WO2018040301A1 - Co-cr-mo alloy, machining method for scalpel for minimally invasive operation, and scalpel for minimally invasive operation - Google Patents

Co-cr-mo alloy, machining method for scalpel for minimally invasive operation, and scalpel for minimally invasive operation Download PDF

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Publication number
WO2018040301A1
WO2018040301A1 PCT/CN2016/106411 CN2016106411W WO2018040301A1 WO 2018040301 A1 WO2018040301 A1 WO 2018040301A1 CN 2016106411 W CN2016106411 W CN 2016106411W WO 2018040301 A1 WO2018040301 A1 WO 2018040301A1
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Prior art keywords
processing
alloy
minimally invasive
treatment
temperature
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PCT/CN2016/106411
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French (fr)
Chinese (zh)
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李云平
聂炎
李军旗
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深圳市圆梦精密技术研究院
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Publication of WO2018040301A1 publication Critical patent/WO2018040301A1/en

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    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B17/00Surgical instruments, devices or methods, e.g. tourniquets
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/07Alloys based on nickel or cobalt based on cobalt
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B17/00Surgical instruments, devices or methods, e.g. tourniquets
    • A61B17/00234Surgical instruments, devices or methods, e.g. tourniquets for minimally invasive surgery
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B17/00Surgical instruments, devices or methods, e.g. tourniquets
    • A61B17/32Surgical cutting instruments
    • A61B17/3209Incision instruments
    • A61B17/3211Surgical scalpels, knives; Accessories therefor
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/02Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working in inert or controlled atmosphere or vacuum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon

