High hardness, high elasticity intermetallic compounds for mechanical components

Patent metadata

Field	Value
Publication number	US-10364483-B1
Application number	US-201414191708-A
Country	US
Kind code	B1
Filing date	Feb 27, 2014
Priority date	Mar 1, 2013
Publication date	Jul 30, 2019
Grant date	Jul 30, 2019

Abstract

One or more substitutional elements may be used to reduce the solution treatment temperature and required quench rates for hardening of 60-NITINOL. The advantages of modified NITINOL include that less energy is consumed during the heat treatment process, the material is subjected to less thermal distortion, and less machining is required. Modified NITINOL may have adequate hardness for bearing applications and may display highly elastic behavior.

First claim

The invention claimed is:

1. A material comprising:
54-57 atomic percent nickel (Ni);
0.1 up to and including 27 atomic percent of the sum of one or more elements from the group consisting of zirconium (Zr), hafnium (Hf), rutherfordium (Rf), lanthanum (La), and tantalum (Ta); and
a balance of the material being titanium (Ti) by atomic percent, wherein the material has a lower solvus temperature than that of 60-NITINOL, wherein the material possesses a hardness between 56 and 62 on the Rockwell C (HRC) hardness scale.

2. The material of claim 1 , wherein the material is formed without quench cracking.

3. The material of claim 1 , wherein the material has a hardness between 58 and 62 HRC.

4. The material of claim 1 , wherein the material exhibits highly elastic behavior with recoverable strains greater than 2%.

5. The material of claim 1 , wherein the material has a Youngs modulus of less than 110 gigapascals (GPa).

6. The material of claim 1 , wherein the material has a density of 6.5 g/cm 3 .

7. The material of claim 1 , wherein no water quenching is used to produce the material.

8. The material of claim 1 , wherein the material
comprises Hf from the one or more elements from the group consisting of Zr, Hf, Rf, La and Ta; and
includes a Ni—Ti parent phase and a secondary HfO 2 phase.

9. The material of claim 8 , wherein the material does not include a Ni 3 Ti phase.

Assignees

• Nasa
• The Us Administrator Of National Aeronautics And Space Administration

Inventors

• Stanford Malcolm K
• Noebe Ronald D
• Dellacorte Christopher
• Bigelow Glen
• Thomas Fransua

Classifications

• C22C19/007 Primary

  with a light metal (alkali metal Li, Na, K, Rb, Cs; earth alkali metal Be, Mg, Ca, Sr, Ba, Al Ga, Ge, Ti) or B, Si, Zr, Hf, Sc, Y, lanthanides, actinides, as the next major constituent · CPC title

• C22C19/03

  based on nickel · CPC title

• C22C14/00

  Alloys based on titanium · CPC title