JP5616845B2 - Method for producing Co-based alloy for living body - Google Patents
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- 238000004519 manufacturing process Methods 0.000 title claims description 24
- 238000005242 forging Methods 0.000 claims description 72
- 238000001816 cooling Methods 0.000 claims description 63
- 238000010438 heat treatment Methods 0.000 claims description 31
- 238000012545 processing Methods 0.000 claims description 19
- 239000000203 mixture Substances 0.000 claims description 13
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- 229910052750 molybdenum Inorganic materials 0.000 claims description 2
- 239000013078 crystal Substances 0.000 description 39
- 238000000034 method Methods 0.000 description 19
- 238000005259 measurement Methods 0.000 description 13
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 229910000531 Co alloy Inorganic materials 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 2
- 210000000629 knee joint Anatomy 0.000 description 2
- 238000000691 measurement method Methods 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
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- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
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Description
本発明は、耐食性が高いのは勿論のこと、強度と延性の両方のバランスが良く、人工骨、特に人工関節の素材として好適に用いることができる生体用Co基合金の製造方法に関するものである。 The present invention relates to a method for producing a Co-based alloy for a living body that has a good balance between strength and ductility as well as high corrosion resistance and can be suitably used as a material for artificial bones, particularly artificial joints. .
生体用Co基合金は、従来から人工骨、特に人工関節の素材として使用されており、この生体用Co基合金としては、ASTM規格のF799が知られている。しかしながら、このASTM−F799には、人工骨用の生体用Co基合金が満たすべき特性として、大まかな化学組成の範囲と機械的性質、および大まかな製造方法の規定はあるものの具体的な規定はされていない。 Background Art Co-based alloys for living bodies have been conventionally used as materials for artificial bones, particularly artificial joints, and ASTM standard F799 is known as this living body Co-based alloy. However, although this ASTM-F799 has a rough chemical composition range and mechanical properties, and a rough manufacturing method as characteristics to be satisfied by a bio-based Co-based alloy for artificial bone, the specific provisions are as follows. It has not been.
人工骨、特に人工関節が求められる主な特性は強度と延性であり、まず、この強度と延性の両方のバランスが良いことが必要である。その中でも、膝関節や股関節には、生体用金属材料(生体用Co基鋳造合金)と、生体用ポリエチレンがこすれ合う部位があり、この生体用金属材料は、生体用ポリエチレンを摩耗させずに、且つ、生体用ポリエチレンによって摩耗されない特性が求められている。また、当然のことではあるが、人工関節そのものが大型化することは問題があるので、強度が基本的特性として必要である。 The main characteristics required of an artificial bone, particularly an artificial joint, are strength and ductility. First, it is necessary to have a good balance between both strength and ductility. Among them, in the knee joint and hip joint, there is a site where the biomedical metal material (Co-based casting alloy for biomedical use) and the biomedical polyethylene rub against each other. In addition, there is a demand for characteristics that are not worn by biomedical polyethylene. As a matter of course, since there is a problem that the artificial joint itself is enlarged, strength is necessary as a basic characteristic.
その上で、特に膝関節などに用いられる生体用金属材料においては、3次元の複雑な形状に加工する必要性がある。 In addition, there is a need to process a three-dimensional complicated shape in a metal material for a living body used particularly for a knee joint or the like.
このような、人工骨に用いられる生体用金属材料、特に生体用Co基合金に関する先行技術としては、例えば、以下の特許文献1〜3に記載された提案がある。 As a prior art regarding such a metal material for a living body used for an artificial bone, particularly a Co-based alloy for a living body, for example, there are proposals described in Patent Documents 1 to 3 below.
特許文献1には、HCP相であるε相を実質的に単相とすることで、十分な延性を得ることができた生体適合性Co基合金とその合金の製造方法が開示されている。しかしながら、800℃で24時間の長時間熱処理を施す必要があるため、十分な延性は確保できるものの、最高強度は800MPa程度に留まっており、人工骨、特に人工関節の素材として用いるには強度不足である。 Patent Document 1 discloses a biocompatible Co-based alloy that can obtain sufficient ductility by making the ε phase, which is an HCP phase, substantially a single phase, and a method for producing the alloy. However, since it is necessary to perform heat treatment for 24 hours at 800 ° C., sufficient ductility can be secured, but the maximum strength remains at about 800 MPa, and the strength is insufficient for use as a material for artificial bones, particularly artificial joints. It is.
特許文献2には、生体用Co基合金とその合金の製造方法が記載されている。この合金は、水冷銅鋳型を用いて急冷鋳造し、得られた鋳塊を鍛造して、平均結晶粒径を50μm以下の組織に調整することで得られるものであるが、その実施例によると、Co−29Cr−6Mo合金の場合で1200MPa近い強度を得ることができている。また、Niを16〜24%添加したCo基合金では、1000MPa程度の強度ながら真歪みで0.5近い破断伸びも得ることができており、一方、Niを添加しないCo基合金では、真歪みで0.2程度までの破断伸びが得られている(強度は1200MPa)。 Patent Document 2 describes a Co-based alloy for living organisms and a method for producing the alloy. This alloy is obtained by quench-casting using a water-cooled copper mold, forging the resulting ingot, and adjusting the average crystal grain size to a structure of 50 μm or less. In the case of Co-29Cr-6Mo alloy, a strength close to 1200 MPa can be obtained. In addition, the Co-based alloy to which Ni is added in an amount of 16 to 24% can obtain a fracture elongation close to 0.5 with a true strain with a strength of about 1000 MPa, while the Co-based alloy to which Ni is not added has a true strain. The elongation at break up to about 0.2 is obtained (strength is 1200 MPa).
しかしながら、Niの添加は生体適合性の観点からは好ましくはなく、たとえ添加するとしても必要最小限の量にすべきであり、16〜24%というNiの多量添加は、生体適合性の観点から特に好ましくはない。また、Niを添加しない場合に得られる強度および延性は、特殊な鋳型を用いて鋳込むという方法を採用することで得られるものであり、大幅なコスト増を避けることはできない。 However, addition of Ni is not preferable from the viewpoint of biocompatibility, and even if it is added, it should be made the minimum necessary amount, and a large amount of Ni of 16 to 24% is added from the viewpoint of biocompatibility. It is not particularly preferable. Further, the strength and ductility obtained when Ni is not added can be obtained by adopting a method of casting using a special mold, and a significant increase in cost cannot be avoided.
