US20020179197A1 - Titanium alloys having improved castability - Google Patents

Titanium alloys having improved castability Download PDF

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US20020179197A1
US20020179197A1 US10/179,310 US17931002A US2002179197A1 US 20020179197 A1 US20020179197 A1 US 20020179197A1 US 17931002 A US17931002 A US 17931002A US 2002179197 A1 US2002179197 A1 US 2002179197A1
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titanium alloy
castability
balance
titanium
alloy
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Jiin-Huey Lin
Chien-Ping Ju
Wen-Wei Cheng
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Cana Lab Corp
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Jiin-Huey Chern Lin
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Priority claimed from US09/548,266 external-priority patent/US6572815B1/en
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Priority to US10/179,310 priority Critical patent/US20020179197A1/en
Assigned to LIN, JIIN-HUEY CHERN, JU, CHIEN-PING reassignment LIN, JIIN-HUEY CHERN ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: CHEN, WEN-WEI, JU, CHIEN-PING, LIN, JIIN-HUEY
Publication of US20020179197A1 publication Critical patent/US20020179197A1/en
Priority to US10/750,755 priority patent/US20040136859A1/en
Assigned to CANA LAB CORPORATION reassignment CANA LAB CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: JU, CHIEN-PING, LIN, JIIN-HUEY CHERN
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium

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  • the present invention relates to a titanium alloy, and more particularly to a titanium alloy casting.
  • the present invention provides a method to improve the castability of a titanium alloy, so that it is more suitable for use in making a dental casting and a medical implant.
  • titanium and its alloys Due to its lightweight, high strength-to-weight ratio, low elastic modulus, superior chemical corrosion resistance, and excellent mechanical properties at high temperature up to 550° C., titanium and its alloys have been widely used on aerospace, chemical, sports, and marine industries. Their superior biocompatibility also makes them ideal as the primary materials used in dental and osteological restorations or implants, such as artificial bone pins, bone plates, shoulders, elbows, hips, knees and other joints, and dental orthopraxy lines.
  • the cast patterns include spiral wax molds, fibrous nylon lines produced by injection molding (Howard et al., JDR, 59, 824-830, 1985), saucer-like molds, cylindrical molds, rectangle sheets, nylon mesh, and taper molds (Mueller et al., J. of Prosth. Den., 69, 367, Abstr. 2072, 1993).
  • a wax mold of a simulated crown has also been designed (Bessing et al., Acta Odontology Scandinavian, 44, 165-172, 1986).
  • Titanium is inherently difficult to cast due to its high melting point and high reactivity. Its low density is another problem in casting. Therefore, the improvement of casting process is the main issue of titanium precision casting.
  • the casting machines used at present utilize argon as the protective atmosphere to prevent high temperature reactions. Induction or arc is used as the heat source in order to shorten melting time as well as lessen high temperature reactivity.
  • the titanium casting machines can be roughly divided into the centrifugal casting type, the vacuum-pressure type, and the centrifugal-vacuum pressure mixed type (Yoshiaki, Conference Paper, 1-7, Australia, 1995).
  • U.S. Pat. No. 2,797,996 discloses titanium base alloys of high strength and ductility, and also of contamination resistance and high strength at elevated temperatures, which contain as essentially constituents titanium and tin, together with one or more additional metals selected from the groups comprising alpha promoters, beta promoters and compound formers.
  • a large number of Ti—Sn base alloys were prepared in this patent, including ternary titanium alloys containing 1-5 wt % Bi.
  • U.S. Pat. No. 4,810,465 discloses a free-cutting Ti alloy.
  • the basic alloy composition of this free-cutting Ti alloy essentially consists of at least one of S: 0.001-10%, Se: 0.001-10% and Te: 0.001-10%; REM: 0.01-10%; and one or both of Ca: 0.001-10% and B: 0.005-5%; and the balance substantially Ti.
