WO2015044997A1 - インプラントとその製造方法 - Google Patents
インプラントとその製造方法 Download PDFInfo
- Publication number
- WO2015044997A1 WO2015044997A1 PCT/JP2013/075635 JP2013075635W WO2015044997A1 WO 2015044997 A1 WO2015044997 A1 WO 2015044997A1 JP 2013075635 W JP2013075635 W JP 2013075635W WO 2015044997 A1 WO2015044997 A1 WO 2015044997A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- magnesium alloy
- implant
- producing
- compression
- implant according
- 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.)
- Ceased
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
- C22C23/06—Alloys based on magnesium with a rare earth metal as the next major constituent
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2/00—Filters implantable into blood vessels; Prostheses, i.e. artificial substitutes or replacements for parts of the body; Appliances for connecting them with the body; Devices providing patency to, or preventing collapsing of, tubular structures of the body, e.g. stents
- A61F2/02—Prostheses implantable into the body
- A61F2/28—Bones
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61L—METHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
- A61L27/00—Materials for grafts or prostheses or for coating grafts or prostheses
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61L—METHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
- A61L31/00—Materials for other surgical articles, e.g. stents, stent-grafts, shunts, surgical drapes, guide wires, materials for adhesion prevention, occluding devices, surgical gloves, tissue fixation devices
- A61L31/02—Inorganic materials
- A61L31/022—Metals or alloys
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61L—METHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
- A61L31/00—Materials for other surgical articles, e.g. stents, stent-grafts, shunts, surgical drapes, guide wires, materials for adhesion prevention, occluding devices, surgical gloves, tissue fixation devices
- A61L31/14—Materials characterised by their function or physical properties, e.g. injectable or lubricating compositions, shape-memory materials, surface modified materials
- A61L31/148—Materials at least partially resorbable by the body
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/001—Extruding metal; Impact extrusion to improve the material properties, e.g. lateral extrusion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K1/00—Making machine elements
- B21K1/76—Making machine elements elements not mentioned in one of the preceding groups
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/06—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2210/00—Particular material properties of prostheses classified in groups A61F2/00 - A61F2/26 or A61F2/82 or A61F9/00 or A61F11/00 or subgroups thereof
- A61F2210/0004—Particular material properties of prostheses classified in groups A61F2/00 - A61F2/26 or A61F2/82 or A61F9/00 or A61F11/00 or subgroups thereof bioabsorbable
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2240/00—Manufacturing or designing of prostheses classified in groups A61F2/00 - A61F2/26 or A61F2/82 or A61F9/00 or A61F11/00 or subgroups thereof
- A61F2240/001—Designing or manufacturing processes
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2310/00—Prostheses classified in A61F2/28 or A61F2/30 - A61F2/44 being constructed from or coated with a particular material
- A61F2310/00005—The prosthesis being constructed from a particular material
- A61F2310/00011—Metals or alloys
- A61F2310/00035—Other metals or alloys
- A61F2310/00041—Magnesium or Mg-based alloys
Definitions
- the present invention relates to an implant and a manufacturing method thereof, and particularly relates to a magnesium alloy implant.
- Magnesium / magnesium alloys are lighter and stronger than other metals, and have been put to practical use in portable electronic devices and automobile parts.
- application research as an absorbable stent or an absorbable osteosynthesis material is progressing (see, for example, Patent Document 1).
- JP 2009-178293 A Japanese Patent No. 4150219
- the a-axis of the magnesium alloy crystal is arranged in the extrusion direction of the magnesium alloy, if a compressive force is applied in a direction parallel to this, plastic working can be performed with a small force, and plastic workability is improved.
- the compressive force acts in a direction perpendicular to the c-axis of the metal crystal.
- a compressive force acts in a direction orthogonal to the c-axis, there is a disadvantage that a structural defect occurs in the crystal structure.
- the strength against a load in the thickness direction is weakened, which may cause material damage.
- the metal particles when a biodegradable metal material is used as a material for manufacturing an implant, the metal particles have a fine structure when pressed, resulting in an increase in grain boundaries and a high decomposition rate. There is.
- the present invention has been made in view of the above-described circumstances, and an object thereof is to provide an implant that suppresses the generation of structural defects and suppresses the decomposition rate, and a method for manufacturing the implant.
- the present invention provides the following means.
- a molding step of forming a molded product by subjecting a raw material piece made of a biodegradable metal material to plastic processing, and heat-treating the molded product molded by the molding step to obtain metal particles.
- a particle diameter adjusting step for increasing the diameter for increasing the diameter.
- the metal particle diameter constituting the biodegradable metal material becomes fine.
- the molded product is heat-treated by a particle size adjusting step, thereby increasing the metal particle size and decreasing the decomposition rate when it is embedded in a living body as an implant.
- the molding step includes extruding a magnesium alloy to obtain a plastically deformed magnesium alloy molding material, and the magnesium alloy molding material obtained by the extrusion step in the extrusion direction.
- the magnesium alloy is extruded to form a magnesium alloy that is plastically deformed so that the c-axis of the magnesium metal crystal is oriented in a direction of approximately 90 ° with respect to the extrusion direction.
- a material is obtained.
- the magnesium alloy molding material is cut at an angle of 70 ° to 110 ° with respect to the extrusion direction to obtain a block magnesium alloy material.
- a plastic processed product is manufactured by applying a compression force in a direction perpendicular to the extrusion direction to the massive magnesium alloy material.
- the compressive force since the compressive force is mainly applied in the c-axis direction, the compressive force acts in a direction perpendicular to the slip surface in the metal crystal of the magnesium alloy.
- the workability is lowered, but a plastic processed product with few structural defects can be manufactured. That is, a plastic processed product with high strength can be manufactured.
- the first aspect may include a heating step of heating the massive magnesium alloy material prior to or in the compression step. By doing in this way, non-bottom slip can be generated and workability can be improved.
- the massive magnesium alloy material may be heated in the heating step at a temperature higher than 300 ° C., more preferably 350 ° C. or higher and below the melting point of the magnesium alloy.
- the compression step may compress the massive magnesium alloy material at a rolling reduction of 45% or more.
- the material particle diameter of a magnesium alloy can be refined
- a compression force may be applied by a mold in a state where a lubricant is applied between the bulk magnesium alloy material.
- the compression step repeats at least twice the application of a lubricant between the mold and the massive magnesium alloy material and the application of a compression force.
