CN1570168A - High-intensity low modulus biological and medical use titanium alloy - Google Patents

High-intensity low modulus biological and medical use titanium alloy Download PDF

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Publication number
CN1570168A
CN1570168A CN 200410020501 CN200410020501A CN1570168A CN 1570168 A CN1570168 A CN 1570168A CN 200410020501 CN200410020501 CN 200410020501 CN 200410020501 A CN200410020501 A CN 200410020501A CN 1570168 A CN1570168 A CN 1570168A
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Prior art keywords
alloy
titanium
kilograms
temperature
titanium alloy
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CN 200410020501
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CN1323181C (en
Inventor
蒋志
兰羽
李海涛
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DALIAN SUNNY TITANIUM INDUSTRY Co Ltd
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DALIAN SUNNY TITANIUM INDUSTRY Co Ltd
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Abstract

The invention discloses an alloy, especially a high-strength low-modulus bio-medical titanium alloy. The alloy is characterized in that the alloy consists of Ti, Nb, and Zr, wherein the content of the components is as follows (by weight): Nb:31-34%, Zr:6-9%, Ti: the rest. Compared to conventional technology, the alloy provided by the invention has the following advantages: 1. good biocompatibility; 2. high alloy strength(-1050MPa); 3. elastic modulus 25-30% less than Ti#-[6]Al#-[4]V; 4. excellent fatigue strength and fracture toughness; 5. good technological formability.