  • the Ti alloy includes one or more of Ti—S (Se, Te) compounds, Ca—S (Se, Te) compounds, REM-S (Se, Te) compounds and their complex compounds as inclusions to improve machinability. Some optional elements can be added to above basic composition.
  • U.S. Pat. No. 5,176,762 discloses an age hardenable beta titanium alloy having exceptional high temperature strength properties in combination with an essential lack of combustibility.
  • the alloy contains chromium, vanadium and titanium the nominal composition of the basic alloy being defined by three points on the ternary titanium-vanadium-chromium phase diagram: Ti—22V—13Cr, Ti—22V—36Cr, and Ti—40V—13% Cr.
  • the alloys of the invention are comprised of the beta phase under all the temperature conditions, have strengths much in excess of the prior art high strength alloys in combination with excellent creep properties, and are nonburning under conditions encountered in gas turbine engine compressor sections. Bismuth up to 1.5% was suggested in this age hardenable beta titanium alloy. However, there is no teaching as to the improvement of castability or reducing surface tension of pure titanium or a titanium alloy.
  • a primary object of the present invention is to provide a method of improving castability of a titanium alloy.
  • Another object of the present invention is to provide a titanium alloy having improved castability.
  • the titanium alloy having improved castability prepared in accordance with the method of the present application consists essentially of 0.1-5 wt % of bismuth, one or more addition metals and the balance Ti, provided that the titanium alloy having improved castability is not a ternary Ti alloy consisting essentially of 5-10 wt % Sn, 1-5 wt % Bi and the balance Ti.
  • the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 6-9 wt % Mo and the balance Ti.
  • the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 6-9 wt % Mo, about 0.1-6 wt % Fe and the balance Ti.
  • the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 14-16 wt % Mo and the balance Ti.
  • the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 10-13 wt % Mo, about 5-7 wt % Zr, about 0.5-3 wt % Fe and the balance Ti.
  • the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 12-14 wt % Nb, about 12-14 wt % Zr and the balance Ti.
  • the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 4-6 wt % Al, about 2-4 wt % Fe and the balance Ti.
  • the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, 5-7 wt % Al, about 6-8 wt % Nb and the balance Ti.
  • the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 6-9 wt % Mo, about 6-9 wt % Hf, about 1 wt % of Fe and the balance Ti.
  • the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 5-7 wt % Al, about 3-5 wt % V and the balance Ti.
  • the titanium alloy having improved castability contains 0.5-3 wt %, more preferably about 1 wt %, of bismuth.
  • FIG. 1 is a schematic drawing showing the copper mold used for the castability test in the present invention
  • FIG. 2 shows the effect on castability by doping 1 wt %, 3 wt % and 5 wt % of bismuth to commercially pure titanium (c.p. Ti) and a Ti alloy containing 7.5 wt % Mo and the balance Ti (Ti—7.5Mo) according to the present invention;
  • FIG. 3 shows the effect on castability by doping 1 wt %, 3 wt % and 5 wt % of bismuth to a Ti alloy containing 6 wt % Al, 4 wt % V and the balance Ti (Ti6Al4V) according to the present invention
  • FIG. 4 shows the effect on castability by doping 1 wt % of bismuth to various titanium alloys according to the present invention, wherein the numerals before the elements in the Ti alloys represent the weight percentage thereof.
  • the present invention provides a method of improving castability of a titanium alloy comprising doping said titanium alloy with 0.1-5 wt %, preferably 0.5-3 wt %, of bismuth, based on the weight of bismuth and said titanium alloy.
  • said titanium alloy comprises about 6-9 wt % Mo and the balance Ti.
  • said titanium alloy comprises about 6-9 wt % Mo, about 0.1-6 wt % Fe and the balance Ti.
  • said titanium alloy comprises about 14-16 wt % Mo and the balance Ti.