また、本発明者らは、多量のNi添加、特殊な鋳型を用いて鋳込む方法を共に採用しなくても、従来の生体用Co基合金と同等もしくはそれ以上の強度および延性を得ることができる生体用Co基合金とその製造方法を提案している。 In addition, the present inventors can obtain a strength and ductility equivalent to or higher than those of conventional biomedical Co-based alloys without adopting both a large amount of Ni addition and a casting method using a special mold. A bio-based Co-based alloy and a method for producing the same are proposed.
この生体用Co合金は、Cr:26〜30質量%、Mo:5〜8質量%、C:0.20質量%以下(0質量%を含まず)、N:0.05〜0.25質量%を含有し、残部が実質的にCoからなると共に、結晶粒径の平均値が1.5〜15μmであり、FCC相の割合が面積率で90%以上である生体用Co基合金である。また、所定の成分組成のCo基合金を、結晶粒径の平均値を1.5〜15μm、FCC相の割合(面積率)を90%以上とするための方法として3種の製造方法を提案している。 The biomedical Co alloy has Cr: 26 to 30% by mass, Mo: 5 to 8% by mass, C: 0.20% by mass or less (not including 0% by mass), and N: 0.05 to 0.25% by mass. Is a bio-based Co-based alloy in which the balance is substantially made of Co, the average value of the crystal grain size is 1.5 to 15 μm, and the ratio of the FCC phase is 90% or more in area ratio . In addition, three types of manufacturing methods are proposed as methods for setting the average value of the crystal grain size to 1.5 to 15 μm and the ratio (area ratio) of the FCC phase to 90% or more for a Co-based alloy having a predetermined component composition. doing.
その製造方法は、所定の成分組成のCo基合金を、950〜1250℃に加熱し、鍛造打ち上がり温度:870℃以上、付与する鍛造歪み:30%以上の条件で鍛造した後、2〜200秒空冷し、しかる後、直ちに水冷する方法、所定の成分組成のCo基合金を、950〜1250℃に加熱し、鍛造打ち上がり温度:870℃以上、付与する鍛造歪み:30%以上の条件で鍛造した後、1〜50℃/sの冷却速度で冷却する方法、所定の成分組成のCo基合金を、1250℃以上の温度に加熱した後、この加熱温度以下1000℃以上の温度で合計30%以上の加工歪を加える鍛造をし、この鍛造の終了後0.5〜20秒以内の間に冷却を開始し、30℃/s以上の冷却速度で300℃以下まで冷却する方法、以上3種の方法である。 The manufacturing method is as follows: a Co-based alloy having a predetermined component composition is heated to 950 to 1250 ° C., forged at a forging temperature of 870 ° C. or higher, and forged strain to be applied: 30% or higher. Air cooling for a second, followed by water cooling immediately, a Co-based alloy having a predetermined component composition is heated to 950 to 1250 ° C., forging launch temperature: 870 ° C. or higher, and forging strain to be applied: 30% or higher. After forging, a method of cooling at a cooling rate of 1 to 50 ° C./s, a Co-based alloy having a predetermined component composition is heated to a temperature of 1250 ° C. or higher, and a total of 30 at a temperature of 1000 ° C. or higher at the heating temperature or lower. % Forging that applies processing strain of at least%, starting cooling within 0.5 to 20 seconds after completion of the forging, and cooling to 300 ° C. or less at a cooling rate of 30 ° C./s or more, 3 Seed method.
しかしながら、これら何れの方法で生体用Co合金を製造したとしても、最終的に3次元の複雑な形状に加工するためには、バリ取りを行った後で必ず切削加工を行う必要があった。このように、高強度な材料を加工するために切削加工を行うと、結果として多大な時間とコストを費やすこととなり、この事後の切削加工が生体用Co基合金を製造するための大きな負担となっていた。 However, even if any of these methods is used to produce a biomedical Co alloy, in order to finally process it into a three-dimensional complicated shape, it is necessary to perform cutting after deburring. As described above, when cutting is performed to process a high-strength material, a lot of time and cost are consumed as a result, and the subsequent cutting processing has a large burden for producing a bio-based Co-based alloy. It was.
本発明は、上記従来の問題を解決せんとしてなされたもので、耐食性が高いことは勿論のこと、強度と延性の両方のバランスが良く、人工骨の素材として好適に用いることができる生体用Co基合金を、最終的な3次元の複雑な仕上がり形状に近い形状にまで鍛造することができ、事後の切削加工の手間の軽減或いは切削加工自体を不要にすることができる生体用Co基合金の製造方法を提供することを課題とするものである。 The present invention has been made as a solution to the above-described conventional problems, and has a high balance of corrosion resistance as well as a high balance between strength and ductility, and can be suitably used as a material for artificial bones. It is possible to forge the base alloy to a shape close to the final three-dimensional complicated finished shape, and reduce the labor of subsequent cutting or eliminate the need for the cutting itself. It is an object of the present invention to provide a manufacturing method.
請求項1記載の発明は、質量%で、Cr:26〜30%、Mo:5〜8%、C:0.20%以下(0%を含まない)、N:0.05〜0.25%を含有し、残部がCoおよび不可避的不純物からなる生体用Co基合金の製造方法であって、前記成分組成のCo基合金を、950℃〜1250℃で加熱した後、この加熱温度以下であり且つ850℃〜1050℃の温度で、合計30%以上の加工歪みを加えて鍛造を行い、この鍛造終了後5秒以内に冷却を開始し、30℃/s以上の冷却速度で300℃以下になるまで冷却を行う第1工程と、その第1工程終了後、Co基合金の表面のバリや余肉を除去した後に850〜1050℃で5〜60分間加熱し、その後、この加熱温度以下であり且つ850〜1000℃の温度で合計15%以下の加工歪みを加えて鍛造を行い、この鍛造終了後20秒以内に冷却を開始し、30℃/s以上の冷却速度で300℃以下になるまで冷却を行う第2工程とよりなることを特徴とする生体用Co基合金の製造方法である。 The invention according to claim 1 is mass%, Cr: 26-30%, Mo: 5-8%, C: 0.20% or less (not including 0%), N: 0.05-0.25. %, And the balance is made of Co and inevitable impurities, and the Co-based alloy having the above component composition is heated at 950 ° C. to 1250 ° C. Yes, forging is performed at a temperature of 850 ° C. to 1050 ° C. with a processing strain of 30% or more in total, and cooling is started within 5 seconds after the completion of the forging, and 300 ° C. or less at a cooling rate of 30 ° C./s or more. After the first step of cooling until the first step is completed, after removing the burrs and surplus on the surface of the Co-based alloy, it is heated at 850 to 1050 ° C. for 5 to 60 minutes, and then below this heating temperature And a total processing of 15% or less at a temperature of 850 to 1000 ° C. And forging is performed, and cooling is started within 20 seconds after the end of the forging, and the second step of cooling to 300 ° C. or less at a cooling rate of 30 ° C./s or more. This is a method for producing a bio-based Co-based alloy.
