Method of diffusion bonding utilizing vapor deposition

Patent metadata

Field	Value
Publication number	US-11612947-B2
Application number	US-202016734577-A
Country	US
Kind code	B2
Filing date	Jan 6, 2020
Priority date	Jan 6, 2020
Publication date	Mar 28, 2023
Grant date	Mar 28, 2023

Abstract

A method of diffusion bonding utilizing vapor deposition comprises depositing a coating from a vapor comprising a temperature suppressant element onto a surface of a first component comprising a metal alloy, thereby forming a vapor deposited coating comprising the temperature suppressant element; assembling the first component with a second component comprising a mating surface to form an assembly, the vapor deposited coating contacting the mating surface; and exposing the assembly to a bonding temperature and a compressive force, thereby diffusion bonding the first component to the second component and forming a monolithic third component.

First claim

What is claimed is:

1. A method of diffusion bonding utilizing vapor deposition, the method comprising:
applying a mask comprising a polymer or a ceramic to a surface of a first component comprising a metal alloy, the surface comprising a discontinuous surface including surface regions separated by gaps, the mask being configured to fill the gaps and leave the surface regions uncovered;
depositing a coating from a vapor comprising a temperature suppressant element onto the surface, a first portion of the coating being deposited onto the surface regions and a second portion of the coating being deposited onto the mask,
after depositing the coating, removing the mask from the discontinuous surface along with the second portion of the coating, the first portion of the coating remaining on the surface regions, thereby forming a vapor deposited coating comprising the temperature suppressant element;
assembling the first component with a second component comprising a mating surface to form an assembly, the vapor deposited coating contacting the mating surface; and assembling the first component with a second component comprising a mating surface to form an assembly, the vapor deposited coating contacting the mating surface; and
exposing the assembly to a bonding temperature and a compressive force, thereby diffusion bonding the first component to the second component and forming a monolithic third component.

2. The method of claim 1 , wherein the metal alloy is selected from the group consisting of nickel-base alloy, cobalt-base alloy, and iron-base alloy.

3. The method of claim 1 , wherein the temperature suppressant element is selected from the group consisting of boron, silicon, and phosphorus.

4. The method of claim 1 , wherein the vapor deposited coating comprises a braze alloy including the temperature suppressant element.

5. The method of claim 4 , wherein the braze alloy is selected from the group consisting of Ni—B alloy, Ni—Si alloy, Ni—P alloy, Ni—B—Si alloy, Ni—B—P alloy, and Ni—Si—P alloy.

6. The method of claim 1 , wherein the vapor deposited coating has an elemental composition selected from the group consisting of boron, silicon and phosphorus.

7. The method of claim 1 , wherein depositing the coating from the vapor comprises physical vapor deposition or chemical vapor deposition.

8. The method of claim 1 , wherein applying the mask to the surface comprising spreading or flowing a mask precursor over the discontinuous surface and into the gaps.

9. A method of diffusion bonding utilizing vapor deposition, the method comprising:
applying a mask comprising a polymer or a ceramic to a surface of a first component comprising a metal alloy, the surface comprising a damaged surface including a damaged region, the mask being configured to surround the damaged region and leave the damaged region uncovered;
depositing a coating from a vapor comprising a temperature suppressant element onto the surface, a first portion of the coating being deposited onto the damaged region and a second portion of the coating being deposited onto the mask;
after depositing the coating, removing the mask along with the second portion of the coating, the first portion of the coating remaining on the damaged region, thereby forming a vapor deposited coating comprising the temperature suppressant element;
assembling the first component with a second component comprising a mating surface to form an assembly, the vapor deposited coating contacting the mating surface; and
exposing the assembly to a bonding temperature and a compressive force, thereby diffusion bonding the first component to the second component and forming a monolithic third component.

10. The method of claim 9 , wherein applying the mask to the surface comprising spreading or flowing a mask precursor over the damaged surface without covering the damaged region.

11. The method of claim 1 , wherein the first component comprises a spar and the second component comprises a coversheet.

12. The method of claim 1 , wherein the monolithic third component comprises an airfoil, a combustion liner or a heat shield for a gas turbine engine.

13. The method of claim 1 , wherein the bonding temperature lies in a range from about 900° C. to about 1275° C.

14. The method of claim 9 , wherein the bonding temperature lies in a range from about 900° C. to about 1275° C.

15. A method of diffusion bonding utilizing vapor deposition, the method comprising:
depositing a coating from a vapor consisting of a temperature suppressant element selected from the group consisting of boron, silicon and phosphorus onto a surface of a first component comprising a metal alloy, whereby the coating consists of the temperature suppressant element;
assembling the first component with a second component comprising a mating surface to form an assembly, the coating contacting the mating surface; and
exposing the assembly to a bonding temperature and a compressive force, thereby diffusion bonding the first component to the second component and forming a monolithic third component.

16. The method of claim 15 , wherein the metal alloy is selected from the group consisting of nickel-base alloy, cobalt-base alloy, and iron-base alloy.

17. The method of claim 15 , wherein the first component comprises a spar and the second component comprises a coversheet.

18. The method of claim 15 , wherein the monolithic third component comprises an airfoil, a combustion liner or a heat shield for a gas turbine engine.

19. The method of claim 15 , wherein the bonding temperature lies in a range from about 900° C. to about 1275° C.

20. The method of claim 15 , wherein depositing the coating from the vapor comprises physical vapor deposition or chemical vapor deposition.

Assignees

• Rolls Royce Corp

Inventors

• Henderkott Joseph P
• Fuesting Timothy

Classifications

• C23C14/24

  Vacuum evaporation · CPC title

• B23K2101/001

  Turbines · CPC title

• C23C14/34

  Sputtering · CPC title

• B23K20/24

  Preliminary treatment · CPC title

• B23K2103/08

  Non-ferrous metals or alloys · CPC title