- a shearing step of cutting a product from the compressed magnesium alloy material may be included, and the shearing step may be performed at a rolling speed of 1.5 mm / sec or less.
- the shearing process is, for example, punching by a press device.
- a relatively smooth shear portion (shear surface) and a fracture portion (fracture surface) that instantaneously separates and presents a rough surface are generated on the cut surface.
- rupture part in a cut surface is suppressed to 50% or less by performing a shearing process with a reduction speed of 1.5 mm / sec or less.
- a shearing process with a reduction speed of 1.5 mm / sec or less.
- the molded product may be heat treated when it is confirmed in the confirmation step that the impurity concentration is not more than a predetermined value.
- the particle size adjustment step is performed when the impurity concentration on the surface of the molded product is not more than a predetermined value, so that the biodegradable metal material and the impurity metal material are prevented from reacting in the heat treatment, and further stable. Implants having a reduced degradation rate can be produced.
- the cleaning step may be a process of peeling the surface of the molded product.
- the cleaning step may be a process of dissolving the surface of the molded product with an acid. By doing in this way, the impurity metal material adhering to the surface of the molded product is dissolved and removed by the acid together with the surface portion of the molded product.
- cleaning process may include the process which melt
- the particle diameter adjusting step may be a volumeification process.
- the said particle diameter adjustment process may perform an aging precipitation process after a solidification process.
- miniaturized by plastic working can be increased by the volume treatment, and the decomposition rate can be reduced.
- the strength of the molded product can be further improved by the aging precipitation treatment after the volumeification treatment.
- the second aspect of the present invention is a magnesium alloy implant in which the c-axis of the metal crystal is oriented in the main load direction. As described above, deformation due to a compressive force parallel to the c-axis is less likely to be deformed than deformation due to a compressive force orthogonal to the c-axis, so that the strength can be improved by orienting the c-axis in the main load direction. it can.
- the average value of the deviation angle of the perpendicular of the (0001) plane of the metal crystal with respect to the thickness direction may be 25 ° or less.
- the average value of the deviation angle of the perpendicular of the (0001) plane of the metal crystal with respect to the direction along the surface is 80 ° or more, and the deviation is 16 to 84% of the maximum value of the deviation angle.
- the width of the cumulative distribution of corners may be 50 ° or less. This also makes it possible to orient the c-axis of the metal crystal of the magnesium alloy substantially in the thickness direction, reduce structural defects, and improve the strength against loads in the thickness direction.
- the ratio of the shear plane in the plane along the thickness direction formed by punching is 50% or more with respect to the thickness.
- the Fe ion concentration contained on the surface may be 0.02% or less, the copper ion concentration may be 0.15% or less, and the nickel concentration may be 0.01% or less.
- FIG. 10 is a first example of the molding process according to the third embodiment, and shows a histogram of a deviation angle with respect to the thickness direction of the normal line of the (0001) plane of the metal crystal of the A material processed by the compression process of FIG. 11. It is. It is a figure which shows the histogram of the shift
- 11 is a graph showing the relationship between the true strain rate and the load when the processing conditions in the compression step of FIG. 11 are a heating temperature of 375 ° C. and a reduction speed of 0.05 mm, which is Example 2 of the molding step of the third embodiment. It is. It is Example 2 of the shaping
- the process conditions in the compression process of FIG. 11 are the graphs which show the relationship between a true strain rate and load in case the heating temperature is 375 degreeC and the reduction speed is 5 mm. .
- Example 11 is a graph showing the relationship between the true strain rate and the load when the processing conditions in the compression process of FIG. 11 are a heating temperature of 450 ° C. and a reduction speed of 0.05 mm, which is Example 2 of the molding process of the third embodiment. It is. It is Example 2 of the shaping
- FIG. 10 is a diagram illustrating a relationship between a ratio of a fractured surface portion in a cut surface formed in a thickness direction and a reduction speed in the punching process of the forming process of FIG. 9. It is a microscope picture of the cut surface which shows the rolling speed
- the implant manufactured by the manufacturing method according to the present embodiment is, for example, an implant used for osteosynthesis, and is composed of a biodegradable metal material, for example, a magnesium alloy material (for example, WE43). Is.
- the manufacturing method of an implant according to the present embodiment is a molding in which a molded product is formed by subjecting a material piece made of a biodegradable metal material to hot plastic processing such as press processing.
- molding process S1 are included.
- the molding step S1 is a step of performing press working at 300 ° C. and 100 MPa for 1 minute, for example.
- the press working temperature, pressure, and working time are merely examples, and other conditions may be adopted.
- the particle size adjustment step S2 is a step of cooling by air cooling after heat treatment (consolidation treatment) at 525 ° C. for 8 hours, for example.
- the temperature and processing time of heat treatment are examples, and other conditions may be adopted.
- a molded product having a desired shape is manufactured from a material piece by performing press working in the molding step S1.
- the particle diameter of the biodegradable metal material is reduced as shown in FIGS. 2A and 2B.
- FIG. 2B is an enlarged micrograph of the portion surrounded by the rectangle in FIG. 2A.
- FIG. 3B is a photomicrograph in which the portion surrounded by the rectangle in FIG. 3A is enlarged.
- the particle diameter of the biodegradable metal material in each after a raw material piece, a press work, and after heat processing is shown in FIG.
- the particle size of the biodegradable metal material refined by the press working in the forming step S1 is increased by the heat treatment in the particle size adjusting step S2. .
- the number of grain boundaries on the surface of the molded product can be reduced, and the decomposition rate can be reduced. That is, there is an advantage that an implant embedded as a structural material for osteosynthesis can maintain strength as a structural material for a long period after implantation, and can assist osteosynthesis by bone formation. After the bone joining is completed, the implant is decomposed and disappears with time, so that no foreign matter remains in the body.
- the solution treatment is performed in the particle size adjustment step S2, but in addition to this, as shown in FIG. 5, after the solution treatment (step S21), at 250 ° C. for 6 hours.
- Heat treatment aging precipitation treatment (step S22)
- the mechanical strength (Vickers hardness) of the implant can be improved as shown in FIG. 7 while maintaining a large particle diameter as shown in FIGS. 6A and 6B.
- FIG. 6B is an enlarged micrograph of a portion surrounded by the rectangle in FIG. 6A.