請求項2記載の発明は、前記生体用Co基合金が、質量%で、Si:0.5〜1.0%、および/または、Mn:0.5〜1.0%を含有する請求項1記載の生体用Co基合金の製造方法である。 The invention according to claim 2 is characterized in that the bio-based Co-based alloy contains Si: 0.5 to 1.0% and / or Mn: 0.5 to 1.0% by mass. 1. A method for producing a living body Co-based alloy according to 1.
本発明の生体用Co基合金の製造方法によると、耐食性が高いのは勿論のこと、強度と延性の両方のバランスが良く、人工骨の素材として好適に用いることができる生体用Co基合金を、最終的な3次元の複雑な仕上がり形状に近い形状にまで鍛造することが可能となり、多大な時間とコストを費やす事後の切削加工の手間を軽減、或いはその切削加工自体を不要にすることができる。 According to the method for producing a bio-based Co-based alloy of the present invention, a bio-based Co-based alloy that has a good balance between strength and ductility as well as high corrosion resistance and can be suitably used as a material for artificial bones. It is possible to forge to a shape that is close to the final three-dimensional complex finished shape, reducing the time and cost of post-cutting work that consumes a lot of time and cost, or making the cutting process itself unnecessary. it can.
以下、本発明を実施形態に基づいて更に詳細に説明する。 Hereinafter, the present invention will be described in more detail based on embodiments.
Co基合金は、耐食性が高いのは勿論のこと、強度と延性の両方のバランスが良いという特長を有するため、従来から人工骨、特に人工関節の素材として好適に用いられていたが、製造時において最終的な3次元の複雑な形状に加工するために、多大な時間とコストを費やす切削加工が必ず必要となっていた。そのため、本発明者らは、この切削加工を不要、或いは少なくとも切削加工の手間の軽減を図ることができる生体用Co基合金の製造方法を開発するために、鋭意研究を重ねた。 Co-based alloys have been characterized as having a good balance between strength and ductility as well as high corrosion resistance, and so far have been used favorably as materials for artificial bones, especially artificial joints. However, in order to machine the final three-dimensional complex shape, cutting that consumes a great deal of time and cost is indispensable. For this reason, the present inventors have conducted extensive research in order to develop a method for producing a bio-based Co-based alloy that does not require this cutting process or at least reduces the labor of the cutting process.
その結果、従来は一工程のみで行っていた鍛造を、二つの工程に分け、第1工程および第2工程の製造条件を適宜規定することで、多大な時間とコストを費やす事後の切削加工を不要とすること、或いは少なくとも切削加工の手間の軽減を図れることを見出し、本発明の完成に至った。 As a result, forging, which has conventionally been performed in only one step, is divided into two steps, and by appropriately defining the manufacturing conditions of the first step and the second step, post-cutting processing that consumes a great deal of time and cost. It has been found that it can be eliminated, or at least the labor of cutting can be reduced, and the present invention has been completed.
(成分組成)
まず、生体用Co基合金に添加する各元素の成分範囲(含有量)の限定理由について説明する。尚、単位は全て%と記載するが、他の明細書中の記載を含め、特に断りのない限り全て質量%のことを示す。
(Component composition)
First, the reason for limiting the component range (content) of each element added to the bio-based Co-based alloy will be described. In addition, although all units are described as%, all the mass% is included unless otherwise specified, including descriptions in other specifications.
Cr:26〜30%
Crは、耐食性を確保する上で必須の元素であるが、その含有量が26%未満であると耐食性が劣化し、逆に30%を超えると加工性が劣化してしまう。従って、Crの含有量の範囲は26〜30%とした。
Cr: 26-30%
Cr is an essential element for ensuring corrosion resistance. However, if its content is less than 26%, corrosion resistance deteriorates, and conversely if it exceeds 30%, workability deteriorates. Therefore, the Cr content range is set to 26-30%.
Mo:5〜8%
Moも、耐食性を確保する上で必要な元素であり、また、耐摩耗性の向上に寄与する元素でもある。しかしながら、その含有量が5%未満であると耐食性が劣化し、逆に8%を超えると加工性が劣化してしまう。従って、Moの含有量の範囲は5〜8%とした。
Mo: 5-8%
Mo is also an element necessary for ensuring corrosion resistance, and is also an element contributing to improvement of wear resistance. However, if the content is less than 5%, the corrosion resistance deteriorates, and conversely if it exceeds 8%, the workability deteriorates. Therefore, the range of the Mo content is set to 5 to 8%.
C:0.20%以下(0%を含まない)
Cは、耐摩耗性の必要性や必要具合によって添加されるべき元素であるが、Cの含有量が0.20%を超えた場合には形成される炭化物によって延性が低下することがある。また、融点の低下によって、鍛造時の加熱で1250℃付近まで昇温したときに、合金の一部が溶融して鍛造ができなくなる場合がある。従って、Cの含有量を0.20%以下とした。尚、Cの含有量の好ましい上限は0.10%である。
C: 0.20% or less (excluding 0%)
C is an element to be added depending on the necessity and degree of wear resistance, but when the C content exceeds 0.20%, ductility may be lowered due to the formed carbide. Also, due to the lowering of the melting point, when the temperature is raised to around 1250 ° C. by heating during forging, a part of the alloy may melt and forging may not be possible. Therefore, the content of C is set to 0.20% or less. In addition, the upper limit with preferable content of C is 0.10%.
N:0.05〜0.25%
Nは、Cと同様に侵入型の元素であるが、FCC相(面心立方晶)を安定させる効果と延性を上昇させる効果があるため、必須添加元素とした。しかしながら、Nの添加量(含有量)が0.05%未満では、そのNの添加効果(FCC相安定化効果)が顕著でなくなる。一方、0.25%を超えると、窒化物形成などの延性を低下させる現象の発生が懸念される。従って、Nの含有量の範囲は0.05〜0.25%とした。尚、FCC相安定化の点からはN含有量を0.10%以上とすることが望ましく、0.15%以上とすることが更に望ましい。
N: 0.05-0.25%
N is an interstitial element similar to C, but has an effect of stabilizing the FCC phase (face-centered cubic crystal) and an effect of increasing ductility. However, if the addition amount (content) of N is less than 0.05%, the addition effect of N (FCC phase stabilization effect) is not significant. On the other hand, if it exceeds 0.25%, there is a concern that the phenomenon of reducing ductility such as nitride formation may occur. Therefore, the content range of N is set to 0.05 to 0.25%. From the viewpoint of stabilizing the FCC phase, the N content is preferably 0.10% or more, and more preferably 0.15% or more.
