Functionally graded metal-metal composite structures

Patent metadata

Field	Value
Publication number	US-9764386-B2
Application number	US-201414463836-A
Country	US
Kind code	B2
Filing date	Aug 20, 2014
Priority date	Aug 23, 2013
Publication date	Sep 19, 2017
Grant date	Sep 19, 2017

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 method of creating a multiple alloy composite structure, comprising:
forming a three-dimensional open cell net structure of a first alloy composition, wherein the three-dimensional open cell net structure has a substantially open and continuous porosity defining voids;
followed by infusing the voids of the three-dimensional open cell net structure of the first alloy composition with at least a second alloy composition, wherein the second alloy composition comprises a shape memory alloy;
consolidating the three-dimensional open cell net structure into a fully dense solid structure, wherein a first shape of the second alloy composition is set for reversible transformation.

2. The method of claim 1 , wherein the three-dimensional open cell net structure has a periodic design.

3. The method of claim 1 , wherein infusing the three-dimensional open cell net structure of the first alloy composition with at least the second alloy composition comprises packing a powdered metal into the voids of the first alloy composition.

4. The method of claim 1 , wherein infusing the three-dimensional open cell net structure of the first alloy composition with at least a second alloy comprises causing a liquid metal to infiltrate the three-dimensional open cell net structure.

5. The method of claim 1 , wherein consolidating the three-dimensional arrangement into a fully dense structure is performed using hot isostatic pressing.

6. The method of claim 5 , wherein the hot isostatic pressing comprises:
subjecting the multiple alloy composite structure to a containment vessel; and
treating the multiple alloy composite structure for about four hours, wherein treating comprises:
heating the containment vessel to about 930° C.; and
applying an inert gas to the containment vessel at about 1,000 psi.

7. The method of claim 1 , wherein the second alloy composition comprises a nickel titanium alloy containing approximately equal atomic percentages of nickel and titanium.

8. The method of claim 1 , wherein the first alloy composition comprises at least one of titanium and aluminum.

9. A method of creating a multiple alloy composite structure, comprising:
forming a three-dimensional arrangement of a first alloy composition, wherein the three-dimensional arrangement has a substantially open and continuous porosity;
infusing the three-dimensional arrangement of the first alloy composition with at least a second alloy composition, wherein the second alloy composition comprises a shape memory alloy;
consolidating the three-dimensional arrangement into a fully dense solid structure, wherein a first shape of the second alloy composition is set for reversible transformation;
mechanically applying strain to the fully dense solid structure; and
treating the fully dense solid structure with heat such that the shape memory alloy composition becomes memory activated to recover the first shape,
wherein an interwoven composite of the first alloy composition and the memory-activated second alloy composition is formed.

10. The method of claim 9 , wherein forming the three-dimensional arrangement of the first alloy composition is performed using, additive manufacturing, and wherein mechanically applying strain to the fully dense solid structure comprises cold rolling.

11. The method of claim 10 , further comprising creating a five-sided box structure of the first alloy composition, wherein the box structure surrounds the three-dimensional arrangement of the first alloy composition.

12. The method of claim 11 , wherein the multiple alloy composite structure is configured to be used in structural components in order to reduce propagation of surface cracks in the structural components.

13. A method of creating a multiple alloy composite structure, comprising:
forming a three-dimensional arrangement of a first alloy composition, wherein the three-dimensional arrangement has a substantially open and continuous porosity;
infusing the three-dimensional arrangement of the first alloy composition with at least a second alloy composition, wherein at least one of the first alloy composition and the second alloy composition comprises a shape memory alloy;
consolidating the three-dimensional arrangement into a fully dense solid structure, wherein a first shape of the second alloy composition is sot for reversible transformation;
applying a first heat treatment comprising vacuum heat pressing;
trimming the multiple alloy composite structure to consistent dimensions using waterjet cutting; and
applying a separate shape setting heat treatment to the multiple alloy composite structure, wherein the separate shape setting heat treatment comprises heating the structure to about 500° C. for about 15 minutes.

Assignees

• The United States Of America Represented By The Administrator Of The Nat Aeronautics And Space Admin
• Nasa

Inventors

• Brice Craig A

Classifications

• Y10T428/12042

  Porous component · CPC title

• B22F2998/10

  Processes characterised by the sequence of their steps · CPC title

• B22F2003/248

  Thermal after-treatment · CPC title

• B22F7/02 Primary

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

• B22F2003/247

  Removing material: carving, cleaning, grinding, hobbing, honing, lapping, polishing, milling, shaving, skiving, turning the surface · CPC title