  • said titanium alloy comprises about 10-13 wt % Mo, about 5-7 wt % Zr, about 0.5-3 wt % Fe and the balance Ti.
  • said titanium alloy comprises about 12-14 wt % Nb, about 12-14 wt % Zr and the balance Ti.
  • said titanium alloy comprises about 4-6 wt % Al, about 2-4 wt % Fe and the balance Ti.
  • said titanium alloy comprises about 5-7 wt % Al, about 6-8 wt % Nb and the balance Ti.
  • said titanium alloy comprises about 6-9 wt % Mo, about 6-9 wt % Hf, about 1 wt % of Fe and the balance Ti.
  • said titanium alloy comprises about 5-7 wt % Al, about 3-5 wt % V and the balance Ti.
  • said titanium alloy is for making a dental casting.
  • said titanium alloy is for making a medical implant.
  • the ingot Prior to casting, the ingot was re-melted again in an open-based copper hearth under an argon pressure of 1.8 kgf/cm 2 .
  • the molten alloy instantly dropped from the open-based copper hearth into a copper mold located in a second chamber at room temperature via a pouring gate because of the pressure difference between the two chambers.
  • the pouring gate 20 has an inlet of 20 mm diameter and an outlet of 10 mm diameter, and a thickness of 18 mm between the inlet and the outlet.
  • the copper mold 10 has two parallel needle-shaped cavities of 1 mm ⁇ 53 mm (diameter ⁇ length).
  • Cast lengths (a measure of castability) of undoped and Bi-doped c.p. Ti as well as Ti—7.5Mo alloy are compared in FIG. 2. As shown in the figure, when 1 or 3 wt % Bi was doped in c.p. Ti, the cast length increased by about 12%. When 5 wt % Bi was added, however, the castability value declined. This “up and down” phenomenon was observed in a more dramatic way in Ti—7.5Mo system. When 1 wt % Bi was doped in Ti—7.5Mo alloy, the cast length largely increased by 34%. Again, when larger amounts of bismuth were added, the castability values decreased.
  • Example 2 The procedures in Example 1 were repeated except that a commercially available Ti—6Al—4V alloy (Titanium Industries, Parsippany, N.J., USA) was used to replace c.p. Ti and Mo metals. The results are shown in FIG. 3.
  • a commercially available Ti—6Al—4V alloy Ti—6Al—4V alloy (Titanium Industries, Parsippany, N.J., USA) was used to replace c.p. Ti and Mo metals. The results are shown in FIG. 3.
  • Example 1 The procedures in Example 1 were repeated except that commercially available alloys TMZF (12 wt % of Mo, 6 wt % of Zr, 2 wt % of Fe, and the balance Ti) (Titanium Industries, Parsippany, N.J., USA), Ti13Nb13Zr (13 wt % of Nb, 13 wt % of Zr and the balance Ti) (Titanium Industries, Parsippany, N.J., USA), Ti5Al2.5Fe (5 wt % of Al, 2.5 wt % of Fe and the balance Ti) (Titanium Industries, Parsippany, N.J., USA), Ti6Al7Nb (6 wt % of Al, 7 wt % of Nb and the balance Ti) (Titanium Industries, Parsippany, N.J., USA), and Ti7Mo7Hf1Fe (7 wt % of Mo, 7 wt % of Hf

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Dental Prosthetics (AREA)

Abstract

In order to improve castability of a titanium alloy, 0.1-5 wt %, preferably 0.5-3 wt %, of bismuth is doped, based on the weight of bismuth and the titanium alloy. The titanium alloy is for making a dental casting or a medical implant.

