JPH04200557A - Implant material for living body - Google Patents
Implant material for living bodyInfo
- Publication number
- JPH04200557A JPH04200557A JP2336099A JP33609990A JPH04200557A JP H04200557 A JPH04200557 A JP H04200557A JP 2336099 A JP2336099 A JP 2336099A JP 33609990 A JP33609990 A JP 33609990A JP H04200557 A JPH04200557 A JP H04200557A
- Authority
- JP
- Japan
- Prior art keywords
- titanium
- layer
- nitrogen
- base material
- temperature
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000000463 material Substances 0.000 title claims abstract description 103
- 239000007943 implant Substances 0.000 title claims abstract description 31
- 239000010936 titanium Substances 0.000 claims abstract description 89
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 83
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 82
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract description 71
- 239000010410 layer Substances 0.000 claims abstract description 52
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 26
- 229910001069 Ti alloy Inorganic materials 0.000 claims abstract description 23
- 239000002344 surface layer Substances 0.000 claims abstract description 20
- 125000004433 nitrogen atom Chemical group N* 0.000 claims abstract description 10
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 claims description 17
- 238000009792 diffusion process Methods 0.000 claims description 15
- 239000000203 mixture Substances 0.000 claims description 9
- 238000010828 elution Methods 0.000 claims description 5
- 238000002407 reforming Methods 0.000 abstract 4
- XOUPWBJVJFQSLK-UHFFFAOYSA-J titanium(4+);tetranitrite Chemical compound [Ti+4].[O-]N=O.[O-]N=O.[O-]N=O.[O-]N=O XOUPWBJVJFQSLK-UHFFFAOYSA-J 0.000 abstract 2
- 238000010438 heat treatment Methods 0.000 description 22
- 229910001873 dinitrogen Inorganic materials 0.000 description 19
- 238000012986 modification Methods 0.000 description 18
- 230000004048 modification Effects 0.000 description 18
- 230000000052 comparative effect Effects 0.000 description 13
- 238000006243 chemical reaction Methods 0.000 description 12
- 230000009466 transformation Effects 0.000 description 9
- 239000013078 crystal Substances 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 8
- 238000002441 X-ray diffraction Methods 0.000 description 7
- 229910000831 Steel Inorganic materials 0.000 description 6
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 239000010959 steel Substances 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 238000005299 abrasion Methods 0.000 description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 4
- 239000010953 base metal Substances 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 230000006866 deterioration Effects 0.000 description 4
- 239000001301 oxygen Substances 0.000 description 4
- 229910052760 oxygen Inorganic materials 0.000 description 4
- 238000012545 processing Methods 0.000 description 4
- 239000000243 solution Substances 0.000 description 4
- 210000001519 tissue Anatomy 0.000 description 4
- QTBSBXVTEAMEQO-UHFFFAOYSA-N Acetic acid Chemical compound CC(O)=O QTBSBXVTEAMEQO-UHFFFAOYSA-N 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 230000003247 decreasing effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000000704 physical effect Effects 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- 238000009864 tensile test Methods 0.000 description 3
- 150000003609 titanium compounds Chemical class 0.000 description 3
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 206010020751 Hypersensitivity Diseases 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 210000000988 bone and bone Anatomy 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 230000000747 cardiac effect Effects 0.000 description 2
- 238000006555 catalytic reaction Methods 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000011156 evaluation Methods 0.000 description 2
- 239000010408 film Substances 0.000 description 2
- 210000003709 heart valve Anatomy 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 238000004020 luminiscence type Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 210000000056 organ Anatomy 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000003746 surface roughness Effects 0.000 description 2
- 238000004381 surface treatment Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 101000975007 Homo sapiens Transcriptional regulator Kaiso Proteins 0.000 description 1
- 206010061218 Inflammation Diseases 0.000 description 1
- 102100023011 Transcriptional regulator Kaiso Human genes 0.000 description 1
- 241000276425 Xiphophorus maculatus Species 0.000 description 1
- 208000026935 allergic disease Diseases 0.000 description 1
- 230000007815 allergy Effects 0.000 description 1
- 229910000147 aluminium phosphate Inorganic materials 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 239000008280 blood Substances 0.000 description 1
- 210000004369 blood Anatomy 0.000 description 1
- 238000011088 calibration curve Methods 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000015271 coagulation Effects 0.000 description 1
- 238000005345 coagulation Methods 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 239000013256 coordination polymer Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000001700 effect on tissue Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000009610 hypersensitivity Effects 0.000 description 1
- 230000004054 inflammatory process Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000002715 modification method Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 238000005121 nitriding Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 150000003608 titanium Chemical class 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Materials For Medical Uses (AREA)
Abstract
Description
【発明の詳細な説明】 (産業上の利用分野) 本発明は生体用インプラント材料に関するものである。[Detailed description of the invention] (Industrial application field) The present invention relates to biomedical implant materials.
詳しく述べると本発明は、本発明は、生体適合性に優れ
かつ長期間安定した性能を発揮し得る生体用インプラン
ト材料に関するものである。More specifically, the present invention relates to a biomedical implant material that has excellent biocompatibility and can exhibit stable performance over a long period of time.
(従来の技術)
チタンまたはチタン合金(以下、チタン材と称する。)
は、鉄鋼材料に匹敵する強度を有するとともにステンレ
ス鋼以上の耐蝕性を示し、さらに比重か鉄鋼の約1/2
と小さいため比強度の優れた軽量強力材料である。また
チタンの生体適合性は、他の金属に見られない独特のも
のである。すなわち、体内組織および体液はチタンには
とんと影響を及はさす、一方、チタンも組織に対してわ
ずかな影響を及はすにすぎず、他の金属の場合とは異な
り、炎症、過敏症、アレルギーあるいは組織拒絶反応を
起こす原因となることはな(、さらに血液と接触しても
凝固反応を引起すことも少ないものである。なお、この
ような生体適合性は純チタンのみならず、例えばT 1
−6AΩ−4Vaなとのチタン合金においても同様に見
られ、臨床的にも応用されている。(Prior art) Titanium or titanium alloy (hereinafter referred to as titanium material)
It has strength comparable to steel materials, exhibits better corrosion resistance than stainless steel, and has a specific gravity that is approximately 1/2 that of steel.
Because of its small size, it is a lightweight and strong material with excellent specific strength. Furthermore, titanium's biocompatibility is unique and not found in other metals. That is, body tissues and fluids have a strong effect on titanium, while titanium also has only a small effect on tissues and, unlike other metals, may cause inflammation, hypersensitivity, It does not cause allergies or tissue rejection reactions (and it also rarely causes coagulation reactions when it comes into contact with blood. This kind of biocompatibility is not limited to pure titanium; for example, T 1
A similar phenomenon is observed in titanium alloys such as -6AΩ-4Va, and is also applied clinically.
このため近年、このようなチタンを例えば人工骨、人工
関節、人工歯根などのような硬組織代替物、あるいは心
臓ペースメーカーのハウジング、人工心臓弁などのよう
な人工臓器等の生体用インプラント材料として用いるこ
とが提唱されている。For this reason, in recent years, such titanium has been used as a hard tissue substitute such as artificial bones, artificial joints, and artificial tooth roots, and as an implant material for living organisms such as artificial organs such as cardiac pacemaker housings and artificial heart valves. It is proposed that.
