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

Patent metadata

Field	Value
Publication number	US-11465243-B2
Application number	US-201816007425-A
Country	US
Kind code	B2
Filing date	Jun 13, 2018
Priority date	Nov 6, 2017
Publication date	Oct 11, 2022
Grant date	Oct 11, 2022

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' solubility within the composition of the first material substrate. 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. At least one of the plurality of interlayers is a sintered powder interlayer.

First claim

What is claimed is:

1. An interlayered structure for joining of dissimilar materials by friction welding, 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 powder interlayers disposed between the first material substrate and the second material substrate, including a first powder interlayer nearest to the first material substrate and a last powder interlayer nearest to the second material substrate,
wherein a barrier material is provided between adjacent powder interlayers and functioning to separate the adjacent powder interlayers, the barrier material comprising one or more compositional components in common with one or both of the adjacent powder interlayers separated by the barrier material, the barrier material including a barrier foil, barrier mesh, or barrier coating,
wherein the first powder interlayer composition is selected to have a maximum solid solubility within the composition of the first material substrate that is greater than or equal to the other powder interlayers' solubility within the composition of the first material substrate,
wherein the last powder interlayer composition is selected to have a maximum solid solubility within the composition of the second material substrate that is greater than or equal to the other powder interlayers' solubility within the composition of the second material substrate, and
wherein the first material substrate is unjoined with the second material substrate, and wherein the first material substrate and second material substrate are capable of being joined by friction welding.

2. The interlayered structure of claim 1 wherein the plurality of powder interlayers each have a thickness of at least 0.001 inch.

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

4. An interlayered structure for joining of titanium-based components with steel-based components by friction welding, comprising:
a first metal substrate comprising titanium;
a second metal substrate comprising steel;
a first powder interlayer disposed between the first metal substrate and the second metal substrate, the first powder interlayer comprising at least one of molybdenum and vanadium; and
a second powder interlayer disposed between the first powder interlayer and the second metal substrate, the second powder interlayer comprising at least one of chromium and nickel,
wherein the first metal substrate is unjoined with the second metal substrate, and wherein the first metal substrate and second metal substrate are capable of being joined by friction welding, and
wherein the second powder interlayer is adjacent the first powder interlayer, and wherein a barrier material coating is provided between the first and second powder interlayers and functions to separate the first and second powder interlayers, the barrier material coating comprising one or more compositional components in common with the first and second powder interlayers separated by the barrier material coating.

5. The interlayered structure of claim 4 wherein the first powder interlayer comprises vanadium and the second powder interlayer comprises chromium.

6. The interlayered structure of claim 5 further comprising a third powder interlayer disposed between the second powder interlayer and the second metal substrate, wherein the third powder interlayer comprises iron.

7. The interlayered structure of claim 4 wherein the first powder interlayer comprises molybdenum.

8. The interlayered structure of claim 4 wherein the first powder interlayer comprises vanadium.

9. The interlayered structure of claim 4 wherein the second powder interlayer comprises chromium.

10. The interlayered structure of claim 4 wherein the second powder interlayer comprises nickel.

11. The interlayered structure of claim 4 further comprising a third powder interlayer disposed between the second powder interlayer and the second metal substrate, the third powder interlayer comprising iron.

12. A method for joining dissimilar metals, comprising:
providing the interlayered structure of claim 4 ;
sintering the plurality of powder interlayers; and
joining the first metal substrate and the second metal substrate by heat of friction derived from relative movement between the first metal substrate and the second metal substrate having the sintered plurality of powder interlayers therebetween.

13. The interlayered structure of claim 1 wherein the plurality of powder interlayers each have a thickness of at least 0.01 inch.

14. The method of claim 12 wherein the plurality of powder interlayers each have a thickness of at least 0.001 inch.

15. The interlayered structure of claim 1 wherein the first and last powder interlayers each have a thickness of at least 0.001 inch.

16. The interlayered structure of claim 4 wherein the plurality of powder interlayers have a total thickness in a range of 0.01 to 1.0 inch.

17. A method for joining dissimilar materials, comprising:
providing the interlayered structure of claim 1 ;
sintering the plurality of powder interlayers; and
joining the first material substrate and the second material substrate by heat of friction derived from relative movement between the first material substrate and the second material substrate having the sintered plurality of powder interlayers therebetween.

18. The method of claim 17 wherein the plurality of powder interlayers include two or more layers that respectively comprise one of chromium, nickel, vanadium, molybdenum, iron, and combinations thereof.

19. The method of claim 17 wherein the plurality of powder interlayers each have a thickness of at least 0.001 inch.

20. The method of claim 17 wherein the plurality of powder interlayers have a total thickness in a range of 0.01 to 1.0 inch.

Assignees

• Boeing Co

Inventors

• Mann Austin E
• Yousefiani Ali

Classifications

• B23K35/002 Primary

  at least one of the workpieces being of light metal · CPC title

• B23K20/12

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

• B22F7/008

  characterised by the composition · CPC title

• B23K2103/24

  Ferrous alloys and titanium or alloys thereof · CPC title

• B32B15/01

  all layers being exclusively metallic {(making layered metal workpieces by pressure cladding B23K20/22; making coatings with a metallic material characterised by its composition C23C30/00)} · CPC title