Description

    CROSS-REFERENCE TO RELATED APPLICATION
  • The present application is a continuation-in-part application of U.S. patent application Ser. No. 09/548,266, filed Apr. 12, 2000. The above-listed application Ser. No. 09/548,266 is commonly assigned with the present invention and the entire content of which is incorporated herein by reference.[0001]
  • FIELD OF THE INVENTION
  • The present invention relates to a titanium alloy, and more particularly to a titanium alloy casting. The present invention provides a method to improve the castability of a titanium alloy, so that it is more suitable for use in making a dental casting and a medical implant. [0002]
  • BACKGROUND OF THE INVENTION
  • Due to its lightweight, high strength-to-weight ratio, low elastic modulus, superior chemical corrosion resistance, and excellent mechanical properties at high temperature up to 550° C., titanium and its alloys have been widely used on aerospace, chemical, sports, and marine industries. Their superior biocompatibility also makes them ideal as the primary materials used in dental and osteological restorations or implants, such as artificial bone pins, bone plates, shoulders, elbows, hips, knees and other joints, and dental orthopraxy lines. [0003]
  • A number of methods for fabricating titanium and its alloys with a desired shape have been developed. Among these, precision casting is the most difficult. Precision casting has the advantage that the cast produced has a near net shape, which greatly decreases the titanium fabrication cost. Also, precision casting is particularly suitable for producing objects with a small volume, high size accuracy, and complicated shape, for example in dental and osteological fields. Moreover, titanium and its alloys could even be utilized in many other everyday products, if the difficulty in precision casting could be solved. [0004]
  • There are many factors that affect the process of the precision casting and the properties of castings. According to the research results issued by Luk et al., in Dent. Mater., 8, 89-99, 1992, the factors include alloy composition, alloy density, alloy surface tension, casting temperature, investment material type, mold temperature, casting machine type, casting surface area/volume ratio, and pouring angle. The castability test is the most frequently used method for assessing various titanium precision casting processes. Castability is the ability of a molten alloy to completely fill a mold space. Castability is a combination factor, and there is no international standard for assessing it today. Since castability is affected by many factors, researchers have designed various test methods in accordance with various cast patterns for assessing the castability. The cast patterns include spiral wax molds, fibrous nylon lines produced by injection molding (Howard et al., JDR, 59, 824-830, 1985), saucer-like molds, cylindrical molds, rectangle sheets, nylon mesh, and taper molds (Mueller et al., J. of Prosth. Den., 69, 367, Abstr. 2072, 1993). A wax mold of a simulated crown has also been designed (Bessing et al., Acta Odontology Scandinavian, 44, 165-172, 1986). [0005]
  • Titanium is inherently difficult to cast due to its high melting point and high reactivity. Its low density is another problem in casting. Therefore, the improvement of casting process is the main issue of titanium precision casting. The casting machines used at present utilize argon as the protective atmosphere to prevent high temperature reactions. Induction or arc is used as the heat source in order to shorten melting time as well as lessen high temperature reactivity. At present, in order to increase the pouring force and to avoid casting defect caused by poor flowability of the molten metal, the titanium casting machines can be roughly divided into the centrifugal casting type, the vacuum-pressure type, and the centrifugal-vacuum pressure mixed type (Yoshiaki, Conference Paper, 1-7, Australia, 1995). [0006]
  • In U.S. patent application Ser. No. 09/548,266, filed Apr. 12, 2000, the inventors of this application first disclose a technique to improve the castability of pure titanium by doping an alloying metal in an amount of 0.01 to 3 wt %, preferably 0.5 to 3 wt %, and more preferably about 1 wt %. Among various alloying metals used in this application bismuth is found the most promising element. [0007]
