Method for manufacturing superelastic beta titanium articles and the articles derived therefrom
Abstract
An article is manufactured from a composition comprising about 8 to about 10 wt % molybdenum, about 2.8 to about 6 wt % aluminum, up to about 2 wt % chromium, up to about 2 wt % vanadium, up to about 4 wt % niobium, with the balance being titanium, wherein the weight percents are based on the total weight of the alloy composition. An article is manufactured by a method comprising forming a shape from a composition comprising about 8 to about 10 wt % molybdenum, about 2.8 to about 6 wt % aluminum, up to about 2 wt % chromium, up to about 2 wt % vanadium, up to about 4 wt % niobium, with the balance being titanium, wherein the weight percents are based on the total weight of the alloy composition; cold working the shape; and heat treating the shape.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . An article manufactured from a composition comprising
about 8 to about 10 wt % molybdenum, about 2.8 to about 6 wt % aluminum, up to about 2 wt % chromium, up to about 2 wt % vanadium, up to about 4 wt % niobium, with the balance being titanium, wherein the weight percents are based on the total weight of the alloy composition.
2 . The article of claim 1 , wherein the composition is cold worked.
3 . The article of claim 2 , wherein the composition has an elastic recovery of greater than or equal to about 75% of the applied change in length, when the applied change in length is 2% of the original length.
4 . The article of claim 2 , wherein the composition has an elastic recovery of greater than or equal to about 50% of the applied change in length when the applied change in length is 4% of the original length.
5 . The article of claim 2 , wherein the composition has a reduction in the elastic modulus of greater than or equal to about 10% when compared with the elastic modulus of an equivalent heat treated composition.
6 . The article of claim 2 , wherein the composition has a reduction in the elastic modulus of greater than or equal to about 20% when compared with the elastic modulus of an equivalent heat treated composition.
7 . The article of claim 2 , wherein the composition has a reduction in the elastic modulus of greater than or equal to about 25% when compared with the elastic modulus of an equivalent heat treated composition.
8 . The article of claim 1 , wherein the composition has a β phase or an α phase and a β phase.
9 . The article of claim 1 , wherein the article is a medical device.
10 . The article of claim 1 , wherein the medical device is a stent or a guide wire.
11 . The article of claim 1 , wherein the medical device has a welded joint.
12 . The article of claim 1 , wherein the medical device has a weld.
13 . The article of claim 1 , wherein the article comprises an orthodontic arch wire, a dental implant, an orthopedic device or an eyewear frame.
14 . The article of claim 13 , wherein the orthopedic device is used in bone.
15 . The article of claim 1 , wherein the orthopedic device is used in the hip, knees, shoulder, elbows, or spine.
16 . The article of claim 1 , wherein the article comprises at least a portion of a golf club.
17 . The article of claim 14 , wherein the article is welded or brazed to the golf club.
18 . The article of claim 1 , wherein the article comprises a golf club head.
19 . The article of claim 1 , wherein the article comprises an insert for a golf club head.
20 . The article of claim 19 , wherein the insert is welded, brazed or mechanically inserted onto the golf club head.
21 . The article of claim 20 , wherein the insert is held in the golf club head by a tight toleranced fit.
22 . The article of claim 1 , wherein the article has a welded joint.
23 . The article of claim 1 , wherein the article has a brazed joint.
24 . The article of claim 1 , wherein the article further comprises a portion having linear elastic properties.
25 . The article of claim 1 , wherein the article further comprises a polymeric coating.
26 . An article manufactured from a composition comprising:
about 8.9 wt % molybdenum, about 3.03 wt % aluminum, about 1.95 wt % vanadium, about 3.86 wt % niobium, with the balance being titanium.
27 . The article of claim 26 , wherein the article is a medical device.
28 . The article of claim 26 , wherein the medical device is a stent, a catheter introducer, a dental implant, a guide wire, an orthodontic arch wire, an orthopedic device used in bones or tissue, or an eyewear frame.
29 . The article of claim 26 , wherein the article comprises at least a portion of a golf club.
30 . The article of claim 26 , wherein the article comprises a golf club head.
31 . The article of claim 26 , wherein the article comprises an insert for a golf club head and further wherein the insert is welded or brazed to the golf club head.
32 . The article of claim 26 , wherein the article has a welded joint.
33 . The article of claim 26 , wherein the article has a soldered joint.
34 . The article of claim 26 , wherein the article further comprises a portion having linear elastic properties.
35 . The article of claim 26 , wherein the article further comprises a portion having pseudoelastic or superelastic properties.
36 . The article of claim 26 , wherein the article further comprises a polymeric coating.
37 . An article manufactured from a composition comprising:
about 9.34 wt % molybdenum, about 3.01 wt % aluminum, about 1.95 wt % vanadium, about 3.79 wt % niobium, with the balance being titanium.
38 . The article of claim 37 , wherein the medical device is a stent, a guide wire, a dental implant, an orthodontic arch wire, an orthopedic device for bone and/or tissue, or an eyewear frame.
39 . An article manufactured by a method comprising:
forming a shape from a composition comprising about 8 to about 10 wt % molybdenum, about 2.8 to about 6 wt % aluminum, up to about 2 wt % chromium, up to about 2 wt % vanadium, up to about 4 wt % niobium, with the balance being titanium, wherein the weight percents are based on the total weight of the alloy composition; cold working the shape; and solution heat treating the shape.
40 . The method of claim 39 , wherein the solution heat treating is conducted at a temperature below the isomorphic temperature for the composition.
41 . The method of claim 39 , wherein the solution heat treating is conducted at a temperature above the isomorphic temperature for the composition.
42 . The method of claim 41 , wherein the shape is further cooled in air.
43 . The method of claim 39 , wherein the shape is further heat aged at a temperature of about 350 to about 550° C.
44 . The method of claim 39 , wherein the heat ageing is conducted for a time period of 10 seconds to about 30 minutes.
45 . An article manufactured by a method comprising:
cold working a wire having a composition comprising about 8 to about 10 wt % molybdenum, about 2.8 to about 6 wt % aluminum, up to about 2 wt % chromium, up to about 2 wt % vanadium, up to about 4 wt % niobium, with the balance being titanium, wherein the weight percents are based on the total weight of the alloy composition.
46 . The article of claim 45 , wherein the wire diameter is about 0.1 to about 10 millimeters.
47 . The article of claim 45 , wherein the article has a martensitic structure.
48 . The article of claim 45 , wherein the article has an elastic recovery of greater than or equal to about 75% of the applied change in length when the applied change in length is 2% of the original length.
49 . The article of claim 45 , wherein the article has an elastic recovery of greater than or equal to about 50% of the applied change in length when the applied change in length is 4% of the original length.
50 . The article of claim 45 , wherein the article is a medical device.
51 . The article of claim 45 , wherein the medical device is a stent, a dental implant, a guide wire, an orthodontic arch wire, an orthopedic device used in bone and/or tissue, or an eyewear frame.
52 . The article of claim 45 , wherein the article is used as a file or a drill in dental applications.
53 . The article of claim 45 , wherein the article comprises an insert for a golf club head and further wherein the insert is welded or brazed to the golf club head.Join the waitlist — get patent alerts
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