なお、上記したような生体適合性は純チタンのみならず
、例えばT 1−6AΩ−4Vaなどのチタン合金にお
いても同様に見られ、臨床的にも応用されている。The biocompatibility described above is found not only in pure titanium, but also in titanium alloys such as T1-6AΩ-4Va, and is also applied clinically.
しかしながら、チタン材は、上記したような優れた生体
適合性、強度、耐蝕性、軽量性等の特性を有する反面、
表面硬度が十分ではないために、表面が傷付き易くまた
耐磨耗性にも劣るものであり、従ってこのようなチタン
材により゛構成される生体用インプラント材料の使用寿
命の低下、摩耗粉による問題等を生じるものであった。However, while titanium materials have the above-mentioned characteristics such as excellent biocompatibility, strength, corrosion resistance, and lightness,
Because the surface hardness is not sufficient, the surface is easily damaged and has poor abrasion resistance. Therefore, the service life of biomedical implant materials made of titanium material is shortened, and the wear particles cause damage to the surface. This caused problems.
このようなチタン材よりなる生体用インプラント材料の
表面硬度の問題に対処するために、種々の表面改質法が
試みられている。チタン材の表面改質技術としては、既
に開発されているCVD法やPVD法を応用して、窒化
チタン(T i N)、炭化チタン(TiC)、硼化チ
タン(T i B)あるいはこれらの複合物質であるチ
タン化合物などの薄い被膜を表面に被着させたり(例え
ば特開昭62−122669号)、反応性ガス等を用い
る接触反応を応用して窒素、炭素、酸素、硼素などの硬
化元素をチタン材の表面より反応浸透させて表面に窒化
チタン、炭化チタン、硼化チタン、−酸化チタン(T
i O)あるいはこれらの複合化合物である炭窒化チタ
ン(TiCN)などの薄いチタンの安定化合物層を形成
させるとともに、表面より内部に向ってチタン母材に窒
素、炭素、酸素、硼素などの硬化元素を拡散固溶させる
技術が知られている。In order to deal with the problem of surface hardness of biological implant materials made of titanium materials, various surface modification methods have been attempted. Surface modification technology for titanium materials applies already developed CVD and PVD methods to modify titanium nitride (T i N), titanium carbide (TiC), titanium boride (T i B), or these materials. By applying a thin film of a composite material such as a titanium compound to the surface (for example, JP-A-62-122669), or by applying a catalytic reaction using a reactive gas, etc., it is possible to harden nitrogen, carbon, oxygen, boron, etc. Titanium nitride, titanium carbide, titanium boride, -titanium oxide (T
i O) or a composite compound of these, such as titanium carbonitride (TiCN), to form a thin stable titanium compound layer, and at the same time inject hardening elements such as nitrogen, carbon, oxygen, and boron into the titanium matrix from the surface toward the inside. There is a known technology for diffusing and solid-dissolving.
しかしながら、チタン材の表面にチタン化合物を直接被
着させる表面改質では、母材と被膜との境界における材
質の物性値の不連続が極めて大きいために使用中の密着
性が不足する場合がある。However, in surface modification in which a titanium compound is directly deposited on the surface of a titanium material, adhesion during use may be insufficient due to extremely large discontinuities in the physical properties of the material at the boundary between the base material and the coating. .
このためインプラント材料としての過酷な使用条件下で
は長年月にわたる使用期間を通じてミクロ的なひずみ分
布の不均一などを生じる結果、被膜が剥離してしまう恐
れがあった。For this reason, under harsh conditions of use as an implant material, there is a risk that the coating may peel off as a result of uneven microscopic strain distribution occurring over many years of use.
また、接触反応を応用して安定化合物層を形成させる表
面改質では、比較的高温度での反応・拡散を行なわせる
必要がある。すなわちチタンの表面は保護性酸化膜によ
り覆われており、接触反応を進めるための反応温度は低
温度では反応性に乏しく、また処理時間が長期化し生産
性が低下するために、できるかぎり高温度とすることが
望まれている。例えば窒素ガスとの直接反応においては
、従来、反応のために好ましい加熱温度は850℃以上
とされていた。なお、加熱温度の上限は加熱炉の維持管
理や運転エネルギーコスト等の観点から1050℃が限
度とされていた。従゛って、この表面改質処理において
チタン母材も高温度に加熱され、この際チタン母材は高
温加熱に伴なう汚染劣化の危険に曝されるとともに、加
熱による内部の金属組織の変化や結晶粒が粗大化すると
いったことがもたらされる。このようなミクロ的な金属
組織の変化やチタンのα=β変態を含む熱履歴は、母材
のチタン材の材質に影響を与え、強度や靭性などの機械
的性質を低下させてしまうといった問題があった。Furthermore, in surface modification in which a stable compound layer is formed by applying a catalytic reaction, it is necessary to carry out the reaction and diffusion at a relatively high temperature. In other words, the surface of titanium is covered with a protective oxide film, and the reaction temperature for proceeding with the contact reaction is as high as possible, since reactivity is poor at low temperatures, and the processing time becomes long, reducing productivity. It is hoped that For example, in a direct reaction with nitrogen gas, the preferred heating temperature for the reaction has conventionally been 850°C or higher. Note that the upper limit of the heating temperature has been set at 1050° C. from the viewpoint of maintenance and management of the heating furnace, operating energy cost, etc. Therefore, in this surface modification treatment, the titanium base material is also heated to high temperatures, and at this time, the titanium base material is exposed to the risk of contamination and deterioration due to high temperature heating, and the internal metal structure is damaged due to heating. This results in changes such as changes and coarsening of crystal grains. Such thermal history, including changes in the microscopic metal structure and α=β transformation of titanium, affects the material quality of the titanium base material, causing problems such as deterioration of mechanical properties such as strength and toughness. was there.
ところで、チタンと上記のような硬化元素との安定化合
物の硬さはマイクロビッカーズ硬さ(Hv)か2000
〜3000程度で、チタン材の硬さ100〜400に比
べると極めて硬く、結晶形やその他の各種物性値も全く
異なっている。By the way, the hardness of a stable compound of titanium and the above hardening elements is micro-Vickers hardness (Hv) or 2000
~3000, which is extremely hard compared to the hardness of titanium materials, which has a hardness of 100 to 400, and the crystal shapes and other physical properties are also completely different.
しかしながら、生体用インプラント材料としては、この
ように極めて硬いHv2000〜3000という硬度を
必要とせず、調質された特殊鋼のレベルであるHv70
0〜1000程度であっても十分であるようなものも数
多くあり、このような場合においては、安定した表面改
質層を有するとともに母材であるチタン材の特性の低下
の少ないことが望まれていた。However, as a living body implant material, it is not necessary to have a hardness of Hv 2000 to 3000, which is extremely hard, but Hv 70, which is the level of tempered special steel.
There are many cases in which a value of about 0 to 1000 is sufficient, and in such cases, it is desirable to have a stable surface modification layer and less deterioration of the properties of the titanium material that is the base material. was.
