Interlayered structures for joining dissimilar materials and methods for joining dissimilar metals

Patent metadata

Field	Value
Publication number	US-10857628-B2
Application number	US-201715804061-A
Country	US
Kind code	B2
Filing date	Nov 6, 2017
Priority date	Nov 6, 2017
Publication date	Dec 8, 2020
Grant date	Dec 8, 2020

Abstract

An interlayered structure for joining of dissimilar materials includes: a first material substrate; a second material substrate having a composition dissimilar from a composition of the first material substrate; and a plurality of interlayers disposed between the first material substrate and the second material substrate, including a first interlayer nearest to the first material substrate and a last interlayer nearest to the second material substrate. The first interlayer has a composition selected to have a maximum solid solubility within the composition of the first material substrate that is greater than or equal to the other interlayers within the composition of the first material substrate, and the last interlayer has a composition selected to have a maximum solid solubility within the composition of the second material substrate that is greater than or equal to the other interlayers within the composition of the second material substrate.

First claim

What is claimed is:

1. An interlayered structure for joining of dissimilar materials through friction welding derived from relative movement between the dissimilar materials, comprising:
a first material substrate;
a second material substrate having a composition dissimilar from a composition of the first material substrate; and
a plurality of interlayers disposed between the first material substrate and the second material substrate, including a first interlayer nearest to the first material substrate and a last interlayer nearest to the second material substrate,
wherein the first interlayer has a composition selected to have a maximum solid solubility within the composition of the first material substrate that is greater than or equal to the other interlayers' solubility within the composition of the first material substrate,
wherein the last interlayer has a composition selected to have a maximum solid solubility within the composition of the second material substrate that is greater than or equal to the other interlayers' solubility within the composition of the second material substrate, and
wherein at least one of the plurality of interlayers has a thickness of at least 0.01 inch and the plurality of interlayers facilitate joining of the first material substrate and the second material substrate by friction welding.

2. The interlayered structure of claim 1 wherein the first interlayer has a composition selected to have a maximum solid solubility within the composition of the first material substrate that is greater than the last interlayer within the composition of the first material substrate, and wherein the last interlayer has a composition selected to have a maximum solid solubility within the composition of the second material substrate that is greater than the first interlayer within the composition of the second material substrate.

3. The interlayered structure of claim 1 wherein the plurality of interlayers includes a second interlayer between the first interlayer and the last interlayer, wherein the second interlayer has a composition selected to have a maximum solid solubility within the composition of the first material substrate that is greater than the last interlayer within the composition of the first material substrate and to have a maximum solid solubility within the composition of the second material substrate that is greater than the first interlayer within the composition of the second material substrate.

4. The interlayered structure of claim 1 wherein the plurality of interlayers are deposited on at least one of the first material substrate and the second material substrate.

5. The interlayered structure of claim 1 wherein the plurality of interlayers include two or more elemental layers that respectively comprise one of chromium, nickel, vanadium, molybdenum, iron, and combinations thereof.

6. An interlayered structure for joining of titanium-based components with iron-based components through friction welding derived from relative movement between the components, comprising:
a first metal substrate comprising titanium;
a second metal substrate comprising steel;
a first interlayer disposed between the first metal substrate and the second metal substrate, the first interlayer comprising at least one of molybdenum and vanadium;
a second interlayer disposed between the first interlayer and the second metal substrate, the second interlayer comprising at least one of chromium and nickel; and
a third interlayer disposed between the second interlayer and the second metal substrate, the third interlayer comprising iron,
wherein the first interlayer, the second interlayer, and the third interlayer each have a thickness of at least 0.01 inch and facilitate joining of the first metal substrate and the second metal substrate by friction welding.

7. The interlayered structure of claim 6 wherein the first metal substrate comprises a titanium-based alloy.

8. The interlayered structure of claim 6 wherein the first interlayer comprises molybdenum.

9. The interlayered structure of claim 6 wherein the first interlayer comprises vanadium.

10. The interlayered structure of claim 6 wherein the second interlayer comprises chromium.

11. The interlayered structure of claim 6 wherein the second interlayer comprises nickel.

12. The interlayered structure of claim 6 wherein the first interlayer and the second interlayer are deposited on the first metal substrate.

13. The interlayered structure of claim 7 wherein the first interlayer comprises vanadium, and the second interlayer comprises chromium.

14. A method for joining dissimilar metals through friction welding, comprising:
providing an interlayered structure, comprising:
a first metal substrate;
a second metal substrate having a composition dissimilar from a composition of the first metal substrate; and
a plurality of interlayers disposed between the first metal substrate and the second metal substrate, including a first interlayer nearest to the first metal substrate and a last interlayer nearest to the second metal substrate, wherein the first interlayer has a composition selected to have a maximum solid solubility within the composition of the first material substrate that is greater than or equal to the other interlayers within the composition of the first material substrate, and wherein the last interlayer has a composition selected to have a maximum solid solubility within the composition of the second material substrate that is greater than or equal to the other interlayers within the composition of the second material substrate;

depositing the first interlayer and last interlayer on the first metal substrate, wherein the plurality of interlayers each have a thickness of at least 0.01 inch that is sufficient to enable joining of the first metal substrate and second metal substrate by friction welding; and
joining the first metal substrate and a second metal substrate by heat of friction derived from relative movement between the first metal substrate and the second metal substrate.

15. The method of claim 14 wherein the joining includes at least one of linear friction welding and inertia friction welding.

16. The interlayered structure of claim 13 wherein the third interlayer comprising iron is deposited directly on the steel of the second metal substrate, the second interlayer comprising chromium is deposited directly on the third interlayer comprising iron, and the first interlayer comprising vanadium is deposited directly on the second interlayer that comprises chromium.

17. The interlayered structure of claim 7 wherein the first interlayer comprises vanadium and is deposited directly on the titanium-based alloy of the first metal substrate.

18. The interlayered structure of claim 17 wherein the second interlayer comprises chromium and is deposited directly on the first interlayer that comprises vanadium.

19. The interlayered structure of claim 18 , wherein the third interlayer is deposited directly on the second interlayer that comprises chromium.

20. The interlayered structure of claim 6 wherein the second metal substrate comprises stainless steel.

21. The interlayered structure of claim 20 wherein the third interlayer comprising iron is deposited directly on the stainless steel of the second metal substrate.

22. The interlayered structure of claim 21 wherein the second interlayer comprising chromium is deposited directly on the third interlayer comprising iron.

Assignees

• Boeing Co

Inventors

• Mann Austin E

Classifications

• B23K2103/24

  Ferrous alloys and titanium or alloys thereof · CPC title

• B23K20/12

  the heat being generated by friction; Friction welding · CPC title

• B23K20/129

  specially adapted for particular articles or work · CPC title

• B23K20/24

  Preliminary treatment · CPC title

• B23K20/227

  with ferrous layer · CPC title