Definitions

  • Co-Cr-Mo alloy processing method of minimally invasive scalpel and minimally invasive scalpel
  • the present invention belongs to the technical field of cobalt-based alloys for medical devices, and more particularly to a Co-Cr-Mo alloy, a processing method for a minimally invasive scalpel, and a minimally invasive scalpel.
  • an embodiment of the present invention provides a Co-Cr-Mo alloy, a processing method of a minimally invasive scalpel, and a minimally invasive scalpel.
  • a Co-Cr-Mo alloy consisting of the following components in mass percentage:
  • the balance is Co and unavoidable impurities, wherein the content of the Zr does not take zero.
  • a method for processing a minimally invasive scalpel comprising at least the following steps:
  • the tool obtained by processing the plate material is subjected to a aging treatment and a nitriding treatment.
  • the Co-Cr-Mo alloy provided by the above embodiments of the present invention increases the alloy ⁇ phase by adding carbon to the Co-Cr-Mo, so that the alloy has a biocompatible homologous to form a dispersed carbide.
  • the corrosion resistance and biocompatibility at the interface are improved, the hot workability of the material is improved, and the elastic modulus, tensile strength and wear resistance of the alloy are finally improved.
  • the method for processing a minimally invasive scalpel uses a plastic processing method to homogenize the alloy obtained by smelting, so that the components of the alloy are uniform, and the carbides and nitrides are dispersed and distributed.
  • the performance of the alloy is uniform and stable.
  • the hardness of the minimally invasive scalpel is 700 ⁇ 900H V and the strength is up to 1200 ⁇ 1300MPa, which greatly improves the elasticity and cutting performance of the scalpel.
  • FIG. 1 is an IQ (Image quality) diagram of EBSD after solution treatment of the Co-24Cr-4Mo-0.15C alloy according to an embodiment of the present invention.
  • FIG. 1b is an embodiment of the present invention, after the solution treatment of Co-24Cr-4Mo-0.1C alloy is carried out at 1100 ° C, the relative speed is
  • FIG. 1c is an IQ diagram of EBSD after a solution treatment of a Co-24Cr-4Mo-0.15C alloy according to an embodiment of the present invention after 1100 ° C, a relative speed of 1.0 s - 60% + 900 ° C, 60% deformation.
  • 1D is an EBSD of a Co-24Cr-4Mo-0.2C alloy after solution treatment at 1100 ° C, a relative speed of 1.0 s - ', 60% + 900 ° C, 60% deformation after the solution treatment of the embodiment of the present invention.
  • IQ diagram
  • FIG. 1 is a sample of Co-24Cr-4Mo-0.2C-0.15N-0.05Zr alloy after solution treatment, after 1100 °C, relative speed is 1.0s - 60% + 900 °C, IQ map of EBSD after 60% deformation;
  • 2a is a topographical view of a Co-24Cr-4Mo-0.2C-0.15N alloy oxidized in air at 700 ° C according to an embodiment of the present invention
  • 2b is a topographical view of the Co-24Cr-4Mo-0.2C-0.15N-0.05Zr alloy oxidized in air at 700 ° C according to an embodiment of the present invention
  • 3a is a cross-sectional view of a Co-24Cr-4Mo-0.2C-0.15N alloy oxidized in air at 700 ° C according to an embodiment of the present invention
  • 3b is a cross-sectional view of a Co-24Cr-4Mo-0.2C-0.15N-0.05Zr alloy oxidized in air at 700 ° C according to an embodiment of the present invention
  • a Co-29Cr-6Mo
  • b Co-24Cr-4Mo
  • c Co-24Cr-4Mo-0.
  • Embodiments of the present invention provide a Co-Cr-Mo alloy.
  • the Co-Cr-Mo alloy consists of the following components:
  • the balance is Co and unavoidable impurities, wherein the content of the Zr is not taken as zero.
  • Cr can improve the corrosion resistance and biocompatibility of the alloy.
  • the Cr content is lower than 22%, the presence of Cr does not improve the corrosion resistance of the alloy; after adding the Zr element, since Zr is in the alloy The surface can quickly form a dense oxide film, so that the Cr content is within 26% to ensure the corrosion resistance and biocompatibility of the alloy, and when the Cr content exceeds 26%, it is prone to occur in the subsequent heat treatment process.
  • the ⁇ phase that causes the brittleness of the alloy.
  • Mo can improve the grain boundary corrosion performance of the alloy, and solid solution strengthening.
  • Zr can form a dense oxide film on the surface of the alloy quickly. Compared with the prior art, the corrosion resistance and biocompatibility of the alloy can be ensured under the condition of Mo content of 3 to 6%. .
  • the C element having a mass percentage of 0.1 to 0.2% can form a carbide in the alloy to increase the strength of the alloy.
  • the cerium element having a mass percentage of 0.05 to 0.2% can improve the alloy processing property and grain refinement in the alloy.
  • the Zr element can repair the passivation film on the surface of the alloy in the alloy, and further increase the metal ion precipitation of the alloy in the body.
  • the Zr element content is above 0.06%, a brittle s phase is formed in the alloy, which is distributed at the grain boundary, which reduces the toughness of the alloy. Therefore, the Zr content is generally controlled at 0 to 0.06%, and the value of 0 is not taken.
  • the mass percentage of Zr is 0.03 to 0.06 ⁇ 3 ⁇ 4.
  • the Zr content is 0.03 0.06% ⁇ , which can ensure that Cr and Mo can play a corresponding role in the alloy at the above content, and ensure the corrosion resistance and biocompatibility of the alloy.
  • the Co-Cr-Mo alloy provided by the above embodiments of the present invention, by adding carbon to Co-Cr-Mo, makes the alloy have a biocompatible homologous to form a dispersed carbide, thereby improving the alloy ⁇ phase.
  • the stability, especially the Zr element repairs the passivation film on the surface of the alloy compensates for the deficiency of Cr and Mo elements at the interface between the carbide and the alloy matrix, improves the corrosion resistance and biocompatibility at the interface, and also improves the alloy. Modulus of elasticity, tensile strength and wear resistance.
  • the present invention further provides a processing method of a minimally invasive scalpel based on the Co-Cr-Mo alloy formulation component provided in the above embodiments.
  • the method for processing the minimally invasive scalpel comprises at least the following steps: weighing the components according to the formulation of the Co-Cr-Mo alloy as described above;
  • the tool obtained by processing the sheet material is subjected to a aging treatment and a nitriding treatment.
  • the melting temperature of the alloy is 1500 ° C and 1500 ° C or more.
  • it is 1500 to 1800 ° C, and in this temperature range, melting of all metal components can be achieved.
  • the temperature exceeds 1800 °C, it will cause waste of energy.
  • the alloy smelting process should be carried out under an argon (Ar) atmosphere to avoid the presence of oxygen in the smelting atmosphere which may cause pitting or voiding of the alloy after smelting.
  • Ar argon
  • the temperature is maintained for 30 to 60 minutes to ensure that the components are uniformly melted.
  • the molten alloy is cast into an alloy block. The alloy is then homogenized.
  • the alloy is homogenized, and the temperature of the homogenization treatment should be 1250 ⁇ 1350 ° C in a vacuum or an inert atmosphere, the heating rate is 10-20 ° C / min, and the temperature is kept for 10-24 h. This is followed by furnace cooling or rapid cooling of the high pressure gas.
  • the high pressure gas is any one of high pressure nitrogen or high pressure inert gas
  • the pressure of the high pressure gas is 0.2 to 0.8 MPa; and the cooling rate of the high pressure nitrogen or high pressure inert gas is 20 to 50 ° C / s.
  • the cooling method has no segregation of the alloy composition.
  • the homogenized alloy is subjected to a hot working treatment.
  • the thermal processing includes a first stage thermal processing and a second stage thermal processing.
  • the first stage of the hot working treatment has a temperature of 1100 to 1200 ° C, a relative processing rate of 1 to 10 / s, a processing rate of 60 to 70%, and then natural cooling to 800 to 1000 ° C.
  • the segment thermal processing after the first thermal processing, achieves homogenization of the alloy and prevents the alloy from splitting during subsequent processing.
  • the second stage thermal processing refers to a temperature of 8 00 to 1000 ° C, a relative processing rate of 1 to 10 / s, and a processing rate of 50 to 70%.
  • the grain of the alloy is sharply refined to the micron or submicron level to improve the hardness of the alloy.
  • the sheet is treated as a two-stage hot rolling process.
  • the first section of the hot rolling treatment has a hot rolling temperature of 1100 to 1200 ° C, a relative processing rate of 1 to 10 / s, a processing rate of 60 to 70%, and then natural cooling to 800 to 1000.
  • the second section of the hot rolling treatment is started at ° C; further preferably, the second section of the hot rolling treatment has a temperature of 800 to 1000 ° C, and the relative processing rate is 1 to 1 0/s, processing rate is 50 ⁇ 70 ⁇ 3 ⁇ 4.
  • the tool is subjected to a treatment effect.
  • the conditions for treatment are in a vacuum or protective atmosphere at 70
  • the nitriding treatment refers to placing the treated tool in an ammonia atmosphere, at 40
  • Insulation from 0 to 600 °C for l ⁇ 5h. After nitriding, the hardness and cutting properties of the alloy (ie, the tool) surface are improved.
  • the Co-Cr-Mo alloy provided by the embodiment of the present invention adopts the above method, that is, plastic processing, to prepare a minimally invasive scalpel, and the surface hardness of the knife edge reaches 700-900 HV (Vickers hardness), and the strength is 1200-1300 MPa.
  • the 0.2% yield strength is greater than 900 MPa, which greatly improves the knife edge hardness and cutting performance of the scalpel.
  • Different embodiments of the alloy are prepared into a scalpel, and the hardness of the knife edge after nitriding can be further improved on the basis of the hardness of the alloy in Table 1, and the cutting performance of the scalpel is greatly improved.
  • the surface contains a trace amount of Zr element, which is favorable for forming a denser oxide film on the surface.
  • a small amount of Zr element on the surface is favorable for forming a denser oxide film on the surface of the alloy, suppressing precipitation of the alloying element through the oxide film in the living environment, and improving the biocompatibility of the alloy.
  • a Co-29Cr-6Mo
  • b Co-24Cr-4Mo
  • c Co-24Cr-4Mo-0.15C-0.

Abstract

A Co-Cr-Mo alloy, composed of the following components in percentage by mass: 22-26% of Cr, 3-6% of Mo, 0.1-0.2% of C, 0.05-0.2% of N, and 0-0.06% of Zr, with the balance being Co and inevitable impurities, wherein the Zr content is not zero. For a scalpel, made of the Co-Cr-Mo alloy, for minimally invasive operation, the hardness of the knife edge is up to 700-900 HV, and the strength is 1200-1300 MPa, so that the elasticity and cutting property of the scalpel are greatly enhanced.