(発明が解決しようとする課題)
従って本発明は、新規な生体用インプラント材料を提供
することを目的とする。本発明はまた、表面硬度、耐磨
耗性、生体適合性、イオン溶出性などの表面特性に優れ
るとともにチタン系母材の機械的特性、特に靭性を低下
させることな(保持する生体用インプラント材料を提供
することを目的とするものである。(Problems to be Solved by the Invention) Therefore, an object of the present invention is to provide a novel implant material for living bodies. The present invention also provides excellent surface properties such as surface hardness, abrasion resistance, biocompatibility, and ion elution properties, and does not reduce the mechanical properties of the titanium-based base material, especially the toughness. The purpose is to provide the following.
(課題を解決するための手段)
上記諸口的は、チタンまたはチタン合金よりなる母材の
表面に、亜窒化チタンを主体とする表面改質層および該
表面改質層に接する下層部位に位置しチタン母材に窒素
原子を拡散・固溶させた窒素拡散硬化層からなる表面層
を0.3〜100μmの平均厚さで有することを特徴と
するイオン溶出を抑えた生体用インプラント材料により
達成される。(Means for solving the problems) The above-mentioned features include a surface-modified layer mainly made of titanium nitride and a lower layer located in contact with the surface-modified layer on the surface of a base material made of titanium or a titanium alloy. This is achieved by a biomedical implant material that suppresses ion elution and has a surface layer consisting of a nitrogen diffusion hardened layer in which nitrogen atoms are diffused and dissolved in a titanium base material with an average thickness of 0.3 to 100 μm. Ru.
(作用) ゛
このように本発明の生体用インプラント材料は、表面に
亜窒化チタンを主体とする表面改質層および該表面改質
層に接する下層部位に位置しチタン母材に窒素原子を傾
斜組成を以て拡散・固溶させた窒素拡散硬化層からなる
表面層を有するチタン材によって構成されるものである
。(Function) As described above, the biomedical implant material of the present invention has a surface-modified layer mainly composed of titanium nitride on the surface and a lower layer in contact with the surface-modified layer, in which nitrogen atoms are tilted to the titanium base material. It is composed of a titanium material having a surface layer consisting of a nitrogen diffusion hardened layer which is diffused and solid-dissolved according to the composition.
窒素濃度12.75%、1100℃以下の領域に存在す
る亜窒化チタンは、窒化チタンと同様に各種水溶液の化
学環境においても極めて安定であり一般的に何ら処理を
施されていないチタン材よりも良好な耐蝕性を示す。ま
たその硬さはマイクロビッカース硬さ(Hv)1400
〜1500程度と極めて硬い。実際、本発明に係わる生
体インプラント材料における亜窒化チタンを主体とする
表面被膜の硬さは、処理温度、保持時間等の処理条件の
さらに細かな違いにより変動するため、測定値に幅があ
るが、HV800〜1500程度である。この硬さは何
ら処理を施していないチタン材の硬さであるHvlOO
〜400に比べるとはるかに大きく、焼入れなどの調質
処理を施した特殊鋼の硬さに匹敵するないしはそれ以上
の硬さであり、生体用インプラント材料の表面硬度とし
て十分なものであると考えられる。Titanium nitride, which exists at a nitrogen concentration of 12.75% and below 1100°C, is extremely stable in the chemical environment of various aqueous solutions, just like titanium nitride, and is generally more stable than untreated titanium materials. Shows good corrosion resistance. Its hardness is micro Vickers hardness (Hv) 1400.
~1500 and extremely hard. In fact, the hardness of the surface film mainly composed of titanium nitride in the biological implant material according to the present invention varies depending on finer differences in processing conditions such as processing temperature and holding time, so there is a wide range of measured values. , HV is about 800 to 1500. This hardness is HvlOO which is the hardness of titanium material without any treatment.
It is much larger than ~400 and has a hardness comparable to or even higher than that of special steel that has been subjected to heat treatment such as quenching, and is considered to be sufficient as a surface hardness for biological implant materials. It will be done.
また本発明の生体用インプラント材料においては、チタ
ン母材と表面改質層の界面の組成は窒素拡散硬化層とし
て連続的に推移していているために、表面層の母材との
密着性は良好である。In addition, in the biological implant material of the present invention, the composition of the interface between the titanium base material and the surface modified layer changes continuously as a nitrogen diffusion hardened layer, so the adhesion of the surface layer to the base material is In good condition.
さらに、このような亜窒化チタンを主成分とする表面改
質層および窒素拡散層からなる表面層は、チタン材を高
純度の窒素ガス雰囲気下で740〜820°C程度に加
熱保持することによって形成することができる。周知の
ように、チタン(純チタン)には880°Cにα=βの
相変態があり、また金属組織においてβ相領域では急激
な結晶粒の成長か起り、結晶粒か粗大化する。β相領域
に保持された粗大粒は冷却の過程で粗大な針状晶を生じ
、機械的性質において靭性に関与する材料特性が劣化す
ることが知られている。またチタン合金のα=β相変態
温度は、合金組成すなわち配合元素の種類とその配合量
によって変化する。゛ここで酸素や窒素などのα安定型
元素はαコβ相変態温度を高温側に移行させるが、大部
分の金属元素はβ安定型元素で、鉄、コバルト、ニッケ
ルなどの金属元素の配合によりα=β相変態温度は低温
側に移行する。実用チタン合金ではα=β相変態温度を
調節するためにα安定型元素とβ安定型元素を同時に配
合して変態温度の調節を行なっている。チタン材に熱履
歴を加えながらも靭性に関与する材料特性の低下を抑制
するためには変態温度以上の加熱は無論、変態温度の直
下であっても可能な限り低い温度を選ぶことが肝要であ
る。本発明の生体用インプラント材料の表面層は、前記
したように比較的低温領域で形成されるものであるため
、本発明の生体用インプラント材料において、チタン材
の持つ本来の靭性は確保されることとなる。Furthermore, the surface layer consisting of a surface modification layer mainly composed of titanium nitride and a nitrogen diffusion layer can be created by heating and holding the titanium material at approximately 740 to 820°C in a high purity nitrogen gas atmosphere. can be formed. As is well known, titanium (pure titanium) undergoes a phase transformation of α=β at 880°C, and in the β phase region of the metal structure, rapid crystal grain growth occurs and the crystal grains become coarse. It is known that coarse grains retained in the β-phase region form coarse acicular crystals during the cooling process, which deteriorates material properties related to toughness in mechanical properties. Further, the α=β phase transformation temperature of a titanium alloy changes depending on the alloy composition, that is, the types of compounded elements and their compounded amounts.゛Here, α-stable elements such as oxygen and nitrogen shift the α-β phase transformation temperature to the high temperature side, but most metal elements are β-stable elements, and the combination of metal elements such as iron, cobalt, and nickel Therefore, the α=β phase transformation temperature shifts to the lower temperature side. In practical titanium alloys, in order to adjust the α=β phase transformation temperature, α-stable elements and β-stable elements are simultaneously blended to adjust the transformation temperature. In order to suppress the deterioration of material properties related to toughness while adding thermal history to titanium materials, it is important not only to heat above the transformation temperature, but also to choose a temperature as low as possible even just below the transformation temperature. be. Since the surface layer of the biological implant material of the present invention is formed in a relatively low temperature region as described above, the inherent toughness of the titanium material is ensured in the biological implant material of the present invention. becomes.
