Functionally graded metal-metal composite structures

Patent metadata

Field	Value
Publication number	US-10857597-B2
Application number	US-201715707479-A
Country	US
Kind code	B2
Filing date	Sep 18, 2017
Priority date	Aug 23, 2013
Publication date	Dec 8, 2020
Grant date	Dec 8, 2020

Abstract

Methods and devices are disclosed for creating a multiple alloy composite structure by forming a three-dimensional arrangement of a first alloy composition in which the three-dimensional arrangement has a substantially open and continuous porosity. The three-dimensional arrangement of the first alloy composition is infused with at least a second alloy composition, where the second alloy composition comprises a shape memory alloy. The three-dimensional arrangement is consolidated into a fully dense solid structure, and the original shape of the second alloy composition is set for reversible transformation. Strain is applied to the fully dense solid structure, which is treated with heat so that the shape memory alloy composition becomes memory activated to recover the original shape. An interwoven composite of the first alloy composition and the memory-activated second alloy composition is thereby formed in the multiple alloy composite structure.

First claim

What is claimed is:

1. A bi-metallic composite material, comprising:
a three-dimensional interior portion comprising a first alloy composition infused with a shape memory alloy composition and consolidated into a fully dense composite, wherein the shape memory alloy composition is held in a constrained shape other than an original shape by the first alloy composition, the original shape being a shape to which the shape memory alloy composition is reverting from the constrained shape thereby generating a net compressive residual stress field in the three-dimensional interior portion; and
a three-dimensional exterior portion surrounding the three-dimensional interior portion and comprising solid load-bearing structural walls.

2. The bi-metallic composite material of claim 1 , wherein the three-dimensional exterior portion is a box structure.

3. The bi-metallic composite material of claim 2 , wherein the box structure is partially enclosed and includes a cover plate.

4. The bi-metallic composite material of claim 3 , wherein the bi-metallic composite material is configured to form structural components in order to eliminate or at least limit propagation of surface cracks in the structural components.

5. The bi-metallic composite material of claim 1 , wherein the shape memory alloy composition comprises a nickel titanium alloy.

6. The bi-metallic composite material of claim 1 , wherein the first alloy composition comprises at least one of titanium and aluminum.

7. The bi-metallic composite material of claim 5 , wherein the nickel titanium alloy contains approximately equal atomic percentages of nickel and titanium.

8. The bi-metallic composite material of claim 1 , wherein the bi-metallic composite material is made by additive manufacturing.

9. The bi-metallic composite material of claim 1 , wherein the net compressive residual stress field limits or eliminates nucleation and/or growth of a surface crack in the three-dimensional exterior portion by counteracting an applied load to the exterior portion.

10. A bi-metallic composite material, comprising:
a three-dimensional interior portion comprising a first alloy composition infused with a shape memory alloy composition and consolidated into a fully dense composite, wherein the shape memory alloy composition is held in a constrained shape other than an original shape by the first alloy composition, the original shape being a shape to which the shape memory alloy composition is reverting from the constrained shape thereby generating a net compressive residual stress field in the three-dimensional interior portion, wherein the first alloy composition comprises at least one of titanium and aluminum, and wherein the shape memory alloy composition comprises a nickel titanium alloy; and
a three-dimensional exterior portion surrounding the three-dimensional interior portion and comprising solid load-bearing structural walls,
wherein the net compressive residual stress field limits or eliminates nucleation and/or growth of a surface crack in the three-dimensional exterior portion by counteracting an applied load to the three-dimensional exterior portion.

11. The bi-metallic composite material of claim 10 , wherein the nickel titanium alloy contains approximately equal atomic percentages of nickel and titanium.

12. The bi-metallic composite material of claim 10 , wherein the bi-metallic composite material is made by additive manufacturing.

13. The bi-metallic composite material of claim 10 , wherein the three-dimensional exterior portion comprises the first alloy composition consolidated into a fully dense state.

Assignees

• Nasa

Inventors

• Brice Craig A

Classifications

• B22F2998/10

  Processes characterised by the sequence of their steps · CPC title

• B22F7/02 Primary

  of composite layers {(B22F7/002 takes precedence)} · CPC title

• Y10T428/12042

  Porous component · CPC title

• Y02P10/25

  Process efficiency · CPC title

• B22F2003/248

  Thermal after-treatment · CPC title