Description

Co-Cr-Mo合金、 微创手术刀的加工方法和微创手术刀 技术领域  Co-Cr-Mo alloy, processing method of minimally invasive scalpel and minimally invasive scalpel
[0001] 本发明属于医疗器具钴基合金技术领域, 特别涉及一种 Co-Cr-Mo合金、 微创手 术刀的加工方法和微创手术刀。  [0001] The present invention belongs to the technical field of cobalt-based alloys for medical devices, and more particularly to a Co-Cr-Mo alloy, a processing method for a minimally invasive scalpel, and a minimally invasive scalpel.
背景技术  Background technique
[0002] 传统微创手术刀一般采用不锈钢、 钛合金。 然而无论是不锈钢还是钛合金, 在 手术过程中, 容易发生由于硬度、 弹性模量等方面性能的不足, 发生刀口钝化 或者断裂, 而且由于刀口钝化, 容易引发血管与手术刀缠结等问题。  [0002] Traditional minimally invasive scalpels generally use stainless steel and titanium alloys. However, whether it is stainless steel or titanium alloy, during the operation, it is prone to insufficient performance due to hardness, elastic modulus, etc., and the blade is passivated or broken, and it is easy to cause tangles between the blood vessel and the scalpel due to the passivation of the knife edge. .
技术问题  technical problem
[0003] 针对目前不锈钢、 钛合金微创手术刀在硬度, 弹性模量等方面的不足, 容易在 手术过程中发生断裂, 刀口钝化及由于刀口钝化而引起的血管与手术刀缠结等 问题, 本发明实施例提供一种 Co-Cr-Mo合金、 微创手术刀的加工方法和微创手 术刀。  [0003] In view of the shortcomings of the stainless steel and titanium alloy minimally invasive scalpel in terms of hardness and elastic modulus, it is easy to break during the operation, the knife edge passivation and the tangles of the blood vessel and the scalpel due to the passivation of the knife edge. Problem, an embodiment of the present invention provides a Co-Cr-Mo alloy, a processing method of a minimally invasive scalpel, and a minimally invasive scalpel.
问题的解决方案  Problem solution
技术解决方案  Technical solution
[0004] 为了实现上述发明目的, 本发明的技术方案如下:  [0004] In order to achieve the above object of the invention, the technical solution of the present invention is as follows:
[0005] 一种 Co-Cr-Mo合金, 由质量百分含量如下的组分组成:  [0005] A Co-Cr-Mo alloy consisting of the following components in mass percentage:
[0006] Cr 22-26%;  [0006] Cr 22-26%;
[0007] Mo 3-6%;  [0007] Mo 3-6%;
[0008] C 0.1-0.2%;  [0008] C 0.1-0.2%;
[0009] N 0.05-0.2%;  [0009] N 0.05-0.2%;
[0010] Zr 0-0.06%;  [0010] Zr 0-0.06%;
[0011] 余量为 Co和不可避免的杂质, 其中, 所述 Zr的含量不取 0。  [0011] The balance is Co and unavoidable impurities, wherein the content of the Zr does not take zero.
[0012] 以及, 一种微创手术刀的加工方法, 至少包括以下步骤:  [0012] And, a method for processing a minimally invasive scalpel, comprising at least the following steps:
[0013] 按照如上所述的 Co-Cr-Mo合金的配方称取各组分;  [0013] weighing each component according to the formulation of the Co-Cr-Mo alloy as described above;
[0014] 将称取的所述各组分进行熔炼处理; [0015] 将所述熔炼后的合金进行均匀化处理; [0014] subjecting the weighed components to a smelting process; [0015] performing homogenization treatment on the smelted alloy;
[0016] 将所述均匀化处理得到的合金进行热加工处理; [0016] subjecting the alloy obtained by the homogenization treatment to a thermal processing;
[0017] 将所述热加工处理得到的合金进行板材处理; [0017] subjecting the alloy obtained by the hot working treatment to a plate treatment;
[0018] 将所述板材处理得到的刀具进行吋效、 氮化处理。 [0018] The tool obtained by processing the plate material is subjected to a aging treatment and a nitriding treatment.
[0019] 相应地, 由上述方法制备的微创手术刀。 [0019] Accordingly, a minimally invasive scalpel prepared by the above method.
[0020] 本发明上述实施例提供的 Co-Cr-Mo合金, 通过向 Co-Cr-Mo中加入了碳元素, 使得合金具有生物相容性的同吋形成弥散碳化物, 提高了合金 γ相的稳定性并且 细化了晶粒; 更重要的是向合金中加入了 Zr元素, Zr元素在合金表面的钝化膜中 起到至关重要的修复作用, 在极大的降低 Cr、 Mo元素含量的基础上, 提高界面 处的抗腐蚀性能和生物相容性, 改善了材料的热加工性能, 最终提高合金的弹 性模量、 拉伸强度及耐磨性。  [0020] The Co-Cr-Mo alloy provided by the above embodiments of the present invention increases the alloy γ phase by adding carbon to the Co-Cr-Mo, so that the alloy has a biocompatible homologous to form a dispersed carbide. The stability and refinement of the grains; more importantly, the Zr element is added to the alloy, and the Zr element plays a crucial role in the repair of the passivation film on the surface of the alloy, greatly reducing the Cr and Mo elements. On the basis of the content, the corrosion resistance and biocompatibility at the interface are improved, the hot workability of the material is improved, and the elastic modulus, tensile strength and wear resistance of the alloy are finally improved.
发明的有益效果  Advantageous effects of the invention
有益效果  Beneficial effect
[0021] 本发明实施例提供的微创手术刀的加工方法, 采用塑性加工的手段, 将熔炼获 得的合金进行均匀化处理, 使得合金各个组分均匀, 碳化物、 氮化物弥散分布 , 使获得的合金性能均一稳定, 加工得到的微创手术刀刀口硬度达到 700~900H V, 强度高达 1200~1300MPa, 极大提高手术刀的弹性和切割性能。  [0021] The method for processing a minimally invasive scalpel according to an embodiment of the present invention uses a plastic processing method to homogenize the alloy obtained by smelting, so that the components of the alloy are uniform, and the carbides and nitrides are dispersed and distributed. The performance of the alloy is uniform and stable. The hardness of the minimally invasive scalpel is 700~900H V and the strength is up to 1200~1300MPa, which greatly improves the elasticity and cutting performance of the scalpel.
