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WO2019054303A1 - Production method for titanium or titanium alloy green compact - Google Patents

Production method for titanium or titanium alloy green compact Download PDF

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Publication number
WO2019054303A1
WO2019054303A1 PCT/JP2018/033265 JP2018033265W WO2019054303A1 WO 2019054303 A1 WO2019054303 A1 WO 2019054303A1 JP 2018033265 W JP2018033265 W JP 2018033265W WO 2019054303 A1 WO2019054303 A1 WO 2019054303A1
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WO
WIPO (PCT)
Prior art keywords
titanium
diameter portion
green compact
producing
mold
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
Application number
PCT/JP2018/033265
Other languages
French (fr)
Japanese (ja)
Inventor
早川 昌志
藤井 秀樹
松秀 堀川
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toho Titanium Co Ltd
Original Assignee
Toho Titanium Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Toho Titanium Co Ltd filed Critical Toho Titanium Co Ltd
Priority to JP2019542034A priority Critical patent/JP6866491B2/en
Publication of WO2019054303A1 publication Critical patent/WO2019054303A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/02Compacting only
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12Both compacting and sintering
    • B22F3/16Both compacting and sintering in successive or repeated steps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/10Processes of additive manufacturing
    • B29C64/106Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/30Auxiliary operations or equipment
    • B29C64/379Handling of additively manufactured objects, e.g. using robots
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y10/00Processes of additive manufacturing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y80/00Products made by additive manufacturing