- the manufacturing method includes a cleaning step S3 for cleaning the molded product between the molding step S1 and the particle diameter adjusting step S2, and impurities on the surface of the molded product. It includes a confirmation step S4 for confirming the concentration and a determination step S5 for determining whether or not the impurity concentration confirmed in the confirmation step S4 is below a predetermined threshold value.
- the cleaning step S3 is a step in which the molded product is degreased, immersed in an acidic solution, then immersed in an alkaline solution, and then dried.
- the confirmation step S4 is a step of measuring the concentration of Fe ions eluted in the acidic solution.
- the acidic solution may be anything other than chromic acid or boric acid that affects the living body, and phosphoric acid or hydrochloric acid may be used.
- Determination step S5 determines whether the Fe ion concentration measured in the confirmation step S4 is equal to or less than a predetermined threshold value. Then, the determination step S5 proceeds to the particle size adjustment step S2 when the Fe ion concentration is equal to or lower than the threshold value, and when the Fe ion concentration is larger than the threshold value, the steps from the cleaning step S3 are repeated again. It has become.
- the iron component constituting the mold adheres to the surface of the molded product by pressing using an iron mold. Therefore, by immersing the molded product in the acidic solution in the cleaning step S3, the iron component adhering to the surface of the molded product is dissolved by the acid and eluted into the acidic solution as Fe ions. Thereby, the iron component which is an impurity metal material in the surface of a molded article can be removed.
- the predetermined threshold value may be set based on an experimentally obtained amount of the iron component adhering to the molded product from the mold in the press working. Further, in the confirmation step S4, the concentration after being immersed in the acidic solution for a predetermined time may be measured, or the Fe ion in the acidic solution is measured with time to determine the concentration change rate, and the concentration change is predetermined. You may decide to measure the density
- the implant for osteosynthesis has been described as an example.
- the present invention may be applied to manufacture of any other implant.
- magnesium alloy was illustrated as a biodegradable metal material, you may apply to other arbitrary biodegradable materials.
- the iron component is exemplified as the impurity metal material adhering to the surface of the molded article
- the copper component or the nickel component may be washed and removed instead of or in addition to this.
- the cleaning step S3 is to remove the impurity metal material by immersing the molded product in an acidic solution, but instead, the surface of the molded product is peeled off by cutting or the like. May be removed. It is desirable that the Fe ion concentration remaining on the implant surface is 0.02% or less, the copper ion concentration is 0.15% or less, and the nickel concentration is 0.01% or less.
- the manufacturing method of the implant which concerns on the 3rd Embodiment of this invention is demonstrated below with reference to FIGS. 9-22C.
- the manufacturing method of the implant according to the present embodiment is different from that of the first embodiment in the molding step S1. Therefore, in the present embodiment, the molding process S1 will be mainly described, and the description of the other processes S2, S21, and S22 that are common to the first embodiment will be omitted.
- the implant manufacturing method of this embodiment may further include the cleaning step S3, the confirmation step S4, and the determination step S5 described in the second embodiment.
- the forming step S1 of the implant manufacturing method according to the present embodiment is extruded with an extrusion step S11 for extruding a magnesium alloy material (material piece) to obtain a plastically deformed magnesium alloy material.
- Extrusion step S11 is a step in which a magnesium alloy material is plastically deformed into a rod-like extruded material 1 having a predetermined cross-sectional shape using a die. Depending on the extrusion conditions, the orientation of the metal crystals changes, and the (0001) plane of the metal crystals is oriented so as to be substantially parallel to the extrusion direction.
- the extruded material 1 produced in the extruding step S11 is cut in a direction substantially perpendicular to the longitudinal direction, 70 ° to 110 °, and is a lump divided in the longitudinal direction.
- This is a step of obtaining the magnesium alloy material 2.
- the orientation of the (0001) plane of the extruded material 1 is measured by pole figure measurement or the like, and is cut at an angle perpendicular to the plane in which the (0001) plane is remarkably oriented. It is preferable to obtain the material 2.
- the compression force F is applied to the massive magnesium alloy material 2 obtained in the cutting step S12 from the die for reduction in a direction orthogonal to the extrusion direction in the extrusion step S11. It is the process of adding and rolling to plate shape.
- a compressive force F is applied to the magnesium alloy metal crystal constituting the massive magnesium alloy material 2 substantially parallel to the c-axis perpendicular to the (0001) plane. It has become.
- the compression force F is applied while the massive magnesium alloy material 2 is heated.
- the temperature at the time of heating is preferably a temperature of 100 ° C. or higher that generates non-bottom slip, and in particular, when using WE43 which is a medical magnesium alloy material, it is preferably higher than 300 ° C., 350 ° C. or higher. More preferably.
- the compression step S13 is performed by applying a lubricant between the mold and the massive magnesium alloy material 2.
- a lubricant a solid lubricant, a fluid lubricant, or the like can be used.
- the step of applying the lubricant and the step of reducing the massive magnesium alloy material 2 with a mold are repeated a plurality of times.
- the massive magnesium alloy material 2 is compressed at a rolling reduction of 45% or more.
- the punching step S14 is a step of punching the plate-like magnesium alloy material obtained in the compression step S13 with a punching die. In this punching step S14, it is preferable to keep the die reduction speed of the magnesium alloy material to 1.5 mm / sec or less.
- the rod-like extruded material 1 is obtained by extruding the magnesium alloy material in the extrusion step S11.
- this extrusion step S11 the orientation of the metal crystal of the magnesium alloy material is changed, and the (0001) plane of the metal crystal is oriented so as to be substantially parallel to the extrusion direction.
- Cutting process S12 is performed with respect to the extrusion material 1 obtained in this way.
- the extrusion material 1 is cut
- a compression step S13 is performed on each massive magnesium alloy material 2.
- a compression force F is applied to the massive magnesium alloy material 2 in a state heated to 100 ° C. or more in a direction orthogonal to the extrusion direction.
- the compressive force F is applied in a direction substantially parallel to the c-axis of the metal crystal oriented substantially in one direction at the position of the diameter where the degree of processing becomes the largest in the massive magnesium alloy material 2.
- the direction of the compressive force F is a direction orthogonal to the slip surface of the metal crystal, and the ease of plastic working is reduced as compared with the case where the compressive force F is applied parallel to the slip surface.
- the compressive force F is applied to the massive magnesium alloy material 2 heated to 100 ° C. or higher, the workability is improved by the occurrence of non-bottom slip as compared with the case where heating is not performed.
- a compression force F is applied in a state where a lubricant is applied between the mold and the massive magnesium alloy material 2.