对附图的简要说明  Brief description of the drawing
附图说明  DRAWINGS
[0022] 图 la为本发明实施例 Co-24Cr-4Mo-0.15C合金固溶处理后 EBSD的 IQ(Image quality)图。  [0022] FIG. 1 is an IQ (Image quality) diagram of EBSD after solution treatment of the Co-24Cr-4Mo-0.15C alloy according to an embodiment of the present invention.
[0023] 图 lb为本发明实施例 Co-24Cr-4Mo-0.1C合金固溶处理后经 1100°C, 相对速度为 [0023] FIG. 1b is an embodiment of the present invention, after the solution treatment of Co-24Cr-4Mo-0.1C alloy is carried out at 1100 ° C, the relative speed is
1.0s ! , 60%+900°C, 60%变形后的 EBSD的 IQ图; 1.0s ! , 60%+900°C, IQ map of EBSD after 60% deformation;
[0024] 图 lc为本发明实施例 Co-24Cr-4Mo-0.15C合金固溶处理后经过 1100°C, 相对速 度为 1.0s - 60%+900°C, 60%变形后的 EBSD的 IQ图 [0024] FIG. 1c is an IQ diagram of EBSD after a solution treatment of a Co-24Cr-4Mo-0.15C alloy according to an embodiment of the present invention after 1100 ° C, a relative speed of 1.0 s - 60% + 900 ° C, 60% deformation.
[0025] 图 Id为本发明实施例 Co-24Cr-4Mo-0.2C合金固溶处理后经过 1100°C, 相对速度 为 1.0s - ', 60%+900°C, 60%变形后的 EBSD的 IQ图; 1D is an EBSD of a Co-24Cr-4Mo-0.2C alloy after solution treatment at 1100 ° C, a relative speed of 1.0 s - ', 60% + 900 ° C, 60% deformation after the solution treatment of the embodiment of the present invention. IQ diagram;
[0026] 图 le为本发明实施例 Co-24Cr-4Mo-0.2C-0.15N-0.05Zr合金固溶处理后经过 1100 °C, 相对速度为 1.0s - 60%+900°C, 60%变形后的 EBSD的 IQ图; [0026] FIG. 1 is a sample of Co-24Cr-4Mo-0.2C-0.15N-0.05Zr alloy after solution treatment, after 1100 °C, relative speed is 1.0s - 60% + 900 °C, IQ map of EBSD after 60% deformation;
[0027] 图 2a为本发明实施例 Co-24Cr-4Mo-0.2C-0.15N合金在 700°C空气里氧化后的表面 形貌图; 2a is a topographical view of a Co-24Cr-4Mo-0.2C-0.15N alloy oxidized in air at 700 ° C according to an embodiment of the present invention;
[0028] 图 2b为本发明实施例 Co-24Cr-4Mo-0.2C-0.15N-0.05Zr合金在 700°C空气里氧化后 的表面形貌图;  2b is a topographical view of the Co-24Cr-4Mo-0.2C-0.15N-0.05Zr alloy oxidized in air at 700 ° C according to an embodiment of the present invention;
[0029] 图 3a为本发明实施例 Co-24Cr-4Mo-0.2C-0.15N合金在 700°C空气里氧化后的断面 形貌图;  3a is a cross-sectional view of a Co-24Cr-4Mo-0.2C-0.15N alloy oxidized in air at 700 ° C according to an embodiment of the present invention;
[0030] 图 3b为本发明实施例 Co-24Cr-4Mo-0.2C-0.15N-0.05Zr合金在 700°C空气里氧化后 的断面形貌图;  3b is a cross-sectional view of a Co-24Cr-4Mo-0.2C-0.15N-0.05Zr alloy oxidized in air at 700 ° C according to an embodiment of the present invention;
[0031] 图 4为为本发明实施例 a: Co-29Cr-6Mo, b: Co-24Cr-4Mo, c: Co-24Cr-4Mo-0.  4 is an embodiment of the present invention: a: Co-29Cr-6Mo, b: Co-24Cr-4Mo, c: Co-24Cr-4Mo-0.
15C-0.1N, d: Co-24Cr-4Mo-0.15C-0.lN-0.05Zr合金的片状样品 (厚度 lmm, 长 50 mm, 宽 10mm), 在 5%乳酸溶液中 37°C, 6个月浸渍后的合金组成元素的析出离 子浓度比较图 (ICP-EOS分析)。  15C-0.1N, d: Co-24Cr-4Mo-0.15C-0.lN-0.05Zr alloy sheet sample (thickness lmm, length 50 mm, width 10 mm), 37 ° C in 5% lactic acid solution, 6 Comparison of precipitation ion concentration of alloy constituent elements after immersion for a month (ICP-EOS analysis).
本发明的实施方式 Embodiments of the invention
[0032] 为了使本发明要解决的技术问题、 技术方案及有益效果更加清楚明白, 以下结 合实施例和说明书附图, 对本发明进行进一步详细说明。 应当理解, 此处所描 述的具体实施例仅仅用以解释本发明, 并不用于限定本发明。  [0032] In order to make the technical problems, technical solutions, and advantageous effects to be solved by the present invention more clearly, the present invention will be further described in detail below with reference to the embodiments and the accompanying drawings. It is understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
[0033] 本发明实施例提供一种 Co-Cr-Mo合金。 该 Co-Cr-Mo合金, 由质量百分含量如 下的组分组成:  [0033] Embodiments of the present invention provide a Co-Cr-Mo alloy. The Co-Cr-Mo alloy consists of the following components:
[0034] Cr 22-26%;  [0034] Cr 22-26%;
[0035] Mo 3-6%;  [0035] Mo 3-6%;
[0036] C 0.1-0.2%;  [0036] C 0.1-0.2%;
[0037] N 0.05-0.2%;  [0037] N 0.05-0.2%;
[0038] Zr 0-0.06%;  [0038] Zr 0-0.06%;
[0039] 余量为 Co和不可避免的杂质, 其中, 所述 Zr的含量不取 0。  [0039] The balance is Co and unavoidable impurities, wherein the content of the Zr is not taken as zero.
[0040] 在任一实施例中, Cr可以提高合金的抗腐蚀性能, 生物相容性。 当 Cr含量低于 22%吋, Cr的存在对合金的抗腐蚀性能改善不大; 添加 Zr元素后, 由于 Zr在合金 的表面可以快速形成致密的氧化膜, 使 Cr含量在 26%以内可以保证合金的抗腐蚀 性与生物相容性, 而当 Cr的含量超过 26%吋, 在后续的吋效热处理过程中容易出 现引起合金脆性的 δ相。 [0040] In any of the embodiments, Cr can improve the corrosion resistance and biocompatibility of the alloy. When the Cr content is lower than 22%, the presence of Cr does not improve the corrosion resistance of the alloy; after adding the Zr element, since Zr is in the alloy The surface can quickly form a dense oxide film, so that the Cr content is within 26% to ensure the corrosion resistance and biocompatibility of the alloy, and when the Cr content exceeds 26%, it is prone to occur in the subsequent heat treatment process. The δ phase that causes the brittleness of the alloy.
