WO2015053137A1 - Superhard alloy composite roll and production method therefor - Google Patents

Superhard alloy composite roll and production method therefor Download PDF

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Publication number
WO2015053137A1
WO2015053137A1 PCT/JP2014/076214 JP2014076214W WO2015053137A1 WO 2015053137 A1 WO2015053137 A1 WO 2015053137A1 JP 2014076214 W JP2014076214 W JP 2014076214W WO 2015053137 A1 WO2015053137 A1 WO 2015053137A1
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Prior art keywords
cemented carbide
outer layer
composite roll
inner layer
layer
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PCT/JP2014/076214
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French (fr)
Japanese (ja)
Inventor
大島 昌彦
拓己 大畑
俊二 松本
裕允 小湊
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日立金属株式会社
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Priority to JP2015541534A priority Critical patent/JP6421758B2/en
Publication of WO2015053137A1 publication Critical patent/WO2015053137A1/en

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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B27/00Rolls, roll alloys or roll fabrication; Lubricating, cooling or heating rolls while in use
    • B21B27/02Shape or construction of rolls
    • B21B27/03Sleeved rolls
    • B21B27/032Rolls for sheets or strips
    • 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
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C29/00Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/02Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
    • C22C29/06Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
    • C22C29/08Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds based on tungsten carbide
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/22Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten

Definitions

  • the present invention comprises an outer layer excellent in wear resistance, rough skin resistance, etc. and an inner layer excellent in toughness, and is a highly durable cemented carbide composite roll suitable for rolling steel materials such as plate materials, wire materials, bar materials, And a manufacturing method thereof.
  • tungsten carbide (WC) cemented carbide with excellent wear resistance, rough skin resistance, etc., to meet the demands for higher quality of rolled materials, such as improved dimensional accuracy, and improved productivity by reducing the number of roll change man-hours.
  • Rolls for rolling are used, and cemented carbide rolling rolls having various structures have been proposed.
  • Japanese Patent Laid-Open No. 3-281007 discloses a roll body 105 having a fastening flange portion 103 fixed at both ends and a detachable fastening flange portion 104, and a thermal expansion coefficient of 15 ⁇ .
  • a cemented carbide rolling roll having a body 110 is proposed.
  • the tightening force of the tightening flange portions 103 and 104 is improved by utilizing the thermal expansion of the ring spacers 111 and 111.
  • the adhesion between the cemented carbide cylinder 110 and the roll body 105 is not sufficient with the tightening force by the tightening flange portions 103 and 104.
  • the cemented carbide cylindrical body 110 may slip with respect to the roll body 105 during rolling.
  • JP 2001-47111 A discloses a cemented carbide composite roll in which an outer layer member made of a WC-based cemented carbide is metal-bonded to the outer periphery of an inner layer member made of a material having excellent toughness.
  • a cemented carbide composite roll is proposed in which a WC-based cemented carbide intermediate layer having a lower content than the outer layer is provided, and the inner layer member and the intermediate layer are joined via a metal layer.
  • the WC has a gradient concentration from the outer layer member to the inner layer member and the physical properties such as the coefficient of thermal expansion and the elastic coefficient are continuously applied from the outer layer member to the inner layer member. It is described that the strength of the boundary joint is improved.
  • JP 2004-167501 is a cemented carbide composite roll in which a cemented carbide outer layer member is joined to the outer periphery of a steel or iron alloy inner layer member, and has a Young's modulus between the inner layer member and the outer layer member.
  • a composite roll for rolling made of cemented carbide characterized by providing an intermediate layer of 190 GPa or less is proposed.
  • Japanese Patent Laid-Open No. 2004-167501 absorbs strain between the outer layer and the inner layer by setting the Young's modulus of the intermediate layer to 190 GPa or less, and even if the thermal expansion coefficient difference between the outer layer and the inner layer is large, it is excessive in the roll.
  • Japanese Patent Application Laid-Open No. 2004-167501 exemplifies Invar alloy and SUS304 as the material of the intermediate layer.
  • JP 2003-275809 has proposed a composite roll for rolling in which a WC cemented carbide outer layer is directly metal-bonded to the outer periphery of an iron alloy inner layer containing 0.5 mass% or more of C.
  • Japanese Unexamined Patent Publication No. 2003-275809 describes that the obtained cemented carbide composite roll does not have a fragile ⁇ phase at the boundary joining portion and has high joining reliability.
  • cemented carbide composite rolls described in JP-A-2001-47111, JP-A-2004-167501, and JP-A-2003-275809 in which a cemented carbide outer layer having excellent wear resistance and an iron-based alloy inner layer are joined. It has been found that there is a possibility that the bonding reliability between the outer layer and the inner layer may not be sufficient to increase the size of the roll as in a hot sheet rolling roll having an outer diameter of 300 mm or more and a roll length of 500 mm or more. Further, when used in more severe rolling conditions, higher bonding strength between the outer layer and the inner layer is required.
  • an object of the present invention is a cemented carbide composite roll comprising a cemented carbide outer layer excellent in wear resistance, rough skin resistance, and the like and an iron-based alloy inner layer excellent in toughness, both of which have extremely high joint strength. And an efficient manufacturing method thereof.
  • the cemented carbide composite roll of the present invention is a cemented carbide outer layer and an iron-based alloy inner layer that are diffusion-bonded, and the inner layer body in the surface layer region of the inner layer adjacent to the bonding boundary with the outer layer. It has a C-enriched layer made of an iron-based alloy having a higher C concentration.
  • the thickness of the C concentrated layer is preferably 0.5 to 6 mm.
  • the C concentration at the junction boundary of the C concentrated layer is preferably 0.7 to 1.2% by mass. It is preferable that the C concentration in the C-concentrated layer gradually decreases from the joining boundary toward the inner layer main body.
  • the reduction rate of the C concentration in the depth direction in the C enriched layer is preferably 0.01% / mm or more.
  • the tensile strength at the boundary between the outer layer and the inner layer is preferably 600 MPa or more.
  • the cemented carbide outer layer preferably contains 70 to 88% by mass of WC particles.
  • the C concentration of the iron-based alloy inner layer body is preferably 0.2 to 0.5% by mass.
  • the iron-based alloy inner layer preferably contains 1.0% by mass or more in total of at least one selected from the group consisting of Cr, Ni, Mo, V, W, Ti and Nb.
  • the method of the present invention for producing a cemented carbide composite roll in which a cylindrical outer layer member made of a cemented carbide and an inner layer member made of an iron-based alloy are joined is obtained by carburizing the outer surface of the inner layer member.
  • the member and the inner layer member are diffusion bonded.
  • the thickness of the carburized layer formed by the carburizing process is preferably 0.5 to 10 mm.
  • the inner layer member is disposed inside the outer layer member, and a hollow cylindrical restraining member having a smaller coefficient of thermal expansion than the outer layer member is disposed outside the outer layer member in a temperature range from room temperature to a bonding temperature.
  • the outer layer member, the inner layer member, and the outer layer member so that the outer surface of the inner layer member that is most thermally expanded presses the inner surface of the outer layer member, and the inner surface of the restraining member that is not thermally expanded presses the outer surface of the outer layer member. It is preferable that a gap with the restraining member is set, and the inner surface of the outer layer member and the outer surface of the inner layer member are brought into close contact with each other by heating, so that the outer layer member and the inner layer member are diffusion bonded.
  • both end portions in the axial direction of the restraining member protrude from both end surfaces in the axial direction of the outer layer member.
  • the restraining member is thicker than the outer layer member.
  • the restraining member is preferably made of graphite or ceramics.
  • the restraining member is formed by coaxially stacking a plurality of ring members.
  • reaction preventing material is interposed between the restraining member and the outer layer member.
  • the cemented carbide outer layer and the iron-based alloy inner layer are joined via the C-concentrated layer, so the joining strength between the outer layer and the inner layer is high. Therefore, even a large rolling roll having an outer diameter of 300 mm or more and a roll length of 500 mm or more can be used for long-term rolling.
  • a large rolling roll having an outer diameter of 300 mm or more and a roll length of 500 mm or more can be used for long-term rolling.
  • the inner layer member made of an iron-based alloy and the outer layer made of a cemented carbide alloy that have been carburized in advance in the surface layer region are joined by the diffusion joining method or the HIP method, a joining boundary without a fragile ⁇ phase can be formed.
  • a cemented carbide composite roll in which an alloy outer layer and an iron-based alloy inner layer are firmly bonded can be obtained.
  • FIG. 4 (a) is an enlarged view of a portion A in the bag. It is sectional drawing which shows the diffusion bonding method using the constraining member comprised by the some ring member piled up coaxially. It is sectional drawing which shows the example which manufactures the cemented carbide composite roll of this invention by HIP method.
  • FIG. 2 is a cross-sectional view showing a joining experiment of Example 1.
  • FIG. It is a front view which shows a tension test piece.
  • 2 is a graph showing a C concentration distribution from the surface to the inside in the carburized layer of Example 1.
  • FIG. 4 is a graph showing the C concentration distribution from the joining boundary to the inside of the inner layer for joining test pieces 4 and 5 of Example 1.
  • FIG. 3 is a partial cross-sectional view showing a cemented carbide rolling roll disclosed in Japanese Patent Laid-Open No. 3-281007.
  • Cemented carbide composite roll 10 of the present invention that can be used for rolling a rolled material such as steel is composed of a cemented carbide outer layer 1 and a ferrous alloy as shown in FIG.
  • the inner layer 2 is made of an alloy, and a C concentrated layer 3 is provided at the boundary between the outer layer 1 and the inner layer 2.
  • the C-enriched layer is an iron-based alloy having a C concentration of 0.6% by mass or more and has a higher C concentration than the inner layer 2.