- the compressive force F is dispersed over the entire contact surface between the massive magnesium alloy material 2 and the mold by the action of the lubricant, and a more uniform compressive force F can be applied over the entire massive magnesium alloy material 2.
- the magnesium alloy material is refined and the particle size is reduced. It is known that there is a relationship between the homogeneity of the material particle size and the corrosion resistance of the material when assuming medical applications, and it is desirable to make the material particle size uniform when the material has corrosion resistance .
- a compressive load is applied to a material, elastic deformation first occurs, and when the compressive load enters a plastic region, plastic deformation occurs with miniaturization.
- the crystal grain size reaches an equilibrium state, and the material grain size becomes uniform.
- the material particle size is uniform.
- compression is performed so that the rolling reduction is 45% or more, and the magnesium alloy material is refined to obtain a uniform particle size.
- compressive force F is applied to the massive magnesium alloy material 2
- the recrystallized grain size almost reaches equilibrium at a rolling reduction of about 45%, so that the material grain size can be made uniform.
- the manufactured product is a product used for medical use such as a magnesium alloy implant
- the homogeneity of the particle size can be achieved, whereby the corrosion resistance can be improved. is there.
- the punching step S14 is a step of obtaining a molded product by punching and removing unnecessary portions with a press machine in order to determine the product shape.
- the punching die is pressed in the plate thickness direction of the plate-like magnesium alloy material and punched by shearing, a cut surface is formed in the thickness direction, but by suppressing the reduction speed of the mold to 1.5 mm / sec or less
- the shearing surface portion in the cut surface can be made larger than the fracture surface portion.
- Example 1 shows the relationship between the direction in which the compressive force F is applied to the massive magnesium alloy material 2 and the orientation of the metal crystals on the surface of the plate-like magnesium alloy material after compression.
- FIG. 13A in the direction perpendicular to the extrusion direction in the extrusion step S11 as in the manufacturing method according to the present embodiment (A material)
- FIG. 13B is parallel to the extrusion direction.
- the orientation of the metal crystal on the surface of the plate-like magnesium alloy material when the compressive force F is applied in any direction (B material) is shown.
- FIG. 13A and FIG. 13B are histograms in which the horizontal axis represents the deviation angle of the normal line of the (0001) plane of the compressed metal crystal with respect to the plate thickness direction, and the vertical axis represents the frequency. From these FIG. 13A and FIG. 13B, the average value of the deviation angle and the accumulation width when compressed by each compression method are calculated as shown in Table 1.
- the accumulated width of the deviation angle refers to the width of the deviation angle in the range of 16% to 84% of the maximum value of the deviation angle in the cumulative distribution curves of FIGS. 13A and 13B.
- the average value of the deviation angle of the A material is 16.8 °
- the average value of the deviation angle of the B material is 26.0 °
- the compression force F of the B material is It can be seen that the crystal orientation greatly changed by the action. Therefore, in the case of a product using a material having an average deviation angle of 25 ° or less, the compression force F is applied in a direction perpendicular to the extrusion direction, and there are few structural defects and the strength is improved. Can do.
- the accumulated width of the deviation angles of the A material is 17.6 °
- the average value of the deviation angles of the B material is 25.2 °.
- FIG. 14A and FIG. 14B show histograms showing the relationship between the deviation angle of the normal line of the (0001) plane of the metal crystal of the A material and the B material with respect to the direction along the surface of the product and the frequency, respectively. From these FIG. 14A and FIG. 14B, the average value of the deviation angle and the accumulation width when compressed by each compression method are calculated as shown in Table 2.
- the average deviation angle between the A material and the B material is the same at about 81 °, but there is a large difference in the integration width. In the case of A material, it is 17.0 °, while in the case of B material, it is 53 °. Therefore, when the average deviation angle of the normal line of the (0001) plane of the metal crystal with respect to the direction along the surface is 80 ° or more and the accumulated width of the deviation angle is 50 ° or less on the surface of the product Moreover, it turns out that it was manufactured by the manufacturing method in this embodiment.
- Example 2 was performed by changing the compression conditions when applying the compression force F to the massive magnesium alloy material 2 (WE43) suitable for medical applications.
- a bulk magnesium alloy material 2 having a diameter of 8 mm and a length of 12 mm was used as a sample.
- Table 3 shows the results of changing the heating temperature in the compression step S13 to 300 ° C., 375 ° C., and 450 ° C., and changing the reduction speed during compression to 5 mm / sec, 0.5 mm / sec, and 0.05 mm / sec.
- Table 4 shows the results of changing the heating temperature to 350 ° C., 400 ° C., and 450 ° C. and changing the reduction speed during compression to 1 mm / sec, 0.1 mm / sec, and 0.01 mm / sec.
- the heating temperature of the block magnesium alloy material 2 at the time of compression is higher than 300 degreeC, and it is further more preferable that it is 350 degreeC or more.
- 15 shows a heating temperature of 375 ° C. and a reduction speed of 0.05 mm
- FIG. 16 shows a heating temperature of 375 ° C. and a reduction speed of 5 mm / sec
- FIG. 17 shows a heating temperature of 450 ° C. and a reduction speed of 0.05 mm / sec
- 18 shows a heating temperature of 450 ° C. and a reduction speed of 5 mm / sec.
- FIG. 19 shows a heating temperature of 350 ° C. and a reduction speed of 1 mm / sec.
- Reduction ratio (Thickness before compression ⁇ Thickness after compression) / Thickness before compression ⁇ 100 (%) It can be expressed as.
- the recrystallized grain size almost reaches equilibrium with a true strain rate ⁇ of about 0.6.
- the rolling reduction is about 45%. Since the recrystallized grain size almost reaches equilibrium at a rolling reduction of about 45%, it can be seen that compression at a rolling reduction of 45% or more can make the material grain size uniform and improve the corrosion resistance.
- the WE43 is considered, but a magnesium alloy other than the WE43 may be used.
- Example 3 A case where a shearing force is applied by changing the rolling speed while the plate-like magnesium alloy material (WE43) 2 having a thickness of 1 mm is heated to 350 ° C. will be described with reference to FIGS. 21 to 22C.
- FIG. 21 shows the relationship between the ratio of the fractured surface portion (fracture surface ratio) on the cut surface formed in the thickness direction and the reduction speed in the punching step S14.
- 22A to 22C are photomicrographs of the cut surface when the rolling speed is changed.