Definitions

  • the present invention relates to a method for producing a titanium or titanium alloy green compact.
  • titanium and titanium alloys have excellent mechanical properties, they are difficult to process and complex shaped products have been conventionally manufactured by cutting. However, in the case of manufacturing by cutting, there is a problem that the yield is bad and the product unit price becomes very high.
  • the method of manufacturing titanium and a titanium alloy green compact using an elementary powder mixing method is known.
  • pure titanium powder and a powder for alloying element addition are mixed at a predetermined ratio, filled into a mold, compacted at room temperature, and then sintered or cold isostatic press (CIP) ) Processing method etc.
  • CIP cold isostatic press
  • JP-A-7-90313 a thermoplastic resin is used to prepare a powder molding die by a blow molding method, the powder molding die is filled with titanium powder, and molding is performed using a hydrostatic pressure press.
  • JP-A-2010-188711 describes a method for producing a bottomed cylindrical container in which a bottomed cylindrical container is stretch blow molded from a thermoplastic resin preform.
  • the present invention provides a method for producing a titanium or titanium alloy green compact capable of producing a titanium or titanium alloy green compact having a complicated shape with high accuracy of external dimensions more economically. Do.
  • the present invention completed on the basis of the above findings is, according to one aspect, a method for producing a titanium or titanium alloy green compact from which a titanium or titanium alloy green compact having a relative density of 80% or more is obtained using a cold isostatic press. It is expressed by (maximum value-minimum value) / (maximum value + minimum value) when thickness is 0.5 to 1.5 mm and thickness of any 10 points in the longitudinal direction of the mold is measured.
  • Mold thickness error range index 0 is 0 to 0.05
  • compression elastic modulus is 800MPa to 2100MPa
  • Shore D hardness is 78 to 85
  • it is made of thermoplastic resin, and powder supply port and cavity for powder filling
  • the method for producing a titanium or titanium alloy green compact according to the present invention is such that the CIP molding mold is continuous with the large diameter portion and the large diameter portion and the cross-sectional area of the horizontal cross section is smaller than that of the large diameter portion.
  • a ratio D of the smallest diameter of the small diameter portion to the largest diameter of the large diameter portion in the horizontal cross section (small diameter portion smallest diameter / large diameter portion largest diameter) is at least 0.5 and less than 0.8. .
  • the outer surface of the small diameter portion is inclined with respect to the outer surface of the large diameter portion,
  • An angle ⁇ between a straight line extending in the extending direction of the outer surface of the large diameter portion from the end of the outer surface and the outer surface of the small diameter portion is 10 degrees or more and less than 60 degrees.
  • the method for producing a titanium or titanium alloy green compact according to the present invention includes producing a CIP molding mold using a 3D printer device.
  • the method for producing a titanium or titanium alloy green compact according to the present invention includes, in yet another embodiment, producing a CIP molding mold using a 3D printer apparatus utilizing a material extrusion method.
  • the method for producing a titanium or titanium alloy green compact according to the present invention includes, in yet another embodiment, producing a CIP molding mold using a 3D printer apparatus utilizing a material injection method.
  • a pure titanium powder having an average particle diameter of 30 ⁇ m to less than 100 ⁇ m, and an alloy element powder or a master alloy having an average particle diameter of 5 ⁇ m to less than 50 ⁇ m. 1 to 20% by mass of the powder is included in the cavity of the CIP mold.
  • FIG. 2 (a) is an explanatory view for explaining an inclination angle ⁇ of the large diameter portion and the small diameter portion of the CIP molding mold according to the embodiment of the present invention
  • FIG. (B) is an example in case a small diameter part has a slope of a curved surface shape.
  • the method for producing a titanium or titanium alloy green compact is a method for producing titanium or titanium alloy green compact having a relative density of 80% or more using a cold isostatic press (CIP)
  • CIP cold isostatic press
  • the material of the CIP molding mold 1 In order to manufacture a titanium or titanium alloy green compact having a high accuracy in external dimensions and a complicated shape, the material of the CIP molding mold 1, the compression modulus, and the Shore D in relation to the manufacturing process of the CIP treatment It is necessary to adjust the hardness to an appropriate range and to increase the accuracy of the thickness and thickness of the CIP molding mold 1.
  • the CIP molding mold 1 needs to have a thickness of 0.5 to 1.5 mm. If the thickness is less than 0.5 mm, the CIP molding mold 1 may be deformed by the weight of the filling powder, and the dimensional accuracy may be reduced. On the other hand, if the thickness is greater than 1.5 mm, the springback force of the CIP molding mold 1 at CIP unloading may be greater than the green compact strength, and breakage of the green compact may occur.
  • the mold thickness error range index ⁇ represented by (maximum value-minimum value) / (maximum value + minimum value) when the thickness of any 10 points in the longitudinal direction of the mold is measured Is preferably from 0 to 0.05.
  • the measurement points of the thickness are locally biased, the variation in the thickness of the CIP molding mold 1 as a whole may not be properly evaluated. Therefore, in this embodiment, it means a place obtained by equally dividing the longest surface of the CIP molding mold 1 into ten as measurement points of “arbitrary 10 points of thickness”. For example, as shown in FIG.
  • the CIP molding mold 1 is allowed to stand on a horizontal surface so that the longitudinal direction along the maximum length of the CIP molding mold 1 is perpendicular to the horizontal surface, and a direction perpendicular to the horizontal surface
  • the thickness at each position (1 to 10) obtained by equally dividing the CIP molding mold 1 into 10 can be measured.
  • “mold thickness error range index ⁇ ” is an arbitrary height of each height when CIP mold 1 is equally divided into 10 along the longitudinal direction of CIP mold 1.
  • the thickness of the measurement point at the position is measured, and the maximum value and the minimum value are used to indicate the error range index evaluated.
  • the thickness can be measured, for example, by using a digital caliper or the like for each measurement point.
  • the mold thickness error range index ⁇ is preferably 0.03 or less, more preferably 0.01 or less, and still more preferably 0.005 or less.
  • the mold thickness error range index ⁇ is a measurement point at any position of each height when divided equally into ten along the longitudinal direction of the CIP molding mold 1 It refers to “(maximum value ⁇ minimum value) / target thickness” when the thickness of each is measured.
  • the target thickness for example, the thickness of three-dimensional CAD original data at the time of molding of the CIP molding mold 1 can be used.
  • the mold thickness error range index ⁇ becomes larger than 0.5, the accuracy of the external dimensions of the titanium or titanium alloy powder compact manufactured using the CIP molding mold 1 is deteriorated and the control of the spring back force is also performed. Becomes difficult and cause breakage.
  • the error of the mold thickness error range index ⁇ of 0.5 or less does not affect the physical properties of the CIP molding mold 1.
  • the mold thickness error range index ⁇ is preferably 0.3 or less, more preferably 0.1 or less, and still more preferably 0.06 or less.
  • the absolute value of any 10 points (thickness / target thickness ⁇ 100-100) of each height when CIP mold 1 is equally divided into 10 along the longitudinal direction of CIP mold 1 The average value of can also be evaluated as a mold thickness error range index ⁇ .
  • the mold thickness error range index ⁇ is preferably less than 1.5, more preferably 1.0 or less, and still more preferably 0.5 or less.
  • thermoplastic resin As a material used for the mold 1 for CIP molding, a thermoplastic resin is preferable, and for example, acrylic resin, polylactic acid (PLA) resin, etc. can be suitably used.
  • the compressive elastic modulus of the thermoplastic resin material is preferably 800 MPa to 2100 MPa. If the compressive elastic modulus is less than 800 MPa, the spring back of the CIP molding mold 1 during CIP unloading may be large, which may lead to green powder fracture. If the compressive elastic modulus is too low, the rigidity of the CIP molding mold 1 may not be sufficient, and the CIP molding mold 1 may be deformed by the own weight of the filling powder, and the dimensional accuracy of the CIP molded product may be significantly reduced.
  • the compressive elastic modulus of the thermoplastic resin used for the CIP molding mold 1 is more preferably 1000 MPa to 1900 MPa, still more preferably 1500 MPa to 1900 MPa.
  • the compressive elastic modulus can be measured by a test method in accordance with JIS K7181 (2011).
  • the Shore D hardness of the thermoplastic resin used for the CIP molding mold 1 is preferably 78 to 85, and more preferably 80 to 83.
  • Shore D hardness is less than 78, the CIP molding mold 1 is deformed by the weight of the filling powder, and the dimensional accuracy is reduced.
  • Shore D hardness is greater than 85, the rigidity of the CIP molding mold 1 becomes high, and the load is not sufficiently transmitted to the internal powder at the time of CIP processing pressurization, and a titanium or titanium alloy green compact having a relative density of 80% or more is obtained I can not do it.
  • Shore D hardness can be measured by a test method in accordance with JIS K 7215 (1986).
  • the CIP molding mold 1 is continuous with the large diameter portion 11 and the large diameter portion 11 and has a small diameter portion 12 having a smaller horizontal cross-sectional area than the large diameter portion 11 and a smaller diameter portion 12
  • the cross section of the horizontal cross section is also large, and it includes a large diameter portion 13 continuous with the small diameter portion 12 and a top portion 14 continuous with the large diameter portion 13 and having a powder supply port 2 at the top.
  • the cross-sectional area in the horizontal direction gradually decreases from the bottom to the top, and the cross-sectional area in the horizontal direction gradually increases from the middle portion of the small diameter portion 12 toward the large diameter portion 13. It can have a shape.
  • the horizontal cross section may have a polygonal shape, or the horizontal cross section may be circular or elliptical, and can be appropriately changed according to the use application, and the specific shape Is not particularly limited.
  • the shapes of the large diameter portions 11 and 13 and the small diameter portion 12 preferably have substantially similar shapes in horizontal cross sections, but may have shapes different from each other.
  • the outer side surface 121 of the small diameter portion 12 is inclined with respect to the outer side surface 111 of the large diameter portion 11.
  • An example of an angle ⁇ (FIG. 2A) between a straight line X extending from the end 112 of the outer surface 111 of the large diameter portion 11 to the outer surface 111 of the large diameter portion 11 and the outer surface 121 of the small diameter portion 12 Then, the angle ⁇ ) between the straight line X and the outer surface 121 of the small diameter portion 12 when measured counterclockwise from the straight line X is 10 degrees or more and less than 60 degrees.
  • the outer surface 121 of the small diameter portion 12 has a curved surface, as shown in FIG.
  • the angle ⁇ between the straight line Y passing through the straight line X and the straight line X is 10 degrees or more and less than 60 degrees.
  • the CIP molding mold 1 having a complicated shape as shown in FIGS. 1 and 2 (a) and 2 (b) can be manufactured using a 3D printer. Thereby, the thickness can be made uniform, and the dimensional accuracy can be improved, as compared with the case where the mold is formed by blow molding as in the prior art. Moreover, since it is not necessary to manufacture a mold etc. in the case of manufacture of a mold, the mold 1 for CIP molding which has a complicated shape more economically can be manufactured so that a dimensional accuracy may become high.
  • a general-purpose device can be used as the 3D printer device, it is preferable to use a 3D printer device using a material extrusion method or a 3D printer device using a material injection method.
  • the titanium according to the present embodiment is implemented by filling pure titanium powder or pure titanium powder and alloy element powder or mother alloy powder in the cavity 3 in the CIP molding mold 1 according to the present embodiment and performing CIP processing. Or a titanium alloy green compact is obtained.
  • the alloying element powder is a powder of a single element such as Al powder or V powder
  • the mother alloy powder is a powder containing a plurality of elements.
  • a filler for example, 80 to 100% by mass of pure titanium powder having an average particle diameter of 30 ⁇ m or more and less than 100 ⁇ m, and filled in a cavity of a CIP molding mold, titanium or titanium alloy green compact having a relative density of 80% or more Is obtained.
  • 1 to 20 mass% of pure titanium powder having an average particle diameter of 30 ⁇ m or more and less than 100 ⁇ m and alloy element powder or mother alloy powder having an average particle diameter of 5 to 50 ⁇ m is filled in the cavity 3 of the CIP molding mold 1
  • a titanium or titanium alloy green compact having a relative density of 80% or more can be obtained.
  • an average particle diameter points out the value of particle diameter D50 (median diameter) of the particle size distribution (volume basis) obtained by the laser diffraction scattering method.
  • Powder filling and CIP treatment can be carried out using generally well known conditions.
  • "pure titanium” means industrial pure titanium that satisfies the composition defined in JIS II.
  • the main alloy systems used for titanium alloy compacts include Ti-6Al-4V, Ti-6Al-6V-2Sn, Ti-6Al-2Sn-4Zr-2Mo, Ti-6Al-2Sn-4Zr-6Mo, Ti. And -10V-2Fe-3Al.
  • a CIP molding mold whose thickness and thickness accuracy are controlled using a predetermined thermoplastic resin using a 3D printer
  • a CIP molding mold whose thickness and thickness accuracy are controlled using a predetermined thermoplastic resin using a 3D printer
  • the CIP molding mold using PLA resin was manufactured by a material extrusion method using a 3D printer apparatus Kuria, manufactured by Kubo Metals Co., Ltd.
  • the CIP molding mold using an acrylic resin was manufactured by a material injection method using a 3D printing apparatus ProJet 3600MAX manufactured by 3D Systems.
  • the silicone resin material was manufactured by a material injection method using a Keyence 3D printer AGILISTA-3200.
  • the ratio D of the large diameter portion to the small diameter portion of the CIP molding mold is 0.6, the angle ⁇ between the large outer diameter and the small outer diameter is set to 27 degrees, and the CIP molding mold having the shape shown in FIG. Made.
  • a hollow in the produced CIP molding mold was filled with Tohotec pure titanium powder TC-150 (particle size width 45-150 ⁇ m, average particle size 90 ⁇ m) and subjected to CIP treatment.
  • TC-150 particle size width 45-150 ⁇ m, average particle size 90 ⁇ m
  • CIP treatment a cold isostatic pressing apparatus CL4-22-60 manufactured by Nikkiso Co., Ltd. was used.
  • a hollow in the produced CIP molding mold is filled with pure titanium powder, tapped, vacuum-packed one sealed with a vinyl tape, and the vacuum-packed pure titanium powder-filled product is set in a cold isostatic molding machine And pressurized. After reaching about 300 MPa, after holding for 1 minute, pressure was released, and the titanium powder-filled product was removed from the cold isostatic pressing apparatus. The obtained molded product was heated at 130 ° C. for 15 minutes at atmospheric pressure, and the softened mold for CIP molding was removed using a cutter, nipper or the like to obtain a green compact.
  • Mold thickness error range indexes ⁇ , ⁇ , ⁇ , compressive modulus, Shore D hardness, and green density (relative density) were measured for CIP molding molds produced using each material and each device.
  • Target thickness used thickness at the time of 3D data creation.
  • the CIP molding mold 1 was divided into 10 equal parts in the longitudinal direction (in this example, 12 mm intervals), and the thickness of 10 points was measured with a tic-ness gauge.
  • the compressive elastic modulus was calculated from the measurement result implemented based on JISK7181 (2011).
  • Shore D hardness was measured in accordance with JIS K 7215 (1986).
  • the green density was calculated from the density / theoretical density 4.51 / cm 3 ⁇ 100 obtained by the Archimedes method. Furthermore, the presence or absence of breakage of the obtained green compact was observed. The results are shown in Table 1.
  • Comparative Examples 1 and 2 in which a CIP molding mold having a thickness of 1.75 mm, which was outside the range of 0.5 to 1.5 mm in thickness, was produced, although the mold could be produced, the pressure of titanium or titanium alloy was used. The powder was broken and the desired green compact could not be produced.
  • Comparative Examples 3 and 4 using a silicone resin whose compressive elastic modulus and Shore D hardness were out of the range of the present invention, it was not possible to produce a CIP mold.
  • the mold was able to be produced, the shape after powder filling was not able to be maintained at the time of CIP processing by lack of intensity