[0041] Mo可以提高合金晶界腐蚀性能, 固溶强化。 在添加 Zr的情况下, 由于 Zr在合 金的表面可以快速形成致密的氧化膜, 相比现有技术, 可以使得 Mo含量在 3~6% 的条件下保证合金的抗腐蚀性能与生物相容性。 [0041] Mo can improve the grain boundary corrosion performance of the alloy, and solid solution strengthening. In the case of adding Zr, Zr can form a dense oxide film on the surface of the alloy quickly. Compared with the prior art, the corrosion resistance and biocompatibility of the alloy can be ensured under the condition of Mo content of 3 to 6%. .
[0042] 质量百分含量为 0.1~0.2%的 C元素, 在合金中可以形成碳化物, 提高合金强度[0042] The C element having a mass percentage of 0.1 to 0.2% can form a carbide in the alloy to increase the strength of the alloy.
、 硬度, 稳定 γ相, 晶粒细化。 , hardness, stable γ phase, grain refinement.
[0043] 质量百分含量为 0.05~0.2%的 Ν元素, 在合金中可以提高合金加工性能, 晶粒细 化。 [0043] The cerium element having a mass percentage of 0.05 to 0.2% can improve the alloy processing property and grain refinement in the alloy.
[0044] Zr元素在合金中能够修复合金表面的钝化膜, 进一步提高合金在生体内的金属 离子析出。 Zr元素含量在 0.06%以上吋, 合金内会产生脆性的 s相, 分布于晶界, 使合金韧性下降。 因此, Zr含量一般控制在 0~0.06%, 不取 0值。  [0044] The Zr element can repair the passivation film on the surface of the alloy in the alloy, and further increase the metal ion precipitation of the alloy in the body. When the Zr element content is above 0.06%, a brittle s phase is formed in the alloy, which is distributed at the grain boundary, which reduces the toughness of the alloy. Therefore, the Zr content is generally controlled at 0 to 0.06%, and the value of 0 is not taken.
[0045] 作为优选地, Zr的质量百分含量为 0.03~0.06<¾。 Zr含量在 0.03 0.06%吋, 可以 保证 Cr和 Mo在上述含量下在合金中能发挥相应的作用, 并确保合金的抗腐蚀性 能和生物相容性。  [0045] Preferably, the mass percentage of Zr is 0.03 to 0.06 < 3⁄4. The Zr content is 0.03 0.06% 吋, which can ensure that Cr and Mo can play a corresponding role in the alloy at the above content, and ensure the corrosion resistance and biocompatibility of the alloy.
[0046] 本发明上述实施例提供的 Co-Cr-Mo合金, 通过向 Co-Cr-Mo中加入了碳元素, 使得合金具有生物相容性的同吋形成弥散碳化物, 提高了合金 γ相的稳定性, 尤 其是 Zr元素修复合金表面的钝化膜、 弥补了碳化物与合金基体界面处的 Cr、 Mo 元素的不足, 提高界面处的抗腐蚀性能和生物相容性, 而且还提高合金的弹性 模量、 拉伸强度及耐磨性。  [0046] The Co-Cr-Mo alloy provided by the above embodiments of the present invention, by adding carbon to Co-Cr-Mo, makes the alloy have a biocompatible homologous to form a dispersed carbide, thereby improving the alloy γ phase. The stability, especially the Zr element repairs the passivation film on the surface of the alloy, compensates for the deficiency of Cr and Mo elements at the interface between the carbide and the alloy matrix, improves the corrosion resistance and biocompatibility at the interface, and also improves the alloy. Modulus of elasticity, tensile strength and wear resistance.
[0047] 本发明在上述实施例提供的 Co-Cr-Mo合金配方组分的基础上, 进一步提供了一 种微创手术刀的一种加工方法。  [0047] The present invention further provides a processing method of a minimally invasive scalpel based on the Co-Cr-Mo alloy formulation component provided in the above embodiments.
[0048] 在一实施例中, 所述微创手术刀的加工方法至少包括以下步骤, 按照如上所述 的 Co-Cr-Mo合金的配方称取各组分;  [0048] In an embodiment, the method for processing the minimally invasive scalpel comprises at least the following steps: weighing the components according to the formulation of the Co-Cr-Mo alloy as described above;
[0049] 按照如上所述的 Co-Cr-Mo合金的配方称取各组分;  [0049] weighing each component according to the formulation of the Co-Cr-Mo alloy as described above;
[0050] 将称取的所述各组分进行熔炼处理;  [0050] subjecting the weighed components to a smelting process;
[0051 ] 将所述熔炼后的合金进行均匀化处理; [0052] 将所述均匀化处理得到的合金进行热加工处理; [0051] homogenizing the smelted alloy; [0052] subjecting the alloy obtained by the homogenization treatment to a hot working treatment;
[0053] 将所述热加工处理得到的合金进行板材处理; [0053] subjecting the alloy obtained by the hot working treatment to a plate treatment;
[0054] 将所述板材处理得到的刀具进行吋效、 氮化处理。 [0054] The tool obtained by processing the sheet material is subjected to a aging treatment and a nitriding treatment.
[0055] 上述加工处理方法中, 在任何实施例, 合金的熔炼温度为 1500°C以及 1500°C以 上。 优选 1500~1800°C, 在该温度范围内, 可以实现全部金属组分的熔融。 当温 度超过 1800°C, 则会造成能源的浪费。  In the above processing method, in any of the examples, the melting temperature of the alloy is 1500 ° C and 1500 ° C or more. Preferably, it is 1500 to 1800 ° C, and in this temperature range, melting of all metal components can be achieved. When the temperature exceeds 1800 °C, it will cause waste of energy.
[0056] 在一优选实施例中, 合金熔炼过程中, 应当在氩气 (Ar)气氛下进行, 以避免熔 炼气氛中含有氧而可能导致熔炼后的合金出现麻点或者孔隙。 In a preferred embodiment, the alloy smelting process should be carried out under an argon (Ar) atmosphere to avoid the presence of oxygen in the smelting atmosphere which may cause pitting or voiding of the alloy after smelting.