  • the outer layer 1 whose surface is in contact with the material to be rolled is required to have excellent wear resistance, rough skin resistance and mechanical strength, and the inner layer 2 constituting the roll shaft whose both ends are supported by bearings (not shown) is a high machine. Strength and toughness are required.
  • the cemented carbide outer layer 1 of the cemented carbide composite roll of the present invention is a sintered alloy in which hard WC particles are bonded with a metal such as Co, Ni, Cr, Fe, etc. Carbides such as Ta and Nb may be contained. Since the outer layer 1 has high wear resistance and mechanical strength, the average particle size of the WC particles is preferably 3 to 10 ⁇ m, the content of the WC particles is preferably 70 to 88% by mass, and more preferably 72 to 85% by mass. preferable. The thickness of the outer layer 1 is preferably set in the range of 5 to 50 mm in consideration of gradual wear due to rolling.
  • the iron-based alloy of the inner layer 2 is preferably steel.
  • inner layer 2 In order for inner layer 2 to have sufficient toughness, 0.2 to 0.5 mass% of C and 1.0 mass% or more in total of at least one selected from the group consisting of Cr, Ni, Mo, V, W, Ti and Nb Steel is preferred.
  • C is less than 0.2% by mass, the inner layer 2 does not have sufficient strength.
  • C exceeds 0.5% by mass, the toughness of the inner layer 2 is insufficient.
  • the content of other elements may be within the general composition range of steel materials.
  • the inner layer 2 Since the inner layer 2 has a larger thermal expansion coefficient than the outer layer 1 made of a cemented carbide having a small thermal expansion coefficient, it needs a transformation expansion characteristic to relieve strain generated by the thermal expansion. If this transformation is a pearlite transformation, due to plastic deformation at a high temperature, a large strain is generated due to a difference in thermal expansion coefficient in the process of cooling to room temperature, which causes roll breakage. For this reason, this transformation must be a bainite transformation or a martensitic transformation that occurs at low temperatures. For this reason, it is preferable that the inner layer contains 1.0% by mass or more in total of at least one selected from the group consisting of Cr, Ni, Mo, V, W, Ti, and Nb. In particular, the Cr content is preferably 0.5 to 1.5 mass%, the Mo content is preferably 0.1 to 0.5 mass%, and the Ni content is preferably 1.5 to 2.5 mass%.
  • a C concentrated layer 3 having a C concentration of 0.6% by mass or more was formed near the surface of the inner layer 1 to be joined with the outer layer 1 made of cemented carbide. It has been found that if formed, the diffusion of C from the cemented carbide outer layer 1 to the inner layer 2 can be substantially suppressed, thereby preventing the generation of ⁇ phase. Furthermore, since the C enriched layer 3 may be formed very close to the inner layer 2, the toughness of the iron-based alloy inner layer 2 is not impaired.
  • the outer diameter of the outer layer 1 is 300 mm or more and the roll length is 500 mm or more. It is possible to obtain a cemented carbide composite roll 10 having an excellent bonding strength.
  • FIG. 2 shows the C concentration distribution in the region including the C concentrated layer of the cemented carbide composite roll 10 of the present invention.
  • the horizontal axis represents the distance from the boundary with the outer layer 1 (the origin is the junction boundary with the outer layer 1), and the vertical axis represents the C concentration.
  • a layer having a C concentration of 0.6% by mass or more from the boundary with the outer layer 1 toward the inner layer 2 is referred to as a C concentrated layer 3.
  • the thickness of the C concentrated layer 3 is preferably 0.5 to 10 mm.
  • the thickness of the C concentrated layer 3 is less than 0.5 mm, C diffuses to the inner layer 2 side when bonded to the outer layer 1 and the C concentration of the C concentrated layer 3 becomes too low, and the cemented carbide of the outer layer 1 Since the ⁇ phase may occur in the inside, it is not preferable.
  • the thickness of the C enriched layer 3 exceeds 10 mm, the time for carburizing treatment for forming the C enriched layer 3 becomes longer, which is not preferable because the manufacturing cost increases.
  • the C concentration in the adjacent region of the outer layer is 0.7 to 1.2. It is preferable that it is mass%. If the C concentration in the adjacent region of the outer layer is 0.7% by mass or more, there is almost no diffusion of C from the outer layer 1 made of cemented carbide to the inner layer 2, and the generation of ⁇ phase in the outer layer 1 made of cemented carbide can be reliably prevented. , The strength reduction can be prevented. On the other hand, if the C concentration in the adjacent region of the outer layer exceeds 1.2% by mass, graphite is generated at the joining boundary, and the strength is lowered, which is not preferable.
  • the C concentration gradually decreases from the boundary with the outer layer 1 toward the inner layer 2.
  • the physical properties such as Young's modulus, thermal expansion coefficient, and hardness continuously change from the joining boundary toward the inner layer 2, the joining reliability increases.
  • the tensile strength at the boundary between the outer layer 1 and the inner layer 2 is preferably 600 MPa or more, more preferably 700 MPa or more so that the outer layer 1 and the inner layer 2 do not peel even when used for a long time in rolling.
  • the tensile strength at the boundary between the outer layer 1 and the inner layer 2 can be measured by a tensile test of a test piece including the boundary between the outer layer 1 and the inner layer 2.
  • FIG. 3 shows a manufacturing process of the cemented carbide composite roll 10 of the present invention.
  • carburizing treatment is performed on the outer peripheral surface of a columnar or cylindrical inner layer member 12 made of an iron-based alloy.
  • a solid carburizing method, a liquid carburizing method, or a gas carburizing method can be used for the carburizing treatment, but a gas carburizing method is preferable in order to form a uniform carburized layer.
  • the carburized layer 13 becomes the C concentrated layer 3 after being joined to the outer layer 1, and the C concentration is preferably 0.7 to 1.2% by mass on the outermost surface (outer layer adjacent region).
  • the C concentration on the surface of the carburized layer 13 is less than 0.7 mass%, the bonding strength with the outer layer 1 is insufficient, and the C concentrated layer 3 may not be formed.
  • the C concentration on the surface of the carburized layer 13 exceeds 1.2% by mass, graphite may be generated at the bonding boundary with the outer layer, resulting in a decrease in bonding strength.
  • the C concentration gradually decreases from the surface toward the inside of the inner layer 2.
  • the thickness of the carburized layer 13 is preferably 0.5 to 10 mm.
  • the thickness of the carburized layer 13 is less than 0.5 mm, not only the bonding strength with the outer layer is insufficient, but also the C concentrated layer 3 may not be formed at the bonding boundary. On the other hand, it takes an excessive amount of time to form the carburized layer 13 having a thickness of more than 10 mm, which increases the manufacturing cost.
  • a preferable thickness of the carburized layer 13 is 2 to 5 mm.
  • the outer layer member 11 made of cemented carbide is joined to the inner layer member 12 on which the carburized layer 13 is formed.
  • the joining method is not limited as long as the inner layer member 12 and the outer layer member 11 are joined without a gap, but a diffusion joining method and a hot isostatic pressure (HIP) method are preferably used.
  • FIG. 4 shows a method for producing the cemented carbide composite roll of the present invention by the diffusion bonding method.
  • an inner layer member (corresponding to a roll shaft) 12 whose surface is carburized is placed on a base 8.
  • the cylindrical outer layer member 11 is placed on the cylindrical cradle 9.
  • the cradle 9 is preferably made of a material that is inactive with respect to the outer layer member 11, similarly to the restraining member described later.
  • the cradle 9 is preferably made of graphite or ceramics.
  • the cylindrical restraining member 16 having a smaller coefficient of thermal expansion than the outer layer member 11 is placed on the base 8 so as to surround the outer layer member 11.
  • the inner layer member 12, the outer layer member 11, and the restraining member 16 arranged in this way are heated in an inert atmosphere to perform diffusion bonding between the outer layer member 11 and the inner layer member 12.
  • the diffusion bonding temperature is preferably 1000 to 1280 ° C. If the diffusion bonding temperature is less than 1000 ° C, sufficient bonding strength may not be obtained. If the diffusion bonding temperature exceeds 1280 ° C, a ⁇ phase is generated in the cemented carbide near the bonding interface, and the bonding strength is reduced. descend.
  • the diffusion bonding temperature is more preferably 1100 to 1280 ° C, and most preferably 1200 to 1260 ° C.
  • the time for maintaining the diffusion bonding temperature may be about 1 to 120 minutes, preferably 30 to 90 minutes.
  • an inert gas such as N 2 or Ar, a reducing gas such as H 2 , or a vacuum can be used.
  • the thermal expansion coefficients of the inner layer member 12, the outer layer member 11, and the restraining member 16 must satisfy the relationship of inner layer member 12> outer layer member 11> restraining member 16. Don't be.
  • the thermal expansion coefficient of the iron alloy inner layer member 12 in the range from room temperature to 1000 to 1280 ° C. is about 11 to 15 ⁇ 10 ⁇ 6 / ° C.
  • the thermal expansion coefficient of the cemented carbide outer layer member 11 is 6 About 10 ⁇ 10 -6 / ° C. Therefore, the thermal expansion coefficient of the restraining member 16 must be sufficiently smaller than these in the temperature range from room temperature to the diffusion bonding temperature.
  • the restraining member 16 is preferably made of graphite or ceramics having a thermal expansion coefficient of about 4 to 9 ⁇ 10 ⁇ 6 / ° C. Further, the restraining member 16 must sufficiently withstand the diffusion bonding temperature and the diffusion bonding stress, and therefore must have high strength and high rigidity at the diffusion bonding temperature. Furthermore, the restraining member 16 is preferably made of a material that is not bonded to the cemented carbide at the diffusion bonding temperature. Graphite or ceramics also satisfy these conditions. Among them, isotropic graphite having a thermal expansion coefficient of 6 ⁇ 10 ⁇ 6 / ° C. or less and a bending strength at 1000 ° C. of 30 MPa or more is particularly preferable.