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Abstract

A production method for a titanium or titanium alloy green compact. The production method uses a cold isostatic press to produce a titanium or titanium alloy green compact that has a relative density of at least 80%. The production method uses a CIP mold 1 that: is 0.5–1.5 mm thick; has a mold thickness error range index α of 0–0.05, given by (maximum thickness-minimum thickness)/(maximum thickness+minimum thickness) when the thickness of the mold is measured at 10 arbitrary points in the longitudinal direction thereof; comprises a thermoplastic resin that has a compressive modulus of elasticity of 800–2,100 MPa and a Shore D hardness of 78–85; and has a powder supply port and a cavity for filling with powder.

Description

チタン又はチタン合金圧粉体の製造方法Method of producing titanium or titanium alloy green compact

 本発明は、チタン又はチタン合金圧粉体の製造方法に関する。 The present invention relates to a method for producing a titanium or titanium alloy green compact.

 チタン及びチタン合金は優れた機械的特性を有するが、加工が難しく、複雑形状製品は従来切削により製造されてきた。しかしながら、切削で製造する場合は歩留まりが悪く、製品単価が非常に高くなるという問題がある。 Although titanium and titanium alloys have excellent mechanical properties, they are difficult to process and complex shaped products have been conventionally manufactured by cutting. However, in the case of manufacturing by cutting, there is a problem that the yield is bad and the product unit price becomes very high.

 上記問題を解決する手法の一つとして、素粉末混合法を用いてチタン及びチタン合金圧粉体の製造を行う方法が知られている。素粉末混合法は、純チタン粉末と合金元素添加用粉末を所定の割合で混合し、これをモールドに充填後、室温で圧粉成形し、その後焼結処理や冷間等方圧プレス(CIP)処理等を行う処理方法である。 As one of the methods of solving the said problem, the method of manufacturing titanium and a titanium alloy green compact using an elementary powder mixing method is known. In the elementary powder mixing method, pure titanium powder and a powder for alloying element addition are mixed at a predetermined ratio, filled into a mold, compacted at room temperature, and then sintered or cold isostatic press (CIP) ) Processing method etc.

 例えば、特開平7-90313号公報には、熱可塑性樹脂を使用してブロー成形法により粉末成形用型を作製し、その粉末成形用型にチタン粉末を充填し、静水圧成形プレスで成形することで、チタン粉体の成形体を製造する方法が記載されている。特開2010-188711号公報には、熱可塑製樹脂製のプリフォームから底付き筒状容器を延伸ブロー成形する底付き筒状容器の製造方法が記載されている。 For example, in JP-A-7-90313, a thermoplastic resin is used to prepare a powder molding die by a blow molding method, the powder molding die is filled with titanium powder, and molding is performed using a hydrostatic pressure press. Thus, a method of producing a compact of titanium powder is described. JP-A-2010-188711 describes a method for producing a bottomed cylindrical container in which a bottomed cylindrical container is stretch blow molded from a thermoplastic resin preform.

特開平7-90313号公報JP 7-90313 A 特開2010-188711号公報JP, 2010-188711, A

 しかしながら、特許文献1及び2に例示されるような熱可塑製樹脂をブロー成形して成形体を形成する方法では、割れなく高密度の成形体が得られるが、厚さの精度が出にくい。そのため、ブロー成形により製造された成形体を用いて製造されたチタン又はチタン合金圧粉体は、外形寸法にずれが生じやすくなる。外形寸法の精度を高めるためには、金属金型などを利用する方法もあるが、高価になる上、複雑形状が製造しにくくなる。 However, according to the method of blow molding thermoplastic resin as exemplified in Patent Documents 1 and 2 to form a molded article, a high-density molded article can be obtained without cracking, but it is difficult to obtain accurate thickness. Therefore, the titanium or titanium alloy green compact manufactured using the molded object manufactured by blow molding becomes easy to produce a gap in an outside dimension. Although there is also a method of using a metal mold or the like in order to improve the accuracy of the outer dimension, it becomes expensive and it becomes difficult to manufacture a complicated shape.

 上記課題を鑑み、本発明は、外形寸法の精度が高く、複雑形状を有するチタン又はチタン合金圧粉体をより経済的に製造することが可能なチタン又はチタン合金圧粉体の製造方法を提供する。 In view of the above problems, the present invention provides a method for producing a titanium or titanium alloy green compact capable of producing a titanium or titanium alloy green compact having a complicated shape with high accuracy of external dimensions more economically. Do.

 本発明者は鋭意検討を重ねたところ、所定の特性を有する熱可塑製樹脂を用いて、所定の厚さ範囲及び厚さ精度を有するCIP成形用モールドを用いることが有用であるとの知見を得た。 As a result of intensive studies, the present inventors have found that it is useful to use a CIP molding mold having a predetermined thickness range and thickness accuracy using a thermoplastic resin having predetermined characteristics. Obtained.

 以上の知見を基礎として完成した本発明は一側面において、冷間等方圧プレスを用いて相対密度80%以上のチタン又はチタン合金圧粉体を得るチタン又はチタン合金圧粉体の製造方法であって、厚さが0.5~1.5mm、且つモールドの長手方向の任意の10点の厚みを測定した場合の(最大値-最小値)/(最大値+最小値)で表されるモールド厚さ誤差範囲指数αが0~0.05であり、圧縮弾性率が800MPa~2100MPa、ショアD硬さが78~85の熱可塑製樹脂からなり、粉末供給口と粉末充填用の空洞とを有するCIP成形用モールドを用いることを特徴とするチタン又はチタン合金圧粉体の製造方法が提供される。 The present invention completed on the basis of the above findings is, according to one aspect, a method for producing a titanium or titanium alloy green compact from which a titanium or titanium alloy green compact having a relative density of 80% or more is obtained using a cold isostatic press. It is expressed by (maximum value-minimum value) / (maximum value + minimum value) when thickness is 0.5 to 1.5 mm and thickness of any 10 points in the longitudinal direction of the mold is measured. Mold thickness error range index 0 is 0 to 0.05, compression elastic modulus is 800MPa to 2100MPa, Shore D hardness is 78 to 85, and it is made of thermoplastic resin, and powder supply port and cavity for powder filling There is provided a method for producing a titanium or titanium alloy green compact characterized by using a CIP molding mold having

 本発明に係るチタン又はチタン合金圧粉体の製造方法は一実施態様において、CIP成形用モールドが、大径部と、大径部に連続し、大径部よりも水平断面の断面積が小さい小径部とを少なくとも備え、且つ水平断面における大径部の最大径に対する小径部の最小径の比率D(小径部最小径/大径部最大径)が、0.5以上0.8未満である。 In one embodiment, the method for producing a titanium or titanium alloy green compact according to the present invention is such that the CIP molding mold is continuous with the large diameter portion and the large diameter portion and the cross-sectional area of the horizontal cross section is smaller than that of the large diameter portion. A ratio D of the smallest diameter of the small diameter portion to the largest diameter of the large diameter portion in the horizontal cross section (small diameter portion smallest diameter / large diameter portion largest diameter) is at least 0.5 and less than 0.8. .