本発明の生体用インプラント材料にいて母材として用い
られるチタン材としては、生理的に安全なものであれば
特に限定されるものではなく、純チタン以外にも、α型
、α−β型あるいはβ型の各種チタン合金が用いられ得
、具体的には例えばT 1−6Aρ−4Vあるいは酸素
0.13%以下、鉄0.25%以下のT 1−6AΩ−
4V ELIなどの合金が好ましく挙げられる。The titanium material used as the base material in the biological implant material of the present invention is not particularly limited as long as it is physiologically safe. Various β-type titanium alloys may be used, specifically, for example, T 1-6Aρ-4V or T 1-6AΩ- with 0.13% or less of oxygen and 0.25% or less of iron.
Preferably, alloys such as 4V ELI are used.
しかして、本発明の生体用インプラント材料においては
、第1図に模式するように、前記したようなチタン材1
の表面には亜窒化チタンを主成分とする表面改質層2お
よび該表面改質層2に接する下層部位に位置しチタン母
材に窒素原子を傾斜組成、すなわち表面側の表面改質層
2の直下では窒素濃度が大で、母材側の窒素拡散層3の
終点で母材に接する部位の窒素濃度は小(母材とほぼ同
じ)となり、この間は窒素濃度が連続的に変化するよう
拡散・固溶させた窒素拡散硬化層3からなる表面層4が
形成されている。Therefore, in the biological implant material of the present invention, as schematically shown in FIG.
A surface modified layer 2 containing titanium nitride as a main component and a surface modified layer 2 located at a lower layer in contact with the surface modified layer 2 with a gradient composition of nitrogen atoms in the titanium base material, that is, a surface modified layer 2 on the surface side. The nitrogen concentration is high immediately below the base metal, and the nitrogen concentration at the end point of the nitrogen diffusion layer 3 on the base metal side, which is in contact with the base metal, is low (almost the same as the base metal), and during this time, the nitrogen concentration changes continuously. A surface layer 4 is formed of a nitrogen diffusion hardened layer 3 which has been diffused and dissolved into solid solution.
この表面層4の厚さは、0.3〜100μm1より好ま
しくは0. 3〜30μmである。すなわち、この表面
層4の厚さが0.3μm未満であると、チタン材の十分
な表面改質がなされず、表面硬度1、耐磨耗性、イオン
溶出性などが所望のものとならない虞れが大きく、一方
、表面層4の厚さを100μmよりも大きいものとして
も、100μm以下の厚さの場合と表面改質効果が実質
的に変らず、作製に非常に長持間を要することとなるた
め経済的に不利であるばかりでなく、チタン母材を加熱
条件下に長持間曝すことによる母材物性の低下の虞れが
あるためである。なお、この表面層4のうち表面改質層
2の厚さは、表面層4の厚さの大小によっても左右され
るが、0.3〜0゜8μm程度であり、残部か窒素拡散
硬化層3である。The thickness of this surface layer 4 is preferably 0.3 to 100 μm1. It is 3 to 30 μm. That is, if the thickness of the surface layer 4 is less than 0.3 μm, sufficient surface modification of the titanium material may not be achieved, and the desired surface hardness 1, abrasion resistance, ion elution properties, etc. may not be obtained. On the other hand, even if the thickness of the surface layer 4 is greater than 100 μm, the surface modification effect is substantially the same as in the case of a thickness of 100 μm or less, and it takes a very long time to manufacture. This is not only economically disadvantageous, but also because there is a risk that the physical properties of the titanium base material may deteriorate if the titanium base material is exposed to heating conditions for a long period of time. The thickness of the surface modified layer 2 of this surface layer 4 depends on the thickness of the surface layer 4, but is about 0.3 to 0.8 μm, and the remaining part is the nitrogen diffusion hardened layer. It is 3.
表面改質層2には、主成分となる亜窒化チタン(T 1
2 N)の他に、窒化チタン(T i N)の存在が見
られるか、窒化チタンの存在量は極めて少ない。The surface modified layer 2 contains titanium nitride (T 1
2N), the presence of titanium nitride (T i N) is observed, or the amount of titanium nitride present is extremely small.
また本発明の生体用インプラント材料において、表面改
質層2の表面粗さは母材の結晶粉炭の影響を受けるため
、母材の結晶粒の大きさを10〜80μmに調整してお
くことにより、本処理による表面粗度は生体適合性の上
から好ましいものとなり、生体用インプラント材料の生
体適合性かより良好なものとなると考えられる。In addition, in the biomedical implant material of the present invention, since the surface roughness of the surface modified layer 2 is affected by the crystalline pulverized coal of the base material, it is possible to adjust the crystal grain size of the base material to 10 to 80 μm. It is thought that the surface roughness obtained by this treatment is preferable from the viewpoint of biocompatibility, and the biocompatibility of the biological implant material is improved.
また窒素拡散硬化層3において、チタン母材に固溶・拡
散した窒素原子の濃度は、表面改質層2より離れる程小
さくなる、すなわち深さに反比例するものであり、この
ように最表面の表面改質層2から窒素拡散硬化層3とし
て連続的に組成が推移してチタン母材に至るために表面
層4は過酷な条件下においても母材より剥離する虞れは
極めて少ない。In addition, in the nitrogen diffusion hardened layer 3, the concentration of nitrogen atoms dissolved and diffused into the titanium base material decreases as the distance from the surface modified layer 2 increases, that is, it is inversely proportional to the depth. Since the composition changes continuously from the surface modified layer 2 to the nitrogen diffusion hardened layer 3 to reach the titanium base material, there is extremely little risk that the surface layer 4 will separate from the base material even under severe conditions.
このような本発明の生体用インプラント材料を得るには
、まず粉末焼結、鋳造あるいは鍛造などの任意の成形方
法により上記のごときチタンないしはチタン合金からな
る成形品を作製し、必要に応じて精密加工を行ない所望
形状となし、さらに必要により洗浄処理を施す。続いて
このようにして所望形状となされたチタン材よりなる成
形品を、窒素ガス雰囲気中で740°C〜820℃、よ
り好ましくは750〜800℃、さらに好ましくは77
0℃〜790℃の温度範囲に加熱保持することにより成
形品表面に上記のような表面層を形成する。なお、この
窒素ガス雰囲気中での処理温度が740℃未満であると
チタンと窒素との反応が十分に進行せず、長持間かけて
もチタン材の表面硬度が向上せず、一方処理温度が82
0°Cを越えると、チタン材の表面には窒化チタン(T
i N)を多(含む改質層が形成されるようになり、
短時間の処理によっても十分な表面硬度が得られるもの
となるが、一方でこのような温度域における加熱はチタ
ン材のミクロ的な金属組織の粗大化をもたらし、機械的
強度や靭性などの特性を低下させてしまい、本発明の意
図するインプラント材料を得ることができない。In order to obtain the biological implant material of the present invention, first, a molded product made of titanium or titanium alloy as described above is produced by any forming method such as powder sintering, casting, or forging, and precision molding is performed as necessary. It is processed into the desired shape, and then cleaned if necessary. Subsequently, the titanium material molded into the desired shape is heated at 740°C to 820°C, more preferably 750 to 800°C, and even more preferably 77°C in a nitrogen gas atmosphere.