  • U.S. Pat. No. 2,797,996 discloses titanium base alloys of high strength and ductility, and also of contamination resistance and high strength at elevated temperatures, which contain as essentially constituents titanium and tin, together with one or more additional metals selected from the groups comprising alpha promoters, beta promoters and compound formers. A large number of Ti—Sn base alloys were prepared in this patent, including ternary titanium alloys containing 1-5 wt % Bi. However, there is no teaching as to the improvement of castability or reducing surface tension of pure titanium or a titanium alloy. [0008]
  • U.S. Pat. No. 4,810,465 discloses a free-cutting Ti alloy. The basic alloy composition of this free-cutting Ti alloy essentially consists of at least one of S: 0.001-10%, Se: 0.001-10% and Te: 0.001-10%; REM: 0.01-10%; and one or both of Ca: 0.001-10% and B: 0.005-5%; and the balance substantially Ti. The Ti alloy includes one or more of Ti—S (Se, Te) compounds, Ca—S (Se, Te) compounds, REM-S (Se, Te) compounds and their complex compounds as inclusions to improve machinability. Some optional elements can be added to above basic composition. Also disclosed are methods of producing the above free-cutting Ti alloy and a specific Ti alloy which is a particularly suitable material for connecting rods. Bismuth up to 10% was suggested in this free-cutting Ti alloy. However, there is no teaching as to the improvement of castability or reducing surface tension of pure titanium or a titanium alloy. [0009]
  • U.S. Pat. No. 5,176,762 discloses an age hardenable beta titanium alloy having exceptional high temperature strength properties in combination with an essential lack of combustibility. In its basic form the alloy contains chromium, vanadium and titanium the nominal composition of the basic alloy being defined by three points on the ternary titanium-vanadium-chromium phase diagram: Ti—22V—13Cr, Ti—22V—36Cr, and Ti—40V—13% Cr. The alloys of the invention are comprised of the beta phase under all the temperature conditions, have strengths much in excess of the prior art high strength alloys in combination with excellent creep properties, and are nonburning under conditions encountered in gas turbine engine compressor sections. Bismuth up to 1.5% was suggested in this age hardenable beta titanium alloy. However, there is no teaching as to the improvement of castability or reducing surface tension of pure titanium or a titanium alloy. [0010]
  • SUMMARY OF THE INVENTION
  • A primary object of the present invention is to provide a method of improving castability of a titanium alloy. [0011]
  • Another object of the present invention is to provide a titanium alloy having improved castability. [0012]
  • The titanium alloy having improved castability prepared in accordance with the method of the present application consists essentially of 0.1-5 wt % of bismuth, one or more addition metals and the balance Ti, provided that the titanium alloy having improved castability is not a ternary Ti alloy consisting essentially of 5-10 wt % Sn, 1-5 wt % Bi and the balance Ti. [0013]
  • Preferably, the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 6-9 wt % Mo and the balance Ti. [0014]
  • Preferably, the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 6-9 wt % Mo, about 0.1-6 wt % Fe and the balance Ti. [0015]
  • Preferably, the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 14-16 wt % Mo and the balance Ti. [0016]
  • Preferably, the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 10-13 wt % Mo, about 5-7 wt % Zr, about 0.5-3 wt % Fe and the balance Ti. [0017]
  • Preferably, the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 12-14 wt % Nb, about 12-14 wt % Zr and the balance Ti. [0018]
  • Preferably, the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 4-6 wt % Al, about 2-4 wt % Fe and the balance Ti. [0019]
  • Preferably, the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, 5-7 wt % Al, about 6-8 wt % Nb and the balance Ti. [0020]
  • Preferably, the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 6-9 wt % Mo, about 6-9 wt % Hf, about 1 wt % of Fe and the balance Ti. [0021]