 本発明に係るチタン又はチタン合金圧粉体の製造方法は別の一実施態様において、CIP成形用モールドは、大径部の外側面に対して小径部の外側面が傾斜し、大径部の外側面の端部から大径部の外側面の延在方向に延びる直線と小径部の外側面とのなす角θが10度以上60度未満である。 In another embodiment of the method for producing a titanium or titanium alloy green compact according to the present invention, in the CIP molding mold, the outer surface of the small diameter portion is inclined with respect to the outer surface of the large diameter portion, An angle θ between a straight line extending in the extending direction of the outer surface of the large diameter portion from the end of the outer surface and the outer surface of the small diameter portion is 10 degrees or more and less than 60 degrees.

 本発明に係るチタン又はチタン合金圧粉体の製造方法は更に別の一実施態様において、CIP成形用モールドを、3Dプリンタ装置を用いて作製することを含む。 The method for producing a titanium or titanium alloy green compact according to the present invention, in yet another embodiment, includes producing a CIP molding mold using a 3D printer device.

 本発明に係るチタン又はチタン合金圧粉体の製造方法は更に別の一実施態様において、CIP成形用モールドを、材料押出法を利用した3Dプリンタ装置を用いて作製することを含む。 The method for producing a titanium or titanium alloy green compact according to the present invention includes, in yet another embodiment, producing a CIP molding mold using a 3D printer apparatus utilizing a material extrusion method.

 本発明に係るチタン又はチタン合金圧粉体の製造方法は更に別の一実施態様において、CIP成形用モールドを、材料噴射法を利用した3Dプリンタ装置を用いて作製することを含む。 The method for producing a titanium or titanium alloy green compact according to the present invention includes, in yet another embodiment, producing a CIP molding mold using a 3D printer apparatus utilizing a material injection method.

 本発明に係るチタン又はチタン合金圧粉体の製造方法は更に別の一実施態様において、平均粒径30μm以上100μm未満の純チタン粉末を80~100質量%、CIP成形用モールドの空洞内に充填することを含む。 In still another embodiment of the method for producing a titanium or titanium alloy green compact according to the present invention, 80 to 100% by mass of pure titanium powder having an average particle diameter of 30 μm or more and less than 100 μm is filled in a cavity of a mold for CIP molding To do.

 本発明に係るチタン又はチタン合金圧粉体の製造方法は更に別の一実施態様において、平均粒径30μm以上100μm未満の純チタン粉末と、平均粒径5μm以上50μm未満の合金元素粉末又は母合金粉末とを1~20質量%、CIP成形用モールドの空洞内に充填することを含む。 In still another embodiment of the method for producing a titanium or titanium alloy green compact according to the present invention, a pure titanium powder having an average particle diameter of 30 μm to less than 100 μm, and an alloy element powder or a master alloy having an average particle diameter of 5 μm to less than 50 μm. 1 to 20% by mass of the powder is included in the cavity of the CIP mold.

 本発明によれば、外形寸法の精度が高く、複雑形状を有するチタン又はチタン合金圧粉体をより経済的に製造することが可能なチタン又はチタン合金圧粉体の製造方法が提供できる。 According to the present invention, it is possible to provide a method for producing a titanium or titanium alloy green compact which can produce titanium or titanium alloy green compact having a complicated shape with high accuracy of external dimensions more economically.

本発明の実施の形態に係るCIP成形用モールドの一例と該一例であるCIP成形用モールドの厚さの測定位置(任意の10点)を示す断面図である。It is sectional drawing which shows an example of the mold for CIP shaping | molding which concerns on embodiment of this invention, and the measurement position (arbitrary ten points | pieces) of the thickness of the mold for CIP shaping | molding which is this example. 本発明の実施の形態に係るCIP成形用モールドの大径部と小径部の傾斜角度θを説明する説明図であり、図2(a)は小径部が平面状の斜面を有し、図2(b)は小径部が曲面状の斜面を有する場合の例である。FIG. 2 (a) is an explanatory view for explaining an inclination angle θ of the large diameter portion and the small diameter portion of the CIP molding mold according to the embodiment of the present invention, and FIG. (B) is an example in case a small diameter part has a slope of a curved surface shape.

 以下、図面を参照しながら本発明の実施の形態について説明する。以下に示す実施の形態はこの発明の技術的思想を具体化するための装置や方法を例示するものであって、この発明の技術的思想は、構成部品の構造、配置等を下記のものに特定するものではない。 Hereinafter, embodiments of the present invention will be described with reference to the drawings. The embodiment shown below is an example of an apparatus and method for embodying the technical idea of the present invention, and the technical idea of the present invention includes the structure, arrangement, and the like of components as described below. It does not identify.

 本発明の実施の形態に係るチタン又はチタン合金圧粉体の製造方法は、冷間等方圧プレス(CIP)を用いて相対密度80%以上のチタン又はチタン合金圧粉体を得るチタン又はチタン合金圧粉体の製造方法であり、例えば図1に例示されるような、粉末供給口2と粉末充填用の空洞3とを有するCIP成形用モールド1を利用することができる。 The method for producing a titanium or titanium alloy green compact according to an embodiment of the present invention is a method for producing titanium or titanium alloy green compact having a relative density of 80% or more using a cold isostatic press (CIP) A CIP molding mold 1 having a powder supply port 2 and a powder filling cavity 3 as illustrated in, for example, FIG. 1, which is a method for producing an alloy powder compact, can be used.

 外形寸法の精度が高く、複雑形状を有するチタン又はチタン合金圧粉体を製造するためには、CIP処理の製造工程との関係において、CIP成形用モールド1の材料、圧縮弾性率、及びショアD硬さを適正な範囲に調整するとともに、CIP成形用モールド1の厚さと厚さの精度を高くすることが必要である。 In order to manufacture a titanium or titanium alloy green compact having a high accuracy in external dimensions and a complicated shape, the material of the CIP molding mold 1, the compression modulus, and the Shore D in relation to the manufacturing process of the CIP treatment It is necessary to adjust the hardness to an appropriate range and to increase the accuracy of the thickness and thickness of the CIP molding mold 1.

 具体的には、本実施形態に係るCIP成形用モールド1としては、厚さが0.5~1.5mmであることを要する。厚さが0.5mm未満の場合、充填粉末の重量でCIP成形用モールド1が変形し、寸法精度が低下する場合がある。一方、厚さを1.5mmより大きくすると、CIP除荷時のCIP成形用モールド1のスプリングバック力が圧粉体強度よりも大きくなり、圧粉体の破断が発生する場合がある。 Specifically, the CIP molding mold 1 according to the present embodiment needs to have a thickness of 0.5 to 1.5 mm. If the thickness is less than 0.5 mm, the CIP molding mold 1 may be deformed by the weight of the filling powder, and the dimensional accuracy may be reduced. On the other hand, if the thickness is greater than 1.5 mm, the springback force of the CIP molding mold 1 at CIP unloading may be greater than the green compact strength, and breakage of the green compact may occur.