A surface layer as described above is formed on the surface of the molded product by heating and maintaining the molded product at a temperature in the range of 0°C to 790°C. Note that if the treatment temperature in this nitrogen gas atmosphere is less than 740°C, the reaction between titanium and nitrogen will not proceed sufficiently, and the surface hardness of the titanium material will not improve even if it is maintained for a long time. 82
When the temperature exceeds 0°C, titanium nitride (T) forms on the surface of the titanium material.
A modified layer containing a large amount of (N) is now formed,
Sufficient surface hardness can be obtained even with short-time treatment, but on the other hand, heating in this temperature range coarsens the microscopic metal structure of the titanium material, impairing properties such as mechanical strength and toughness. Therefore, the implant material intended by the present invention cannot be obtained.
またこのチタンHの表面改質処理において、反応時にお
ける窒素カス雰囲気は、チタン材を汚染しないような高
純度であることが必要である。さらに窒素カス雰囲気の
圧力は、5〜760 Torr。Further, in this surface modification treatment of titanium H, the nitrogen gas atmosphere during the reaction needs to be of high purity so as not to contaminate the titanium material. Furthermore, the pressure of the nitrogen gas atmosphere is 5 to 760 Torr.
より好ましくは76〜760 Torr程度とされる。More preferably, it is about 76 to 760 Torr.
さらにこのようなチタン材の表面改質方法において、加
熱保持時間は、処理温度によっても左右されるが、1〜
30時間、生産性を考慮するとより好ましくは4〜16
時間程度とされる。加熱処理温度か同一であった場合、
亜窒化チタンを主体とする表面改質層の厚さやその含有
量は、保持時間に依存し、その時間が長くなる程太き(
なる。Furthermore, in such a method for surface modification of titanium materials, the heating holding time depends on the treatment temperature, but
30 hours, more preferably 4 to 16 hours considering productivity
It is said to be about an hour. If the heat treatment temperature is the same,
The thickness and content of the surface-modified layer mainly composed of titanium nitride depends on the holding time, and the longer the holding time, the thicker it becomes (
Become.
次に、本発明の生体用インプラント材料の特性を具体的
に説明するためにいくつかの参考データを示す。Next, some reference data will be shown to specifically explain the characteristics of the biological implant material of the present invention.
参考例1および参考例2 チタン(工業用純チタン)からなる厚さl m m 。Reference example 1 and reference example 2 Made of titanium (industrial pure titanium) with a thickness of 1 mm.
長さ15mm、幅10rnmの板状試料(参考例1)お
よびチタン合金(Ti−6Aρ−4V)からなる同形状
の板状試料(参考例2)をそれぞれ真空炉中に入れ、そ
して高真空(10−5Torr以下)を維持するように
排気しながら、参考例1の試料については750℃まで
、また参考例2の試料については800℃まで約り0℃
/分の速度で昇温加熱した。炉内温度が所望温度に達し
たらこの温度で一定に保持しながら、炉内雰囲気を高純
度の窒素ガスで置換して窒素ガス圧760Torrとし
、そのまま参考例1の試料については25時間、参考例
2の試料については9時間にわたって加熱保持し、その
後500℃までは約20°C/分の降温速度で冷却し、
以降は炉冷(自然放冷)した。A plate-shaped sample with a length of 15 mm and a width of 10 nm (Reference Example 1) and a plate-shaped sample of the same shape made of titanium alloy (Ti-6Aρ-4V) (Reference Example 2) were placed in a vacuum furnace, and then heated under high vacuum ( 10-5 Torr or less), the sample of Reference Example 1 was heated to 750°C, and the sample of Reference Example 2 was heated to 800°C, and the temperature was 0°C.
The temperature was increased at a rate of 1/min. When the temperature inside the furnace reaches the desired temperature, while keeping it constant at this temperature, the atmosphere inside the furnace is replaced with high-purity nitrogen gas to make the nitrogen gas pressure 760 Torr, and the sample of Reference Example 1 is heated for 25 hours. Sample No. 2 was heated and held for 9 hours, and then cooled to 500°C at a cooling rate of about 20°C/min.
After that, it was furnace cooled (naturally cooled).
このようにして表面改質処理を行なった板状試料の表面
組成をX線回折によって調べた。得られた結果を第2図
に示す。なおX線回折はモノクロメータによるCu
K 線を用いて行なった。The surface composition of the plate-shaped sample subjected to surface modification treatment in this manner was investigated by X-ray diffraction. The results obtained are shown in FIG. X-ray diffraction was performed using a monochromator.
This was done using K line.
α
第2図において、横軸はX線回折条件として銅の特性線
を使った時の回折角を、また縦軸は各結晶面からの回折
線の相対濃度をそれぞれ示すものである。第2図(a)
は参考例1の純チタン試料から得られた回折パターン、
第2図(b)は参考例2のチタン合金試料から得られた
回折パターンであり、また第2図(C)〜(e)はそれ
ぞれ評価の指針を与えるための標準組成のT i 2
N %TiNおよびチタン(α−Ti)のX線回折パタ
ーンである。α In FIG. 2, the horizontal axis shows the diffraction angle when the characteristic line of copper is used as the X-ray diffraction condition, and the vertical axis shows the relative concentration of the diffraction line from each crystal plane. Figure 2(a)
is the diffraction pattern obtained from the pure titanium sample of Reference Example 1,
FIG. 2(b) is a diffraction pattern obtained from the titanium alloy sample of Reference Example 2, and FIG. 2(C) to (e) are the diffraction patterns of T i 2 of standard composition for providing evaluation guidelines, respectively.
X-ray diffraction patterns of N%TiN and titanium (α-Ti).
第2図から明らかなように参考例ユおよび参考例2のい
ずれの回折パターンにおいても、主に存在する物質はT
L 2 N相で、重複してTiNおよびα−Tiから
の回折線が認められるがいずれも微弱である。As is clear from Figure 2, in both the diffraction patterns of Reference Example U and Reference Example 2, the main substance present is T.
In the L 2 N phase, overlapping diffraction lines from TiN and α-Ti are observed, but both are weak.
なおチタン材と窒素ガスとの反応を利用する表面改質処
理において、加熱保持温度を高くするとTiN相が生成
し易くなってX線回折パターンにおいてはTiN相に特
有なイオン結晶構造が明瞭となり、1050℃での処理
では主成分かTiN相となる。一方、加熱保持温度を低
くするとチタン材と窒素ガスとの反応かほとんど起らな
いため、700°Cでの処理ではチタン材の表面に生成
するチタン窒化物の総量がわずかであるため、X線回折
パターンにおいてTiN相やT 12 N相からの回折
線が微弱で、窒化は不十分であり表面硬さは不足するこ
ととなる。In addition, in surface modification treatment that utilizes the reaction between titanium material and nitrogen gas, increasing the heating temperature makes it easier to generate a TiN phase, and the ionic crystal structure unique to the TiN phase becomes clear in the X-ray diffraction pattern. In the treatment at 1050°C, the main component becomes a TiN phase. On the other hand, if the heating and holding temperature is lowered, almost no reaction between the titanium material and nitrogen gas will occur, so when processing at 700°C, the total amount of titanium nitride generated on the surface of the titanium material is small, so X-ray In the diffraction pattern, the diffraction lines from the TiN phase and the T 12 N phase are weak, nitriding is insufficient, and the surface hardness is insufficient.
