Metastable beta-titanium alloys and methods of processing the same by direct aging

• US 8,568,540 B2
• Filed: 08/17/2010
• Issued: 10/29/2013
• Est. Priority Date: 05/21/2004
• Status: Active Grant

• Current Assignee: ATI Properties LLC (CNH Industrial N.V.)
• Original Assignee: ATI Properties Incorporated (Allegheny Technologies Incorporated)
• Inventors: Marquardt, Brian, Wood, John Randolph, Freese, Howard L., Jablokov, Victor R.
• Primary Examiner(s): Roe, Jessee
• Application Number:
  US12/857,789
• Publication Number:
  US 20100307647A1
• Time in Patent Office: 1,169 Days
• Field of Search: 148/671, 148/421
• US Class Current: 148/671
• CPC Class Codes: C22C 14/00 Alloys based on titanium
• CPC Class Codes: C22F 1/183 of titanium or alloys based thereon

Abstract

Metastable beta titanium alloys and methods of processing metastable β-titanium alloys are disclosed. For example, certain non-limiting embodiments relate to metastable β-titanium alloys, such as binary β-titanium alloys comprising greater than 10 weight percent molybdenum, having tensile strengths of at least 150 ksi and elongations of at least 12 percent. Other non-limiting embodiments relate to methods of processing metastable β-titanium alloys, and more specifically, methods of processing binary β-titanium alloys comprising greater than 10 weight percent molybdenum, wherein the method comprises hot working and direct aging the metastable β-titanium alloy at a temperature below the β-transus temperature of the metastable β-titanium alloy for a time sufficient to form α-phase precipitates in the metastable β-titanium alloy. Articles of manufacture comprising binary β-titanium alloys according to various non-limiting embodiments disclosed herein are also disclosed.

Claims

1. A method of processing a binary β

-titanium alloy, the method comprising;

hot working a binary β

-titanium alloy consisting essentially of titanium, from 14 weight percent to 16 weight percent molybdenum, and incidental impurities at a hot working temperature above the β

-transus temperature of the binary β

-titanium alloy; and

direct aging the binary β

-titanium alloy, wherein direct aging comprises heating the binary β

-titanium alloy in the hot worked condition at an aging temperature ranging from 850°

F. to 1375°

F. for a time sufficient to form α

-phase precipitates within the binary β

-titanium alloy.

2. The method of claim 1 wherein hot working the binary β

-titanium alloy comprises one of;

hot rolling the binary β

-titanium alloy and hot extruding the binary β

-titanium alloy.

3. The method of claim 1 wherein the binary β

-titanium alloy is hot worked to a percent reduction in area ranging from 95% to 99%.

4. The method of claim 1 wherein the aging temperature ranges from greater than 900°

F. up to 1200°

F.

5. The method of claim 1 wherein the aging temperature ranges from 925°

F. to 1150°

F.

6. The method of claim 1 wherein the aging temperature ranges from 950°

F. to 1100°

F.

7. The method of claim 1 wherein prior to hot working the binary β

-titanium alloy, the binary β

-titanium alloy is produced by a process comprising at least one of plasma arc cold hearth melting and vacuum arc remelting.

8. The method of claim 1 wherein after processing, the binary β

-titanium alloy has a tensile strength of at least 150 ksi.

9. The method of claim 1 wherein after processing, the binary β

-titanium alloy has a tensile strength of at least 170 ksi.

10. The method of claim 1 wherein after processing, the binary β

-titanium alloy has a tensile strength of at least 180 ksi.

11. The method of claim 1 wherein after processing, the binary β

-titanium alloy has an elongation of at least 12 percent.

12. The method of claim 1 wherein after processing, the binary β

-titanium alloy has an elongation of at least 15 percent.

13. The method of claim 1 wherein after processing, the binary β

-titanium alloy has an elongation of at least 20 percent.

14. The method of claim 1 wherein after processing, the binary β

-titanium alloy has a tensile strength of at least 150 ksi and an elongation of at least 12 percent.

15. A method of processing a metastable β

-titanium alloy, comprising;

hot working a metastable β

-titanium alloy consisting essentially of titanium, from 14 weight percent to 16 weight percent molybdenum, up to 0.05 weight percent nitrogen, up to 0.10 weight percent carbon, up to 0.015 weight percent hydrogen;

up to 0.10 weight percent iron, and up to 0.20 weight percent oxygen at a hot working temperature above the β

-transus temperature of the metastable β

-titanium alloy; and

direct aging the metastable β

-titanium alloy, wherein direct aging comprises heating the metastable β

-titanium alloy in the hot worked condition at a first aging temperature below the β

-transus temperature of the metastable titanium alloy for a time sufficient to form and at least partially coarsen at least one α

-phase precipitate within at least a portion of the metastable β

-titanium alloy.

16. The method of claim 15 further comprising heating the metastable β

-titanium alloy at a second aging temperature that is lower than the first aging temperature for a time sufficient to form at least one additional α

-phase precipitate within at least a portion of the metastable β

-titanium alloy.

17. The method of claim 15 wherein after processing, the metastable β

-titanium alloy has a tensile strength of at least 187 ksi and an elongation of at least 9percent.