- the rolling speed is 0.24 mm / sec (FIG. 22A)
- the rolling speed is 1.44 mm / sec (FIG. 22B)
- the case of a reduction speed of 1.92 mm / sec (FIG. 22C) is shown.
- FIG. 22C it is shown that the fracture surface ratio increases as the rolling speed increases, and it was found that the fracture surface ratio and the rolling speed are in a substantially proportional relationship.
- the fracture surface portion in the cut surface in the thickness direction can be suppressed to 50% or less.
- the WE43 is considered, but a magnesium alloy other than the WE43 may be used.
Landscapes
- Health & Medical Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Public Health (AREA)
- Veterinary Medicine (AREA)
- Life Sciences & Earth Sciences (AREA)
- Animal Behavior & Ethology (AREA)
- General Health & Medical Sciences (AREA)
- Vascular Medicine (AREA)
- Heart & Thoracic Surgery (AREA)
- Epidemiology (AREA)
- Transplantation (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Materials Engineering (AREA)
- Surgery (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Cardiology (AREA)
- Orthopedic Medicine & Surgery (AREA)
- Biomedical Technology (AREA)
- Crystallography & Structural Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Dermatology (AREA)
- Inorganic Chemistry (AREA)
- Medicinal Chemistry (AREA)
- Materials For Medical Uses (AREA)
- Prostheses (AREA)
- Extrusion Of Metal (AREA)
- Forging (AREA)
Abstract
Description
本発明の第1の態様は、生分解性金属材料からなる素材片に塑性加工処理を施して成形品を成形する成形工程と、該成形工程により成形された前記成形品を熱処理して金属粒子径を増大させる粒子径調整工程とを含むインプラントの製造方法である。
このようにすることで、非底面すべりを発生させて加工性を向上することができる。
このようにすることで、医療用マグネシウム合金で代表的な希土類を含む合金、より具体的にはWE43に対しても割れを発生させることなく塑性加工することができる。
このようにすることで、マグネシウム合金の材料粒径を微細化させ均質にすることができる。すなわち、塊状マグネシウム合金材料に圧縮力を加えていくと、45%程度の圧下率において、再結晶粒径がほぼ平衡に達するので、材料粒径を均質にして耐食性を向上することができる。ここで、圧下率は、
圧下率=(圧縮前の厚さ-圧縮後の厚さ)/圧縮前の厚さ×100(%)
により算出することができる。
このようにすることで、金型から塊状マグネシウム合金材料に加えられる圧力を潤滑剤によって分散させ、均一変形に近づけることができる。
このようにすることで、塑性加工に伴い金属新生面が発生しても、該金属新生面が金型に直接接触して凝着あるいは焼き付きを生じないように、潤滑剤によって保護することができる。その結果、不良品の発生や、金型の損傷の発生を防止することができる。
このようにすることで、圧縮工程によって圧縮されたマグネシウム合金材料が、せん断工程にかけられることによって塑性加工製品が製造される。せん断工程は、例えば、プレス装置による打ち抜き加工である。この場合に、せん断加工に伴い、切断面には比較的滑らかなせん断部分(せん断面)と瞬間的に分離し荒れた面を呈する破断部分(破断面)が発生する。そこで、せん断工程を1.5mm/sec以下の圧下速度で行うことにより、切断面における破断部分が50%以下に抑えられる。これにより、応力集中の原因となる破断領域を少なくして、高い強度の塑性加工製品を製造することができる。
このようにすることで、塑性加工処理において金型に接触した成形品の表面には金属成分が不純物として残留する。残留した不純物は洗浄工程において洗浄され、その後の確認工程において、その濃度が確認される。そして、粒子径調整工程においては、成形品表面の不純物濃度が所定値以下である場合に行われるので、生分解性金属材料と不純物金属材料とが熱処理において反応することを防止して、さらに安定した分解速度を有するインプラントを製造することができる。
このようにすることで、成形品の表面に付着していた不純物金属材料は剥離された成形品の表面部分とともに確実に除去することができる。
このようにすることで、成形品の表面に付着していた不純物金属材料は、成形品の表面部分とともに酸により溶解され、除去されることになる。
このようにすることで、成形品の表面に付着していた不純物金属材料は、成形品の表面部分とともに酸により溶解され、除去される。そして、アルカリ溶液に浸漬することにより、酸による溶解反応を停止させることができる。
このようにすることで、塑性加工によって微細化した粒子径を容体化処理によって増大させて分解速度を低下させるとともに、成形品の強度を向上することができる。
このようにすることで、塑性加工によって微細化した粒子径を容体化処理によって増大させて分解速度を低下させることができる。また、容体化処理後の時効析出処理によって、成形品の強度をさらに向上することができる。
上述したように、c軸に平行な圧縮力に対する変形は、c軸に直交する圧縮力に対する変形よりも変形し難いので、主たる荷重方向にc軸を配向することによって、強度を向上することができる。
このようにすることで、マグネシウム合金の金属結晶のc軸をほぼ厚さ方向に配向させ、構造欠陥が少なく、厚さ方向の荷重に対する強度を向上することができる。
このようにすることによっても、マグネシウム合金の金属結晶のc軸をほぼ厚さ方向に配向させ、構造欠陥が少なく、厚さ方向の荷重に対する強度を向上することができる。
この場合に、打ち抜き加工により形成された厚さ方向に沿う面におけるせん断面の割合が厚さに対して50%以上であることが好ましい。
このようにすることで、応力集中の原因となる破断部分を少なくして強度の高いマグネシウム合金製インプラントを提供することができる。
本発明の第1の実施形態に係るインプラントの製造方法について、図1から図7を参照して以下に説明する。
本実施形態に係る製造方法により製造されるインプラントは、例えば、骨接合のために使用されるインプラントであって、生分解性金属材料、例えば、マグネシウム合金材料(例えば、WE43)により構成されているものである。
粒子径調整工程S2は、例えば、525℃で8時間熱処理(容体化処理)した後、空冷で冷却する工程である。熱処理の温度および処理時間は一例であり、他の条件を採用してもよい。
また、図4に、素材片、プレス加工後および熱処理後のそれぞれにおける生分解性金属材料の粒子径を示す。
このようにすることで、図6Aおよび図6Bに示されるように粒子径を大きく維持したままで、図7に示されるように、インプラントの機械的強度(ビッカース硬さ)を向上することができる。図6Bは、図6Aの矩形で囲まれた部分を拡大した顕微鏡写真である。