  • Preferably, the titanium alloy having improved castability consists essentially of 0.1-5 wt % of bismuth, about 5-7 wt % Al, about 3-5 wt % V and the balance Ti. [0022]
  • Preferably, the titanium alloy having improved castability contains 0.5-3 wt %, more preferably about 1 wt %, of bismuth.[0023]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The present invention will be described in detail with reference to the illustrated embodiments and the accompany drawings, in which: [0024]
  • FIG. 1 is a schematic drawing showing the copper mold used for the castability test in the present invention; [0025]
  • FIG. 2 shows the effect on castability by doping 1 wt %, 3 wt % and 5 wt % of bismuth to commercially pure titanium (c.p. Ti) and a Ti alloy containing 7.5 wt % Mo and the balance Ti (Ti—7.5Mo) according to the present invention; [0026]
  • FIG. 3 shows the effect on castability by doping 1 wt %, 3 wt % and 5 wt % of bismuth to a Ti alloy containing 6 wt % Al, 4 wt % V and the balance Ti (Ti6Al4V) according to the present invention; and [0027]
  • FIG. 4 shows the effect on castability by doping 1 wt % of bismuth to various titanium alloys according to the present invention, wherein the numerals before the elements in the Ti alloys represent the weight percentage thereof.[0028]
  • DETAILED DESCRIPTION OF THE INVENTION
  • The present invention provides a method of improving castability of a titanium alloy comprising doping said titanium alloy with 0.1-5 wt %, preferably 0.5-3 wt %, of bismuth, based on the weight of bismuth and said titanium alloy. [0029]
  • Preferably, said titanium alloy comprises about 6-9 wt % Mo and the balance Ti. [0030]
  • Preferably, said titanium alloy comprises about 6-9 wt % Mo, about 0.1-6 wt % Fe and the balance Ti. [0031]
  • Preferably, said titanium alloy comprises about 14-16 wt % Mo and the balance Ti. [0032]
  • Preferably, said titanium alloy comprises about 10-13 wt % Mo, about 5-7 wt % Zr, about 0.5-3 wt % Fe and the balance Ti. [0033]
  • Preferably, said titanium alloy comprises about 12-14 wt % Nb, about 12-14 wt % Zr and the balance Ti. [0034]
  • Preferably, said titanium alloy comprises about 4-6 wt % Al, about 2-4 wt % Fe and the balance Ti. [0035]
  • Preferably, said titanium alloy comprises about 5-7 wt % Al, about 6-8 wt % Nb and the balance Ti. [0036]
  • Preferably, said titanium alloy comprises about 6-9 wt % Mo, about 6-9 wt % Hf, about 1 wt % of Fe and the balance Ti. [0037]
  • Preferably, said titanium alloy comprises about 5-7 wt % Al, about 3-5 wt % V and the balance Ti. [0038]
  • Preferably, said titanium alloy is for making a dental casting. [0039]
  • Preferably, said titanium alloy is for making a medical implant. [0040]
  • EXAMPLE 1
  • c.p. Ti and Ti—Mo Alloys Doped with 1 wt %, 3 wt % and 5 wt % of Bi [0041]
  • In this example 0, 1, 3 and 5 wt % of bismuth of 99.5% in purity were melted into a grade II commercially pure titanium (c.p. Ti) and Ti—7.5Mo alloy containing 7.5 wt % of Mo and the balance Ti by using a commercial arc-melting vacuum/pressure type casting system (Castmatic, Iwatani Corp., Japan). Appropriate amounts of c.p. Ti, molybdenum and bismuth were melted in a U-shaped copper hearth with a tungsten electrode. The melting chamber was first evacuated and purged with argon. An argon pressure of 1.8 kgf/cm[0042] 2 was maintained during melting. After solidification/cooling in the same chamber in argon atmosphere, the thin oxidized layer of the ingot was removed by grinding and the ground surface was ultrasonically cleaned in alcohol. The ingot was re-melted three times to improve chemical homogeneity.
  • Prior to casting, the ingot was re-melted again in an open-based copper hearth under an argon pressure of 1.8 kgf/cm[0043] 2. The molten alloy instantly dropped from the open-based copper hearth into a copper mold located in a second chamber at room temperature via a pouring gate because of the pressure difference between the two chambers. As shown in FIG. 1, the pouring gate 20 has an inlet of 20 mm diameter and an outlet of 10 mm diameter, and a thickness of 18 mm between the inlet and the outlet. The copper mold 10 has two parallel needle-shaped cavities of 1 mm×53 mm (diameter×length).