以上が本発明で規定する必須の含有元素であって、残部はCoおよび不可避的不純物である。不可避的不純物の例としてO、Ni、Fe等を挙げることができるが、Oの含有量が100ppmを超えると、伸びや絞りを低下させる影響がある。Oの含有量を100ppm以下に制御することによって、同様の強度であっても伸びや絞りを向上させることができる。従って、Oの含有量を100ppm以下とすることが望ましい。尚、Oの含有量を100ppm以下とするには、この合金の溶製を真空溶製により行えばよい。酸素濃度を特に制御する必要がない場合には、溶製方法として大気溶製方法を採用することができる。 The above are the essential contained elements specified in the present invention, and the balance is Co and inevitable impurities. Examples of unavoidable impurities include O, Ni, Fe, and the like, but if the O content exceeds 100 ppm, there is an effect of reducing elongation and drawing. By controlling the O content to 100 ppm or less, elongation and drawing can be improved even with the same strength. Therefore, the O content is desirably 100 ppm or less. In order to reduce the O content to 100 ppm or less, the alloy may be melted by vacuum melting. When it is not necessary to control the oxygen concentration, an air melting method can be adopted as a melting method.
また、生体用Co基合金には、更に以下に示す元素を積極的に含有させることも有効であり、含有される化学成分(元素)の種類によって生体用Co基合金の特性が更に改善される。 In addition, it is also effective to positively contain the following elements in the biomedical Co-based alloy, and the characteristics of the biomedical Co-based alloy are further improved depending on the type of chemical component (element) contained. .
Si:0.5〜1.0%、および/または、Mn:0.5〜1.0%
SiおよびMnは、生体用Co基合金を固溶強化し、強度を上げるととともに、熱間加工時およびその直後の空冷において、粒成長を幾分抑制する効果がある。その効果は0.5%未満では顕著ではなく、1.0%を超えるとF799合金の規格外となってしまう。従って、Si:0.5〜1.0%、および/または、Mn:0.5〜1.0%とした。
Si: 0.5 to 1.0% and / or Mn: 0.5 to 1.0%
Si and Mn strengthen the solid solution of the Co-based alloy for biomedical use, increase the strength, and have the effect of somewhat suppressing grain growth during hot working and in air cooling immediately thereafter. The effect is not remarkable when the content is less than 0.5%, and when the content exceeds 1.0%, the F799 alloy becomes out of specification. Therefore, Si: 0.5 to 1.0% and / or Mn: 0.5 to 1.0%.
(製造条件)
次に、以上説明した成分組成のCo基合金を用いて生体用Co基合金を製造する方法について説明する。通常、生体用Co基合金を鍛造により製造する場合は、一度の鍛造で行っており、結晶粒径の平均値を1.5〜15μm、FCC相の割合を面積率で90%以上とすることで、強度と延性の両方のバランスが良い生体用Co基合金を製造することができていたが、本発明の製造方法では二つの工程に分けて鍛造を行う。このように鍛造を二つの工程に分けて行うことにより、生体用Co基合金を、鍛造のみで最終的な3次元の複雑な仕上がり形状に近い形状にすることが可能となる。
(Production conditions)
Next, a method for producing a living body Co-based alloy using the Co-based alloy having the component composition described above will be described. Usually, when a bio-based Co-based alloy is manufactured by forging, it is performed by forging once, the average value of the crystal grain size is 1.5 to 15 μm, and the ratio of the FCC phase is 90% or more in area ratio. Thus, a bio-based Co-based alloy having a good balance between strength and ductility could be manufactured. In the manufacturing method of the present invention, forging is performed in two steps. By performing forging in two steps in this way, it is possible to make the living body Co-based alloy into a shape close to the final three-dimensional complicated finished shape only by forging.
尚、第1工程では結晶粒径はより小さめとし、第2工程で結晶粒径の平均値を最終的な大きさの1.5〜15μmとする。このように第1工程で結晶粒径をより小さめとする理由は、次に説明するとおりである。すなわち、第2工程では大きな加工歪みを加えることができないため、再結晶が発生せず結晶粒径を微細にすることができない。しかし、第2工程の加熱でどうしても結晶粒の粗大化が発生してしまう。よって、大きな加工歪みを加えることが可能な第1工程で結晶粒径を事前に小さくした上で次の第2工程に渡せば、第2工程で結晶粒径の平均値を最終的な大きさの1.5〜15μmとすることが可能となるためである。 In the first step, the crystal grain size is made smaller, and in the second step, the average value of the crystal grain size is set to a final size of 1.5 to 15 μm. The reason why the crystal grain size is made smaller in the first step is as described below. That is, in the second step, since a large processing strain cannot be applied, recrystallization does not occur and the crystal grain size cannot be made fine. However, the coarsening of the crystal grains is inevitably caused by the heating in the second step. Therefore, if the crystal grain size is reduced in advance in the first step where a large processing strain can be applied and then passed to the next second step, the average value of the crystal grain size in the second step is the final size. It is because it becomes possible to set it as 1.5-15 micrometers.
