Method for diffusion bonding of alloys having low solubility oxides

• US 4,732,312 A
• Filed: 11/10/1986
• Issued: 03/22/1988
• Est. Priority Date: 11/10/1986
• Status: Expired due to Term

• Current Assignee: Vought Aircraft Industries, Inc. (Triumph Group, Inc.)
• Original Assignee: Grumman Aerospace Corporation (Northrop Grumman Corporation)
• Inventors: Ting, Edmund Y., Kennedy, James R.
• Primary Examiner(s): Godici, Nicholas P.
• Assistant Examiner(s): Heinrich, Samuel M.
• Application Number:
  US06/928,898
• Time in Patent Office: 498 Days
• Field of Search: 228/157, 228/193, 228/118, 228/265, 228/172, 228/205, 228/263.17, 228/203, 148/11.5 A
• US Class Current: 148/535
• CPC Class Codes: B23K 20/2336 both layers being aluminium
• CPC Class Codes: B23K 20/24 Preliminary treatment

Abstract

Diffusion bonding of surface layers of an alloy, such as an aluminum alloy, having surface oxides of low solubility in the alloy includes treating the surface layers to be bonded to remove existing surface oxide coatings, and diffusion bonding the surface layers to one another by placing the alloy to be bonded under sufficient pressure to cause disruption of the oxide coatings by localized surface deformation of the alloy, enhanced by a superplastic microstructure, without substantial deformation of the alloy, i.e., macroscopic deformation approaching zero percent, while heating the alloy in a non-oxidizing atmosphere for a time sufficient for diffusion bonding to occur. The alloy may be treated so that at least the surface layers thereof have a fine grain structure of the type associated with superplastic forming properties. Components may be formed by diffusion bonding and superplastic forming.

Claims

1. A method for diffusion bonding surface layers of an alloy having surface oxide coatings of low solubility in the alloy, comprising the steps of:

treating said alloy so that at least the surface layers to be bonded have a fine grain structure;

removing existing surface oxide coatings from the surface layers to be bonded;

diffusion bonding the surface layers to one another by placing the alloy to be bonded under a pressure sufficient to cause disruption of the oxide coatings and insufficient to cause macroscopic deformation of the alloy while heating the alloy in a non-oxidizing atmosphere for a time sufficient for diffusion bonding to occur.

2. The method of claim 1, wherein said alloy is an aluminum alloy.

3. The method of claim 2, wherein said aluminum alloy is 7475 aluminum.

4. The method of claim 2, wherein said aluminum alloy is 7075 aluminum.

5. The method of claim 1, wherein said step of treating said alloy comprises:

thermomechanically processing the surface layers sufficiently to deform the near surface microstructure; and

recrystalizing the deformed microstructure to create said fine-grained structure.

6. The method of claim 1, wherein said step of treating said alloy comprises localized mechanical surface deformation and heating of the alloy to cause recrystallization.

7. The method of claim 1, wherein said pressure is less than 1000 pounds per square inch.

8. The method of claim 1, wherein said pressure is less than 100 pounds per square inch.

9. The method of claim 1, wherein said step of heating is performed for a time ranging from one half hour to ten hours.

10. The method of claim 1, further comprising the step of heat treating the alloy after diffusion bonding.

11. The method of claim 1, further comprising the step of tempering after diffusion bonding has occured.

12. The method of claim 1, further comprising the step of:

cooling the alloy to room temperature, after bonding, over a period of at least approximately twenty minutes.

13. The method of claim 1, wherein said step of treating the surface layers comprises:

abrading with successively finer grades of grinding paper;

rinsing with one of high purity acetone and distilled water;

abrading with a metallic brush; and

removing the brushings.

14. The method of claim 13, wherein said step of abrading with a metallic brush comprises:

abrading in a first direction;

abrading in a second direction at an angle of approximately ninety degrees with respect to said first direction.

15. The method of claim 13, wherein said step of removing the brushings comprises:

exposing brushed surfaces to a stream of compressed, filtered air moving at a velocity sufficiently high to remove said brushings.

16. The method of claim 13, wherein said grades of grinding paper vary from 240 grit to 600 grit SiC grinding paper.

17. The method of claim 1, further comprising the step of:

placing components of said alloy in a fixture;

exposing a first opposite surface to a first surface layer to be diffusion bonded to one of a partial vacuum and a pressurized gas; and

exposing a second opposite surface of a second surface layer to be diffusion bonded to another of said partial vacuum and pressurized gas.

18. The method of claim 1, wherein said non-oxidizing atmosphere is produced by surrounding said alloy with one of an inert gas and a soft vacuum.

19. The method of claim 1, further comprising the step of:

superplastically forming at least one of the alloys to change the shape thereof.

20. The method of claim 1, wherein at least the surface layers of the alloy have superplastic properties.

26. The method of claim 11, wherein said step of tempering comprises the steps of

solution treating;

quenching; and

aging the alloy.

27. The method of claim 1, wherein said fine grain structure includes grains having a size equal to or less than substantially ten microns.

21. A method for diffusion bonding surface layers of alloys having surface oxide coatings of low solubility in the alloy, comprising the steps of:

treating the surface layer of a first of said alloys so that it has a fine grained microstructure characteristic of superplasticity;

treating the surface layers to be bonded to remove existing surface oxide coatings;

diffusion bonding the surface layers to one another by placing the alloys to be bonded under sufficient pressure to cause disruption of the oxide coatings and insufficient to cause macroscopic deformation of the alloys while heating the alloys in a nonoxidizing atmosphere for a time sufficient for diffusion bonding to occur.

22. The method of claim 21, wherein the surface layer of a second of said alloys has a coarse grained microstructure which is non-superplastic.

23. The method of claim 22, wherein said first alloy is 7475 aluminum and said second alloy is 2219 aluminum.

24. The method of claim 21, wherein said alloys are each of a different material.

25. The method of claim 21, wherein said alloys are each different alloys of aluminum.