  • the outer surface of the inner layer member 12 that is most thermally expanded by heating sufficiently presses the inner surface of the outer layer member 11, and the inner surface of the restraining member 16 that is least thermally expanded is the outer layer member 11. It is necessary to set a gap G 1 between the inner layer member 12 and the outer layer member 11 and a gap G 2 between the outer layer member 11 and the restraining member 16 so as to sufficiently press the outer surface of the member [see FIG. 4 (b)]. .
  • the diameter of the steel inner layer member 12 (thermal expansion coefficient: 13 ⁇ 10 ⁇ 6 / ° C.) is 275 mm and the outer layer member 11 made of cemented carbide (thermal expansion coefficient: 8 ⁇ 10 ⁇ 6 / ° C.)
  • the gap G 1 between the outer layer member 11 and the inner layer member 12 is preferably 0.3 to 1.5 mm
  • the gap G 2 between the outer layer member 11 and the restraining member 16 is 1 to 2 mm.
  • the restraint member 16 having a smaller coefficient of thermal expansion than the outer layer member 11 is disposed outside the outer layer member 11, and the thermal expansion of the outer layer member 11 and the inner layer member 12 is restrained by the restraint member 16, so that the inner layer that is most thermally expanded.
  • the outer surface of the member 12 is in close contact with the inner surface of the outer layer member 11 with a surface pressure (bonding surface pressure) necessary for diffusion bonding. This makes it possible to obtain a cemented carbide composite roll with good bonding reliability even when the outer diameter is 300 mm or more and the roll length is 500 mm or more.
  • the outer layer member 11 of the restraining member 16 long the preferably than the total length L 1 of the total length L 3 is the outer layer member 11 of the restraining member 16, also the axial end faces 6a of the restraining member 16, 6b are axial outer member 11 It is preferable that the length D projects from both end faces 1a and 1b. Accordingly, since the outer member 11 can be uniformly constrained between axially opposite ends, uniformly diffusion bonding to the inner layer member 12 over the entire length L 1 of the outer member 11. For example, when the total length L 2 of the inner layer member 12 is 800 mm and the total length L 1 of the outer layer member 11 is 700 mm, D is preferably 10 to 100 mm.
  • the restraining member 16 Since the restraining member 16 must sufficiently restrain the outer layer member 11 without being deformed or damaged at the diffusion bonding temperature, it is preferable that the restraining member 16 is sufficiently thicker than the outer layer member 11 in the radial direction.
  • the thickness T 3 of the restraining member 16 is preferably 100 to 150 mm.
  • the constraining member 16 can be configured by stacking a plurality (six in the illustrated example) of relatively short ring members 61 to 66 coaxially in the axial direction. Since the thermal expansion restraining force of the restraining member 16 acts in the radial direction, even if the ring members 61 to 66 separated in the axial direction are used, the thermal expansion restraining effect is the same.
  • each of the ring members 61 to 66 is preferably made of graphite or ceramics.
  • reaction preventing material between the restraining member 16 and the outer layer member 11 so that the reaction does not occur even when contacting the outer layer member 11 at the diffusion bonding temperature.
  • the reaction preventing material ceramics such as alumina having low reactivity with the outer layer member 11 is preferable.
  • the reaction inhibitor may be in the form of powder or woven fabric. In the case of powder, the slurry may be applied to the outer surface of the outer layer member 11 or the inner surface of the restraining member 16. In the case of a woven fabric shape, the outer layer member 11 may be wound around the outer periphery.
  • the outer layer member 11 and the inner layer member 12 are diffusion bonded, the outer layer member 11 becomes the outer layer 1 and the inner layer member 12 becomes the inner layer 2. Further, the carburized layer 13 of the inner layer member 12 becomes the C concentrated layer 3. Thereafter, the restraining member 16 is removed to obtain a cemented carbide composite roll 10 in which the outer layer 1 and the inner layer 2 are integrated. If necessary, a desired portion of the cemented carbide composite roll 10 is machined to obtain a dimension and shape suitable for hot sheet rolling.
  • Hot isostatic pressure (HIP) method As shown in FIG. 6, an iron-based alloy obtained by putting a cylindrical outer layer member 11 into a cylindrical HIP can body 20 a and then carburizing inside the cylindrical outer layer member 11.
  • the inner layer member 12 is disposed, the donut plates 20b, 20b covering the end surface of the outer layer member 11 are welded to the cylindrical HIP can body 20a, and the cup portions 20c, 20c covering the inner layer member 12 are further attached to the donut plates 20b, 20b. Weld and depressurize the resulting HIP can. Then, the HIP can is put into the HIP device and the HIP process is performed.
  • the HIP temperature is preferably 1100 to 1300 ° C.
  • the HIP pressure is preferably 100 to 140 MPa.
  • the outer layer member 11 and the inner layer member 12 are firmly joined by HIP, the outer layer member 11 becomes the outer layer 1, and the inner layer member 12 becomes the inner layer 2. Further, the carburized layer 13 of the inner layer member 12 becomes the C concentrated layer 3.
  • the HIP can 20 is removed by machining to obtain a cemented carbide composite roll 10 in which the outer layer 1 and the inner layer 2 are integrated. Also in this case, a desired portion of the cemented carbide composite roll 10 may be machined as necessary.
  • the gap between the outer layer member 11 and the inner layer member 12 may be filled with a powder having a high C concentration. Examples of such high C concentration powder include WC 50 -Co 50 cemented carbide.
  • Example 1 Using a cemented carbide having the composition shown in Table 1, a cylindrical outer layer test piece 31 having an outer diameter of 20 mm and a thickness of 20 mm shown in FIG. 7 was produced. Further, a disk-shaped inner layer test piece 32 having an outer diameter of 30 mm and a thickness of 10 mm shown in FIG. 7 was prepared using an iron-based alloy having the composition shown in Table 2. The inner layer test piece 32 was subjected to gas carburizing treatment to form a carburized layer 13 having a target depth of 4 mm and a target C concentration of 0.75 to 0.9% by mass on the surface. FIG. 9 shows the C concentration distribution from the surface to the inside of the carburized layer 13.
  • the C concentration was measured by cutting out a small sample from the test piece 32 and using a carbon analyzer. As a result of the measurement, the thickness of the carburized layer was about 4 mm, and the maximum value of C concentration (concentration on the surface) was 0.92% by mass. The surface layer portion of the carburized layer 13 was removed by machining to a depth of 0.2 mm.
  • the average particle size of the WC particles was 5 ⁇ m.
  • the outer layer test piece 31 and the inner layer test piece 32 are stacked as shown in FIG. 7, and after being placed in a graphite jig 34, they are pressurized from above in a vacuum, diffusion bonded under the conditions shown in Table 3, and bonded test pieces 1 ⁇ 5 was obtained. Each bonding test piece 1 to 5 was cut and the bonding interface was observed. For the bonding specimens 4 and 5, the C concentration distribution from the bonding boundary to the inner layer was examined. The results are shown in FIG. In Table 3, the C-concentrated layer means that the C concentration is in the range of 0.6% by mass or more.
  • the ⁇ phase at the bonding interface between the inner layer test piece 32 and the outer layer test piece 31 was not observed in the bonding test pieces 1 to 4, but was confirmed in the bonding test piece 5.
  • Example 2 An outer layer test piece 31 ′ having a composition shown in Table 1 having a diameter of 25 mm ⁇ a length of 75 mm and an inner layer test piece 32 ′ made of an iron-based alloy having a composition shown in Table 2 having a diameter of 25 mm ⁇ a length of 75 mm (implemented) A carburized layer 13 was formed under the same conditions as in Example 1.). After placing the outer layer test piece 31 ′ and the inner layer test piece 32 ′ in the graphite jig 34 as shown in FIG. 7, the jig 34 is pressed from above in vacuum, and diffusion bonding is performed under the conditions shown in Table 4. The test specimens 1 ′ to 5 ′ were prepared.
  • a tensile test piece 40 having a shape shown in FIG. 8 (consisting of an outer layer test piece part 41 and an inner layer test piece part 42 having a boundary in the center between the gauge points) was prepared from each of the joining test pieces 1 ′ to 5 ′. .
  • the outer layer test piece portion 41 was formed from the outer layer test piece 31 ', and the inner layer test piece portion 42 was formed from the inner layer test piece 32'.
  • the diameter of the tensile test piece 40 was 6.3 mm, and the gauge distance was 19 mm.
  • the tensile strength at the joining boundary was measured by a tensile test.
  • the results are shown in Table 4.
  • the tensile strength at the boundary between the outer layer test piece portion 41 and the inner layer test piece portion 42 was 600 MPa or more for the tensile test pieces 1 to 4, but 530 MPa for the tensile test piece 5 It was low. This is considered to be because the ⁇ phase was formed at the bonding interface in the bonding test piece 5 '.
  • Example 3 Using a ferrous alloy having the composition shown in Table 2, a roll shaft-shaped inner layer member 12 having an outer diameter of 276 mm and a total length of 1930 mm was produced. A carburized layer 13 having a target thickness of 4 mm and a target C concentration of 0.75 to 0.9% by mass was formed on the surface of the inner layer member 12 by a gas carburizing method. A test piece was collected from the end of the inner layer member 12, and the C concentration was measured in the depth direction of the carburized layer 13. As a result, it was found that the C concentration distribution was the same as in FIG. Thereafter, the carburized layer 13 was removed by machining by a depth of 0.5 mm.
  • a hollow cylindrical outer layer member 11 having an outer diameter of 364 mm, an inner diameter of 276 mm, and a total length of 680 mm was manufactured using a cemented carbide having the composition shown in Table 1. Further, a graphite hollow cylindrical restraining member 16 having an outer diameter of 600 mm, an inner diameter of 365.5 mm, and a total length of 800 mm was produced.
