IP Library Granted Patent US 8,882,941
Granted Patent B2
US 8,882,941 · App. 12/580,858 · Granted Nov 11, 2014

Mechanism of structural formation for metallic glass based composites with enhanced ductility

Inventors: Daniel James Branagan (Idaho Falls, ID); Jeffrey E. Shield (Lincoln, NE); Alla V. Sergueeva (Idaho Falls, ID)
Assignee: The NanoSteel Company, Inc.
C22C45/02
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Quick Facts
Patent No.
US 8,882,941
App. No.
12/580,858
Granted
Nov 11, 2014
Kind
B2
Abstract

An aspect of the present disclosure relates to an alloy composition, which may include 52 atomic percent to 68 atomic percent iron, 13 to 21 atomic percent nickel, 2 to 12 atomic percent cobalt, 10 to 19 atomic percent boron, optionally 1 to 5 atomic percent carbon, and optionally 0.3 to 16 atomic percent silicon. The alloy may include 5 to 95% by volume of one or more spinodal microconstituents, wherein the microconstituents exhibit a length scale less than 50 nm in a glass matrix.

Claims (24)

1. A method of forming spinodal microconstituents in an alloy comprising:

melting alloy constituents including 52 atomic percent to 60 atomic percent iron, 15.5 to 21 atomic percent nickel, 6.3 to 11.6 atomic percent cobalt, 10.3 to 13.2 atomic percent boron, 3.7 to 4.8 atomic percent carbon, and 0.3 to 0.5 atomic percent silicon to form an alloy;

cooling said alloy; and

forming one or more spinodal microconstituents in a glass matrix through spinodal decomposition wherein said alloy separates into distinct regions with different chemical compositions and physical properties and is not nucleation controlled, wherein said spinodal microconstituents are present in the range of 5% to 95% by volume and said spinodal microconstituents exhibit a length scale less than 50 nm in a glass matrix.

2. A method of forming spinodal microconstituents in an alloy comprising:

melting alloy constituents including 58.4 atomic percent to 67.6 atomic percent iron, 16.0 to 16.6 atomic percent nickel, 2.9 to 3.1 atomic percent cobalt, 12.0 to 18.5 atomic percent boron, optionally 1.5 to 4.6 atomic percent carbon and optionally 0.4 to 3.5 atomic percent silicon, to form an alloys

cooling said alloy; and

forming one or more spinodal microconstituents in a glass matrix through spinodal decomposition wherein said alloy separates into distinct regions with different chemical compositions and physical properties and is not nucleation controlled, wherein said spinodal microconstituents are present in the range of 5% to 95% by volume and said spinodal microconstituents exhibit a length scale less than 50 nm in a glass matrix.

3. A method of forming spinodal microconstituents in an alloy comprising:

melting alloy constituents including 53.6 atomic percent to 60.9 atomic percent iron, 13.6 to 15.5 atomic percent nickel, 2.4 to 2.9 atomic percent cobalt, 12 to 14.1 atomic percent boron, 1 to 4 atomic percent carbon 3.9 to 15.4 atomic percent silicon, and 1.6 to 2.9 atomic percent chromium, to form an alloy;

cooling said alloy; and

forming one or more spinodal microconstituents in a glass matrix through spinodal decomposition wherein said alloy separates into distinct regions with different chemical compositions and physical properties and is not nucleation controlled, wherein said spinodal microconstituents are present in the range of 5% to 95% by volume and said spinodal microconstituents exhibit a length scale less than 50 nm in a glass matrix.

4. The method of claim 1 , wherein said alloy is cooled at a rate at or greater than the critical cooling rate of the alloy.

5. The method of claim 1 , wherein said alloy is cooled by melt spinning.

6. The method of claim 1 , wherein said alloy is formed into a ribbon.

7. The method of claim 1 , wherein said alloy is formed into a product having a thickness from 1 μm to 2000 μm.

8. The method of claim 2 , wherein said alloy is cooled at a rate at or greater than the critical cooling rate of the alloy.

9. The method of claim 2 , wherein said alloy is cooled by melt spinning.

10. The method of claim 2 , wherein said alloy is formed into a ribbon.

11. The method of claim 2 , wherein said alloy is formed into a product having a thickness from 1 μm to 2000 μm.

12. The method of claim 3 , wherein said alloy is cooled at a rate at or greater than the critical cooling rate of the alloy.

13. The method of claim 3 , wherein said alloy is cooled by melt spinning.

14. The method of claim 3 , wherein said alloy is formed into a ribbon.

15. The method of claim 3 , wherein said alloy is formed into a product having a thickness from 1 μm to 2000 μm.

Assignments (3)
SECURITY INTEREST Recorded Dec 3, 2018
From: THE NANOSTEEL COMPANY, INC.
To: HORIZON TECHNOLOGY FINANCE CORPORATION
Reel/Frame 047713/0163 →
SECURITY INTEREST Recorded Jun 11, 2015
From: THE NANOSTEEL COMPANY, INC.
To: HORIZON TECHNOLOGY FINANCE CORPORATION
Reel/Frame 035889/0122 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 8, 2010
From: BRANAGAN, DANIEL JAMES; SHIELDS, JEFFREY E.; SERGUEEVA, ALLA V.
To: THE NANOSTEEL COMPANY, INC.
Reel/Frame 024044/0352 →
Continuity (2)
Provisional Application 61107037 · Oct 21, 2008
Related Publication 20100154942A1 · Jun 24, 2010