 厚さの寸法精度については、モールドの長手方向の任意の10点の厚みを測定した場合の(最大値-最小値)/(最大値+最小値)で表されるモールド厚さ誤差範囲指数αが0~0.05であることが好ましい。厚さの寸法精度の評価に際し、厚さの測定点が局所に偏ると、CIP成形用モールド1の全体としての厚さのバラツキを適切に評価できない場合がある。よって、本実施形態においては、「任意の10点の厚み」の測定点として、CIP成形用モールド1の最長面を10等分した場所を意味する。例えば、図1に示すように、CIP成形用モールド1の最大長に沿った長手方向が水平面と垂直な方向に向くようにCIP成形用モールド1を水平面上に静置させ、水平面に垂直な方向にCIP成形用モールド1を10等分したそれぞれの位置(1~10)における厚みを測定することができる。 As for the dimensional accuracy of thickness, the mold thickness error range index α represented by (maximum value-minimum value) / (maximum value + minimum value) when the thickness of any 10 points in the longitudinal direction of the mold is measured Is preferably from 0 to 0.05. When evaluating the dimensional accuracy of the thickness, if the measurement points of the thickness are locally biased, the variation in the thickness of the CIP molding mold 1 as a whole may not be properly evaluated. Therefore, in this embodiment, it means a place obtained by equally dividing the longest surface of the CIP molding mold 1 into ten as measurement points of “arbitrary 10 points of thickness”. For example, as shown in FIG. 1, the CIP molding mold 1 is allowed to stand on a horizontal surface so that the longitudinal direction along the maximum length of the CIP molding mold 1 is perpendicular to the horizontal surface, and a direction perpendicular to the horizontal surface The thickness at each position (1 to 10) obtained by equally dividing the CIP molding mold 1 into 10 can be measured.

 即ち、「モールド厚さ誤差範囲指数α」は、図1に示すように、CIP成形用モールド1の長手方向に沿ってCIP成形用モールド1を10等分した場合のそれぞれの高さの任意の位置の測定点の厚さをそれぞれ測定し、その最大値と最小値を用いて評価した誤差範囲指数を指す。厚さの測定は、例えば、各測定点に対してデジタルノギス等を用いることにより行うことができる。 That is, as shown in FIG. 1, “mold thickness error range index α” is an arbitrary height of each height when CIP mold 1 is equally divided into 10 along the longitudinal direction of CIP mold 1. The thickness of the measurement point at the position is measured, and the maximum value and the minimum value are used to indicate the error range index evaluated. The thickness can be measured, for example, by using a digital caliper or the like for each measurement point.

 モールド厚さ誤差範囲指数αが0.05よりも大きくなると、CIP成形用モールド1を用いて製造されるチタン又はチタン合金圧粉体の外形寸法の精度が悪くなる上に、スプリングバック力の制御が困難になり、破断発生の原因となる。モールド厚さ誤差範囲指数αは、0.03以下とすることが好ましく、より好ましくは0.01以下、更には0.005以下とすることが好ましい。 When the mold thickness error range index α becomes larger than 0.05, the accuracy of the external dimensions of the titanium or titanium alloy powder compact manufactured using the CIP molding mold 1 is deteriorated and the control of the springback force is also performed. Becomes difficult and cause breakage. The mold thickness error range index α is preferably 0.03 or less, more preferably 0.01 or less, and still more preferably 0.005 or less.

 CIP成形用モールド1の狙い厚さ、即ち製造時のCIP成形用モールド1の厚さデータが既知の場合は、モールド厚さ誤差範囲指数βによって、CIP成形用モールド1の寸法精度を評価することもできる。モールド厚さ誤差範囲指数βは、モールド厚さ誤差範囲指数αの測定と同様に、CIP成形用モールド1の長手方向に沿って10等分した場合のそれぞれの高さの任意の位置の測定点の厚さをそれぞれ測定した場合の「(最大値-最小値)/狙い厚さ」を指す。狙い厚さとしては、例えば、CIP成形用モールド1の成形時の三次元CAD元データの厚さを用いることができる。 If the target thickness of the CIP molding mold 1, that is, the thickness data of the CIP molding mold 1 at the time of manufacture is known, evaluate the dimensional accuracy of the CIP molding mold 1 by the mold thickness error range index β. You can also. Similar to the measurement of the mold thickness error range index α, the mold thickness error range index β is a measurement point at any position of each height when divided equally into ten along the longitudinal direction of the CIP molding mold 1 It refers to “(maximum value−minimum value) / target thickness” when the thickness of each is measured. As the target thickness, for example, the thickness of three-dimensional CAD original data at the time of molding of the CIP molding mold 1 can be used.

 モールド厚さ誤差範囲指数βが0.5よりも大きくなると、CIP成形用モールド1を用いて製造されるチタン又はチタン合金圧粉体の外形寸法の精度が悪くなる上に、スプリングバック力の制御が困難になり、破断発生の原因となる。モールド厚さ誤差範囲指数βが0.5以下の誤差はCIP成形用モールド1の物性に影響しない。モールド厚さ誤差範囲指数βは0.3以下が好ましく、より好ましくは0.1以下、更に好ましくは0.06以下である。 When the mold thickness error range index β becomes larger than 0.5, the accuracy of the external dimensions of the titanium or titanium alloy powder compact manufactured using the CIP molding mold 1 is deteriorated and the control of the spring back force is also performed. Becomes difficult and cause breakage. The error of the mold thickness error range index β of 0.5 or less does not affect the physical properties of the CIP molding mold 1. The mold thickness error range index β is preferably 0.3 or less, more preferably 0.1 or less, and still more preferably 0.06 or less.

 或いは、CIP成形用モールド1の長手方向に沿ってCIP成形用モールド1を10等分した場合のそれぞれの高さの任意の10点の(厚さ/狙い厚さ×100-100)の絶対値の平均値をモールド厚さ誤差範囲指数γとして評価することもできる。モールド厚さ誤差範囲指数γは1.5未満が好ましく、より好ましくは1.0以下、更に好ましくは0.5以下である。 Alternatively, the absolute value of any 10 points (thickness / target thickness × 100-100) of each height when CIP mold 1 is equally divided into 10 along the longitudinal direction of CIP mold 1 The average value of can also be evaluated as a mold thickness error range index γ. The mold thickness error range index γ is preferably less than 1.5, more preferably 1.0 or less, and still more preferably 0.5 or less.

 CIP成形用モールド1に使用する材料としては、熱可塑製樹脂が好ましく、例えば、アクリル樹脂、ポリ乳酸(PLA)樹脂等が好適に利用できる。熱可塑製樹脂材料の圧縮弾性率は、800MPa~2100MPaとすることが好ましい。圧縮弾性率を800MPa未満とすると、CIP除荷時のCIP成形用モールド1のスプリングバックが大きくなり、圧粉体破断に繋がる場合がある。また、圧縮弾性率が低すぎるとCIP成形用モールド1の剛性が足りず、充填粉末の自重でCIP成形用モールド1が変形し、CIP成形品の寸法精度が著しく低下する場合がある。 As a material used for the mold 1 for CIP molding, a thermoplastic resin is preferable, and for example, acrylic resin, polylactic acid (PLA) resin, etc. can be suitably used. The compressive elastic modulus of the thermoplastic resin material is preferably 800 MPa to 2100 MPa. If the compressive elastic modulus is less than 800 MPa, the spring back of the CIP molding mold 1 during CIP unloading may be large, which may lead to green powder fracture. If the compressive elastic modulus is too low, the rigidity of the CIP molding mold 1 may not be sufficient, and the CIP molding mold 1 may be deformed by the own weight of the filling powder, and the dimensional accuracy of the CIP molded product may be significantly reduced.

