Annealing of NiTi martensitic memory alloys and product produced thereby

• US 3,953,253 A
• Filed: 12/21/1973
• Issued: 04/27/1976
• Est. Priority Date: 12/21/1973
• Status: Expired due to Term

• Current Assignee: Texas Instruments, Inc.
• Original Assignee: Texas Instruments, Inc.
• Inventors: Clark, Joel P.
• Primary Examiner(s): Dean, R.
• Application Number:
  US05/427,164
• Time in Patent Office: 858 Days
• Field of Search: 148/13, 148/131, 148/133, 148/32, 148/11.5 R, 148/11.5 F, 148/2, 148/3, 75/170
• US Class Current: 148/563
• CPC Class Codes: C22F 1/006 Resulting in heat recoverable alloys with a memory effect

Abstract

A process for increasing the tensile strength of a martensitic alloy of titanium and nickel and for improving the alloy'"'"'s ability to retain its original properties during use by stabilizing it against progressive elongation when cycled through successive martensitic transformations. The process comprises maintaining the alloy under a tensile stress of between about 30,000 and 100,000 psi while annealing the alloy at a temperature above a first diffusional phase transformation temperature. The first diffusional phase temperature is the first temperature above the martensitic transformation range at which there is a negative slope in the electrical resistivity versus temperature curve for the alloy. The product of this process has a tensile strength of at least about 175,000 psi and a martensitic elongation activity under stress of at least about 2% and will survive over one million martensitic transformation cycles when placed under sufficient stress that the elongation activity is about 2%.

Claims

1. A process for increasing the tensile strength of a selected martensitic alloy of titanium and nickel and improving the alloy'"'"'s cyclic creep resistance by stabilizing it against progressive elongation when cycled through successive martensitic transformations, said alloy having a martensitic transformation temperature range and a first diffusional phase transformation temperature constituting the first temperature above said martensitic transformation range at which there is a negative slope in the electrical resistivity versus temperature curve for said alloy, said first diffusional phase transformation temperature being in the range from about 300°

to 500°

C., the process comprising maintaining said alloy under a tensile stress of between about 30,000 and 100,000 psi while heating the alloy at a temperature above said first diffusional phase transformation temperature to anneal said alloy for substantially increasing the tensile strength thereof.

2. A process as set forth in claim 1 wherein the annealing temperature is on the order of 50°

C. above said diffusional phase transformation temperature.

3. A process as set forth in claim 1 wherein said alloy contains between about 50 and about 58% by weight nickel and the balance is essentially titanium.

4. A process as set forth in claim 1 wherein said alloy is in the form of a wire and said wire is passed continuously through a hot zone where it is annealed while being maintained under said tensile stress.

5. A process as set forth in claim 4 wherein said wire is quenched as it leaves the hot zone.

6. A high strength martensitic alloy of nickel and titanium in annealed condition having a tensile strength greater than about 175,000 psi and a martensitic elongation activity of at least about 2.0% even under tension greater than 100,000 psi, said high strength alloy being resistant to fatigue for at least one million cycles through its martensitic transformation range when under sufficient stress that its elongation activity is about 2%, said high strength alloy being formed from a selected martensitic starting alloy of titanium and nickel having a martensitic transformation temperature range and a first diffusional phase transformation temperature constituting the first temperature above said martensitic transformation temperature range at which there is a negative slope in the electrical resistivity versus temperature curve for said starting alloy, said first diffusional phase transformation temperature for said starting alloy being in the range from about 300°

to 500°

C., said high strength alloy being formed by maintaining said starting alloy under a tensile stress of between about 30,000 and 100,000 psi while heating said starting alloy at a temperature above said first diffusional phase transformation temperature of said starting alloy to anneal said alloy for substantially increasing the tensile strength thereof.