Description

A kind of high-strength low-modulus bio-medical titanium
Technical field:
The present invention relates to a kind of alloy material, particularly a kind of high-strength low-modulus bio-medical titanium.
Background technology:
Most widely used clinically at present general surgery is metal material embedded to mainly contain three kinds of stainless steels, cobalt base alloy, titanium alloy.Titanium alloy is as emerging metallic substance, advantages such as, solidity to corrosion strong, good biocompatibility with its height ratio, and it is powerful to substitute the demand growth of implanting product as the human body hard tissue reparation.But the titanium alloy kind that can provide for medical circle seldom at present, what the use of prison bed was maximum is to transplant the Ti6Al4V alloy of coming from aircraft industry, this alloy is owing to contain vanadium metal, its toxicity is generally acknowledged by medical circle, the technological forming of this alloy is bad in addition, brings difficulty for the moulding, mechanical workout etc. of the press working of material and product.
Summary of the invention:
The purpose of this invention is to provide a kind of nontoxic, high and low modulus of intensity, anti-corrosion, good biocompatibility, easy a kind of high-strength low-modulus bio-medical titanium of machine-shaping, overcome the deficiencies in the prior art.
Technical solution of the present invention is: a kind of high-strength low-modulus bio-medical titanium is characterized in that: it is made up of titanium (Ti), niobium (Nb), zirconium (Zr), and each set of dispense is such as following:
The title weight percent
Niobium (Nb) (31~34) %
Zirconium (Zr) (6~9) %
Titanium (Ti) surplus.
Described each set of dispense ratio can be:
The title weight percent
Niobium (Nb) (32~33) %
Zirconium (Zr) (7~8) %
Titanium (Ti) surplus.
The present invention compared with prior art has following advantage: 1, do not contain the toxicity constituent element, biocompatibility is good; 2, the alloy strength height (~1050Mpa) and can in a big way, adjust to satisfy the needs of dissimilar products; 3, modular ratio Ti6Al4V alloy low (25~30) %; 4, fatigue strength and fracture toughness property all are better than the Ti6Al4V alloy; 5, technological forming is good, and unit elongation exceeds 20% than Ti6Al4V alloy, and rate of compression exceeds 30% than Ti6Al4V alloy, hot processing temperature low (100 ℃~150 ℃).
Alloy bar material mechanical property of the present invention and with the comparison of existing alloy
Embodiment:
Embodiment 1: with titanium sponge, zirconium sponge, niobium titanium master alloy is the preparation of raw material alloy material, and the designing quality of each component is respectively: 60 kilograms of titaniums (Ti), 33 kilograms of niobiums (Nb), 7 kilograms of zirconiums (Zr).Become ingot casting through the secondary vacuum arc melting behind the compacting electrode, cogging under the temperature of (900~1050) ℃, be processed into bar or sheet material under the temperature of (800~900) ℃, total deformation is controlled between (65~95) %, and thermal treatment temp is (500~800) ℃.Above-mentioned complete processing gets final product by the method for prior art.
Embodiment 2:
With titanium sponge, zirconium sponge, niobium titanium master alloy is the preparation of raw material alloy material, and the designing quality of each component is respectively: 57 kilograms of titaniums (Ti), 34 kilograms of niobiums (Nb), 9 kilograms of zirconiums (Zr).Become ingot casting through the secondary vacuum arc melting, cogging under the temperature of (900~1050) ℃ is processed into bar or sheet material under the temperature of (800~900) ℃, and total deformation is controlled between (65~95) %, and thermal treatment temp is (500~800) ℃.Above-mentioned complete processing gets final product by the method for prior art.
Embodiment 3:
With titanium sponge, zirconium sponge, niobium titanium master alloy is the preparation of raw material alloy material, and the designing quality of each component is respectively: 61 kilograms of titaniums (Ti), 31 kilograms of niobiums (Nb), 8 kilograms of zirconiums (Zr).Become ingot casting through the secondary vacuum arc melting, cogging under the temperature of (900~1050) ℃ is processed into bar or sheet material under the temperature of (800~900) ℃, and total deformation is controlled between (65~95) %, and thermal treatment temp is (500~800) ℃.Above-mentioned complete processing gets final product by the method for prior art.
Embodiment 4:
With titanium sponge, zirconium sponge, niobium titanium master alloy is the preparation of raw material alloy material, and the designing quality of each component is respectively: 62 kilograms of titaniums (Ti), 32 kilograms of niobiums (Nb), 6 kilograms of zirconiums (Zr).Become ingot casting through the secondary vacuum arc melting, cogging under the temperature of (900~1050) ℃ is processed into bar or sheet material under the temperature of (800~900) ℃, and total deformation is controlled between (65~95) %, and thermal treatment temp is (500~800) ℃.Above-mentioned complete processing gets final product by the method for prior art.
Embodiment 5:
With titanium sponge, zirconium sponge, niobium titanium master alloy is the preparation of raw material alloy material, and the designing quality of each component is respectively: 63 kilograms of titaniums (Ti), 31 kilograms of niobiums (Nb), 6 kilograms of zirconiums (Zr).Become ingot casting through the secondary vacuum arc melting, cogging under the temperature of (900~1050) ℃ is processed into bar or sheet material under the temperature of (800~900) ℃, and total deformation is controlled between (65~95) %, and thermal treatment temp is (500~800) ℃.Above-mentioned complete processing gets final product by the method for prior art.
Embodiment 6:
With titanium sponge, zirconium sponge, niobium titanium master alloy is the preparation of raw material alloy material, and the designing quality of each component is respectively: 59 kilograms of titaniums (Ti), 34 kilograms of niobiums (Nb), 7 kilograms of zirconiums (Zr).Become ingot casting through the secondary vacuum arc melting, cogging under the temperature of (900~1050) ℃ is processed into bar or sheet material under the temperature of (800~900) ℃, and total deformation is controlled between (65~95) %, and thermal treatment temp is (500~800) ℃.Above-mentioned complete processing gets final product by the method for prior art.
Embodiment 7:
With titanium sponge, zirconium sponge, niobium titanium master alloy is the preparation of raw material alloy material, and the designing quality of each component is respectively: 58 kilograms of titaniums (Ti), 33 kilograms of niobiums (Nb), 9 kilograms of zirconiums (Zr).Become ingot casting through the secondary vacuum arc melting, cogging under the temperature of (900~1050) ℃ is processed into bar or sheet material under the temperature of (800~900) ℃, and total deformation is controlled between (65~95) %, and thermal treatment temp is (500~800) ℃.Above-mentioned complete processing gets final product by the method for prior art.
Embodiment 8:
With titanium sponge, zirconium sponge, niobium titanium master alloy is the preparation of raw material alloy material, and the designing quality of each component is respectively: 58 kilograms of titaniums (Ti), and 33 kilograms of niobiums (Nb), 8 kilograms of zirconiums (Zr), gross weight is a double centner.Become ingot casting through the secondary vacuum arc melting, cogging under the temperature of (900~1050) ℃ is processed into bar or sheet material under the temperature of (800~900) ℃, and total deformation is controlled between (65~95) %, and thermal treatment temp is (500~800) ℃.Above-mentioned complete processing gets final product by the method for prior art.
Because of containing small amount of impurities in the raw material, the amount of titanium can not be definite fully, thus in claims titanium be chosen as surplus.
Material of the present invention can be made artificial bone, articular prosthesis, orthopedic fixation device tool, mouth cavity planting body etc., also can be used for making spectacle frame, spring, can also be as chemical industry ocean exploitation structured material.