[0057] 在优选实施例中, 熔炼温度达到 1450~1600°C后, 保温 30~60min, 以确保各组 分均熔化。 保温结束对熔化的合金进行浇注成合金块。 然后对合金进行均匀化 处理。 [0057] In a preferred embodiment, after the melting temperature reaches 1450 to 1600 ° C, the temperature is maintained for 30 to 60 minutes to ensure that the components are uniformly melted. At the end of the incubation, the molten alloy is cast into an alloy block. The alloy is then homogenized.
[0058] 优选地, 合金进行均匀化处理吋, 应当在真空或者惰性气氛中, 均匀化处理的 温度为 1250~1350°C, 升温速率为 10~20°C/min, 保温 10~24h。 随后进行炉冷或快 速高压气体快速冷却。 其中, 高压气体为高压氮气或高压惰性气体中的任一种  [0058] Preferably, the alloy is homogenized, and the temperature of the homogenization treatment should be 1250~1350 ° C in a vacuum or an inert atmosphere, the heating rate is 10-20 ° C / min, and the temperature is kept for 10-24 h. This is followed by furnace cooling or rapid cooling of the high pressure gas. Wherein, the high pressure gas is any one of high pressure nitrogen or high pressure inert gas
[0059] 进一步优选地, 高压气体的气压为 0.2~0.8MPa; 高压氮气或高压惰性气体冷却 的冷却速率为 20~50°C/s, 该冷却方式, 合金成分无偏析现象。 Further preferably, the pressure of the high pressure gas is 0.2 to 0.8 MPa; and the cooling rate of the high pressure nitrogen or high pressure inert gas is 20 to 50 ° C / s. The cooling method has no segregation of the alloy composition.
[0060] 优选地, 对均匀化处理的合金进行热加工处理。 热加工处理包括第一段热加工 处理和第二段热加工处理。 所述第一段热加工处理的温度为 1100~1200°C, 相对 加工速率为 l~10/s, 加工率为 60~70%, 随后自然冷却至 800~1000°C吋进行所述 第二段热加工处理, 经过第一段热加工处理, 使得合金达到组织均匀化, 并且 防止合金在随后的加工过程中幵裂。 所述第二段热加工处理指的是, 在温度为 8 00~1000°C, 相对加工速率为 l~10/s, 加工率为 50~70%。 经过第二段热加工处理 后, 合金的晶粒急剧细化到微米或亚微米级别, 实现合金硬度的提升。  [0060] Preferably, the homogenized alloy is subjected to a hot working treatment. The thermal processing includes a first stage thermal processing and a second stage thermal processing. The first stage of the hot working treatment has a temperature of 1100 to 1200 ° C, a relative processing rate of 1 to 10 / s, a processing rate of 60 to 70%, and then natural cooling to 800 to 1000 ° C. The segment thermal processing, after the first thermal processing, achieves homogenization of the alloy and prevents the alloy from splitting during subsequent processing. The second stage thermal processing refers to a temperature of 8 00 to 1000 ° C, a relative processing rate of 1 to 10 / s, and a processing rate of 50 to 70%. After the second stage of thermal processing, the grain of the alloy is sharply refined to the micron or submicron level to improve the hardness of the alloy.
[0061] 在任一实施例中个, 板材处理为两段热轧处理。  [0061] In either embodiment, the sheet is treated as a two-stage hot rolling process.
[0062] 作为优选地, 第一段热轧处理的热轧温度为 1100~1200°C, 相对加工速率为 1~1 0/s , 加工率为 60~70%, 随后自然冷却至 800~1000°C吋幵始进行第二段的热轧处 理; 进一步优选地, 第二段热轧处理的温度为 800~1000°C, 相对加工速率为 1~1 0/s, 加工率为 50~70<¾。 [0062] Preferably, the first section of the hot rolling treatment has a hot rolling temperature of 1100 to 1200 ° C, a relative processing rate of 1 to 10 / s, a processing rate of 60 to 70%, and then natural cooling to 800 to 1000. The second section of the hot rolling treatment is started at ° C; further preferably, the second section of the hot rolling treatment has a temperature of 800 to 1000 ° C, and the relative processing rate is 1 to 1 0/s, processing rate is 50~70<3⁄4.
[0063] 进一步地, 对刀具进行吋效处理。 吋效处理的条件为在真空或保护气氛下于 70[0063] Further, the tool is subjected to a treatment effect. The conditions for treatment are in a vacuum or protective atmosphere at 70
0~900°C保温 3~10h。 经过吋效处理, 使得合金基体内析出弥散分布碳化物与氮 化物, 最终提高合金的硬度、 强度。 0~900 °C insulation 3~10h. After the treatment, the dispersed carbides and nitrogen compounds are precipitated in the alloy matrix, and the hardness and strength of the alloy are finally improved.
[0064] 在一优选实施例中, 氮化处理是指将吋效处理后的刀具置于氨气气氛中, 在 40[0064] In a preferred embodiment, the nitriding treatment refers to placing the treated tool in an ammonia atmosphere, at 40
0~600°C中保温 l~5h。 经过氮化处理, 提高合金 (也就是刀具)表面的硬度和切割 性能。 Insulation from 0 to 600 °C for l~5h. After nitriding, the hardness and cutting properties of the alloy (ie, the tool) surface are improved.
[0065] 本发明实施例提供的 Co-Cr-Mo合金采用上述方法, 也即塑性加工的手段制备了 微创手术刀, 刀口表面硬度达到 700~900HV (维氏硬度), 强度为 1200~1300MPa , 0.2%屈服强度大于 900MPa, 极大的提高了手术刀的刀口硬度和切割性能。  [0065] The Co-Cr-Mo alloy provided by the embodiment of the present invention adopts the above method, that is, plastic processing, to prepare a minimally invasive scalpel, and the surface hardness of the knife edge reaches 700-900 HV (Vickers hardness), and the strength is 1200-1300 MPa. The 0.2% yield strength is greater than 900 MPa, which greatly improves the knife edge hardness and cutting performance of the scalpel.