次に、本発明の第2の実施形態に係るインプラントの製造方法について、図8を参照して以下に説明する。
本実施形態の説明において、上述した第1の実施形態に係る製造方法と構成を共通とする箇所には同一符号を付して説明を省略する。
確認工程S4は、酸性溶液内に溶出したFeイオンの濃度を測定する工程である。
酸性溶液としては、生体に影響を及ぼすクロム酸やホウ酸など以外であればよく、リン酸や塩酸などを使用してよい。
また、確認工程S4においては、酸性溶液に所定時間浸漬した後の濃度を測定してもよいし、酸性溶液内におけるFeイオンを経時的に測定して濃度の変化率を求め、濃度変化が所定の閾値を下回った時点でのFeイオンの濃度を測定することにしてもよい。
また、インプラントの表面組成を蛍光X線装置によって直接分析し、Feイオン濃度を測定することにしてもよい。
また、生分解性金属材料としてマグネシウム合金を例示したが、他の任意の生分解性材料に適用してもよい。
また、上記実施形態においては、洗浄工程S3が成形品を酸性溶液に浸漬することにより、不純物金属材料を除去することとしたが、これに代えて、成形品の表面を切削等により剥離させることで除去することにしてもよい。
インプラント表面に残存するFeイオン濃度は0.02%以下、銅イオン濃度は0.15%以下、ニッケル濃度は0.01%以下であることが望ましい。
次に、本発明の第3の実施形態に係るインプラントの製造方法について、図9から図22Cを参照して以下に説明する。
本実施形態に係るインプラントの製造方法は、図9に示されるように、成形工程S1において第1の実施形態と異なる。したがって、本実施形態においては、成形工程S1について主に説明し、第1の実施形態と共通する他の工程S2,S21,S22については説明を省略する。本実施形態のインプラントの製造方法は、第2の実施形態において説明した洗浄工程S3、確認工程S4および判定工程S5をさらに備えていてもよい。
実際には、極点図測定等によって、押出し材1の(0001)面の配向性を測定し、(0001)面が顕著に配向されている面に対して直交する角度で切断して塊状マグネシウム合金材料2を得ることが好ましい。
そして、圧縮工程S13は、潤滑剤を塗布する工程と、金型によって塊状マグネシウム合金材料2を圧下する工程とを複数回繰り返して行うようになっている。
ここで、圧下率は、下式により表される。
圧下率=(圧縮前の厚さ-圧縮後の厚さ)/圧縮前の厚さ×100(%)
本実施形態に係るインプラントの製造方法によりマグネシウム合金材料を塑性加工するには、まず、マグネシウム合金素材を押出し工程S11によって押出し加工することにより、棒状の押出し材1を得る。
また、圧縮工程S13においては、金型と塊状マグネシウム合金材料2との間に潤滑剤が塗布された状態で圧縮力Fが加えられる。これにより、潤滑剤の作用によって、圧縮力Fが塊状マグネシウム合金材料2と金型との接触面全面に分散され、塊状マグネシウム合金材料2の全体にわたってより均一な圧縮力Fを加えることができる。
(実施例1)
実施例1は、塊状マグネシウム合金材料2に対する圧縮力Fの印加方向と、圧縮後の板状のマグネシウム合金材料の表面における金属結晶の配向性との関係を示す。
図13Aに、本実施形態に係る製造方法と同様に、押出し工程S11における押出し方向に対して垂直な方向に圧縮力Fを加えた場合(A材)、図13Bに、押出し方向に対して平行な方向に圧縮力Fを加えた場合(B材)の、板状のマグネシウム合金材料の表面における金属結晶の配向性を示す。
これらの図13Aおよび図13Bから、各圧縮方法で圧縮した場合のズレ角の平均値および集積幅を算出すると、表1の通りとなる。
これらの図14Aおよび図14Bから、各圧縮方法で圧縮した場合のズレ角の平均値および集積幅を算出すると、表2の通りとなる。
実施例2は、医療応用に適した塊状マグネシウム合金材料2(WE43)に対して圧縮力Fを加える際の圧縮条件を変化させて行われたものである。
試料としては、直径8mm長さ12mmの塊状マグネシウム合金材料2を使用した。圧縮工程S13における加熱温度を300℃、375℃、450℃と変化させ、圧縮時の圧下速度を5mm/sec、0.5mm/sec、0.05mm/secと変化させた結果を表3に示す。さらに、加熱温度を350℃、400℃、450℃と変化させ、圧縮時の圧下速度を1mm/sec、0.1mm/sec、0.01mm/secと変化させた結果を表4に示す。
また、図15に加熱温度375℃、圧下速度0.05mmの場合、図16に加熱温度375℃、圧下速度5mm/secの場合、図17に加熱温度450℃、圧下速度0.05mm/secの場合、図18に加熱温度450℃、圧下速度5mm/secの場合、図19に加熱温度350℃、圧下速度1mm/secの場合、図20に加熱温度350℃、圧下速度0.01mm/secの場合の、真ひずみ率εと負荷σとの関係をそれぞれ示す。
ここで、圧下率は、
圧下率=(圧縮前の厚さ-圧縮後の厚さ)/圧縮前の厚さ×100(%)
と表すことができる。
厚さ1mmの板状のマグネシウム合金材料(WE43)2を350℃に加熱した状態で、圧下速度を変化させてせん断力を加えた場合について、図21から図22Cを参照して説明する。
図21は、打ち抜き工程S14において、厚さ方向に形成された切断面における破断面部分の比率(破断面率)と、圧下速度との関係を示している。また、図22Aから図22Cは、圧下速度を変化させたときの、切断面の顕微鏡写真であり、圧下速度0.24mm/sec(図22A)、圧下速度1.44mm/sec(図22B)、圧下速度1.92mm/sec(図22C)の場合をそれぞれ示している。これらの図によれば、圧下速度が大きくなればなるほど、破断面率が大きくなることが示され、破断面率と圧下速度とは略比例関係にあることがわかった。
S2 粒子径調整工程
S3 洗浄工程
S4 確認工程
F 圧縮力
1 押出し材(マグネシウム合金成形材料)
2 塊状マグネシウム合金材料
S11 押出し工程
S12 切断工程
S13 圧縮工程
S14 打ち抜き工程(せん断工程)
Claims (21)
- 生分解性金属材料からなる素材片に塑性加工処理を施して成形品を成形する成形工程と、
該成形工程により成形された前記成形品を熱処理して金属粒子径を増大させる粒子径調整工程とを含むインプラントの製造方法。 - 前記成形工程が、
マグネシウム合金を押出し加工することにより、塑性変形したマグネシウム合金成形材料を得る押出し工程と、
該押出し工程により得られたマグネシウム合金成形材料を押出し方向に対して70°~110°の角度で切断する切断工程と、
該切断工程により得られた塊状マグネシウム合金材料に対して前記押出し方向に直交する方向の圧縮力を加える圧縮工程とを含む請求項1に記載のインプラントの製造方法。 - 前記圧縮工程に先立って、または前記圧縮工程において、前記塊状マグネシウム合金材料を加熱する加熱工程を含む請求項2に記載のインプラントの製造方法。
- 前記加熱工程が、300℃より高く、マグネシウム合金の融点以下の温度で前記塊状マグネシウム合金材料を加熱する請求項3に記載のインプラントの製造方法。
- 前記加熱工程が、350℃以上、マグネシウム合金の融点以下の温度で前記塊状マグネシウム合金材料を加熱する請求項3に記載のインプラントの製造方法。
- 前記圧縮工程が、45%以上の圧下率で前記塊状マグネシウム合金材料を圧縮する請求項3から請求項5のいずれかに記載のインプラントの製造方法。
- 前記圧縮工程が、前記塊状マグネシウム合金材料との間に潤滑剤を塗布した状態の金型によって圧縮力を加える請求項2から請求項6のいずれかに記載のインプラントの製造方法。
- 前記圧縮工程が、前記金型との前記塊状マグネシウム合金材料との間への潤滑剤の塗布と、圧縮力の印加とを少なくとも2回繰り返す請求項7に記載のインプラントの製造方法。
- 前記圧縮工程の後に、圧縮されたマグネシウム合金材料から製品を切り出すせん断工程を含み、
該せん断工程が、1.5mm/sec以下の圧下速度で行われる請求項2から請求項8のいずれかに記載のインプラントの製造方法。 - 前記成形工程により成形された成形品の表面を洗浄する洗浄工程と、
該洗浄工程により洗浄された前記成形品の表面の不純物濃度を確認する確認工程とを含み、
前記粒子径調整工程が、前記確認工程において不純物濃度が所定値以下であると確認された場合に前記成形品に熱処理を施す請求項1または請求項2に記載のインプラントの製造方法。 - 前記洗浄工程が、前記成形品の表面を剥離する処理である請求項10に記載のインプラントの製造方法。