Claims (2)

1, a kind of high-strength low-modulus bio-medical titanium is characterized in that: it is made up of titanium (Ti), niobium (Nb), zirconium (Zr), and each set of dispense is such as following:
The title weight percent
Niobium (Nb) (31~34) %
Zirconium (Zr) (6~9) %
Titanium (Ti) surplus.
2, a kind of high-strength low-modulus bio-medical titanium according to claim 1 is characterized in that: described each set of dispense ratio is:
The title weight percent
Niobium (Nb) (32~33) %
Zirconium (Zr) (7~8) %
Titanium (Ti) surplus.
CNB2004100205012A 2004-04-29 2004-04-29 High-intensity low modulus biological and medical use titanium alloy Expired - Fee Related CN1323181C (en)

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CN1323181C CN1323181C (en) 2007-06-27

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005064026A1 (en) * 2003-12-25 2005-07-14 Institute Of Metal Research Chinese Academy Of Sciences Super elasticity and low modulus ti alloy and its manufacture process
CN1298874C (en) * 2003-12-25 2007-02-07 中国科学院金属研究所 Super elasticity low modulus titanium alloy and preparing and processing method
CN102443718A (en) * 2011-12-13 2012-05-09 广西大学 Metastable beta-type Ti-Mo-Si system biomedical alloy and preparation method thereof
CN105463249A (en) * 2015-12-03 2016-04-06 华南理工大学 High-strength low-modulus medical beta-Ti alloy material and preparing method thereof
CN106312060A (en) * 2015-06-29 2017-01-11 中国科学院金属研究所 Preparation method for high-performance low-modulus medical titanium alloy three-dimensional metal part
CN108220682A (en) * 2018-01-29 2018-06-29 东北大学 A kind of low anti-infective titanium alloy of modulus cupric
CN109259879A (en) * 2018-09-28 2019-01-25 江阴金泰克生物技术有限公司 Titanium alloy one-part form Immediate prosthesis dental implant and preparation method thereof
CN110284020A (en) * 2019-07-08 2019-09-27 东南大学 A kind of corrosion-resistant high-ductility titanium based composites and preparation method thereof

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US5477864A (en) * 1989-12-21 1995-12-26 Smith & Nephew Richards, Inc. Cardiovascular guidewire of enhanced biocompatibility
US5573401A (en) * 1989-12-21 1996-11-12 Smith & Nephew Richards, Inc. Biocompatible, low modulus dental devices
US5169597A (en) * 1989-12-21 1992-12-08 Davidson James A Biocompatible low modulus titanium alloy for medical implants
AU705336B2 (en) * 1994-10-14 1999-05-20 Osteonics Corp. Low modulus, biocompatible titanium base alloys for medical devices
US5820707A (en) * 1995-03-17 1998-10-13 Teledyne Industries, Inc. Composite article, alloy and method
US6409852B1 (en) * 1999-01-07 2002-06-25 Jiin-Huey Chern Biocompatible low modulus titanium alloy for medical implant
US6238491B1 (en) * 1999-05-05 2001-05-29 Davitech, Inc. Niobium-titanium-zirconium-molybdenum (nbtizrmo) alloys for dental and other medical device applications
CN1360073A (en) * 2000-12-22 2002-07-24 天津鸥洋表业有限公司 Biosome embedded Ti-base alloy
CN1461816A (en) * 2002-05-30 2003-12-17 王新敏 Ti-base trielement alloy product and application
CN1217021C (en) * 2003-08-08 2005-08-31 西北有色金属研究院 Beta type titanium alloy for vascular stent

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005064026A1 (en) * 2003-12-25 2005-07-14 Institute Of Metal Research Chinese Academy Of Sciences Super elasticity and low modulus ti alloy and its manufacture process
CN1298874C (en) * 2003-12-25 2007-02-07 中国科学院金属研究所 Super elasticity low modulus titanium alloy and preparing and processing method
US7722805B2 (en) 2003-12-25 2010-05-25 Institute Of Metal Research Chinese Academy Of Sciences Titanium alloy with extra-low modulus and superelasticity and its producing method and processing thereof
CN102443718A (en) * 2011-12-13 2012-05-09 广西大学 Metastable beta-type Ti-Mo-Si system biomedical alloy and preparation method thereof
CN106312060A (en) * 2015-06-29 2017-01-11 中国科学院金属研究所 Preparation method for high-performance low-modulus medical titanium alloy three-dimensional metal part
CN106312060B (en) * 2015-06-29 2019-02-26 中国科学院金属研究所 A kind of preparation method of the low modulus medical titanium alloy 3-dimensional metal part of high-performance
CN105463249A (en) * 2015-12-03 2016-04-06 华南理工大学 High-strength low-modulus medical beta-Ti alloy material and preparing method thereof
CN105463249B (en) * 2015-12-03 2018-02-23 华南理工大学 A kind of high-strength low mould medical beta Ti alloy materials and preparation method thereof
CN108220682A (en) * 2018-01-29 2018-06-29 东北大学 A kind of low anti-infective titanium alloy of modulus cupric
CN109259879A (en) * 2018-09-28 2019-01-25 江阴金泰克生物技术有限公司 Titanium alloy one-part form Immediate prosthesis dental implant and preparation method thereof
CN110284020A (en) * 2019-07-08 2019-09-27 东南大学 A kind of corrosion-resistant high-ductility titanium based composites and preparation method thereof

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