[0066] 为了更好的说明本发明实施例提供的 Co-Cr-Mo合金及微创手术刀, 下面通过多 个实施例进一步解释说明。  [0066] In order to better illustrate the Co-Cr-Mo alloy and the minimally invasive scalpel provided by the embodiments of the present invention, the following is further explained by various embodiments.
实施例  Example
[0067] 为节约篇幅, 将各个实施例的配方组分列于表 1中。  [0067] To save space, the formulation components of the various examples are listed in Table 1.
[0068] 表 1各实施例配方表及不同热加工状态下合金的力学性能 [0068] Table 1 formula of each embodiment and mechanical properties of the alloy under different hot working conditions
[] []
Figure imgf000009_0001
Figure imgf000009_0001
C , 1100°CC , 1100 ° C
10 Co-24Cr-4Mo-0.15 964 392 1260 23.2 热加工 60% 10 Co-24Cr-4Mo-0.15 964 392 1260 23.2 Thermal processing 60%
C-0.05N , 1100°C C-0.05N, 1100°C
11 Co-24Cr-4Mo-0.15 985 395 1275 25.2 热加工 60% 11 Co-24Cr-4Mo-0.15 985 395 1275 25.2 Thermal processing 60%
C-0.1N , 1100°C C-0.1N, 1100 ° C
12 Co-24Cr-4Mo-0.15 990 398 1281 25.5 热加工 60% 12 Co-24Cr-4Mo-0.15 990 398 1281 25.5 Thermal processing 60%
C-0.15N , 1100°C C-0.15N , 1100 ° C
13 Co-24Cr-4Mo-0.15 1005 403 1310 25.2 热加工 60% 13 Co-24Cr-4Mo-0.15 1005 403 1310 25.2 Thermal processing 60%
C-0.2N , 1100°C C-0.2N, 1100°C
14 Co-24Cr-4Mo-0.15 991 394 1282 25.6 热加工 60% 14 Co-24Cr-4Mo-0.15 991 394 1282 25.6 Thermal processing 60%
C-0.15N-0.01Zr , 1100°C C-0.15N-0.01Zr , 1100 ° C
15 Co-24Cr-4Mo-0.15 992 395 1283 25.5 热加工 60% 15 Co-24Cr-4Mo-0.15 992 395 1283 25.5 Thermal processing 60%
C-0.15N-0.05Zr , 1100°C C-0.15N-0.05Zr , 1100 ° C
16 Co-24Cr-4Mo-0.15 994 397 1285 21.0 热加工 60% 16 Co-24Cr-4Mo-0.15 994 397 1285 21.0 Thermal processing 60%
C-0.15N-0.1Zr , 1100°C  C-0.15N-0.1Zr , 1100 ° C
[0069] 表 2合金经表 1热加工且加工成手术刀并氮化处理后手术刀表面硬度 [0069] Table 2 alloy after hot processing of Table 1 and processed into a scalpel and nitrided surface hardness of the scalpel
[] []
[表 2] [Table 2]
Figure imgf000011_0001
Figure imgf000011_0001
[0070] 从表 1和表 2可见, 合金随碳含量与氮含量的增加, 经热加工后合金的力学性能 显著增强, 硬度增加。  [0070] As can be seen from Tables 1 and 2, the mechanical properties of the alloy are significantly enhanced and the hardness is increased with the increase of carbon content and nitrogen content.
[0071] 不同实施例合金在制备成手术刀, 经氮化后的刀口硬度可在表 1内合金硬度的 基础上, 更加得到提高, 大大改善手术刀的切割性能。  [0071] Different embodiments of the alloy are prepared into a scalpel, and the hardness of the knife edge after nitriding can be further improved on the basis of the hardness of the alloy in Table 1, and the cutting performance of the scalpel is greatly improved.
[0072] 从图 la〜图 le可知, 随着碳、 氮含量的增加, 由于限制了晶粒再结晶的长大, 有利于形成更加细小的晶粒, 从而可以提高合金的强度。 [0072] As can be seen from FIG. 1 to FIG. 11, as the carbon and nitrogen contents increase, the growth of crystal grains is restricted, which is advantageous for forming finer crystal grains, thereby improving the strength of the alloy.
[0073] 从图 2a、 2b可知, 表面含有微量的 Zr元素, 有利于表面形成更加致密的氧化膜 [0074] 而从 3a、 3b可知, 表面微量的 Zr元素有利于合金表面形成更加致密的氧化膜, 抑制合金元素在生物体环境中通过氧化膜析出, 提高合金的生物相容性。 [0073] It can be seen from FIGS. 2a and 2b that the surface contains a trace amount of Zr element, which is favorable for forming a denser oxide film on the surface. [0074] It can be seen from 3a and 3b that a small amount of Zr element on the surface is favorable for forming a denser oxide film on the surface of the alloy, suppressing precipitation of the alloying element through the oxide film in the living environment, and improving the biocompatibility of the alloy.
[0075] 从图 4可知, 将 a: Co-29Cr-6Mo、 b: Co-24Cr-4Mo、 c: Co-24Cr-4Mo-0.15C-0.  [0075] As can be seen from FIG. 4, a: Co-29Cr-6Mo, b: Co-24Cr-4Mo, c: Co-24Cr-4Mo-0.15C-0.
1N、 d: Co-24Cr-4Mo-0.15C-0.lN-0.05Zr四种合金置于 37°C的质量百分含量为 5% 的乳酸溶液中浸泡 6个月后用 ICP-EOS分析, 添加了 Zr元素的合金, Co、 Cr、 Mo 离子析出的浓度均有较大幅度降低, 也就是说 Zr元素修复了合金表面的钝化膜, 提高合金的抗腐蚀性能, 避免合金形成的刀具在生物体内的金属离子析出, 进 一步提高了该微创手术刀的安全性能。  1N, d: Co-24Cr-4Mo-0.15C-0.lN-0.05Zr four alloys were placed in a 5% lactic acid solution at 37 ° C for 6 months and analyzed by ICP-EOS. The alloy with Zr element added has a large decrease in the concentration of Co, Cr and Mo ions. That is to say, the Zr element repairs the passivation film on the surface of the alloy, improves the corrosion resistance of the alloy, and avoids the formation of the alloy. The precipitation of metal ions in the living body further improves the safety performance of the minimally invasive scalpel.
[0076] 以上所述仅为本发明的较佳实施例而已, 并不用以限制本发明, 凡在本发明的 精神和原则之内所作的任何修改、 等同替换和改进等, 均应包含在本发明的保 护范围之内。  The above are only the preferred embodiments of the present invention, and are not intended to limit the present invention, and any modifications, equivalents, and improvements made within the spirit and scope of the present invention should be included in the present invention. Within the scope of protection of the invention.