  • Cast lengths (a measure of castability) of undoped and Bi-doped c.p. Ti as well as Ti—7.5Mo alloy are compared in FIG. 2. As shown in the figure, when 1 or 3 wt % Bi was doped in c.p. Ti, the cast length increased by about 12%. When 5 wt % Bi was added, however, the castability value declined. This “up and down” phenomenon was observed in a more dramatic way in Ti—7.5Mo system. When 1 wt % Bi was doped in Ti—7.5Mo alloy, the cast length largely increased by 34%. Again, when larger amounts of bismuth were added, the castability values decreased. [0044]
  • According to the theory of Ragone et al. [RAGONE, D. V. ADAMS, C. M., and TAYLOR, H. F. (1956) [0045] Some Factors Affecting Fluidity of Metals. AFS Trans., 64, 640.], addition of an alloy element to a pure metal always lowers the fluidity (increasing viscosity) of the metal due to the formation of dendrites that causes resistance to fluid flow at the early stage of solidification. This factor might satisfactorily explain why the castability value decreased when a relatively large amount (3 or 5 wt %) of bismuth was added. However, the dendrite factor could not explain the increase in castability when only 1 wt % Bi was added.
  • EXAMPLE 2
  • Ti6Al4V Alloy Doped with 1 wt %, 3 wt % and 5 wt % of Bi [0046]
  • The procedures in Example 1 were repeated except that a commercially available Ti—6Al—4V alloy (Titanium Industries, Parsippany, N.J., USA) was used to replace c.p. Ti and Mo metals. The results are shown in FIG. 3. [0047]
  • From the measurement of casting lengths (a measure of castability, FIG. 3), it is interesting to note that the castability of Ti—6Al—4V alloy could be largely enhanced by almost 30% by the addition of 1 wt % Bi in the alloy, compared to that of undoped one. When a larger amount (3 or 5 wt %) of bismuth was added, however, the castability value of Ti—6Al—4V was not improved. [0048]
  • EXAMPLE 3
  • Castability of Some Commercial Ti Alloys with 1 wt % Bi Doped and without Bi Doped [0049]
  • The procedures for preparing the doped and undoped Ti—7.5Mo alloys in Example 1 were repeated to prepare Ti7.5Mo—Fe alloys with 1 wt % Bi doped and without Bi doped except that an additional metal Fe was added in an amount of 1, 3 and 5 wt %, separately. [0050]
  • The procedures for preparing the doped and undoped Ti—7.5Mo alloys in Example 1 were repeated to prepare Ti15Mo alloy with 1 wt % Bi doped and without Bi doped except that the amount of Mo added was 15 wt %. [0051]
  • The procedures in Example 1 were repeated except that commercially available alloys TMZF (12 wt % of Mo, 6 wt % of Zr, 2 wt % of Fe, and the balance Ti) (Titanium Industries, Parsippany, N.J., USA), Ti13Nb13Zr (13 wt % of Nb, 13 wt % of Zr and the balance Ti) (Titanium Industries, Parsippany, N.J., USA), Ti5Al2.5Fe (5 wt % of Al, 2.5 wt % of Fe and the balance Ti) (Titanium Industries, Parsippany, N.J., USA), Ti6Al7Nb (6 wt % of Al, 7 wt % of Nb and the balance Ti) (Titanium Industries, Parsippany, N.J., USA), and Ti7Mo7Hf1Fe (7 wt % of Mo, 7 wt % of Hf, 1 wt % of Fe and the balance Ti) (Titanium Industries, Parsippany, N.J., USA) were used to replace c.p. Ti and Mo metals. The results are shown in FIG. 4 together with the 1 wt % Bi doped and undoped c.p. Ti, Ti7.5Mo, Ti6Al4V alloys prepared in Examples 1 and 2. [0052]
  • From the measurement of casting lengths (a measure of castability, FIG. 4), it can be seen that the castability of Ti alloys enhanced by the addition of 1 wt % Bi in the alloy ranges from about 17% (Ti5Al2.5Fe) to about 115% (Ti7.5Mo5Fe), compared to that of undoped one, while the castability improvement for c.p. Ti by the addition of 1 wt % Bi is only about 12%. [0053]

Claims (13)

What is claimed is:
1. A method of improving castability of a titanium alloy comprising doping said titanium alloy with 0.1-5 wt % of bismuth, based on the weight of bismuth and said titanium alloy.