 一方、圧縮弾性率を2100MPaよりも大きくすると、CIP成形用モールド1の剛性が高くなり、CIP処理加圧時に内部粉末に荷重が十分伝わらず、相対密度80%以上のチタン又はチタン合金圧粉体を得ることができない。CIP成形用モールド1に使用する熱可塑製樹脂の圧縮弾性率はより好ましくは1000MPa~1900MPa、更に好ましくは1500MPa~1900MPaである。圧縮弾性率は、JIS K7181(2011)に準拠する試験方法によって測定することができる。 On the other hand, when the compressive elastic modulus is larger than 2100 MPa, the rigidity of the CIP molding mold 1 becomes high, and the load is not sufficiently transmitted to the internal powder at the time of CIP processing pressurization, and titanium or titanium alloy green compact having a relative density of 80% or more Can not get. The compressive elastic modulus of the thermoplastic resin used for the CIP molding mold 1 is more preferably 1000 MPa to 1900 MPa, still more preferably 1500 MPa to 1900 MPa. The compressive elastic modulus can be measured by a test method in accordance with JIS K7181 (2011).

 CIP成形用モールド1に使用する熱可塑製樹脂のショアD硬さは78~85、より好ましくは80~83とすることが好ましい。ショアD硬さが78未満の場合は充填粉末の重量でCIP成形用モールド1が変形し、寸法精度が低下する。ショアD硬さを85より大きくすると、CIP成形用モールド1の剛性が高くなり、CIP処理加圧時に内部粉末に荷重が十分伝わらず、相対密度80%以上のチタン又はチタン合金圧粉体を得ることができない。ショアD硬さは、JIS K7215(1986)に準拠する試験方法によって測定することができる。 The Shore D hardness of the thermoplastic resin used for the CIP molding mold 1 is preferably 78 to 85, and more preferably 80 to 83. When the Shore D hardness is less than 78, the CIP molding mold 1 is deformed by the weight of the filling powder, and the dimensional accuracy is reduced. When the Shore D hardness is greater than 85, the rigidity of the CIP molding mold 1 becomes high, and the load is not sufficiently transmitted to the internal powder at the time of CIP processing pressurization, and a titanium or titanium alloy green compact having a relative density of 80% or more is obtained I can not do it. Shore D hardness can be measured by a test method in accordance with JIS K 7215 (1986).

 図1に示すように、CIP成形用モールド1は、大径部11と、大径部11に連続し、大径部11よりも水平断面の断面積が小さい小径部12と、小径部12よりも水平断面の断面積が大きく、小径部12に連続する大径部13と、大径部13に連続し、頂部に粉末供給口2を有する頂部14とを含む。 As shown in FIG. 1, the CIP molding mold 1 is continuous with the large diameter portion 11 and the large diameter portion 11 and has a small diameter portion 12 having a smaller horizontal cross-sectional area than the large diameter portion 11 and a smaller diameter portion 12 The cross section of the horizontal cross section is also large, and it includes a large diameter portion 13 continuous with the small diameter portion 12 and a top portion 14 continuous with the large diameter portion 13 and having a powder supply port 2 at the top.

 小径部12は、底部から頂部に向かって水平方向の断面積が徐々に小さくなり、小径部12の中間部分から大径部13に向けて水平方向の断面積が徐々に大きくなるようなくびれを有する形状とすることができる。 In the small diameter portion 12, the cross-sectional area in the horizontal direction gradually decreases from the bottom to the top, and the cross-sectional area in the horizontal direction gradually increases from the middle portion of the small diameter portion 12 toward the large diameter portion 13. It can have a shape.

 大径部11、13は、水平断面が多角形状を有していてもよいし、水平断面が円又は楕円状であってもよく、利用用途に応じて適宜変更することができ、具体的形状は特に限定されない。水平断面における大径部11、13の最大径D11に対する小径部12の最小径D12の比率D(小径部最小径D12/大径部最大径D11)が、0.5以上0.8未満である。大径部11、13と小径部12の形状は、水平断面同士が略相似形であることが好ましいが、互いに異なる形状を有していてもよい。 In the large diameter parts 11 and 13, the horizontal cross section may have a polygonal shape, or the horizontal cross section may be circular or elliptical, and can be appropriately changed according to the use application, and the specific shape Is not particularly limited. The ratio D of the minimum diameter D 12 of the small-diameter portion 12 to the maximum diameter D 11 of the large diameter portion 11, 13 in the horizontal section (small-diameter portion minimum diameter D 12 / large diameter portion maximum diameter D 11), 0.5 or 0. It is less than eight. The shapes of the large diameter portions 11 and 13 and the small diameter portion 12 preferably have substantially similar shapes in horizontal cross sections, but may have shapes different from each other.

 図2(a)の拡大図に示すように、CIP成形用モールド1は、大径部11の外側面111に対して小径部12の外側面121が傾斜している。大径部11の外側面111の端部112から大径部11の外側面111の延在方向に延びる直線Xと小径部12の外側面121とのなす角θ(図2(a)の例では直線Xから半時計回りに測定した場合の小径部12の外側面121とのなす角θ)が10度以上60度未満である。なお、小径部12の外側面121が曲面を有する場合は、図2(b)に示すように、小径部12の水平断面において最小径D12となる位置と大径部11の端部112とを通る直線Yと直線Xとのなす角θ(即ち、直線Xを基点として直線Xから反時計回りに測定した場合の直線Yとのなす角)が、10度以上60度未満である。 As shown in the enlarged view of FIG. 2A, in the CIP molding mold 1, the outer side surface 121 of the small diameter portion 12 is inclined with respect to the outer side surface 111 of the large diameter portion 11. An example of an angle θ (FIG. 2A) between a straight line X extending from the end 112 of the outer surface 111 of the large diameter portion 11 to the outer surface 111 of the large diameter portion 11 and the outer surface 121 of the small diameter portion 12 Then, the angle θ) between the straight line X and the outer surface 121 of the small diameter portion 12 when measured counterclockwise from the straight line X is 10 degrees or more and less than 60 degrees. When the outer surface 121 of the small diameter portion 12 has a curved surface, as shown in FIG. 2B, the position where the minimum diameter D 12 is in the horizontal cross section of the small diameter portion 12 and the end 112 of the large diameter portion 11 The angle θ between the straight line Y passing through the straight line X and the straight line X (that is, the angle between the straight line X and the straight line Y when measured counterclockwise from the straight line X based on the straight line X) is 10 degrees or more and less than 60 degrees.

 図1及び図2(a)、図2(b)に示すような複雑形状を有するCIP成形用モールド1は、3Dプリンタ装置を用いて作製することができる。これにより、従来のようにブロー成形してモールドを形成する場合に比べて、厚さを均一にすることができ、寸法精度を向上させることができる。また、モールドの製造に際し、金型等を作製する必要がないため、より経済的に複雑形状を有するCIP成形用モールド1を、寸法精度が高くなるように製造することができる。 The CIP molding mold 1 having a complicated shape as shown in FIGS. 1 and 2 (a) and 2 (b) can be manufactured using a 3D printer. Thereby, the thickness can be made uniform, and the dimensional accuracy can be improved, as compared with the case where the mold is formed by blow molding as in the prior art. Moreover, since it is not necessary to manufacture a mold etc. in the case of manufacture of a mold, the mold 1 for CIP molding which has a complicated shape more economically can be manufactured so that a dimensional accuracy may become high.

 3Dプリンタ装置としては汎用の装置を用いることができるが、材料押出法を利用した3Dプリンタ装置、或いは材料噴射法を利用した3Dプリンタ装置を用いて作製することが好ましい。 Although a general-purpose device can be used as the 3D printer device, it is preferable to use a 3D printer device using a material extrusion method or a 3D printer device using a material injection method.

