IP Library Granted Patent US 10,844,464
Granted Patent B1
US 10,844,464 · App. 15/953,137 · Granted Nov 24, 2020

Niobium metal alloy

Inventors: Gavin J. Garside (Hawthorne, CA); Kevin A. Lohner (Hawthorne, CA); Meagan R. Slater (Hawthorne, CA); Charles Kuehmann (Hawthorne, CA); David R. Snyder (Evanston, IL); Jason T. Sebastian (Evanston, IL); Gregory B. Olson (Evanston, IL)
Assignee: Space Exploration Technologies Corp.
C22C27/02C22F1/18
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Quick Facts
Patent No.
US 10,844,464
App. No.
15/953,137
Granted
Nov 24, 2020
Kind
B1
Abstract

In one embodiment of the present disclosure, a niobium metal alloy composition includes: a vanadium content in the range of about 1.5 to about 12 weight percent; a hafnium content in the range of about 5 to about 13 weight percent; a titanium or zirconium content or a mixture of titanium and zirconium content in the range of about 0.25 to about 2.5 weight percent; and a niobium content as a balance of the alloy.

Claims (32)

1. A niobium metal alloy composition, comprising:

a vanadium content in the range of 5.75 to about 12 weight percent, a hafnium content in the range of about 5 to about 13 weight percent,

a titanium or zirconium content or a mixture of titanium and zirconium content in the range of about 0.25 to about 2.5 weight percent; and

a niobium content of about 77 to about 85 weight percent.

2. The niobium metal alloy composition of claim 1 , wherein the vanadium content is 6 to about 12 weight percent.

3. The niobium metal alloy composition of claim 1 , wherein the hafnium content is in a range selected from the group consisting of greater-than-5 to about 13 weight percent.

4. The niobium metal alloy composition of claim 2 , wherein the titanium or zirconium content or a mixture of titanium and zirconium content is in a range selected from the group consisting of about 0.5 to about 2.0 weight percent.

5. The niobium metal alloy composition of claim 4 , further comprising another alloying metal selected from the group consisting of tungsten, molybdenum, tantalum, rhenium, and combinations thereof.

6. The niobium metal alloy composition of claim 4 , wherein the alloy has a ductile-brittle transition temperature of less than −196° C. (−321° F.).

7. The niobium metal alloy composition of claim 4 , wherein the alloy has a specific yield strength at 2000° F. of greater than 90 ksi/lb/in 3 .

8. The niobium metal alloy composition of claim 4 , wherein the alloy has a specific yield strength at 2000° F. of greater than 100 ksi/lb/in 3 .

9. The niobium metal alloy composition of claim 1 , wherein

the vanadium content is 6 to about 9 weight percent;

the hafnium content is about 8 to about 13 weight percent; or

the titanium or zirconium content or a mixture of titanium and zirconium is about 0.7 to about 1.5 weight percent.

10. A niobium metal alloy composition, consisting of:

a vanadium content in the range of about 1.5 to about 12 weight percent;

a hafnium content in the range of about 5 to about 13 weight percent;

a titanium or zirconium content or a mixture of titanium and zirconium content in the range of about 0.25 to about 2.5 weight percent; and

a niobium content as a balance of the alloy.

11. The niobium metal alloy composition of claim 10 , wherein the niobium content is in a range selected from the group consisting of about 70 to about 90 weight percent.

12. The niobium metal alloy composition of claim 10 , wherein the vanadium content is in a range selected from the group consisting of about 2 to about 12 percent.

13. The niobium metal alloy composition of claim 10 , wherein the hafnium content is in a range selected from the group consisting of greater-than-5 to about 13 weight percent.

14. The niobium metal alloy composition of claim 10 , wherein the titanium or zirconium content or a mixture of titanium and zirconium content is in a range selected from the group consisting of about 0.5 to about 2.0 weight percent.

15. The niobium metal alloy composition of claim 10 , wherein the alloy has a ductile-brittle transition temperature of less than −196° C. (−321° F.).

16. The niobium metal alloy composition of claim 10 , wherein the alloy has a specific yield strength at 2000° F. of greater than 90 ksi/lb/in 3 .

17. The niobium metal alloy composition of claim 10 , wherein the alloy has a specific yield strength at 2000° F. of greater than 100 ksi/lb/in 3 .

18. A niobium metal alloy composition of claim 10 , wherein

the niobium content is about 77 to about 85 weight percent;

the vanadium content is about 5 to about 12 weight percent;

the hafnium content is about 8 to about 13 weight percent; or

the titanium or zirconium content or a mixture of titanium and zirconium content is about 0.7 to about 1.5 weight percent.

Assignments (8)
RELEASE OF SECURITY INTEREST Recorded Feb 14, 2025
From: BANK OF AMERICA, N.A.
To: SPACE EXPLORATION TECHNOLOGIES CORP.
Reel/Frame 070237/0157 →
RELEASE OF SECURITY INTEREST Recorded Feb 14, 2025
From: BANK OF AMERICA, N.A.
To: SPACE EXPLORATION TECHNOLOGIES CORP.
Reel/Frame 070225/0780 →
CERTIFICATE OF CONVERSION (STATE OF DELAWARE TO STATE OF TEXAS; NEW FILE NO.: 805421124 ; FILED: 02-14-2024) Recorded Feb 12, 2025
From: SPACE EXPLORATION TECHNOLOGIES CORP.
To: SPACE EXPLORATION TECHNOLOGIES CORP.
Reel/Frame 070203/0322 →
SECURITY INTEREST Recorded Feb 8, 2021
From: SPACE EXPLORATION TECHNOLOGIES CORP.
To: BANK OF AMERICA, N.A.
Reel/Frame 055184/0674 →
SECURITY AGREEMENT Recorded Feb 18, 2020
From: SPACE EXPLORATION TECHNOLOGIES CORP.
To: BANK OF AMERICA, N.A.
Reel/Frame 051952/0699 →
RELEASE OF SECURITY INTEREST Recorded Dec 18, 2019
From: BANK OF AMERICA, N.A. AS ADMINISTRATIVE AGENT
To: SPACE EXPLORATION TECHNOLOGIES CORP.
Reel/Frame 051322/0076 →
SECURITY AGREEMENT Recorded Nov 21, 2018
From: SPACE EXPLORATION TECHNOLOGIES CORP.
To: BANK OF AMERICA, N.A.
Reel/Frame 047618/0430 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 8, 2018
From: GARSIDE, GAVIN J.; LOHNER, KEVIN A.; SLATER, MEAGAN R.; KUEHMANN, CHARLES; SNYDER, DAVID R.; SEBASTIAN, JASON T.; OLSON, GREGORY B.
To: SPACE EXPLORATION TECHNOLOGIES CORP.
Reel/Frame 047455/0470 →
Continuity (1)
Provisional Application 62485919 · Apr 15, 2017