2. The method according to claim 1, wherein 0.5-3 wt % of bismuth is doped, based on the weight of the bismuth and said titanium alloy.
3. The method according to claim 2, wherein said titanium alloy comprises about 6-9 wt % Mo and the balance Ti.
4. The method according to claim 2, wherein said titanium alloy comprises about 6-9 wt % Mo, about 0.1-6 wt % Fe and the balance Ti.
5. The method according to claim 2, wherein said titanium alloy comprises about 14-16 wt % Mo and the balance Ti.
6. The method according to claim 2, wherein said titanium alloy comprises about 10-13 wt % Mo, about 5-7 wt % Zr, about 0.5-3 wt % Fe and the balance Ti.
7. The method according to claim 2, wherein said titanium alloy comprises about 12-14 wt % Nb, about 12-14 wt % Zr and the balance Ti.
8. The method according to claim 2, wherein said titanium alloy comprises about 4-6 wt % Al, about 2-4 wt % Fe and the balance Ti.
9. The method according to claim 2, wherein said titanium alloy comprises about 5-7 wt % Al, about 6-8 wt % Nb, about 1 wt % of Fe and the balance Ti.
10. The method according to claim 2, wherein said titanium alloy comprises about 6-9 wt % Mo, about 6-9 wt % Hf and the balance Ti.
11. The method according to claim 2, wherein said titanium alloy comprises about 5-7 wt % Al, about 3-5 wt % V and the balance Ti.
12. The method according to claim 2, wherein said titanium alloy is for making a dental casting.
13. The method according to claim 2, wherein said titanium alloy is for making a medical implant.
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US20060225818A1 (en) * 2005-03-08 2006-10-12 Waldemar Link Gmbh & Co. Kg Process for casting a beta-titanium alloy
US20060235536A1 (en) * 2005-03-08 2006-10-19 Waldemar Link Gmbh & Co. Kg Joint prosthesis made from a titanium alloy
US20070068647A1 (en) * 2005-03-08 2007-03-29 Waldemar Link Gmbh & Co. Kg Process for producing an implant from a titanium alloy, and corresponding implant
US20070125124A1 (en) * 2005-11-23 2007-06-07 David South Sizable titanium ring and method of making same

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US5954724A (en) * 1997-03-27 1999-09-21 Davidson; James A. Titanium molybdenum hafnium alloys for medical implants and devices

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* Cited by examiner, † Cited by third party
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US20060225818A1 (en) * 2005-03-08 2006-10-12 Waldemar Link Gmbh & Co. Kg Process for casting a beta-titanium alloy
US20060235536A1 (en) * 2005-03-08 2006-10-19 Waldemar Link Gmbh & Co. Kg Joint prosthesis made from a titanium alloy
US20070068647A1 (en) * 2005-03-08 2007-03-29 Waldemar Link Gmbh & Co. Kg Process for producing an implant from a titanium alloy, and corresponding implant
US7802611B2 (en) 2005-03-08 2010-09-28 Waldemar Link Gmbh & Co., Kg Process for producing an implant from a titanium alloy, and corresponding implant
US9675730B2 (en) * 2005-03-08 2017-06-13 Waldemar Link Gmbh & Co. Kg Joint prosthesis made from a titanium alloy
US20070125124A1 (en) * 2005-11-23 2007-06-07 David South Sizable titanium ring and method of making same

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