  • the end portions of the outer layer 1 and the inner layer 2 in the cemented carbide composite roll 10 were visually inspected, and the entire bonding surface was inspected. As a result, no boundary defect was observed over the entire bonding surface. Further, no peeling between the outer layer 1 and the inner layer 2 was observed.
  • Outer layer 2 Inner layer 3: C thickened layer 8: Base 9: cradle 10: Cemented carbide composite roll 11: Outer layer member 12: Inner layer member 13: Carburized layer 16: Restraint member 20: HIP can 31: Outer layer specimen 32: Inner layer specimen 34: Graphite jig 61-66: Ring member for restraint member L 1 : Length of outer layer member L 2 : Length of inner layer member L 3 : Length of restraint member D: Length of the restraining member extending from each end of the outer layer member T 1 : Thickness of outer layer member T 2 : Diameter of inner layer member T 3 : Thickness of restraining member G 1 : Gap between the outer layer member and the inner layer member G 2 : Gap between the outer layer member and the restraining member

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Abstract

A superhard alloy composite roll having: a superhard alloy outer layer and an iron-based alloy inner layer diffusion-bonded therein; a carbon concentrated layer comprising an iron-based alloy having a higher carbon concentration than an inner layer main body, in a surface area of the inner layer adjacent to the bonding boundary with the outer layer; a carbon concentration of 0.7%-1.2% by mass in said bonding boundary of the carbon concentrated layer; and a thickness of 0.5-6 mm.

Description

超硬合金複合ロール及びその製造方法Cemented carbide composite roll and manufacturing method thereof
 本発明は、耐摩耗性、耐肌荒れ性等に優れた外層と靱性に優れた内層とからなり、板材、線材、棒材等の鋼材の圧延に好適な高耐久性の超硬合金複合ロール、及びその製造方法に関する。 The present invention comprises an outer layer excellent in wear resistance, rough skin resistance, etc. and an inner layer excellent in toughness, and is a highly durable cemented carbide composite roll suitable for rolling steel materials such as plate materials, wire materials, bar materials, And a manufacturing method thereof.
 寸法精度の向上等圧延材の高品質化、及びロール替え工数の低減による生産性向上の要求に応えるため、耐摩耗性、耐肌荒れ性等に優れた炭化タングステン(WC)系超硬合金からなる圧延用ロールが使用されており、種々の構造の超硬合金圧延ロールが提案されている。 Made of tungsten carbide (WC) cemented carbide with excellent wear resistance, rough skin resistance, etc., to meet the demands for higher quality of rolled materials, such as improved dimensional accuracy, and improved productivity by reducing the number of roll change man-hours. Rolls for rolling are used, and cemented carbide rolling rolls having various structures have been proposed.
 例えば、特開平3-281007号は、図11に示すように、両端に固定の締付フランジ部103と着脱自在な締付フランジ部104とを備えたロール本体105と、熱膨張係数が15×10-6/℃以上で熱伝導率が0.4 cal/cm・sec・℃以上の金属製リング状スペーサ111,111及び筒状スペーサ114を介してロール本体105に嵌合された超硬合金製円筒体110とを具備する超硬合金圧延ロールを提案している。リング状スペーサ111,111の熱膨張を利用して、締付フランジ部103,104の締付力を向上させている。しかし、リング状スペーサ111,111及び筒状スペーサ114があっても、締付フランジ部103,104による締付力では超硬合金製円筒体110とロール本体105との密着性は不十分であり、圧延中に超硬合金製円筒体110がロール本体105に対してスリップを起こしてしまうおそれがあった。 For example, as shown in FIG. 11, Japanese Patent Laid-Open No. 3-281007 discloses a roll body 105 having a fastening flange portion 103 fixed at both ends and a detachable fastening flange portion 104, and a thermal expansion coefficient of 15 ×. A cemented carbide cylinder fitted to the roll body 105 via metal ring spacers 111 and 111 and a cylindrical spacer 114 having a thermal conductivity of 0.4 cal / cm · sec · ° C or higher at 10 -6 / ° C or higher. A cemented carbide rolling roll having a body 110 is proposed. The tightening force of the tightening flange portions 103 and 104 is improved by utilizing the thermal expansion of the ring spacers 111 and 111. However, even with the ring- shaped spacers 111 and 111 and the cylindrical spacer 114, the adhesion between the cemented carbide cylinder 110 and the roll body 105 is not sufficient with the tightening force by the tightening flange portions 103 and 104. In addition, the cemented carbide cylindrical body 110 may slip with respect to the roll body 105 during rolling.
 このような組立構造の超硬合金圧延ロールの問題点を解決するために、超硬合金製外層と金属製内層とを拡散接合した超硬合金複合ロールが提案されている。例えば、特開2001-47111号は、靱性に優れた材料からなる内層部材の外周に、WC系超硬合金製外層部材を金属接合した超硬合金複合ロールにおいて、外層部材の内側にWC粒子の含有量が外層より少ないWC系超硬合金製中間層を設け、内層部材と中間層とを金属層を介して接合した超硬合金複合ロールを提案している。特開2001-47111号は、中間層を外層部材から内層部材にかけてWCが傾斜的な濃度を有する組成とすることにより、熱膨張率、弾性係数等の物性値を外層部材から内層部材にかけて連続的に変化させ、もって境界接合部の強度を向上させると記載している。 In order to solve the problem of the cemented carbide rolling roll having such an assembly structure, a cemented carbide composite roll in which a cemented carbide outer layer and a metal inner layer are diffusion-bonded has been proposed. For example, JP 2001-47111 A discloses a cemented carbide composite roll in which an outer layer member made of a WC-based cemented carbide is metal-bonded to the outer periphery of an inner layer member made of a material having excellent toughness. A cemented carbide composite roll is proposed in which a WC-based cemented carbide intermediate layer having a lower content than the outer layer is provided, and the inner layer member and the intermediate layer are joined via a metal layer. Japanese Patent Laid-Open No. 2001-47111 discloses that the WC has a gradient concentration from the outer layer member to the inner layer member and the physical properties such as the coefficient of thermal expansion and the elastic coefficient are continuously applied from the outer layer member to the inner layer member. It is described that the strength of the boundary joint is improved.
 特開2004-167501号は、鋼系又は鉄系合金製内層部材の外周に超硬合金製外層部材を接合した超硬合金複合ロールであって、内層部材と外層部材との間にヤング率が190 GPa以下の中間層を設けたことを特徴とする超硬合金製圧延用複合ロールを提案している。特開2004-167501号は、中間層のヤング率を190 GPa以下とすることにより、外層と内層間の歪を吸収し、外層と内層との熱膨張係数差が大きくても、ロール内部に過大な残留応力が発生せず、ロール製造時に境界接合部が剥離する問題を回避防止できると記載している。特開2004-167501号は、中間層の材質としてインバー系合金及びSUS304を例示している。 JP 2004-167501 is a cemented carbide composite roll in which a cemented carbide outer layer member is joined to the outer periphery of a steel or iron alloy inner layer member, and has a Young's modulus between the inner layer member and the outer layer member. A composite roll for rolling made of cemented carbide characterized by providing an intermediate layer of 190 GPa or less is proposed. Japanese Patent Laid-Open No. 2004-167501 absorbs strain between the outer layer and the inner layer by setting the Young's modulus of the intermediate layer to 190 GPa or less, and even if the thermal expansion coefficient difference between the outer layer and the inner layer is large, it is excessive in the roll. No residual stress is generated, and it is described that it is possible to avoid and avoid the problem of separation of the boundary joint during roll production. Japanese Patent Application Laid-Open No. 2004-167501 exemplifies Invar alloy and SUS304 as the material of the intermediate layer.
 特開2003-275809号は、0.5質量%以上のCを含有する鉄系合金製内層の外周にWC系超硬合金製外層を直接金属接合した圧延用複合ロールを提案している。特開2003-275809号は、得られた超硬合金製複合ロールの境界接合部には脆弱なη相がなく、高い接合信頼性を有すると記載している。 JP 2003-275809 has proposed a composite roll for rolling in which a WC cemented carbide outer layer is directly metal-bonded to the outer periphery of an iron alloy inner layer containing 0.5 mass% or more of C. Japanese Unexamined Patent Publication No. 2003-275809 describes that the obtained cemented carbide composite roll does not have a fragile η phase at the boundary joining portion and has high joining reliability.
 しかし、耐摩耗性に優れた超硬合金製外層と鉄系合金製内層を接合した特開2001-47111号、特開2004-167501号及び特開2003-275809号に記載の超硬合金複合ロールを、外径が300 mm以上でロール長が500 mm以上の熱間薄板圧延用ロールのように大型化するには、外層と内層の接合信頼性が十分でないおそれがあることが分った。また、より厳しい圧延条件に使用する場合には、外層と内層のより高い接合強度が求められる。 However, cemented carbide composite rolls described in JP-A-2001-47111, JP-A-2004-167501, and JP-A-2003-275809, in which a cemented carbide outer layer having excellent wear resistance and an iron-based alloy inner layer are joined. It has been found that there is a possibility that the bonding reliability between the outer layer and the inner layer may not be sufficient to increase the size of the roll as in a hot sheet rolling roll having an outer diameter of 300 mm or more and a roll length of 500 mm or more. Further, when used in more severe rolling conditions, higher bonding strength between the outer layer and the inner layer is required.
 従って、本発明の目的は、耐摩耗性、耐肌荒れ性等に優れた超硬合金製外層と靱性に優れた鉄系合金製内層とからなり、両者の接合強度が極めて高い超硬合金複合ロール、及びその効率的な製造方法を提供することである。 Accordingly, an object of the present invention is a cemented carbide composite roll comprising a cemented carbide outer layer excellent in wear resistance, rough skin resistance, and the like and an iron-based alloy inner layer excellent in toughness, both of which have extremely high joint strength. And an efficient manufacturing method thereof.