本発明の生体用Co基合金の製造方法は、より詳しくは、前記した所定の成分組成のCo基合金を、950℃〜1250℃で加熱した後、この加熱温度以下であり且つ850℃〜1050℃の温度で、合計30%以上の加工歪みを加えて鍛造を行い、この鍛造終了後5秒以内に冷却を開始し、30℃/s以上の冷却速度で300℃以下になるまで冷却を行う第1工程と、その第1工程終了後、Co基合金の表面のバリや余肉を除去した後に850〜1050℃で5〜60分間加熱し、その後、この加熱温度以下であり且つ850〜1000℃の温度で合計15%以下の加工歪みを加えて鍛造を行い、この鍛造終了後20秒以内に冷却を開始し、30℃/s以上の冷却速度で300℃以下になるまで冷却を行う第2工程とよりなる。以下、第1工程および第2工程に分けて、その製造条件を更に詳細に説明する。 More specifically, in the method for producing a bio-based Co-based alloy of the present invention, the Co-based alloy having the above-mentioned predetermined component composition is heated at 950 ° C. to 1250 ° C., and is below this heating temperature and 850 ° C. to 1050 ° C. Forging is performed at a temperature of 0 ° C. by adding processing strain of 30% or more in total, and cooling is started within 5 seconds after completion of the forging, and cooling is performed at a cooling rate of 30 ° C./s or more until 300 ° C. or less. After completion of the first step and the first step, after removing burrs and surplus on the surface of the Co-based alloy, heating is performed at 850 to 1050 ° C. for 5 to 60 minutes, and thereafter, the heating temperature is equal to or lower than 850 to 1000. Forging is performed by adding a processing strain of 15% or less in total at a temperature of 0 ° C., cooling is started within 20 seconds after the completion of this forging, and cooling is performed until the temperature becomes 300 ° C. or less at a cooling rate of 30 ° C./s or more. It consists of two steps. Hereinafter, the manufacturing conditions will be described in more detail in the first step and the second step.
・第1工程
まず、所定の成分組成のCo基合金を、鍛造前に加熱するが、その加熱温度は950℃〜1250℃とする。鍛造前の加熱温度の下限を950℃とした理由は、その温度が950℃未満では十分なFCC相が得られず、かつ、鍛造するには変形抵抗が高くなりすぎるからである。一方、鍛造前の加熱温度の上限を1250℃とした理由は、加熱温度が1250℃を超えると、Co基合金の炭素濃度によっては一部溶融するおそれがあり、また、鍛造温度まで下げるのに待ち時間が長くかかりすぎるからである。
-1st process First, although Co base alloy of a predetermined component composition is heated before forging, the heating temperature shall be 950 to 1250 degreeC. The reason why the lower limit of the heating temperature before forging is 950 ° C. is that if the temperature is lower than 950 ° C., a sufficient FCC phase cannot be obtained, and the deformation resistance becomes too high for forging. On the other hand, the reason for setting the upper limit of the heating temperature before forging to 1250 ° C. is that if the heating temperature exceeds 1250 ° C., there is a risk of partial melting depending on the carbon concentration of the Co-based alloy. This is because the waiting time takes too long.
続いて、この加熱温度以下であり且つ850℃〜1050℃の温度で、合計30%以上の加工歪みを加えて鍛造を行うが、鍛造温度の下限を850℃とした理由は、鍛造温度が850℃未満では延性を劣化させるε相が生成されるからである。一方、鍛造温度の上限を1050℃とした理由は、鍛造温度が1050℃を超えた場合、結晶粒径が粗大化してしまうからである。 Subsequently, forging is performed at a temperature of 850 ° C. to 1050 ° C. with a processing strain of 30% or more in total and the lower limit of the forging temperature is 850 ° C. The forging temperature is 850 ° C. This is because an ε phase that deteriorates ductility is generated at a temperature lower than ℃. On the other hand, the reason why the upper limit of the forging temperature is 1050 ° C. is that when the forging temperature exceeds 1050 ° C., the crystal grain size becomes coarse.
また、この鍛造の際に付与する加工歪みを合計で30%以上としているのは、FCC相に歪みを加え、動的および静的再結晶を促し、結晶粒径の微細化を促進するためである。加工歪を合計で30%未満にすると再結晶が不十分になり、結晶粒径が粗大化し、平均結晶粒径が15μm超となる。結晶粒径の微細化の点からは、付与する加工歪みを50%以上とすることが望ましい。 The total processing strain applied during forging is 30% or more in order to add strain to the FCC phase, promote dynamic and static recrystallization, and promote refinement of the crystal grain size. is there. When the processing strain is less than 30% in total, recrystallization becomes insufficient, the crystal grain size becomes coarse, and the average crystal grain size exceeds 15 μm. From the viewpoint of refinement of the crystal grain size, it is desirable that the applied processing strain be 50% or more.
この鍛造終了後5秒以内に冷却を開始する。冷却開始が鍛造終了後5秒を超えた場合は、結晶粒径が粗大化してしまう。 Cooling is started within 5 seconds after the end of this forging. When the cooling start exceeds 5 seconds after completion of forging, the crystal grain size becomes coarse.
この冷却の際の冷却速度は30℃/s以上とし、水冷で行うことが望ましい。冷却速度が30℃/s未満の場合、例えば冷却を空冷で行った場合は、結晶粒径が粗大化すると共に、ε相が生成されてしまう。 The cooling rate at the time of this cooling is preferably 30 ° C./s or more, and it is desirable to carry out by water cooling. When the cooling rate is less than 30 ° C./s, for example, when cooling is performed by air cooling, the crystal grain size becomes coarse and an ε phase is generated.
また、冷却は300℃以下になるまで実施する。300℃に到達する前に冷却を停止すると、ε相が生成されてしまう可能性がある。 Moreover, cooling is implemented until it becomes 300 degrees C or less. If cooling is stopped before reaching 300 ° C., an ε phase may be generated.
・第2工程
第1工程終了後、Co基合金の表面に僅かに形成されたバリや余肉を、打ち抜きやレーザー加工などによって除去した後に第2工程を開始するが、まず、鍛造前を開始する前にCo基合金を加熱する。その加熱温度は850〜1050℃とし、加熱時間は5〜60分とする。鍛造前の加熱温度の下限を850℃とした理由は、加熱温度が850℃未満ではε相が生成されてしまう可能性があるからである。一方、鍛造前の加熱温度の上限を1050℃とした理由は、結晶粒径が粗大化するからである。
・ Second step After the first step, the second step is started after removing burrs and surplus slightly formed on the surface of the Co-based alloy by punching or laser processing. The Co-based alloy is heated before the heating. The heating temperature is 850 to 1050 ° C., and the heating time is 5 to 60 minutes. The reason why the lower limit of the heating temperature before forging is 850 ° C. is that if the heating temperature is less than 850 ° C., an ε phase may be generated. On the other hand, the reason why the upper limit of the heating temperature before forging is set to 1050 ° C. is that the crystal grain size becomes coarse.
また、鍛造前の加熱時間の下限を5分とした理由は、加熱時間がそれ未満であると素材の均熱を確保できなくなるためである。一方、鍛造前の加熱時間の上限を60分とした理由は、加熱時間が60分を超えると、結晶粒径が粗大化するからである。 The reason why the lower limit of the heating time before forging is set to 5 minutes is that if the heating time is less than that, it is impossible to ensure soaking of the material. On the other hand, the reason for setting the upper limit of the heating time before forging to 60 minutes is that when the heating time exceeds 60 minutes, the crystal grain size becomes coarse.