参考例3〜5および比較例1〜2
チタン(工業用純チタン)からなる厚さ1mm、長さ1
5mm、幅10mmの板状試料およびチタン合金(T
1−6Aρ−4V)からなる同形状の板状試料(参考例
2)をそれぞれ真空炉中に入れ、そして高真空(10−
”Torr以下)を維゛持するように排気しながら、純
チタンの試料については750℃まで(参考例3)、ま
たチタン合金の試料については700℃(比較例1)、
750℃(参考例4) 、800℃(参考例5)、85
0°C(比較例2)まで約り0℃/分の速度で昇温加熱
した。Reference Examples 3 to 5 and Comparative Examples 1 to 2 Made of titanium (industrial pure titanium), thickness 1 mm, length 1
A plate-shaped sample with a size of 5 mm and a width of 10 mm and a titanium alloy (T
Platy samples of the same shape (Reference Example 2) consisting of 1-6Aρ-4V) were placed in a vacuum furnace, and then placed in a high vacuum (10-4V).
While evacuation was maintained to maintain a temperature of 750° C. for pure titanium samples (Reference Example 3), and 700° C. for titanium alloy samples (Comparative Example 1),
750°C (Reference Example 4), 800°C (Reference Example 5), 85
The temperature was increased to 0°C (Comparative Example 2) at a rate of about 0°C/min.
炉内温度が所望温度に達したらこの温度で一定に保持し
ながら、炉内雰囲気を高純度の窒素ガスで置換して窒素
ガス圧760Torrとし、そのまま1〜16時間にわ
たって加熱保持し、その後500℃までは約り0℃/分
の降温速度で冷却し、以降は炉冷した。When the temperature inside the furnace reaches the desired temperature, while keeping it constant at this temperature, the atmosphere inside the furnace is replaced with high-purity nitrogen gas to bring the nitrogen gas pressure to 760 Torr, heated and maintained for 1 to 16 hours, and then heated to 500°C. It was cooled at a temperature decreasing rate of about 0° C./min until then, and then it was cooled in a furnace.
このようにして表面改質処理を行なった板状試料の表面
硬さをマイクロビッカース硬度計を用いて測定した。得
られた結果を第3図に示す。The surface hardness of the plate sample subjected to the surface modification treatment in this manner was measured using a micro Vickers hardness meter. The results obtained are shown in FIG.
第3図において縦軸はマイクロビッカース硬さ(Hv)
を、横軸は加熱保持時間をそれぞれ示すものである。In Figure 3, the vertical axis is micro Vickers hardness (Hv)
, and the horizontal axis indicates the heating holding time.
第3図に示す結果から明かなように、加熱保持温度か高
くなるに従い、また加熱保持時間か長くなるに従い表面
硬度が大となっているか、処理温度が700℃(比較例
1)ではチタン材と窒素ガスとの反応が不足するために
、十分な硬さが得られなかった。これに対し処理温度か
750℃以上(参考例3〜5および比較例2)ではほぼ
Hv800〜1500程度の硬さとなって調質した特殊
鋼の硬さに匹敵するまたはそれ以上の硬さとなった。As is clear from the results shown in Figure 3, the surface hardness increases as the heating holding temperature increases and as the heating holding time increases. Sufficient hardness could not be obtained due to insufficient reaction between the steel and nitrogen gas. On the other hand, when the treatment temperature was 750°C or higher (Reference Examples 3 to 5 and Comparative Example 2), the hardness was approximately Hv800 to 1500, which was comparable to or higher than the hardness of tempered special steel. .
参考例6〜7および比較例3
チタン(工業用純チタン)の1mm厚さの板材より小型
の板状引張試験片(全長が45mmで、平行部の幅およ
び長さが4mmX12mmである)を切出し、この試験
片を真空炉中に入れ、そして高真空(10−5Torr
以下)を維持するように排気しながら、750℃(参考
例6) 、800℃(参考例7)および850°C(比
較例3)まで、約り0℃/分の速度で昇温加熱した。炉
内温度が所望温度に達したらこの温度で一定に保持しな
がら、炉内雰囲気を高純度の窒素ガスで置換して窒素ガ
ス圧を760 Torrとし、そのまま1〜16時間に
わたって加熱保持し、その後500℃までは約り0℃/
分の降温速度で冷却し、以降は炉冷した。Reference Examples 6 to 7 and Comparative Example 3 A smaller plate-like tensile test piece (total length is 45 mm, and the width and length of the parallel part are 4 mm x 12 mm) is cut out from a 1 mm thick plate of titanium (industrial pure titanium). , this specimen was placed in a vacuum furnace and placed under high vacuum (10-5 Torr).
The temperature was increased at a rate of approximately 0°C/min to 750°C (Reference Example 6), 800°C (Reference Example 7), and 850°C (Comparative Example 3) while evacuation was maintained to maintain . When the temperature inside the furnace reaches the desired temperature, while keeping it constant at this temperature, replace the atmosphere inside the furnace with high-purity nitrogen gas to bring the nitrogen gas pressure to 760 Torr, keep it heated for 1 to 16 hours, and then Approximately 0℃ up to 500℃/
The temperature was lowered at a temperature drop rate of 100 min, and then the furnace was cooled.
このようにして表面改質処理を行なった試験片に対して
引張り強さ、伸びおよび破断モードの観察を行なった。The tensile strength, elongation, and fracture mode of the test pieces subjected to surface modification treatment in this manner were observed.
第4図は上記表面改質処理を施された純チタンの試験片
の引張試験データを示す図である。第4図において縦軸
はそれぞれ伸びおよび引張強さを示し、横軸は加熱保持
時間をそれぞれ示す。FIG. 4 is a diagram showing tensile test data of a pure titanium test piece subjected to the above-mentioned surface modification treatment. In FIG. 4, the vertical axis represents elongation and tensile strength, and the horizontal axis represents heating holding time.
第4図に示す結果から明かなように、引張強さはいずれ
も32〜34 k g f /mm2程度で、加熱温度
が高い程、また保持時間が長い程大となる傾向が見られ
る。一方、伸びについては引張強さとは逆の傾向にあり
、750℃(参考例6)および800°C(参考例7)
で処理したものは未処理のものとほぼ同様の特性を示し
、母材の靭性が保たれているが、850℃で処理したも
の(比較例3)は加熱保持時間が長くなると著しく伸び
値が低下する。As is clear from the results shown in FIG. 4, the tensile strength is about 32 to 34 kgf/mm2 in all cases, and tends to increase as the heating temperature increases and the holding time increases. On the other hand, elongation has a tendency opposite to that of tensile strength, at 750°C (Reference Example 6) and 800°C (Reference Example 7).
The material treated at 850°C showed almost the same properties as the untreated material, and the toughness of the base material was maintained, but the material treated at 850°C (Comparative Example 3) showed a remarkable elongation value as the heating holding time became longer. descend.
また破断後の破面観察によれば、850℃で処理したも
の(比較例3)では、破断部にネッキングが認められず
、脆性破断モードを示すとともに、引張試験片の平行部
には引張軸に直角方向のヒビ割れが多数観察された。Furthermore, according to observation of the fracture surface after fracture, in the specimen treated at 850°C (Comparative Example 3), necking was not observed at the fracture part, indicating a brittle fracture mode, and the parallel part of the tensile test piece had a tensile axis. Many cracks in the direction perpendicular to the surface were observed.