 本実施形態に係るCIP成形用モールド1内の空洞3に、純チタン粉末又は純チタン粉末と合金元素粉末又は母合金粉末とを充填し、CIP処理を実施することにより、本実施形態に係るチタン又はチタン合金圧粉体が得られる。ここで、合金元素粉末とは例えばAl粉末やV粉末等単一元素の粉末であって、母合金粉末とは複数の元素を含む粉末である。 The titanium according to the present embodiment is implemented by filling pure titanium powder or pure titanium powder and alloy element powder or mother alloy powder in the cavity 3 in the CIP molding mold 1 according to the present embodiment and performing CIP processing. Or a titanium alloy green compact is obtained. Here, the alloying element powder is a powder of a single element such as Al powder or V powder, and the mother alloy powder is a powder containing a plurality of elements.

 充填材としては、例えば平均粒径30μm以上100μm未満の純チタン粉末を80~100質量%、CIP成形用モールドの空洞内に充填することにより、相対密度80%以上のチタン又はチタン合金圧粉体が得られる。或いは、平均粒径30μm以上100μm未満の純チタン粉末と、平均粒径5μm以上50μm未満の合金元素粉末又は母合金粉末とを1~20質量%、CIP成形用モールド1の空洞内3に充填し、CIP処理を実施することにより、相対密度80%以上のチタン又はチタン合金圧粉体が得られる。なお、平均粒径は、レーザー回折散乱法によって得られた粒度分布(体積基準)の粒子径D50(メジアン径)の値を指す。粉体の充填、CIP処理は一般的に良く知られる条件を用いて実施することができる。本実施形態において「純チタン」とはJIS2種に規定の組成を満たす工業用純チタンを意味する。チタン合金圧粉体に用いられる主な合金系としては、Ti-6Al-4V、Ti-6Al-6V-2Sn、Ti-6Al-2Sn-4Zr-2Mo、Ti-6Al-2Sn-4Zr-6Mo、Ti-10V-2Fe-3Al等が挙げられる。 As a filler, for example, 80 to 100% by mass of pure titanium powder having an average particle diameter of 30 μm or more and less than 100 μm, and filled in a cavity of a CIP molding mold, titanium or titanium alloy green compact having a relative density of 80% or more Is obtained. Alternatively, 1 to 20 mass% of pure titanium powder having an average particle diameter of 30 μm or more and less than 100 μm and alloy element powder or mother alloy powder having an average particle diameter of 5 to 50 μm is filled in the cavity 3 of the CIP molding mold 1 By performing the CIP process, a titanium or titanium alloy green compact having a relative density of 80% or more can be obtained. In addition, an average particle diameter points out the value of particle diameter D50 (median diameter) of the particle size distribution (volume basis) obtained by the laser diffraction scattering method. Powder filling and CIP treatment can be carried out using generally well known conditions. In the present embodiment, "pure titanium" means industrial pure titanium that satisfies the composition defined in JIS II. The main alloy systems used for titanium alloy compacts include Ti-6Al-4V, Ti-6Al-6V-2Sn, Ti-6Al-2Sn-4Zr-2Mo, Ti-6Al-2Sn-4Zr-6Mo, Ti. And -10V-2Fe-3Al.

 本発明の実施の形態に係るチタン又はチタン合金圧粉体によれば、3Dプリンタを用いて、所定の熱可塑製樹脂を利用して、厚さ及び厚さ精度が制御されたCIP成形用モールド1を得て、これを利用してCIP処理を実施することにより、外形寸法の精度が高く、複雑形状を有するチタン又はチタン合金圧粉体をより経済的に製造することができる。 According to the titanium or titanium alloy compact according to the embodiment of the present invention, a CIP molding mold whose thickness and thickness accuracy are controlled using a predetermined thermoplastic resin using a 3D printer By obtaining C.1 and performing CIP processing using this, it is possible to manufacture a titanium or titanium alloy green compact having high accuracy of external dimensions and a complicated shape more economically.

 以下に本発明の実施例および比較例について説明するが、本発明は以下の実施例に制限されないことは勿論である。 Examples of the present invention and comparative examples are described below, but the present invention is of course not limited to the following examples.

 厚さを0.5~1.75mmの間で調整したCIP成形用モールドの3Dデータに基づいて、樹脂を3種類(PLA樹脂、アクリル樹脂、シリコン樹脂)を用いて、3DプリンタによりCIP成形用モールドを作製した。PLA樹脂を用いたCIP成形用モールドについては、久宝金属製作所製の3Dプリンタ装置クホリアを用いて材料押出法により作製した。アクリル樹脂を用いたCIP成形用モールドについては、3DSystems製3Dプリンタ装置ProJet3600MAXを用いて材料噴射法により作製した。シリコン樹脂材料については、キーエンス製3Dプリンタ装置AGILISTA-3200を用いて材料噴射法により作製した。CIP成形用モールドの大径部と小径部の比率Dは0.6、大外径と小外径とのなす角θを27度と設定して、図1に示す形状のCIP成形用モールドを作製した。 Based on 3D data of CIP molding mold whose thickness is adjusted between 0.5 and 1.75 mm, using 3 types of resin (PLA resin, acrylic resin, silicon resin), for CIP molding by 3D printer A mold was made. The CIP molding mold using PLA resin was manufactured by a material extrusion method using a 3D printer apparatus Kuria, manufactured by Kubo Metals Co., Ltd. The CIP molding mold using an acrylic resin was manufactured by a material injection method using a 3D printing apparatus ProJet 3600MAX manufactured by 3D Systems. The silicone resin material was manufactured by a material injection method using a Keyence 3D printer AGILISTA-3200. The ratio D of the large diameter portion to the small diameter portion of the CIP molding mold is 0.6, the angle θ between the large outer diameter and the small outer diameter is set to 27 degrees, and the CIP molding mold having the shape shown in FIG. Made.

 作製されたCIP成形用モールド内の空洞に、トーホーテック製純チタン粉末TC-150(粒度幅45-150μm、平均粒径90μm)を充填し、CIP処理を行った。CIP処理は、日機装製冷間静水圧成形装置CL4-22-60を用いた。 A hollow in the produced CIP molding mold was filled with Tohotec pure titanium powder TC-150 (particle size width 45-150 μm, average particle size 90 μm) and subjected to CIP treatment. For the CIP process, a cold isostatic pressing apparatus CL4-22-60 manufactured by Nikkiso Co., Ltd. was used.

 作製されたCIP成形用モールド内の空洞に純チタン粉末を充填し、タッピングし、ビニールテープで封じたものを真空パックし、真空パックした純チタン粉末充填品を、冷間静水圧成形装置にセットし、加圧した。約300MPaに到達したところで1分保持後、除圧し、チタン粉末充填品を冷間静水圧成形装置から取り出した。得られた成形体を大気圧、130℃で15分間加熱し、軟化したCIP成形用モールドをカッター、ニッパー等を使用して除去して、圧粉体を得た。 A hollow in the produced CIP molding mold is filled with pure titanium powder, tapped, vacuum-packed one sealed with a vinyl tape, and the vacuum-packed pure titanium powder-filled product is set in a cold isostatic molding machine And pressurized. After reaching about 300 MPa, after holding for 1 minute, pressure was released, and the titanium powder-filled product was removed from the cold isostatic pressing apparatus. The obtained molded product was heated at 130 ° C. for 15 minutes at atmospheric pressure, and the softened mold for CIP molding was removed using a cutter, nipper or the like to obtain a green compact.

 各材料及び各装置を用いて作製したCIP成形用モールドに対し、モールド厚さ誤差範囲指数α、β、γ、圧縮弾性率、ショアD硬さと、圧粉体密度(相対密度)を測定した。狙い厚さは3Dデータ作成時の厚さを用いた。CIP成形用モールド1を長手方向に10等分し(本実施例では12mm間隔)、10点の厚さをチックネスゲージで測定した。圧縮弾性率はJIS K7181(2011)に準拠して実施した測定結果より算出した。ショアD硬さはJIS K7215(1986)に準拠して測定した。圧粉体密度は、アルキメデス法で求めた密度/理論密度4.51/cm3×100から算出した。更に、得られた圧粉体の破断の有無を観察した。結果を表1に示す。 Mold thickness error range indexes α, β, γ, compressive modulus, Shore D hardness, and green density (relative density) were measured for CIP molding molds produced using each material and each device. Target thickness used thickness at the time of 3D data creation. The CIP molding mold 1 was divided into 10 equal parts in the longitudinal direction (in this example, 12 mm intervals), and the thickness of 10 points was measured with a tic-ness gauge. The compressive elastic modulus was calculated from the measurement result implemented based on JISK7181 (2011). Shore D hardness was measured in accordance with JIS K 7215 (1986). The green density was calculated from the density / theoretical density 4.51 / cm 3 × 100 obtained by the Archimedes method. Furthermore, the presence or absence of breakage of the obtained green compact was observed. The results are shown in Table 1.