- 前記洗浄工程が、前記成形品の表面を酸により溶解する処理である請求項11に記載のインプラントの製造方法。
- 前記洗浄工程が、前記成形品の表面を酸により溶解する処理と、その後にアルカリ溶液に浸漬する処理とを含む請求項11に記載のインプラントの製造方法。
- 前記粒子径調整工程が、容体化処理である請求項10から請求項13のいずれかに記載のインプラントの製造方法。
- 前記粒子径調整工程が、容体化処理の後に時効析出処理を行う請求項10から請求項13のいずれかに記載のインプラントの製造方法。
- 主たる荷重方向に金属結晶のc軸が配向されているマグネシウム合金製インプラント。
- 厚さ方向に対する金属結晶の(0001)面の法線のズレ角の平均値が、25°以下である請求項16に記載のマグネシウム合金製インプラント。
- 表面に沿う方向に対する金属結晶の(0001)面の法線のズレ角の平均値が、80°以上であり、かつ、ズレ角の最大値の16~84%となるズレ角の累計分布の幅が50°以下である請求項16に記載のマグネシウム合金製インプラント。
- 打ち抜き加工により製造された請求項16から請求項18のいずれかに記載のマグネシウム合金製インプラント。
- 打ち抜き加工により形成された厚さ方向に沿う切断面におけるせん断部分の割合が厚さに対して50%以上である請求項18に記載のマグネシウム合金製インプラント。
- その表面に含まれるFeイオン濃度が0.02%以下、銅イオン濃度が0.15%以下、ニッケル濃度が0.01%以下である請求項16から請求項20のいずれかに記載のマグネシウム合金製インプラント。
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201380079687.6A CN105555985A (zh) | 2013-09-24 | 2013-09-24 | 植入物及其制造方法 |
| JP2015538650A JPWO2015044997A1 (ja) | 2013-09-24 | 2013-09-24 | インプラントとその製造方法 |
| PCT/JP2013/075635 WO2015044997A1 (ja) | 2013-09-24 | 2013-09-24 | インプラントとその製造方法 |
| EP13894102.6A EP3050996A4 (en) | 2013-09-24 | 2013-09-24 | Implant and manufacturing method therefor |
| US15/072,406 US20160199186A1 (en) | 2013-09-24 | 2016-03-17 | Implant and method of manufacturing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/JP2013/075635 WO2015044997A1 (ja) | 2013-09-24 | 2013-09-24 | インプラントとその製造方法 |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US15/072,406 Continuation US20160199186A1 (en) | 2013-09-24 | 2016-03-17 | Implant and method of manufacturing the same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2015044997A1 true WO2015044997A1 (ja) | 2015-04-02 |
Family
ID=52742211
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP2013/075635 Ceased WO2015044997A1 (ja) | 2013-09-24 | 2013-09-24 | インプラントとその製造方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20160199186A1 (ja) |
| EP (1) | EP3050996A4 (ja) |
| JP (1) | JPWO2015044997A1 (ja) |
| CN (1) | CN105555985A (ja) |
| WO (1) | WO2015044997A1 (ja) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| PL3192886T3 (pl) * | 2014-09-09 | 2019-05-31 | National Univ Corporation Kobe Univ | Urządzenie do mocowania biologicznych tkanek miękkich i sposób jego wytwarzania |
| US20180029097A1 (en) * | 2016-10-05 | 2018-02-01 | Ghader Faraji | Hydrostatic cyclic expansion extrusion process for producing ultrafine-grained rods |
| FR3104407B1 (fr) * | 2019-12-12 | 2021-12-10 | Etablissements Maurice Marle | Procede de formage de lopin pour implant |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2007058276A1 (ja) * | 2005-11-16 | 2007-05-24 | National Institute For Materials Science | マグネシウム系生分解性金属材料 |
| JP4150219B2 (ja) | 2002-06-27 | 2008-09-17 | 松下電器産業株式会社 | 塊状マグネシウム合金材料の塑性加工方法 |
| JP2009178293A (ja) | 2008-01-30 | 2009-08-13 | Terumo Corp | 医療用インプラント |
| JP2009535504A (ja) * | 2006-04-28 | 2009-10-01 | バイオマグネシウム システムズ リミテッド | 生分解性マグネシウム合金およびその使用 |
| JP2013524004A (ja) * | 2010-03-25 | 2013-06-17 | マグネシウム エレクトロン リミテッド | 重希土類元素含有マグネシウム合金 |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3525439B2 (ja) * | 1992-03-04 | 2004-05-10 | 日立金属株式会社 | ターゲット部材およびその製造方法 |
| CN101411891B (zh) * | 2008-12-01 | 2012-11-21 | 天津理工大学 | 一种可降解纳米钙磷化合物增强镁锌合金骨折内固定材料 |
| US20120215301A1 (en) * | 2009-10-30 | 2012-08-23 | Acrostak Corp Bvi, Tortola | Biodegradable implantable medical devices formed from super - pure magnesium-based material |
| CN101845607B (zh) * | 2009-11-23 | 2014-03-12 | 北京有色金属研究总院 | 镁合金强韧化变形加工方法 |
| CN103243283B (zh) * | 2013-05-27 | 2015-10-07 | 中国科学院长春应用化学研究所 | 超细晶稀土镁合金的制备方法 |
-
2013
- 2013-09-24 WO PCT/JP2013/075635 patent/WO2015044997A1/ja not_active Ceased
- 2013-09-24 EP EP13894102.6A patent/EP3050996A4/en not_active Withdrawn