続いて、この加熱温度以下であり且つ850〜1000℃の温度で、合計15%以下の加工歪みを加えて鍛造を行うが、鍛造温度の下限を850℃とした理由は、鍛造温度が850℃未満では素材の均熱を確保できなくなるためである。一方、鍛造温度の上限を1000℃とした理由は、鍛造温度が1000℃を超えた場合、結晶粒径が粗大化してしまうからである。 Subsequently, forging is performed at a temperature of 850 to 1000 ° C. at a temperature of 850 to 1000 ° C. with a processing strain of 15% or less in total, but the lower limit of the forging temperature is 850 ° C. The forging temperature is 850 ° C. This is because it is impossible to ensure the soaking of the material if it is less than 1. On the other hand, the reason why the upper limit of the forging temperature is 1000 ° C. is that when the forging temperature exceeds 1000 ° C., the crystal grain size becomes coarse.
また、この鍛造の際に付与する加工歪みを合計で15%以下としているのは、加工歪みが合計で15%を超えるとバリが発生する歪み量となってしまい、第2工程終了後にもバリ取りが必要になってしまうからである。 In addition, the total processing strain applied during forging is 15% or less. If the total processing strain exceeds 15%, the amount of strain that generates burrs is generated. This is because it is necessary to take it.
この鍛造終了後20秒以内に冷却を開始する。冷却開始が鍛造終了後20秒を超えた場合は、結晶粒径が粗大化してしまう。 Cooling is started within 20 seconds after this forging is completed. When the start of cooling exceeds 20 seconds after the end of forging, the crystal grain size becomes coarse.
この冷却の際の冷却速度は30℃/s以上とし、水冷で行うことが望ましい。冷却速度が30℃/s未満の場合、例えば冷却を空冷で行った場合は、結晶粒径が粗大化すると共に、ε相が生成されてしまう。 The cooling rate at the time of this cooling is preferably 30 ° C./s or more, and it is desirable to carry out by water cooling. When the cooling rate is less than 30 ° C./s, for example, when cooling is performed by air cooling, the crystal grain size becomes coarse and an ε phase is generated.
また、冷却は300℃以下になるまで実施する。300℃に到達する前に冷却を停止すると、ε相が生成されてしまう可能性がある。 Moreover, cooling is implemented until it becomes 300 degrees C or less. If cooling is stopped before reaching 300 ° C., an ε phase may be generated.
以上の条件で生体用Co基合金を製造することで、結晶粒径の平均値が1.5〜15μm、FCC相の割合が面積率で90%以上、且つ、最終的な3次元の複雑な仕上がり形状に近い形状とすることができる。このように、結晶粒径の平均値を1.5〜15μm、FCC相の割合を面積率で90%以上とすることで、強度と延性の両方のバランスが良い生体用Co基合金を製造することができる理由は以下に説明する通りである。 By producing a bio-based Co-based alloy under the above conditions, the average value of the crystal grain size is 1.5 to 15 μm, the ratio of the FCC phase is 90% or more in area ratio, and the final three-dimensional complex It can be a shape close to the finished shape. Thus, by setting the average value of the crystal grain size to 1.5 to 15 μm and the ratio of the FCC phase to 90% or more in area ratio, a bio-based Co-based alloy having a good balance between strength and ductility is manufactured. The reason why this can be done is as described below.
(結晶粒径の平均値)
結晶粒径の平均値が1.5μm未満であると、強度は高くなるものの延性が低下する。一方、結晶粒径の平均値が15μmを超えると、人工骨に求められる強度が維持できない。従って、結晶粒径の平均値は1.5〜15μmとすれば良い。延性の点からは結晶粒径の平均値は3.0μm以上とすることが望ましく、5.0μm以上とすることがより望ましく、7.0μm以上とすることが更に望ましい。強度の点からは結晶粒径の平均値は13μm以下とすることが望ましく、10μm以下とすることがより望ましい。
(Average value of crystal grain size)
When the average value of the crystal grain size is less than 1.5 μm, the strength is increased, but the ductility is lowered. On the other hand, if the average value of the crystal grain size exceeds 15 μm, the strength required for the artificial bone cannot be maintained. Therefore, the average value of the crystal grain size may be 1.5 to 15 μm. From the viewpoint of ductility, the average value of the crystal grain size is preferably 3.0 μm or more, more preferably 5.0 μm or more, and further preferably 7.0 μm or more. From the viewpoint of strength, the average value of the crystal grain size is desirably 13 μm or less, and more desirably 10 μm or less.
(FCC相の割合)
FCC相は延性に富む相であり、延性を向上させる作用効果がある。FCC相の割合が面積率で90%未満であると、延性が低下して不十分となる。よって、FCC相の割合は面積率で90%以上とすれば良い。延性の点からは、FCCの割合は面積率で93%以上とすることが望ましい。尚、FCC相とは、面心立方格子の結晶構造を有する相のことである。
(Percentage of FCC phase)
The FCC phase is a phase rich in ductility and has an effect of improving ductility. If the ratio of the FCC phase is less than 90% in terms of area ratio, the ductility is lowered and becomes insufficient. Therefore, the ratio of the FCC phase may be 90% or more in terms of area ratio. From the viewpoint of ductility, the FCC ratio is desirably 93% or more in terms of area ratio. The FCC phase is a phase having a face-centered cubic lattice crystal structure.
以下、実施例を挙げて本発明をより具体的に説明するが、本発明はもとより下記実施例によって制限を受けるものではなく、本発明の趣旨に適合し得る範囲で適宜変更を加えて実施することも可能であり、それらは何れも本発明の技術的範囲に含まれる。 EXAMPLES Hereinafter, the present invention will be described more specifically with reference to examples. However, the present invention is not limited by the following examples, and the present invention is implemented with appropriate modifications within a range that can meet the gist of the present invention. These are all included in the technical scope of the present invention.
まず、表1に示す成分組成のCo基合金を真空溶製で溶製して溶製材を得た。この溶製材を一旦φ26mmに熱間鍛造し、長さ180mmに切り揃えて試験用のCo基合金素材(試料)とした。 First, a Co-based alloy having the composition shown in Table 1 was melted by vacuum melting to obtain a melted material. This melted material was once hot forged to φ26 mm and cut to a length of 180 mm to obtain a Co-based alloy material (sample) for testing.