Claims

权利要求书 Claim
[权利要求 1] 一种 Co-Cr-Mo合金, 其特征在于: 由质量百分含量如下的组分组成  [Claim 1] A Co-Cr-Mo alloy characterized by: consisting of the following components
Cr 22-26%; Cr 22-26%;
Mo 3-6%;  Mo 3-6%;
C 0.1-0.2%;  C 0.1-0.2%;
N 0.05-0.2%;  N 0.05-0.2%;
Zr 0-0.06%;  Zr 0-0.06%;
余量为 Co和不可避免的杂质, 其中, 所述 Zr的含量不取 0。  The balance is Co and unavoidable impurities, wherein the content of Zr is not taken as zero.
[权利要求 2] 如权利要求 1所述的 Co-Cr-Mo合金, 其特征在于: 所述 Zr的含量为 0.0 [Claim 2] The Co-Cr-Mo alloy according to claim 1, wherein: the Zr content is 0.0
3~0.06<¾。  3~0.06<3⁄4.
[权利要求 3] —种微创手术刀的加工方法, 至少包括以下步骤:  [Claim 3] A method for processing a minimally invasive scalpel, comprising at least the following steps:
按照权利要求 1~2任一所述的 Co-Cr-Mo合金的配方称取各组分; 将称取的所述各组分进行熔炼处理;  The composition of the Co-Cr-Mo alloy according to any one of claims 1 to 2, wherein each component is weighed; and the weighed components are subjected to smelting treatment;
将所述熔炼后的合金进行均匀化处理;  Homogenizing the smelted alloy;
将所述均匀化处理得到的合金进行热加工处理;  The alloy obtained by the homogenization treatment is subjected to a hot working treatment;
将所述热加工处理得到的合金进行板材处理;  The alloy obtained by the hot working treatment is subjected to sheet metal treatment;
将所述板材处理得到的刀具进行吋效、 氮化处理。  The tool obtained by processing the plate material is subjected to aging and nitriding treatment.
[权利要求 4] 如权利要求 3所述的微创手术刀的加工方法: 其特征在于: 所述热加 工处理工艺包括第一段热加工处理和第二段热加工处理; 所述第一段 热加工处理的温度为 1100~1200°C, 相对加工速率为 0.1~10/s, 加工率 为 60~70%, 随后自然冷却至 800~1000°C吋进行所述第二段热加工处 理; 所述第二段热加工处理的温度为 800~1000°C, 相对加工速率为 0. l-10/s, 加工率为 50~70<¾。  [Claim 4] The method for processing a minimally invasive scalpel according to claim 3, wherein: the thermal processing process comprises a first stage thermal processing and a second thermal processing; The temperature of the hot working treatment is 1100~1200°C, the relative processing rate is 0.1~10/s, the processing rate is 60~70%, and then the natural cooling is performed to 800~1000°C, and the second stage thermal processing is performed; The processing temperature is 50~70<3⁄4. The processing speed is 50~70<3⁄4. The processing temperature is 0. l-10/s, and the processing rate is 50~70<3⁄4.
[权利要求 5] 如权利要求 3所述的微创手术刀的加工方法: 其特征在于: 所述熔炼 在氩气气氛中, 温度为 1450~1600°C, 保温吋间 30~60min。  [Claim 5] The method for processing a minimally invasive scalpel according to claim 3, wherein the smelting is performed in an argon atmosphere at a temperature of 1450 to 1600 ° C and a holding time of 30 to 60 minutes.
[权利要求 6] 如权利要求 3所述的微创手术刀的加工方法: 其特征在于: 所述均匀 化温度为 1250~1350°C, 升温速率为 10~20°C/min, 且在真空或惰性气 氛中保温吋间为 10~24h。 [Claim 6] The method for processing a minimally invasive scalpel according to claim 3, wherein: the homogenization temperature is 1250 to 1350 ° C, the heating rate is 10 to 20 ° C / min, and the vacuum is Or inert gas In the atmosphere, the insulation time is 10~24h.
[权利要求 7] 如权利要求 3所述的微创手术刀的加工方法: 其特征在于: 所述均匀 化处理后还包括炉冷或高压气体快速冷却; 所述高压气体快速冷却速 率为 10~50°C/s, 气压为 0.2~0.8MPa; 所述高压气体为氮气或惰性气体 中的任一种。  [Claim 7] The method for processing a minimally invasive scalpel according to claim 3, wherein: the homogenization treatment further comprises rapid cooling of the furnace or high pressure gas; and the rapid cooling rate of the high pressure gas is 10~ 50 ° C / s, the gas pressure is 0.2 ~ 0.8MPa; the high pressure gas is either nitrogen or an inert gas.
[权利要求 8] 如权利要求 3所述的微创手术刀的加工方法: 其特征在于: 所述板材 处理为两段热轧处理; 其中第一段热轧处理的热轧温度为 1100~1200 °C, 相对加工速率为 l~10/s, 加工率为 60~70%, 随后自然冷却至 800~ 1000°C吋进行第二段热轧处理; 所述第二段热轧处理的温度为 800~10 00°C, 相对加工速率为 l~10/s, 加工率为 50~70<¾。  [Claim 8] The method for processing a minimally invasive scalpel according to claim 3, wherein: the sheet material is processed into two sections of hot rolling; wherein the hot rolling temperature of the first section of hot rolling is 1100 to 1200 °C, the relative processing rate is l~10/s, the processing rate is 60~70%, and then naturally cooled to 800~1000°C, the second hot rolling process is performed; the temperature of the second hot rolling process is 800~10 00 °C, the relative processing rate is l~10/s, and the processing rate is 50~70<3⁄4.
[权利要求 9] 如权利要求 3所述的微创手术刀的加工方法: 其特征在于: 所述吋效 处理为在真空或保护气氛下 700~900°C保温 3~10h; 所述氮化处理为在 氨气气氛下, 于 400~700°C的环境中保温 l~5h。  [Claim 9] The method for processing a minimally invasive scalpel according to claim 3, wherein: the aging treatment is performed at 700 to 900 ° C for 3 to 10 hours under vacuum or a protective atmosphere; The treatment is carried out for 1 to 5 hours in an environment of 400 to 700 ° C under an ammonia atmosphere.
[权利要求 10] 一种如权利要求 3~9所述的微创手术刀。  [Claim 10] A minimally invasive scalpel according to any of claims 3-9.
PCT/CN2016/106411 2016-08-29 2016-11-18 Co-cr-mo alloy, machining method for scalpel for minimally invasive operation, and scalpel for minimally invasive operation WO2018040301A1 (en)

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101052734A (en) * 2004-11-19 2007-10-10 国立大学法人岩手大学 Bio-Co-Cr-Mo alloy with ion elution suppressed by regulation of texture, and process for producing the same
JP5156943B2 (en) * 2006-10-31 2013-03-06 国立大学法人岩手大学 Method for producing bio-based Co-based alloy having excellent plastic workability
JP5592600B2 (en) * 2007-07-24 2014-09-17 株式会社神戸製鋼所 Bio-based Co-based alloy material for hot die forging and manufacturing method thereof
JP5616845B2 (en) * 2011-05-25 2014-10-29 株式会社神戸製鋼所 Method for producing Co-based alloy for living body
CN104263999A (en) * 2014-10-11 2015-01-07 上海大学兴化特种不锈钢研究院 Novel high-plasticity medical cobalt-based alloy

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005126041A (en) * 2003-07-31 2005-05-19 Takata Corp Occupant protection device
EP1696044A1 (en) * 2005-02-16 2006-08-30 BEGO Bremer Goldschlägerei Wilh. Herbst GmbH &amp; Co. KG Alloy for producing ceramic dental restorations
JP5303718B2 (en) * 2006-06-22 2013-10-02 国立大学法人岩手大学 Porous Co-based alloy sintered coating material and method for producing the same
JP6086444B2 (en) * 2011-09-08 2017-03-01 国立大学法人東北大学 Alloy composition for aluminum die-cast mold and method for producing the same
CN105750553A (en) * 2016-02-21 2016-07-13 谭陆翠 Tumor exsector

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101052734A (en) * 2004-11-19 2007-10-10 国立大学法人岩手大学 Bio-Co-Cr-Mo alloy with ion elution suppressed by regulation of texture, and process for producing the same
JP5156943B2 (en) * 2006-10-31 2013-03-06 国立大学法人岩手大学 Method for producing bio-based Co-based alloy having excellent plastic workability
JP5592600B2 (en) * 2007-07-24 2014-09-17 株式会社神戸製鋼所 Bio-based Co-based alloy material for hot die forging and manufacturing method thereof
JP5616845B2 (en) * 2011-05-25 2014-10-29 株式会社神戸製鋼所 Method for producing Co-based alloy for living body
CN104263999A (en) * 2014-10-11 2015-01-07 上海大学兴化特种不锈钢研究院 Novel high-plasticity medical cobalt-based alloy

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