Figure JPOXMLDOC01-appb-T000001
Figure JPOXMLDOC01-appb-T000001

 厚さ0.5~1.5mmの範囲外である厚さ1.75mmのCIP成形用モールドを作製した比較例1、2では、モールドを作製することはできたが、チタン又はチタン合金の圧粉体に破断が生じ、所望の圧粉体を作製することができなかった。圧縮弾性率及びショアD硬さが本発明の範囲外であるシリコン樹脂を用いた比較例3及び4では、CIP成形用モールドを作製することもできなかった。比較例5では、モールドを作製することはできたが、強度不足により、CIP処理時に粉末充填後の形状を維持することができなかった。一方、実施例1~4では、いずれも相対密度80%以上で破断のない圧粉体を作製することができた。 In Comparative Examples 1 and 2 in which a CIP molding mold having a thickness of 1.75 mm, which was outside the range of 0.5 to 1.5 mm in thickness, was produced, although the mold could be produced, the pressure of titanium or titanium alloy was used. The powder was broken and the desired green compact could not be produced. In Comparative Examples 3 and 4 using a silicone resin whose compressive elastic modulus and Shore D hardness were out of the range of the present invention, it was not possible to produce a CIP mold. In the comparative example 5, although the mold was able to be produced, the shape after powder filling was not able to be maintained at the time of CIP processing by lack of intensity | strength. On the other hand, in Examples 1 to 4, it was possible to produce a green compact having a relative density of 80% or more and no breakage.

1…CIP成形用モールド
2…粉末供給口
3…空洞
11…大径部
12…小径部
13…大径部
14…頂部
111,121…外側面
112…端部
DESCRIPTION OF SYMBOLS 1 ... CIP molding mold 2 ... powder supply port 3 ... cavity 11 ... large diameter part 12 ... small diameter part 13 ... large diameter part 14 top part 111, 121 ... outside surface 112 ... end part

Claims (8)

 冷間等方圧プレスを用いて相対密度80%以上のチタン又はチタン合金圧粉体を得るチタン又はチタン合金圧粉体の製造方法であって、
 厚さが0.5~1.5mm、且つモールドの長手方向の任意の10点の厚みを測定した場合の(最大値-最小値)/(最大値+最小値)で表されるモールド厚さ誤差範囲指数αが0~0.05であり、圧縮弾性率が800MPa~2100MPa、ショアD硬さが78~85の熱可塑製樹脂からなり、粉末供給口と粉末充填用の空洞とを有するCIP成形用モールドを用いることを特徴とするチタン又はチタン合金圧粉体の製造方法。
A method for producing a titanium or titanium alloy green compact, comprising obtaining a titanium or titanium alloy green compact having a relative density of 80% or more using a cold isostatic press,
Mold thickness represented by (maximum value-minimum value) / (maximum value + minimum value) when the thickness is 0.5 to 1.5 mm and the thickness of any 10 points in the longitudinal direction of the mold is measured CIP comprising a thermoplastic resin having an error range index α of 0 to 0.05, a compressive elastic modulus of 800 MPa to 2100 MPa, and a Shore D hardness of 78 to 85, and having a powder supply port and a cavity for powder filling A method for producing a titanium or titanium alloy green compact characterized by using a molding mold.
 前記CIP成形用モールドが、大径部と、前記大径部に連続し、前記大径部よりも水平断面の断面積が小さい小径部とを少なくとも備え、且つ水平断面における前記大径部の最大径に対する前記小径部の最小径の比率D(小径部最小径/大径部最大径)が、0.5以上0.8未満であることを含む請求項1に記載のチタン又はチタン合金圧粉体の製造方法。 The CIP molding mold comprises at least a large diameter portion and a small diameter portion continuous to the large diameter portion and having a smaller cross sectional area in horizontal cross section than the large diameter portion, and the largest diameter portion in the horizontal cross section The titanium or titanium alloy compact according to claim 1, wherein the ratio D of the minimum diameter of the small diameter portion to the diameter (small diameter portion minimum diameter / large diameter portion maximum diameter) is 0.5 or more and less than 0.8. How to make the body.  前記CIP成形用モールドは、前記大径部の外側面に対して前記小径部の外側面が傾斜し、前記大径部の前記外側面の端部から前記大径部の前記外側面の延在方向に延びる直線と前記小径部の外側面とのなす角θが10度以上60度未満である請求項1又は2に記載のチタン又はチタン合金圧粉体の製造方法。 In the CIP molding mold, the outer surface of the small diameter portion is inclined with respect to the outer surface of the large diameter portion, and the outer surface of the large diameter portion extends from the end of the outer surface of the large diameter portion. The method for producing a titanium or titanium alloy green compact according to claim 1 or 2, wherein an angle θ between the straight line extending in the direction and the outer surface of the small diameter portion is 10 degrees or more and less than 60 degrees.  前記CIP成形用モールドを、3Dプリンタ装置を用いて作製することを含む請求項1~3のいずれか1項に記載のチタン又はチタン合金圧粉体の製造方法。 The method for producing a titanium or titanium alloy green compact according to any one of claims 1 to 3, comprising producing the CIP molding mold using a 3D printer device.  前記CIP成形用モールドを、材料押出法を利用した3Dプリンタ装置を用いて作製することを含む請求項1~3のいずれか1項に記載のチタン又はチタン合金圧粉体の製造方法。 The method for producing a titanium or titanium alloy green compact according to any one of claims 1 to 3, comprising producing the CIP molding mold using a 3D printer apparatus utilizing a material extrusion method.  前記CIP成形用モールドを、材料噴射法を利用した3Dプリンタ装置を用いて作製することを含む請求項1~3のいずれか1項に記載のチタン又はチタン合金圧粉体の製造方法。 The method for producing a titanium or titanium alloy green compact according to any one of claims 1 to 3, comprising producing the CIP molding mold using a 3D printer apparatus utilizing a material injection method.  平均粒径30μm以上100μm未満の純チタン粉末を80~100質量%、前記CIP成形用モールドの前記空洞内に充填することを含む請求項1~6のいずれか1項に記載のチタン又はチタン合金圧粉体の製造方法。 The titanium or titanium alloy according to any one of claims 1 to 6, which comprises filling 80 to 100% by mass of pure titanium powder having an average particle diameter of 30 μm or more and less than 100 μm into the cavity of the CIP molding mold. Production method of green compact.  平均粒径30μm以上100μm未満の純チタン粉末と、平均粒径5μm以上50μm未満の合金元素粉末又は母合金粉末とを1~20質量%、前記CIP成形用モールドの前記空洞内に充填することを含む請求項1~6のいずれか1項に記載のチタン又はチタン合金圧粉体の製造方法。 Filling 1 to 20% by mass of pure titanium powder having an average particle diameter of 30 μm or more and less than 100 μm and alloy element powder or mother alloy powder having an average particle diameter of 5 μm or more and less than 50 μm in the cavity of the CIP molding mold The method for producing a titanium or titanium alloy green compact according to any one of claims 1 to 6, which comprises.
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JP7177302B1 (en) * 2021-03-12 2022-11-22 東邦チタニウム株式会社 Method for producing titanium-based green compact and method for producing titanium-based sintered compact

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