これら試料を用いて表2に示す条件で第1工程の鍛造を実施した。より詳しくは、作製した各試料を用い、高周波加熱→鍛造→冷却の順序を経て鍛造を実施した。その際の、加熱温度、鍛造温度、鍛造歪(加工歪)、鍛造後保持時間(冷却開始までの時間)、冷却の種別、冷却速度を表2に示す。 The forging of the 1st process was implemented on the conditions shown in Table 2 using these samples. More specifically, forging was carried out using each of the produced samples in the order of high-frequency heating → forging → cooling. Table 2 shows the heating temperature, forging temperature, forging strain (working strain), post-forging retention time (time to start cooling), cooling type, and cooling rate.
次いで、第1工程での鍛造を終了した各試料を用いて表3に示す条件で第2工程の鍛造を実施した。より詳しくは、第1工程で鍛造を終了した各試料の表面のバリや余肉を除去した後、高周波加熱→鍛造→冷却の順序を経て鍛造を実施した。その際の、加熱温度、加熱時間、鍛造温度、鍛造歪(加工歪)、鍛造後保持時間(冷却開始までの時間)、冷却の種別、冷却速度を、表3に示す。 Next, forging in the second step was performed under the conditions shown in Table 3 using each sample for which forging in the first step was completed. More specifically, after removing burrs and surplus on the surface of each sample for which forging was completed in the first step, forging was performed through the sequence of high-frequency heating → forging → cooling. Table 3 shows the heating temperature, heating time, forging temperature, forging strain (working strain), post-forging holding time (time to start cooling), cooling type, and cooling rate.
このように、第1工程および第2工程を経て得られた各Co基合金から試験片を採取し、下記する結晶粒径の測定、引張り試験、およびバリの発生の有無の確認を実施した。尚、参考ではあるが第1工程終了後にも試験片を採取し、結晶粒径の測定、および引張り試験を実施した。試験結果を表3に、第1工程終了後の結果を表3に、それぞれ示す。 Thus, a test piece was collected from each Co-based alloy obtained through the first step and the second step, and the following measurement of crystal grain size, tensile test, and confirmation of the occurrence of burrs were performed. In addition, although it was reference, the test piece was extract | collected even after completion | finish of the 1st process, and the measurement of the crystal grain size and the tensile test were implemented. The test results are shown in Table 3, and the results after the first step are shown in Table 3, respectively.
<結晶粒径の測定方法>
結晶粒径は以下に示すEBSP測定のイメージクオリティマップを用いて測定した。これは、上記Co基合金は非常に耐食性が高く、且つ、結晶粒径が微細なものもあるため、光学顕微鏡での組織観察が困難であったためである。上記イメージクオリティマップの組織写真上で、直線交切法にて粒径を測定し、5点以上の測定を行い、その平均切片長さを測定粒径(平均粒径)とした。
<Measurement method of crystal grain size>
The crystal grain size was measured using an image quality map of EBSP measurement shown below. This is because the Co-based alloy has very high corrosion resistance and has a fine crystal grain size, and thus it is difficult to observe the structure with an optical microscope. On the structure photograph of the image quality map, the particle size was measured by the linear crossing method, five or more points were measured, and the average slice length was taken as the measured particle size (average particle size).
この測定に用いた装置および測定条件は下記のとおりである。
・装置: SEM JEOL JSM 5410
EBSP測定解析システム TSL 社OIM
解析ソフト OIMAnalysis
・測定条件: 測定面積50μmx50μm〜500μmx500μm
・測定間隔: 0.1〜0.4μm
The apparatus and measurement conditions used for this measurement are as follows.
・ Device: SEM JEOL JSM 5410
EBSP Measurement Analysis System TSL OIM
Analysis software OIMA Analysis
Measurement conditions: measurement area 50 μm × 50 μm to 500 μm × 500 μm
・ Measurement interval: 0.1 to 0.4 μm
<FCC率の測定方法>
上記EBSP測定にて、0.1〜0.4μmの測定点ごとにFCC相、ε相(HCP相)もしくはそれ以外の相(今回は殆どない)に自動で判定される。それを図示させるとある種の写真のごとくFCCとHCPの相別に表示させることができる。本実施例では、FCCの測定点数を全測定点数で割ってFCC率(面積率)、すなわちFCC相の割合とした。
<Measurement method of FCC rate>
In the EBSP measurement, it is automatically determined for each measurement point of 0.1 to 0.4 μm as an FCC phase, an ε phase (HCP phase), or other phases (almost no current time). When it is shown in the figure, it can be displayed separately for FCC and HCP as a kind of photograph. In this example, the number of FCC measurement points was divided by the total number of measurement points to obtain the FCC rate (area ratio), that is, the FCC phase ratio.
<引張り試験方法>
φ6.5mmx25mmの平行部を有する引張り試験片を製作し、これを用いて引張り試験を行い、YS:降伏応力(0.2%耐力)、TS:抗張力(引張り強度)、伸び(EL)、絞り(RA)を測定した。このとき、0.2%耐力までは0.5%/minの引張り速度、0.2%耐力から以降破断するまでは10%/minの引張り速度とした。引張り試験機としては、島津200KN油圧式万能試験機を用いた。
<Tensile test method>
A tensile test piece having a parallel portion of φ6.5 mm × 25 mm is manufactured, and a tensile test is performed by using the tensile test piece. YS: Yield stress (0.2% proof stress), TS: Tensile strength (tensile strength), Elongation (EL), Drawing (RA) was measured. At this time, the tensile speed was 0.5% / min up to 0.2% proof stress, and the tensile speed was 10% / min from the 0.2% proof stress until breaking. Shimadzu 200KN hydraulic universal testing machine was used as the tensile testing machine.
本実施例では、YS:降伏応力(0.2%耐力)が800MPa以上、TS:抗張力(引張り強度)が1150MPa以上であり、EL:伸びが12%以上、RA:絞りが12%以上という条件を合格判定条件とし、それら条件を全て満たすものを、強度と延性の両方のバランスが良い生体用Co基合金とした。 In this example, YS: Yield stress (0.2% yield strength) is 800 MPa or more, TS: Tensile strength (tensile strength) is 1150 MPa or more, EL: Elongation is 12% or more, and RA: Drawing is 12% or more. Is a bio-based Co-based alloy having a good balance between strength and ductility.