 上記目的に鑑み鋭意研究の結果、鉄系合金製内層の表面にあらかじめC濃化層を設けておくことにより、接合境界部に脆弱なη相が形成されずに、外層と内層とが強固に接合されることを発見し、本発明に想到した。 As a result of earnest research in view of the above-mentioned purpose, by providing a C-enriched layer in advance on the surface of the iron-based alloy inner layer, the outer layer and the inner layer are strengthened without forming a fragile η phase at the joint boundary. It was discovered that they were joined, and the present invention was conceived.
 すなわち、本発明の超硬合金複合ロールは、超硬合金製外層と鉄系合金製内層とが拡散接合したもので、前記外層との接合境界に隣接する前記内層の表層域に、前記内層本体よりC濃度が高い鉄系合金からなるC濃化層を有することを特徴とする。 That is, the cemented carbide composite roll of the present invention is a cemented carbide outer layer and an iron-based alloy inner layer that are diffusion-bonded, and the inner layer body in the surface layer region of the inner layer adjacent to the bonding boundary with the outer layer. It has a C-enriched layer made of an iron-based alloy having a higher C concentration.
 前記C濃化層の厚さは0.5~6 mmであるのが好ましい。 The thickness of the C concentrated layer is preferably 0.5 to 6 mm.
 前記C濃化層の前記接合境界におけるC濃度は0.7~1.2質量%であるのが好ましい。前記C濃化層中のC濃度は前記接合境界から内層本体に向けて徐々に低下するのが好ましい。前記C濃化層内の深さ方向のC濃度の減少率は0.01%/mm以上であるのが好ましい。 The C concentration at the junction boundary of the C concentrated layer is preferably 0.7 to 1.2% by mass. It is preferable that the C concentration in the C-concentrated layer gradually decreases from the joining boundary toward the inner layer main body. The reduction rate of the C concentration in the depth direction in the C enriched layer is preferably 0.01% / mm or more.
 前記外層と前記内層との境界の引張強度は600 MPa以上であるのが好ましい。 The tensile strength at the boundary between the outer layer and the inner layer is preferably 600 MPa or more.
 前記超硬合金製外層は70~88質量%のWC粒子を含有するのが好ましい。 The cemented carbide outer layer preferably contains 70 to 88% by mass of WC particles.
 本発明の超硬合金複合ロールにおいて、前記鉄系合金製内層本体のC濃度は0.2~0.5質量%であるのが好ましい。 In the cemented carbide composite roll of the present invention, the C concentration of the iron-based alloy inner layer body is preferably 0.2 to 0.5% by mass.
 前記鉄系合金製内層は、Cr、Ni、Mo、V、W、Ti及びNbからなる群から選ばれた少なくとも一種を合計で1.0質量%以上含有するのが好ましい。 The iron-based alloy inner layer preferably contains 1.0% by mass or more in total of at least one selected from the group consisting of Cr, Ni, Mo, V, W, Ti and Nb.
 超硬合金からなる円筒状外層部材と鉄系合金からなる内層部材とが接合した超硬合金複合ロールを製造する本発明の方法は、前記内層部材の外面に浸炭処理を施した後に、前記外層部材と前記内層部材を拡散接合することを特徴とする。 The method of the present invention for producing a cemented carbide composite roll in which a cylindrical outer layer member made of a cemented carbide and an inner layer member made of an iron-based alloy are joined is obtained by carburizing the outer surface of the inner layer member. The member and the inner layer member are diffusion bonded.
 前記浸炭処理により形成された浸炭層の厚さは0.5~10 mmであるのが好ましい。 The thickness of the carburized layer formed by the carburizing process is preferably 0.5 to 10 mm.
 前記浸炭処理をガス浸炭処理法により行うのが好ましい。 It is preferable to perform the carburizing process by a gas carburizing process.
 前記外層部材の内側に前記内層部材を配置し、前記外層部材の外側に、室温から接合温度までの温度範囲において前記外層部材より熱膨張率が小さい中空円筒状の拘束部材を配置し、加熱により最も熱膨張した前記内層部材の外面が前記外層部材の内面を押圧するとともに、最も熱膨張しない前記拘束部材の内面が前記外層部材の外面を押圧するように、前記外層部材と前記内層部材及び前記拘束部材との間隙を設定し、かつ加熱により前記外層部材の内面と前記内層部材の外面とを密接させ、もって前記外層部材と前記内層部材とを拡散接合するのが好ましい。 The inner layer member is disposed inside the outer layer member, and a hollow cylindrical restraining member having a smaller coefficient of thermal expansion than the outer layer member is disposed outside the outer layer member in a temperature range from room temperature to a bonding temperature. The outer layer member, the inner layer member, and the outer layer member so that the outer surface of the inner layer member that is most thermally expanded presses the inner surface of the outer layer member, and the inner surface of the restraining member that is not thermally expanded presses the outer surface of the outer layer member. It is preferable that a gap with the restraining member is set, and the inner surface of the outer layer member and the outer surface of the inner layer member are brought into close contact with each other by heating, so that the outer layer member and the inner layer member are diffusion bonded.
 前記拘束部材の軸線方向両端部は、前記外層部材の軸線方向両端面より突出しているのが好ましい。 It is preferable that both end portions in the axial direction of the restraining member protrude from both end surfaces in the axial direction of the outer layer member.
 前記拘束部材は前記外層部材より厚いのが好ましい。 It is preferable that the restraining member is thicker than the outer layer member.
 前記拘束部材は黒鉛又はセラミックスからなるのが好ましい。 The restraining member is preferably made of graphite or ceramics.
 複数個のリング部材を同軸的に積み重ねることにより、前記拘束部材を形成するのが好ましい。 It is preferable that the restraining member is formed by coaxially stacking a plurality of ring members.
 前記拘束部材と前記外層部材との間に反応防止材を介在させるのが好ましい。 It is preferable that a reaction preventing material is interposed between the restraining member and the outer layer member.
 本発明の超硬合金製複合ロールは、超硬合金製外層と鉄系合金製内層とがC濃化層を介して接合しているので、外層と内層の接合強度が大きい。そのため、300 mm以上の外径及び500 mm以上のロール長を有する大型の圧延ロールにしても、長期間の圧延に使用できる。また、あらかじめ表層域を浸炭した鉄系合金製内層部材と超硬合金製外層とを拡散接合法又はHIP法により接合すると、脆弱なη相がない接合境界を形成することができ、もって超硬合金製外層と鉄系合金製内層とが強固に接合した超硬合金複合ロールを得ることができる。 In the cemented carbide alloy composite roll of the present invention, the cemented carbide outer layer and the iron-based alloy inner layer are joined via the C-concentrated layer, so the joining strength between the outer layer and the inner layer is high. Therefore, even a large rolling roll having an outer diameter of 300 mm or more and a roll length of 500 mm or more can be used for long-term rolling. In addition, when the inner layer member made of an iron-based alloy and the outer layer made of a cemented carbide alloy that have been carburized in advance in the surface layer region are joined by the diffusion joining method or the HIP method, a joining boundary without a fragile η phase can be formed. A cemented carbide composite roll in which an alloy outer layer and an iron-based alloy inner layer are firmly bonded can be obtained.
本発明の超硬合金複合ロールを示す部分断面正面図である。It is a fragmentary sectional front view which shows the cemented carbide composite roll of this invention. 本発明の超硬合金複合ロールのC濃度分布を示すグラフである。It is a graph which shows C concentration distribution of the cemented carbide composite roll of this invention. 本発明の超硬合金複合ロールの製造工程を示すフローチャートである。It is a flowchart which shows the manufacturing process of the cemented carbide composite roll of this invention. 本発明の超硬合金複合ロールを拡散接合法により製造する例を示す断面図である。It is sectional drawing which shows the example which manufactures the cemented carbide composite roll of this invention by the diffusion bonding method. 図4(a) における部分Aの拡大図である。FIG. 4 (a) is an enlarged view of a portion A in the bag. 同軸的に積み重ねた複数のリング部材により構成した拘束部材を用いる拡散接合法を示す断面図である。It is sectional drawing which shows the diffusion bonding method using the constraining member comprised by the some ring member piled up coaxially. 本発明の超硬合金複合ロールをHIP法により製造する例を示す断面図である。It is sectional drawing which shows the example which manufactures the cemented carbide composite roll of this invention by HIP method. 実施例1の接合実験を示す断面図である。2 is a cross-sectional view showing a joining experiment of Example 1. FIG. 引張試験片を示す正面図である。It is a front view which shows a tension test piece. 実施例1の浸炭層における表面から内部へのC濃度分布を示すグラフである。2 is a graph showing a C concentration distribution from the surface to the inside in the carburized layer of Example 1. FIG. 実施例1の接合試験片4及び5について、接合境界から内層内部へのC濃度分布を示すグラフである。4 is a graph showing the C concentration distribution from the joining boundary to the inside of the inner layer for joining test pieces 4 and 5 of Example 1. FIG. 特開平3-281007号に開示された超硬合金圧延ロールを示す部分断面図である。FIG. 3 is a partial cross-sectional view showing a cemented carbide rolling roll disclosed in Japanese Patent Laid-Open No. 3-281007.
 本発明を添付図面を参照して以下詳細に説明するが、本発明はそれらに限定されるものではなく、本発明の技術的思想を逸脱しない範囲内で適宜変更又は改良することができる。本発明の一実施形態に関する説明は、特に断りがなければ他の実施形態にも適用される。 The present invention will be described in detail below with reference to the accompanying drawings. However, the present invention is not limited to these, and can be appropriately changed or improved without departing from the technical idea of the present invention. The description relating to one embodiment of the present invention also applies to other embodiments unless otherwise specified.