- 2013-09-24 JP JP2015538650A patent/JPWO2015044997A1/ja active Pending
- 2013-09-24 CN CN201380079687.6A patent/CN105555985A/zh active Pending
-
2016
- 2016-03-17 US US15/072,406 patent/US20160199186A1/en not_active Abandoned
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4150219B2 (ja) | 2002-06-27 | 2008-09-17 | 松下電器産業株式会社 | 塊状マグネシウム合金材料の塑性加工方法 |
| WO2007058276A1 (ja) * | 2005-11-16 | 2007-05-24 | National Institute For Materials Science | マグネシウム系生分解性金属材料 |
| JP2009535504A (ja) * | 2006-04-28 | 2009-10-01 | バイオマグネシウム システムズ リミテッド | 生分解性マグネシウム合金およびその使用 |
| JP2009178293A (ja) | 2008-01-30 | 2009-08-13 | Terumo Corp | 医療用インプラント |
| JP2013524004A (ja) * | 2010-03-25 | 2013-06-17 | マグネシウム エレクトロン リミテッド | 重希土類元素含有マグネシウム合金 |
Non-Patent Citations (1)
| Title |
|---|
| See also references of EP3050996A4 |
Also Published As
| Publication number | Publication date |
|---|---|
| JPWO2015044997A1 (ja) | 2017-03-02 |
| EP3050996A4 (en) | 2017-10-04 |
| EP3050996A1 (en) | 2016-08-03 |
| US20160199186A1 (en) | 2016-07-14 |
| CN105555985A (zh) | 2016-05-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP5758204B2 (ja) | チタン合金部材およびその製造方法 | |
| JP6296558B2 (ja) | 銅合金およびその製造方法 | |
| Han et al. | Effect of ECAP numbers on microstructure and properties of titanium matrix composite | |
| JP5050199B2 (ja) | マグネシウム合金材料製造方法及び装置並びにマグネシウム合金材料 | |
| TW201718895A (zh) | 鎳-鈦合金之熱機械處理 | |
| JP6737686B2 (ja) | 純チタン金属ワイヤおよびその加工方法 | |
| CN103180473A (zh) | 由镁合金构成的线状体、螺栓、螺帽和垫圈 | |
| JP6300375B2 (ja) | Cu−Be合金およびその製造方法 | |
| Meng et al. | Deformation behavior and microstructure evolution in thermal-aided mesoforming of titanium dental abutment | |
| CN105579168A (zh) | 液相烧结铝合金部件的制造方法以及液相烧结铝合金部件 | |
| Omranpour et al. | Nanostructure development in refractory metals: ECAP processing of Niobium and Tantalum using indirect-extrusion technique | |
| WO2015044997A1 (ja) | インプラントとその製造方法 | |
| KR20090118404A (ko) | 동적 변형 특성이 개선된 알루미늄 합금의 제조방법 | |
| TWI279446B (en) | The method for producing magnesium alloy molding | |
| JP5959260B2 (ja) | マグネシウム合金製インプラントの加工方法 | |
| CN103619506B (zh) | 镁合金材料制造方法及镁合金制棒材 | |
| JP5871490B2 (ja) | チタン合金部材およびその製造方法 | |
| Kurzydlowski et al. | Effect of severe plastic deformation on the microstructure and mechanical properties of Al and Cu | |
| Ghorbani et al. | Microstructural evolution and room temperature mechanical properties of AZ31 alloy processed through hot constrained compression | |
| Derakhshandeh et al. | Microstructure and mechanical properties of ultrafine-grained titanium processed by multi-pass ECAP at room temperature using core–sheath method | |
| KR102084304B1 (ko) | 강도와 내부식성이 우수한 마그네슘 합금 및 이의 제조방법 | |
| CN103290344A (zh) | 一种无粗晶2618铝合金等温模锻件的制备方法 | |
| JPWO2018030231A1 (ja) | 純チタン金属材料薄板の製造方法およびスピーカ振動板の製造方法 | |
| Masouleh et al. | Enhancing mechanical properties in Mg microtubes using tubular channel angular pressing-extrusion (TCAPE): A promising severe plastic deformation method | |
| CN101754824B (zh) | 挤压用坯料的制造方法和镁合金原材料的制造方法 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WWE | Wipo information: entry into national phase |
Ref document number: 201380079687.6 Country of ref document: CN |
|
| 121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 13894102 Country of ref document: EP Kind code of ref document: A1 |
|
| ENP | Entry into the national phase |
Ref document number: 2015538650 Country of ref document: JP Kind code of ref document: A |
|
| NENP | Non-entry into the national phase |
Ref country code: DE |
|
| REEP | Request for entry into the european phase |
Ref document number: 2013894102 Country of ref document: EP |
|
| WWE | Wipo information: entry into national phase |
Ref document number: 2013894102 Country of ref document: EP |