なお、チタン合金(Ti −6AN−4V)の場合にお
いても純チタンの場合とほぼ同様の傾向が見られ、75
0℃および800°Cで処理したものは未処理のものと
ほぼ同様の引張強さ・伸びを示し、母材の靭性が保たれ
ているが、850℃で処理したものの破断モードは脆性
的な様相を示し、伸び値も低下する。In addition, in the case of titanium alloy (Ti-6AN-4V), almost the same tendency as in the case of pure titanium is observed, and 75
Those treated at 0℃ and 800℃ showed almost the same tensile strength and elongation as the untreated ones, and the toughness of the base material was maintained, but the fracture mode of the one treated at 850℃ was brittle. The elongation value also decreases.
参考例8および9 チタン(工業用純チタン)からなる厚さ5 m m 。Reference examples 8 and 9 5 mm thick made of titanium (industrial pure titanium).
直径30mmの円板状試料(参考例8)およびチタン合
金(T i −6A、Q 4V)からなる同形状の円
板状試料(参考例9)をそれぞれ真空炉中に入れ、そし
て高真空(10−5Torr以下)を維持するように排
気しながら、750℃まで約り0℃/分の速度で昇温加
熱した。炉内温度が750℃に達したらこの温度で一定
に保持しながら、炉内雰囲気を高純度の窒素ガスで置換
して窒素ガス圧760Torrとし、そのまま9時間に
わたって加熱保持し、その後500℃までは約り0℃/
分の降温速度で冷却し、その後は炉冷した。A disk-shaped sample with a diameter of 30 mm (Reference Example 8) and a disk-shaped sample of the same shape (Reference Example 9) made of titanium alloy (T i -6A, Q 4V) were placed in a vacuum furnace, and then heated under high vacuum ( The temperature was increased to 750° C. at a rate of about 0° C./min while evacuation was maintained at a temperature of 10 −5 Torr or less. When the temperature inside the furnace reached 750℃, while keeping it constant at this temperature, the atmosphere inside the furnace was replaced with high-purity nitrogen gas to bring the nitrogen gas pressure to 760 Torr, and the temperature was kept heated for 9 hours. Approximately 0℃/
The sample was cooled at a temperature decreasing rate of 10 minutes, and then furnace-cooled.
このように表面改質処理を施した試料の切断面における
表面から内部への硬さの変化をマイクロビッカース硬度
計を用いて調べた。得られた結果を第5図に示す。The change in hardness from the surface to the inside of the cut surface of the sample subjected to surface modification treatment was investigated using a micro Vickers hardness meter. The results obtained are shown in FIG.
第5図において、縦軸はマイクロビッカース硬さを、横
軸は表面からの距離(μm)をそれぞれ示すものである
。In FIG. 5, the vertical axis represents the micro-Vickers hardness, and the horizontal axis represents the distance (μm) from the surface.
第5図に示すように、表面改質処理を施した純チタン材
(参考例8)では、表面より30μm付近まで窒素原子
の固溶拡散によると思われる硬化が見られ、母材の硬さ
であるHv約170に向って表面より漸次硬度が低下し
ている。一方、表面改質処理を施したチタン合金材(参
考例9)では、表面より10μm付近まで窒素原子の固
溶拡散によると思われる硬化が見らる。いずれの素材に
おいても硬さの移行は連続的で表面硬化層と母材との密
着性は良好である。As shown in Figure 5, in the surface-modified pure titanium material (Reference Example 8), hardening was observed up to about 30 μm from the surface, which was thought to be due to solid solution diffusion of nitrogen atoms, and the hardness of the base material The hardness gradually decreases from the surface toward Hv of about 170. On the other hand, in the surface-modified titanium alloy material (Reference Example 9), hardening is observed up to about 10 μm from the surface, which appears to be due to solid solution diffusion of nitrogen atoms. In either material, the hardness transition is continuous, and the adhesion between the hardened surface layer and the base material is good.
参考例10〜11および比較例4〜5
チタン(工業用純チタン)粉末およびチタン合金(Ti
−6Aρ−4V)粉末をそれぞれ真空炉中に入れ、そし
て高真空(10−5Torr以下)を維持するように排
気しながら、750℃まで約り0℃/分の速度で昇温加
熱した。炉内温度が750℃に達したらこの温度で一定
に保持しながら、炉内雰囲気を高純度の窒素ガスで置換
して窒素ガス圧760 Torrとし、そのまま18時
間にわたって加熱保持し、その後500℃までは約り0
℃/分の降温速度で冷却し、その後は炉冷した。Reference Examples 10-11 and Comparative Examples 4-5 Titanium (industrial pure titanium) powder and titanium alloy (Ti
-6Aρ-4V) powders were placed in a vacuum furnace and heated to 750° C. at a rate of approximately 0° C./min while evacuating to maintain a high vacuum (10 −5 Torr or less). When the temperature inside the furnace reached 750°C, while keeping it constant at this temperature, the atmosphere inside the furnace was replaced with high-purity nitrogen gas to bring the nitrogen gas pressure to 760 Torr, and the temperature was kept heated for 18 hours, and then the temperature was increased to 500°C. Approximately 0
It was cooled at a temperature decreasing rate of °C/min, and then furnace-cooled.
このように表面改質処理を施した純チタン(参考例10
)およびチタン合金(参考例11)ならびに未処理の純
チタン(比較例4)およびチタン合金(比較例5)を、
第1表に示す量で40℃に加熱した5%塩酸、5%リン
酸、5%酢酸および純水中に浸漬し、振盪を加えながら
6時間保持した。その後、処理液を濾過し、200m1
に調整し、各処理液中のTi、Aρ、■の濃度を調べた
。Pure titanium subjected to surface modification treatment in this way (Reference Example 10)
) and titanium alloy (Reference Example 11), untreated pure titanium (Comparative Example 4) and titanium alloy (Comparative Example 5),
The samples were immersed in 5% hydrochloric acid, 5% phosphoric acid, 5% acetic acid, and pure water heated to 40° C. in the amounts shown in Table 1, and held for 6 hours while being shaken. After that, the treated liquid was filtered and 200ml
The concentrations of Ti, Aρ, and ■ in each treatment solution were examined.
得られた結果を第2表に示す。なお、処理液中の濃度は
発光分析装置(■CP)を用いて分析し、検量線法によ
り濃度を測定した。また未処理の純チタンおよびチタン
合金と塩酸との組合せにおいて、Tiには発光強度が飽
和してしまったために1000倍希釈液を、また開祖合
せにおいてAρ、■には10倍希釈液を測定に用いた。The results obtained are shown in Table 2. The concentration in the treatment solution was analyzed using a luminescence analyzer (CP), and the concentration was measured by a calibration curve method. In addition, in the combination of untreated pure titanium or titanium alloy with hydrochloric acid, the luminescence intensity was saturated for Ti, so a 1000-fold diluted solution was used for measurement, and a 10-fold diluted solution was used for Aρ and ■ in the Kaiso combination. Using.
第1表
なお、表面処理を行なったものについては、この表面処
理による重量増分を補正した。Table 1 Note that for those that were subjected to surface treatment, the weight increase due to this surface treatment was corrected.