No.1,No.6,No.9は、Co基合金の成分組成が本発明の要件を満たすと共に製造条件も本発明の要件を満たす発明例である。その結果、強度と延性の両方のバランスが良いCo基合金を、バリが発生することなく製造することができた。 No. 1, No. 1 6, no. 9 is an invention example in which the component composition of the Co-based alloy satisfies the requirements of the present invention and the manufacturing conditions also satisfy the requirements of the present invention. As a result, a Co-based alloy having a good balance between strength and ductility could be produced without generating burrs.
これに対し、No.2は、第1工程での冷却開始が鍛造終了後5秒を超えた比較例、No.3は、第2工程での加熱温度が1050℃を超え、鍛造温度も1000℃を超えた比較例、No.4は、第1工程での鍛造温度が1050℃を超えた比較例である。また、No.5−1は、第2工程での加工歪みが15%を超えた比較例、No.5−2は第2工程での冷却開始が鍛造終了後20秒を超えた比較例である。尚、No.5−1とNo.5−2は、第1工程は同じ条件であるので、表2にはNo.5として示す。 In contrast, no. No. 2 is a comparative example in which the start of cooling in the first step exceeded 5 seconds after completion of forging, No. 2 No. 3 is a comparative example in which the heating temperature in the second step exceeded 1050 ° C. and the forging temperature exceeded 1000 ° C., No. 3 4 is a comparative example in which the forging temperature in the first step exceeded 1050 ° C. No. 5-1 is a comparative example in which the processing strain in the second step exceeded 15%, No. 5-1. 5-2 is a comparative example in which the start of cooling in the second step exceeds 20 seconds after the end of forging. No. 5-1. As for 5-2, since the 1st process is the same conditions, in Table 2, it is No. Shown as 5.
更に、No.10−1とNo.10−2は、第1工程での冷却を空冷で行ったため冷却速度が30℃/s未満となった比較例である。尚、No.10−2は第2工程での冷却も空冷で行ったため第2工程での冷却速度も30℃/s未満となった。因みに、No.10−1とNo.10−2は、第1工程での鍛造温度が1050℃を超えると共に、第1工程での冷却開始も鍛造終了後5秒を超えており、これらの条件でも本発明の条件を満たしていない。尚、No.10−1とNo.10−2は、第1工程は同じ条件であるので、表2にはNo.10として示す。 Furthermore, no. 10-1 and no. 10-2 is a comparative example in which the cooling rate was less than 30 ° C./s because the cooling in the first step was performed by air cooling. No. In No. 10-2, the cooling in the second step was also performed by air cooling, so the cooling rate in the second step was also less than 30 ° C./s. Incidentally, no. 10-1 and no. In No. 10-2, the forging temperature in the first step exceeds 1050 ° C., and the cooling start in the first step also exceeds 5 seconds after the end of forging, and these conditions do not satisfy the conditions of the present invention. No. 10-1 and no. No. 10-2 is No. 1 in Table 2 because the first step is under the same conditions. Shown as 10.
その結果、No.2〜4、No.5−2、No.10−1、No.10−2では、YS:降伏応力(0.2%耐力)、TS:抗張力(引張り強度)、EL:伸び、RA:絞りの何れか1項目以上で合格判定条件を満足することができず、強度と延性の両方のバランスが良いCo基合金を製造することができなかった。また、No.5−1では、鍛造で得たCo基合金にバリが発生してしまった。 As a result, no. 2-4, no. 5-2, no. 10-1, no. 10-2, YS: Yield stress (0.2% proof stress), TS: Tensile strength (tensile strength), EL: Elongation, RA: It is not possible to satisfy the pass judgment condition in any one or more of the items, A Co-based alloy having a good balance between strength and ductility could not be produced. No. In 5-1, burrs were generated in the Co-based alloy obtained by forging.
尚、No.2,No.4,No.10(No.10−1、No.10−2)では第1工程の製造条件が好ましくないので、第1工程終了後の結晶粒径が粗大化しており、また、No.10−1、No.10−2では、FCC相の割合が面積率で90%未満となっている。 No. 2, no. 4, no. 10 (No. 10-1, No. 10-2), the manufacturing conditions of the first step are not preferable, so the crystal grain size after the first step is coarsened. 10-1, no. In 10-2, the ratio of the FCC phase is less than 90% in area ratio.
また、No.7はCの含有量が多すぎる比較例、No.8はNの含有量が多すぎる比較例である。このようにCやNの含有量が多すぎるため、第1工程の鍛造時に割れが発生してしまい、第2工程に進むことができなかった。 No. No. 7 is a comparative example in which the C content is too high, No. 7 8 is a comparative example in which the content of N is too large. Thus, since there was too much content of C and N, the crack generate | occur | produced at the time of the forge of a 1st process, and it could not progress to a 2nd process.
Claims (2)
前記成分組成のCo基合金を、950℃〜1250℃で加熱した後、この加熱温度以下であり且つ850℃〜1050℃の温度で、合計30%以上の加工歪みを加えて鍛造を行い、この鍛造終了後5秒以内に冷却を開始し、30℃/s以上の冷却速度で300℃以下になるまで冷却を行う第1工程と、
その第1工程終了後、Co基合金の表面のバリや余肉を除去した後に850〜1050℃で5〜60分間加熱し、その後、この加熱温度以下であり且つ850〜1000℃の温度で合計15%以下の加工歪みを加えて鍛造を行い、この鍛造終了後20秒以内に冷却を開始し、30℃/s以上の冷却速度で300℃以下になるまで冷却を行う第2工程とよりなることを特徴とする生体用Co基合金の製造方法。 In mass%, Cr: 26-30%, Mo: 5-8%, C: 0.20% or less (excluding 0%), N: 0.05-0.25%, the balance being Co And a method for producing a bio-based Co-based alloy comprising inevitable impurities,
After the Co-based alloy having the above component composition is heated at 950 ° C. to 1250 ° C., forging is performed at a temperature not higher than this heating temperature and at a temperature of 850 ° C. to 1050 ° C. with a working strain of 30% or more in total. A first step of starting cooling within 5 seconds after the end of forging, and cooling to 300 ° C. or lower at a cooling rate of 30 ° C./s or higher;
After completion of the first step, after removing burrs and surplus on the surface of the Co-based alloy, heating is performed at 850 to 1050 ° C. for 5 to 60 minutes, and then the heating temperature is equal to or lower than 850 to 1000 ° C. Forging is performed by applying a processing strain of 15% or less, and cooling is started within 20 seconds after the forging is completed, and cooling is performed until the temperature becomes 300 ° C. or less at a cooling rate of 30 ° C./s or more. A method for producing a bio-based Co-based alloy.
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