[1] 超硬合金複合ロール
 鋼等の被圧延材を圧延するのに用いることができる本発明の超硬合金複合ロール10は、図1に示すように、超硬合金製外層1と鉄系合金製内層2とからなり、外層1と内層2の境界部にC濃化層3を有する。C濃化層はC濃度が0.6質量%以上の鉄系合金であり、内層2よりC濃度が高い。表面に被圧延材が接触する外層1は優れた耐摩耗性、耐肌荒れ性及び機械的強度が要求され、両端が軸受(図示せず)で支持されるロール軸を構成する内層2は高い機械的強度及び強靭性が要求される。
[1] Cemented carbide composite roll A cemented carbide composite roll 10 of the present invention that can be used for rolling a rolled material such as steel is composed of a cemented carbide outer layer 1 and a ferrous alloy as shown in FIG. The inner layer 2 is made of an alloy, and a C concentrated layer 3 is provided at the boundary between the outer layer 1 and the inner layer 2. The C-enriched layer is an iron-based alloy having a C concentration of 0.6% by mass or more and has a higher C concentration than the inner layer 2. The outer layer 1 whose surface is in contact with the material to be rolled is required to have excellent wear resistance, rough skin resistance and mechanical strength, and the inner layer 2 constituting the roll shaft whose both ends are supported by bearings (not shown) is a high machine. Strength and toughness are required.
(1) 外層
 本発明の超硬合金複合ロールの超硬合金製外層1は、硬質WC粒子をCo、Ni、Cr、Fe等の金属で結合した焼結合金であり、WCの他にTi、Ta、Nb等の炭化物を含有しても良い。外層1が高い耐摩耗性及び機械的強度を有するために、WC粒子の平均粒径は3~10μmが好ましく、WC粒子の含有量は70~88質量%が好ましく、72~85質量%がより好ましい。外層1の厚さは、圧延により徐々に摩耗することを考慮して、5~50 mmの範囲に設定するのが好ましい。
(1) Outer layerThe cemented carbide outer layer 1 of the cemented carbide composite roll of the present invention is a sintered alloy in which hard WC particles are bonded with a metal such as Co, Ni, Cr, Fe, etc. Carbides such as Ta and Nb may be contained. Since the outer layer 1 has high wear resistance and mechanical strength, the average particle size of the WC particles is preferably 3 to 10 μm, the content of the WC particles is preferably 70 to 88% by mass, and more preferably 72 to 85% by mass. preferable. The thickness of the outer layer 1 is preferably set in the range of 5 to 50 mm in consideration of gradual wear due to rolling.
(2) 内層
 内層2の鉄系合金は鋼であるのが好ましい。内層2が十分な靱性を有するために、Cを0.2~0.5質量%、及びCr、Ni、Mo、V、W、Ti及びNbからなる群から選ばれた少なくとも一種を合計で1.0質量%以上含有する鋼が好ましい。Cが0.2質量%未満であると、内層2は十分な強度を有さない。一方、Cが0.5質量%を超えると、内層2の靱性が不足する。その他の元素の含有量に関しては、鋼材の一般的な組成範囲内であれば良い。
(2) Inner layer The iron-based alloy of the inner layer 2 is preferably steel. In order for inner layer 2 to have sufficient toughness, 0.2 to 0.5 mass% of C and 1.0 mass% or more in total of at least one selected from the group consisting of Cr, Ni, Mo, V, W, Ti and Nb Steel is preferred. When C is less than 0.2% by mass, the inner layer 2 does not have sufficient strength. On the other hand, if C exceeds 0.5% by mass, the toughness of the inner layer 2 is insufficient. The content of other elements may be within the general composition range of steel materials.
 熱膨張係数の小さな超硬合金製の外層1に対して、内層2は大きな熱膨張係数を有するので、熱膨張により発生する歪みを緩和させる変態膨張特性が必要である。この変態がパーライト変態であると、高温での塑性変形のために、常温への冷却過程での熱膨張係数差により大きな歪みが発生し、ロール破壊の原因となる。このため、この変態は、低温で起こるベイナイト変態又はマルテンサイト変態でなければならない。このため、内層にはCr、Ni、Mo、V、W、Ti及びNbからなる群から選ばれた少なくとも一種を合計で1.0質量%以上含むのが好ましい。特に、Cr含有量は0.5~1.5質量%が好ましく、Mo含有量は0.1~0.5質量%が好ましく、Ni含有量は1.5~2.5質量%が好ましい。 Since the inner layer 2 has a larger thermal expansion coefficient than the outer layer 1 made of a cemented carbide having a small thermal expansion coefficient, it needs a transformation expansion characteristic to relieve strain generated by the thermal expansion. If this transformation is a pearlite transformation, due to plastic deformation at a high temperature, a large strain is generated due to a difference in thermal expansion coefficient in the process of cooling to room temperature, which causes roll breakage. For this reason, this transformation must be a bainite transformation or a martensitic transformation that occurs at low temperatures. For this reason, it is preferable that the inner layer contains 1.0% by mass or more in total of at least one selected from the group consisting of Cr, Ni, Mo, V, W, Ti, and Nb. In particular, the Cr content is preferably 0.5 to 1.5 mass%, the Mo content is preferably 0.1 to 0.5 mass%, and the Ni content is preferably 1.5 to 2.5 mass%.
(3) C濃化層
 超硬合金製外層1と鉄系合金製内層2を焼結接合する際、両者の炭素活量の差により接合界面で炭素が超硬合金製外層1から内層2に拡散するので、超硬合金製外層1内の炭素濃度が低下することが知られている。その結果、低炭素組成の炭化物であるη相が超硬合金内に生成され、超硬合金の機械的強度が劣化する。
(3) C-enriched layer When the cemented carbide outer layer 1 and the iron-based alloy inner layer 2 are sintered and bonded, the carbon is changed from the cemented carbide outer layer 1 to the inner layer 2 at the bonding interface due to the difference in carbon activity between the two. It is known that the carbon concentration in the outer layer 1 made of cemented carbide decreases due to diffusion. As a result, a η phase, which is a carbide having a low carbon composition, is generated in the cemented carbide and the mechanical strength of the cemented carbide is deteriorated.
 超硬合金製外層1と鉄系合金製内層2との接合実験の結果、超硬合金製外層1と接合する内層1の表面近傍に、C濃度が0.6質量%以上のC濃化層3を形成すれば、超硬合金製外層1から内層2へのCの拡散をほぼ抑制でき、もってη相の発生を防止できることを発見した。さらにC濃化層3は内層2のごく表面近傍に形成すれば良いので、鉄系合金製内層2の強靭性は損なわれない。 As a result of the joining experiment of the outer layer 1 made of cemented carbide and the inner layer 2 made of iron alloy, a C concentrated layer 3 having a C concentration of 0.6% by mass or more was formed near the surface of the inner layer 1 to be joined with the outer layer 1 made of cemented carbide. It has been found that if formed, the diffusion of C from the cemented carbide outer layer 1 to the inner layer 2 can be substantially suppressed, thereby preventing the generation of η phase. Furthermore, since the C enriched layer 3 may be formed very close to the inner layer 2, the toughness of the iron-based alloy inner layer 2 is not impaired.
 このように、外層1との境界となる内層2の表面近傍(表層)にC濃化層3を設けることにより、外層1の外径が300 mm以上で、ロール長が500 mm以上でも、十分な接合強度を有する超硬合金複合ロール10を得ることができる。 Thus, by providing the C-concentrated layer 3 near the surface (surface layer) of the inner layer 2 that becomes the boundary with the outer layer 1, the outer diameter of the outer layer 1 is 300 mm or more and the roll length is 500 mm or more. It is possible to obtain a cemented carbide composite roll 10 having an excellent bonding strength.
 図2は、本発明の超硬合金複合ロール10のC濃化層を含む領域におけるC濃度分布を示す。図2において、横軸は外層1との境界からの距離(原点は外層1との接合境界)であり、縦軸はC濃度である。本発明の超硬合金複合ロール10では、外層1との境界から内層2に向けてC濃度が0.6質量%以上である層をC濃化層3と呼ぶ。C濃化層3の厚さは0.5~10 mmが好ましい。C濃化層3の厚さが0.5 mm未満であると、外層1との接合時にCが内層2側に拡散してC濃化層3のC濃度が低くなりすぎ、外層1の超硬合金内にη相が発生することもあるため好ましくない。一方、C濃化層3の厚さが10 mmを超えると、C濃化層3を形成するための浸炭処理の時間が長くなり、製造コストが上昇するため好ましくない。 FIG. 2 shows the C concentration distribution in the region including the C concentrated layer of the cemented carbide composite roll 10 of the present invention. In FIG. 2, the horizontal axis represents the distance from the boundary with the outer layer 1 (the origin is the junction boundary with the outer layer 1), and the vertical axis represents the C concentration. In the cemented carbide composite roll 10 of the present invention, a layer having a C concentration of 0.6% by mass or more from the boundary with the outer layer 1 toward the inner layer 2 is referred to as a C concentrated layer 3. The thickness of the C concentrated layer 3 is preferably 0.5 to 10 mm. If the thickness of the C concentrated layer 3 is less than 0.5 mm, C diffuses to the inner layer 2 side when bonded to the outer layer 1 and the C concentration of the C concentrated layer 3 becomes too low, and the cemented carbide of the outer layer 1 Since the η phase may occur in the inside, it is not preferable. On the other hand, if the thickness of the C enriched layer 3 exceeds 10 mm, the time for carburizing treatment for forming the C enriched layer 3 becomes longer, which is not preferable because the manufacturing cost increases.