第2表に示す結果から明らかなように、本発明に係わる
表面処理を施したもの(参考例10および11)は、各
種環境において安定しており、そのイオン溶出性は未処
理のもの(比較例4および5)と比較して同等ないしそ
れ以上に優れたものであった。As is clear from the results shown in Table 2, the surface-treated products according to the present invention (Reference Examples 10 and 11) are stable in various environments, and their ion elution properties are lower than that of the untreated products (comparison). Compared with Examples 4 and 5), it was equivalent to or even better.
(発明の効果)
以上述べたように本発明の生体用インプラント材料は、
チタンまたはチタン合金よりなる母材の表面に、亜窒化
チタンを主体とする表面改質層および該表面改質層に接
する下層部位に位置しチタン母材に窒素原子を拡散・固
溶させた窒素拡散硬化層からなる表面層を0.3〜10
0μmの平均厚さで有することを特徴とするものであり
、生体用インプラント材料として必要とされる特性、す
なわち、表面硬度、耐磨耗性、生体適合性、靭性、耐蝕
性、軽量性等に優れるものであるために、人工骨、人工
関節、人工歯根などのような硬組織代替物、あるいは心
臓ペースメーカーのハウジンク、人工心臓弁なとのよう
な人工臓器等として好適に応用できるものである。(Effects of the invention) As described above, the biological implant material of the present invention has
On the surface of the base material made of titanium or titanium alloy, there is a surface-modified layer mainly made of titanium nitride, and a nitrogen layer that is located in the lower layer in contact with the surface-modified layer and diffuses and solidly dissolves nitrogen atoms into the titanium base material. The surface layer consisting of a diffusion hardened layer has a thickness of 0.3 to 10
It is characterized by having an average thickness of 0 μm, and has the characteristics required as a biological implant material, such as surface hardness, abrasion resistance, biocompatibility, toughness, corrosion resistance, and light weight. Because of its excellent properties, it can be suitably used as hard tissue substitutes such as artificial bones, artificial joints, and artificial tooth roots, or as artificial organs such as cardiac pacemaker housings and artificial heart valves.
第1図は、本発明の生体用インプラント材料の表面近傍
の構成を模式的に示す断面図、第2図は本発明の生体用
インプラント材料に係わる参考例の表面のX線回折パタ
ーンおよびその評価の指針となる標準組成のTi2N、
TiNおよびα −TiのX線回折パターン、第3図は
未発明の生体用インプラント材料に係わる参考例、およ
び比較例の表面硬度と加熱保持時間との関係を示すグラ
フ、第4図は本発明の生体用インプラント材料に係わる
参考例、および比較例の引張強さおよび伸びと加熱保持
時間との関係を示すグラフであり、また第5図は本発明
の生体用インプラント材料に係わる参考例の表面から内
部への硬度の推移を示すグラフである。
1・・・チタン材、2・・・表面改質層、3・・・窒素
拡散硬化層、4・・・表面層。
特許出願人 亘起物産株式会社
代理人 弁理士 八 1) 幹 雄(他1名)p、
面のX椙勿り竹ベグーン
− I司折弓
′三; ノン−a 万づこnヌcg
;134寸 ヒ め 関イ本已
−スnロ り烹5イ琢待Rそ1丁A (hr
)第4図FIG. 1 is a cross-sectional view schematically showing the structure near the surface of the biological implant material of the present invention, and FIG. 2 is an X-ray diffraction pattern of the surface of a reference example of the biological implant material of the present invention and its evaluation. Ti2N with standard composition as a guideline for
X-ray diffraction patterns of TiN and α-Ti; FIG. 3 is a graph showing the relationship between surface hardness and heating retention time of reference and comparative examples of uninvented biological implant materials; FIG. FIG. 5 is a graph showing the relationship between the tensile strength and elongation and the heating holding time of Reference Examples and Comparative Examples related to the biological implant materials of the present invention, and FIG. It is a graph showing the transition of hardness from to the inside. DESCRIPTION OF SYMBOLS 1...Titanium material, 2...Surface modification layer, 3...Nitrogen diffusion hardening layer, 4...Surface layer. Patent applicant Waki Bussan Co., Ltd. Agent Patent attorney 8 1) Mikio (and 1 other person) p.
Men's
; 134 cm Hime Sekii Honmi - Sun Ro Ripan 5 I Takumachi R So 1 Cho A (hr
) Figure 4
Claims (1)
亜窒化チタンを主体とする表面改質層および該表面改質
層に接する下層部位に位置しチタン母材に窒素原子を傾
斜組成を以て拡散・固溶させた窒素拡散硬化層からなる
表面層を0.3〜100μmの平均厚さで有することを
特徴とするイオン溶出を抑えた生体用インプラント材料
。(1) On the surface of the base material made of titanium or titanium alloy,
A surface layer consisting of a surface modified layer mainly composed of titanium nitride and a nitrogen diffusion hardened layer located in the lower layer in contact with the surface modified layer and in which nitrogen atoms are diffused and dissolved in the titanium base material with a gradient composition. An implant material for biological use that suppresses ion elution, characterized by having an average thickness of 3 to 100 μm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2336099A JPH04200557A (en) | 1990-11-30 | 1990-11-30 | Implant material for living body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2336099A JPH04200557A (en) | 1990-11-30 | 1990-11-30 | Implant material for living body |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH04200557A true JPH04200557A (en) | 1992-07-21 |
Family
ID=18295686
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2336099A Pending JPH04200557A (en) | 1990-11-30 | 1990-11-30 | Implant material for living body |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH04200557A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0726387A (en) * | 1993-07-09 | 1995-01-27 | Mitsubishi Steel Mfg Co Ltd | Surface modification method of titanium or titanium alloy |
| WO1996025960A1 (en) * | 1995-02-22 | 1996-08-29 | Miladin Lazarov | Implant |
| JP2008506532A (en) * | 2004-07-09 | 2008-03-06 | フラウンホーファー−ゲゼルシャフト ツル フェルデルング デル アンゲヴァンテン フォルシュング エー ファウ | Method for producing a wear-resistant and fatigue-resistant edge layer in the form of a titanium alloy and components produced by said method |
| JP2015519470A (en) * | 2012-03-23 | 2015-07-09 | コリア インスティテュート オブ マシーナリィ アンド マテリアルズ | Method for forming a hard layer on titanium and titanium alloy having a hard layer formed thereby |
-
1990
- 1990-11-30 JP JP2336099A patent/JPH04200557A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0726387A (en) * | 1993-07-09 | 1995-01-27 | Mitsubishi Steel Mfg Co Ltd | Surface modification method of titanium or titanium alloy |
| WO1996025960A1 (en) * | 1995-02-22 | 1996-08-29 | Miladin Lazarov | Implant |
| JP2008506532A (en) * | 2004-07-09 | 2008-03-06 | フラウンホーファー−ゲゼルシャフト ツル フェルデルング デル アンゲヴァンテン フォルシュング エー ファウ | Method for producing a wear-resistant and fatigue-resistant edge layer in the form of a titanium alloy and components produced by said method |
| JP2015519470A (en) * | 2012-03-23 | 2015-07-09 | コリア インスティテュート オブ マシーナリィ アンド マテリアルズ | Method for forming a hard layer on titanium and titanium alloy having a hard layer formed thereby |
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