200° C. with a holding time of from about 2 min to about 10 min and/or under protective gas or vacuum.

12. The process of claim 1 , wherein soldering is carried out at a temperature of from about 1150° C. to about 1200° C.

13. The process of claim 1 , wherein at least one of the one or more diffusion zones comprises one or more intermetallic phases based on one or more of the binary systems Co-Ti, Co—Al, Ti—B, and Mo—Si.

14. The process of claim 1 , wherein the cobalt based solder is formed from an alloy which comprises from 6.5% to 7.5% by weight tungsten, from 3% to 4% by weight tantalum, from 22.5% to 24.35% by weight chromium, from 0.55% to 0.65% by weight carbon, from 9% to 11% by weight nickel as well as titanium and zirconium, remainder cobalt.

15. The process of claim 1 , wherein the wear-resistant layer comprises at least two diffusion zones, one diffusion zone comprising about 11% by weight chromium, about 4% by weight nickel, about 13% by weight molybdenum, about 2% by weight silicon, about 13% by weight titanium, about 8% by weight aluminum and about 1% by weight niobium, remainder cobalt, and another diffusion zone comprising about 21% by weight chromium, about 12% by weight molybdenum, about 1% by weight silicon, about 12% by weight titanium, about 6% by weight aluminum and about 1% by weight niobium, remainder cobalt.

16. A process for producing a wear-resistant layer on a component, wherein the process comprises:
providing a component which comprises a titanium material on at least part of a surface of the component on which the wear-resistant layer is to be produced,
contacting the titanium material with a solder in the form of a paste or semifinished product formed from a cobalt base alloy which comprises from 6.5% to 7.5% by weight tungsten, from 3% to 4% by weight tantalum, from 22.5% to 24.35% by weight chromium, from 0.55% to 0.65% by weight carbon, from 9% to 11% by weight nickel as well as titanium and zirconium, remainder cobalt,
soldering the solder to the titanium material by applying heat to thereby produce one or more diffusion zones between solder and titanium material, which one or more diffusion zones comprise one or more intermetallic phases and form the wear-resistant layer.

17. The process of claim 16 , wherein the wear-resistant layer comprises at least two diffusion zones, one diffusion zone comprising about 11% by weight chromium, about 4% by weight nickel, about 13% by weight molybdenum, about 2% by weight silicon, about 13% by weight titanium, about 8% by weight aluminum and about 1% by weight niobium, remainder cobalt, and another diffusion zone comprising about 21% by weight chromium, about 12% by weight molybdenum, about 1% by weight silicon, about 12% by weight titanium, about 6% by weight aluminum and about 1% by weight niobium, remainder cobalt.

18. The process of claim 16 , wherein soldering is carried out at a temperature of from about 1150° C. to about 1200° C.

19. A process for producing a wear-resistant layer on a component, wherein the process comprises:
providing a component which comprises a titanium material on at least part of a surface of the component on which the wear-resistant layer is to be produced,
contacting the titanium material with a solder in the form of a paste or semifinished product formed from a cobalt base material,
soldering the solder to the titanium material by applying heat to thereby produce at least two diffusion zones between solder and titanium material, one diffusion zone comprising about 11% by weight chromium, about 4% by weight nickel, about 13% by weight molybdenum, about 2% by weight silicon, about 13% by weight titanium, about 8% by weight aluminum and about 1% by weight niobium, remainder cobalt, and another diffusion zone comprising about 21% by weight chromium, about 12% by weight molybdenum, about 1% by weight silicon, about 12% by weight titanium, about 6% by weight aluminum and about 1% by weight niobium, remainder cobalt, which at least two diffusion zones comprise one or more intermetallic phases and form the wear-resistant layer.

20. The process of claim 19 , wherein soldering is carried out at a temperature of from about 1150° C. to about 1200° C.

Assignees

• MTU Aero Engines AG

Inventors

• Werner André
• Daniels Bernd
• Strasser Michael

Classifications

• B23K2101/001

  Turbines · CPC title

• B23K1/0018 Primary

  Brazing of turbine parts · CPC title

• F05D2230/237

  Brazing · CPC title

• C23C10/60

  After-treatment · CPC title

• Y10T428/12097

  Nonparticulate component encloses particles · CPC title