 本発明の超硬合金複合ロール10のC濃化層3において、外層1との境界から0.5 mmまでの範囲を外層1に隣接する領域と定義した場合、外層隣接領域のC濃度は0.7~1.2質量%であるのが好ましい。外層隣接領域のC濃度が0.7質量%以上であると、超硬合金製外層1から内層2へのCの拡散はほとんどなく、超硬合金製外層1内におけるη相の発生を確実に防止でき、その強度低下を防止できる。一方、外層隣接領域のC濃度が1.2質量%を超えると、接合境界に黒鉛が発生し、強度が低下することもあり好ましくない。 In the C concentrated layer 3 of the cemented carbide composite roll 10 of the present invention, when the range from the boundary with the outer layer 1 to 0.5 mm is defined as a region adjacent to the outer layer 1, the C concentration in the adjacent region of the outer layer is 0.7 to 1.2. It is preferable that it is mass%. If the C concentration in the adjacent region of the outer layer is 0.7% by mass or more, there is almost no diffusion of C from the outer layer 1 made of cemented carbide to the inner layer 2, and the generation of η phase in the outer layer 1 made of cemented carbide can be reliably prevented. , The strength reduction can be prevented. On the other hand, if the C concentration in the adjacent region of the outer layer exceeds 1.2% by mass, graphite is generated at the joining boundary, and the strength is lowered, which is not preferable.
 C濃化層3において、C濃度は外層1との境界から内層2に向けて徐々に減少するのが好ましい。接合境界から内層2に向けて、ヤング率、熱膨張係数、硬度等の物性が連続的に変化することにより、接合信頼性が高くなる。 In the C enriched layer 3, it is preferable that the C concentration gradually decreases from the boundary with the outer layer 1 toward the inner layer 2. As the physical properties such as Young's modulus, thermal expansion coefficient, and hardness continuously change from the joining boundary toward the inner layer 2, the joining reliability increases.
 圧延に長期間使用しても外層1と内層2が剥離しないように、外層1と内層2の境界部の引張強度は600 MPa以上であるのが好ましく、700 MPa以上がより好ましい。なお、外層1と内層2の境界部の引張強度は、外層1と内層2の境界部を含む試験片の引張試験により測定することができる。 The tensile strength at the boundary between the outer layer 1 and the inner layer 2 is preferably 600 MPa or more, more preferably 700 MPa or more so that the outer layer 1 and the inner layer 2 do not peel even when used for a long time in rolling. The tensile strength at the boundary between the outer layer 1 and the inner layer 2 can be measured by a tensile test of a test piece including the boundary between the outer layer 1 and the inner layer 2.
[2] 超硬合金複合ロールの製造方法
(1) 浸炭処理
 図3は本発明の超硬合金複合ロール10の製造工程を示す。まず、鉄系合金からなる円柱状又は円筒状の内層部材12の外周面に浸炭処理を行う。浸炭処理に、固体浸炭法、液体浸炭法又はガス浸炭法を用いることができるが、均一な浸炭層を形成するためにガス浸炭法が好ましい。浸炭層13は、外層1と接合した後にC濃化層3になるもので、そのC濃度は最表面(外層隣接領域)で0.7~1.2質量%であるのが好ましい。浸炭層13の表面におけるC濃度が0.7質量%未満であると、外層1との接合強度が不十分であり、またC濃化層3が形成できないこともある。一方、浸炭層13の表面におけるC濃度が1.2質量%を超えると、外層との接合境界に黒鉛が発生して接合強度が低下することがある。浸炭層13内において、C濃度は表面から内層2の内部に向けて徐々に低下する。
[2] Manufacturing method of cemented carbide composite roll
(1) Carburizing treatment FIG. 3 shows a manufacturing process of the cemented carbide composite roll 10 of the present invention. First, carburizing treatment is performed on the outer peripheral surface of a columnar or cylindrical inner layer member 12 made of an iron-based alloy. A solid carburizing method, a liquid carburizing method, or a gas carburizing method can be used for the carburizing treatment, but a gas carburizing method is preferable in order to form a uniform carburized layer. The carburized layer 13 becomes the C concentrated layer 3 after being joined to the outer layer 1, and the C concentration is preferably 0.7 to 1.2% by mass on the outermost surface (outer layer adjacent region). When the C concentration on the surface of the carburized layer 13 is less than 0.7 mass%, the bonding strength with the outer layer 1 is insufficient, and the C concentrated layer 3 may not be formed. On the other hand, if the C concentration on the surface of the carburized layer 13 exceeds 1.2% by mass, graphite may be generated at the bonding boundary with the outer layer, resulting in a decrease in bonding strength. In the carburized layer 13, the C concentration gradually decreases from the surface toward the inside of the inner layer 2.
 浸炭層13の厚さは0.5~10 mmが好ましい。浸炭層13の厚さが0.5 mm未満の場合、外層との接合強度が不十分であるだけでなく、接合境界にC濃化層3が形成されないこともある。一方、厚さが10 mm超の浸炭層13を形成するのに過大な時間がかかり、製造コストが上昇する。浸炭層13の好ましい厚さは2~5 mmである。 The thickness of the carburized layer 13 is preferably 0.5 to 10 mm. When the thickness of the carburized layer 13 is less than 0.5 mm, not only the bonding strength with the outer layer is insufficient, but also the C concentrated layer 3 may not be formed at the bonding boundary. On the other hand, it takes an excessive amount of time to form the carburized layer 13 having a thickness of more than 10 mm, which increases the manufacturing cost. A preferable thickness of the carburized layer 13 is 2 to 5 mm.
(2) 接合
 浸炭層13を形成した内層部材12に超硬合金製外層部材11を接合する。内層部材12と外層部材11が隙間なく接合する限り接合方法は限定されないが、拡散接合法及び熱間静水圧(HIP)法を用いるのが好ましい。
(2) Joining The outer layer member 11 made of cemented carbide is joined to the inner layer member 12 on which the carburized layer 13 is formed. The joining method is not limited as long as the inner layer member 12 and the outer layer member 11 are joined without a gap, but a diffusion joining method and a hot isostatic pressure (HIP) method are preferably used.
(a) 拡散接合法
 図4は本発明の超硬合金複合ロールを拡散接合法により製造する方法を示す。図4に示すように、表面に浸炭処理がなされた内層部材(ロール軸に相当)12を基台8の上に載置する。内層部材12を囲むように基台8上に円筒状受台9を載置した後、円筒状外層部材11を円筒状受台9の上に載置する。受台9は後述する拘束部材と同様に、外層部材11に対して不活性な材質からなるのが好ましい。具体的には、受台9は黒鉛又はセラミックスからなるのが好ましい。次いで、外層部材11より熱膨張率が小さい円筒状拘束部材16を外層部材11を囲むように基台8上に載置する。
(a) Diffusion Bonding Method FIG. 4 shows a method for producing the cemented carbide composite roll of the present invention by the diffusion bonding method. As shown in FIG. 4, an inner layer member (corresponding to a roll shaft) 12 whose surface is carburized is placed on a base 8. After the cylindrical cradle 9 is placed on the base 8 so as to surround the inner layer member 12, the cylindrical outer layer member 11 is placed on the cylindrical cradle 9. The cradle 9 is preferably made of a material that is inactive with respect to the outer layer member 11, similarly to the restraining member described later. Specifically, the cradle 9 is preferably made of graphite or ceramics. Next, the cylindrical restraining member 16 having a smaller coefficient of thermal expansion than the outer layer member 11 is placed on the base 8 so as to surround the outer layer member 11.
 このように配置した内層部材12、外層部材11及び拘束部材16を不活性雰囲気中で加熱し、外層部材11と内層部材12の拡散接合を行う。拡散接合温度は1000~1280℃が好ましい。拡散接合温度が1000℃未満であると十分な接合強度が得られないことがあり、また拡散接合温度が1280℃を超えると接合界面付近の超硬合金内にη相が生成し、接合強度が低下する。拡散接合温度はより好ましくは1100~1280℃であり、最も好ましくは1200~1260℃である。拡散接合温度に保持する時間は1~120分間程度で良く、30~90分間が好ましい。不活性雰囲気として、N2、Ar等の不活性ガス、H2等の還元性ガス、又は真空を用いることができる。 The inner layer member 12, the outer layer member 11, and the restraining member 16 arranged in this way are heated in an inert atmosphere to perform diffusion bonding between the outer layer member 11 and the inner layer member 12. The diffusion bonding temperature is preferably 1000 to 1280 ° C. If the diffusion bonding temperature is less than 1000 ° C, sufficient bonding strength may not be obtained. If the diffusion bonding temperature exceeds 1280 ° C, a η phase is generated in the cemented carbide near the bonding interface, and the bonding strength is reduced. descend. The diffusion bonding temperature is more preferably 1100 to 1280 ° C, and most preferably 1200 to 1260 ° C. The time for maintaining the diffusion bonding temperature may be about 1 to 120 minutes, preferably 30 to 90 minutes. As the inert atmosphere, an inert gas such as N 2 or Ar, a reducing gas such as H 2 , or a vacuum can be used.
 室温から1000~1280℃の拡散接合温度までの温度範囲において、内層部材12、外層部材11及び拘束部材16の熱膨張率は、内層部材12>外層部材11>拘束部材16の関係を満たさなければならない。室温から1000~1280℃の温度までの範囲における鉄系合金製内層部材12の熱膨張率は11~15×10-6/℃程度であり、超硬合金製外層部材11の熱膨張率は6~10×10-6/℃程度である。従って、拘束部材16の熱膨張率は、室温から拡散接合温度までの温度範囲においてこれらより十分に小さくなければならない。 In the temperature range from room temperature to the diffusion bonding temperature of 1000 to 1280 ° C., the thermal expansion coefficients of the inner layer member 12, the outer layer member 11, and the restraining member 16 must satisfy the relationship of inner layer member 12> outer layer member 11> restraining member 16. Don't be. The thermal expansion coefficient of the iron alloy inner layer member 12 in the range from room temperature to 1000 to 1280 ° C. is about 11 to 15 × 10 −6 / ° C., and the thermal expansion coefficient of the cemented carbide outer layer member 11 is 6 About 10 × 10 -6 / ° C. Therefore, the thermal expansion coefficient of the restraining member 16 must be sufficiently smaller than these in the temperature range from room temperature to the diffusion bonding temperature.
 このような熱膨張率条件を満たすために、拘束部材16は熱膨張率が4~9×10-6/℃程度の黒鉛又はセラミックスからなるのが好ましい。拘束部材16はさらに拡散接合温度及び拡散接合応力に十分に耐えなければならないので、拡散接合温度で高強度かつ高剛性でなければならない。さらに、拘束部材16は、拡散接合温度で超硬合金と接合しない材質からなるのが望ましい。黒鉛又はセラミックスはこのような条件も満たす。中でも、熱膨張率が6×10-6/℃以下で、1000℃における曲げ強さが30 MPa以上の等方性黒鉛が特に好ましい。 In order to satisfy such a thermal expansion coefficient condition, the restraining member 16 is preferably made of graphite or ceramics having a thermal expansion coefficient of about 4 to 9 × 10 −6 / ° C. Further, the restraining member 16 must sufficiently withstand the diffusion bonding temperature and the diffusion bonding stress, and therefore must have high strength and high rigidity at the diffusion bonding temperature. Furthermore, the restraining member 16 is preferably made of a material that is not bonded to the cemented carbide at the diffusion bonding temperature. Graphite or ceramics also satisfy these conditions. Among them, isotropic graphite having a thermal expansion coefficient of 6 × 10 −6 / ° C. or less and a bending strength at 1000 ° C. of 30 MPa or more is particularly preferable.
 このような熱膨張率の差を考慮して、加熱により最も熱膨張した内層部材12の外面が外層部材11の内面を十分に押圧するとともに、最も熱膨張しない拘束部材16の内面が外層部材11の外面を十分に押圧するように、内層部材12と外層部材11との間隙G1、及び外層部材11と拘束部材16との間隙G2を設定する必要がある[図4(b)参照]。例えば、鋼製内層部材12(熱膨張率:13×10-6/℃)の直径が275 mmであり、かつ超硬合金製外層部材11(熱膨張率:8×10-6/℃)の厚さが69 mmである場合、外層部材11と内層部材12との間隙G1は0.3~1.5 mmであるのが好ましく、外層部材11と拘束部材16との間隙G2は1~2 mmであるのが好ましい。例えば、外層部材11の内径は276 mmが好ましく(G1=1 mm)、かつ黒鉛製拘束部材16(熱膨張率:5.5×10-6/℃)の内径は346.5 mmが好ましい(外層部材11の外径が345 mmであるので、G2=1.5 mm)。 In consideration of such a difference in coefficient of thermal expansion, the outer surface of the inner layer member 12 that is most thermally expanded by heating sufficiently presses the inner surface of the outer layer member 11, and the inner surface of the restraining member 16 that is least thermally expanded is the outer layer member 11. It is necessary to set a gap G 1 between the inner layer member 12 and the outer layer member 11 and a gap G 2 between the outer layer member 11 and the restraining member 16 so as to sufficiently press the outer surface of the member [see FIG. 4 (b)]. . For example, the diameter of the steel inner layer member 12 (thermal expansion coefficient: 13 × 10 −6 / ° C.) is 275 mm and the outer layer member 11 made of cemented carbide (thermal expansion coefficient: 8 × 10 −6 / ° C.) When the thickness is 69 mm, the gap G 1 between the outer layer member 11 and the inner layer member 12 is preferably 0.3 to 1.5 mm, and the gap G 2 between the outer layer member 11 and the restraining member 16 is 1 to 2 mm. Preferably there is. For example, the inner diameter of outer layer member 11 is preferably 276 mm (G 1 = 1 mm), and the inner diameter of graphite constraining member 16 (thermal expansion coefficient: 5.5 × 10 −6 / ° C.) is preferably 346.5 mm (outer layer member 11 ) Because the outer diameter of 345 mm is G 2 = 1.5 mm).
 上記の通り、外層部材11の外側に外層部材11より熱膨張率が小さい拘束部材16を配置し、外層部材11及び内層部材12の熱膨張を拘束部材16により拘束するので、最も熱膨張する内層部材12の外面は外層部材11の内面と拡散接合に必要な面圧(接合面圧)で密接する。これにより外径が300 mm以上でロール長が500 mm以上と大型でも、良好な接合信頼性の超硬合金複合ロールが得られる。 As described above, the restraint member 16 having a smaller coefficient of thermal expansion than the outer layer member 11 is disposed outside the outer layer member 11, and the thermal expansion of the outer layer member 11 and the inner layer member 12 is restrained by the restraint member 16, so that the inner layer that is most thermally expanded. The outer surface of the member 12 is in close contact with the inner surface of the outer layer member 11 with a surface pressure (bonding surface pressure) necessary for diffusion bonding. This makes it possible to obtain a cemented carbide composite roll with good bonding reliability even when the outer diameter is 300 mm or more and the roll length is 500 mm or more.
 図4(a) に示すように、拘束部材16の全長L3は外層部材11の全長L1より長いのが好ましく、また拘束部材16の軸線方向両端面6a、6bは外層部材11の軸線方向両端面1a、1bより長さDだけ突出しているのが好ましい。これにより、外層部材11を軸線方向両端間で均一に拘束できるので、外層部材11の全長L1にわたって内層部材12に均一に拡散接合する。例えば、内層部材12の全長L2が800 mmで、外層部材11の全長L1が700 mmの場合、Dは10~100 mmが好ましい。 As shown in FIG. 4 (a), long the preferably than the total length L 1 of the total length L 3 is the outer layer member 11 of the restraining member 16, also the axial end faces 6a of the restraining member 16, 6b are axial outer member 11 It is preferable that the length D projects from both end faces 1a and 1b. Accordingly, since the outer member 11 can be uniformly constrained between axially opposite ends, uniformly diffusion bonding to the inner layer member 12 over the entire length L 1 of the outer member 11. For example, when the total length L 2 of the inner layer member 12 is 800 mm and the total length L 1 of the outer layer member 11 is 700 mm, D is preferably 10 to 100 mm.
 拘束部材16は拡散接合温度で変形又は破損したりせずに、外層部材11を十分に拘束しなければならないので、径方向に拘束部材16を外層部材11より十分に厚くするのが好ましい。例えば、内層部材12の直径T2が275 mmで、外層部材11の厚さT1が35 mmの場合、拘束部材16の厚さT3は100~150 mmが好ましい。 Since the restraining member 16 must sufficiently restrain the outer layer member 11 without being deformed or damaged at the diffusion bonding temperature, it is preferable that the restraining member 16 is sufficiently thicker than the outer layer member 11 in the radial direction. For example, when the diameter T 2 of the inner layer member 12 is 275 mm and the thickness T 1 of the outer layer member 11 is 35 mm, the thickness T 3 of the restraining member 16 is preferably 100 to 150 mm.
 図5に示すように、拘束部材16は、複数(図示の例では6個)の比較的短尺なリング部材61~66を軸線方向に同軸的に積み重ねることにより構成することができる。拘束部材16の熱膨張拘束力は径方向に作用するので、軸線方向に分離したリング部材61~66を用いても、熱膨張拘束効果は同じである。勿論、各リング部材61~66は黒鉛又はセラミックスからなるのが好ましい。500 mm以上と長尺な超硬合金複合ロールを製造する場合、製造の容易さの観点から複数のリング部材61~66を用いるのが好ましい。 As shown in FIG. 5, the constraining member 16 can be configured by stacking a plurality (six in the illustrated example) of relatively short ring members 61 to 66 coaxially in the axial direction. Since the thermal expansion restraining force of the restraining member 16 acts in the radial direction, even if the ring members 61 to 66 separated in the axial direction are used, the thermal expansion restraining effect is the same. Of course, each of the ring members 61 to 66 is preferably made of graphite or ceramics. When manufacturing a cemented carbide composite roll having a length of 500 mm or more, it is preferable to use a plurality of ring members 61 to 66 from the viewpoint of ease of manufacturing.
 拡散接合温度で外層部材11と接しても反応が起こらないように、拘束部材16と外層部材11との間に反応防止材を介在させるのが好ましい。反応防止材としては外層部材11との反応性の低いアルミナ等のセラミックスが好ましい。反応防止材は粉末状でも織布状でも良い。粉末の場合、スラリーにして外層部材11の外面又は拘束部材16の内面に塗布しても良い。また織布状の場合、外層部材11の外周に巻き付けても良い。 It is preferable to interpose a reaction preventing material between the restraining member 16 and the outer layer member 11 so that the reaction does not occur even when contacting the outer layer member 11 at the diffusion bonding temperature. As the reaction preventing material, ceramics such as alumina having low reactivity with the outer layer member 11 is preferable. The reaction inhibitor may be in the form of powder or woven fabric. In the case of powder, the slurry may be applied to the outer surface of the outer layer member 11 or the inner surface of the restraining member 16. In the case of a woven fabric shape, the outer layer member 11 may be wound around the outer periphery.
 外層部材11と内層部材12が拡散接合すると、外層部材11は外層1となり、内層部材12は内層2となる。また、内層部材12の浸炭層13はC濃化層3になる。その後拘束部材16を取り外し、外層1と内層2が一体化した超硬合金複合ロール10を得る。必要に応じて超硬合金複合ロール10の所望箇所を機械加工し、熱間薄板圧延に好適な寸法形状とする。 When the outer layer member 11 and the inner layer member 12 are diffusion bonded, the outer layer member 11 becomes the outer layer 1 and the inner layer member 12 becomes the inner layer 2. Further, the carburized layer 13 of the inner layer member 12 becomes the C concentrated layer 3. Thereafter, the restraining member 16 is removed to obtain a cemented carbide composite roll 10 in which the outer layer 1 and the inner layer 2 are integrated. If necessary, a desired portion of the cemented carbide composite roll 10 is machined to obtain a dimension and shape suitable for hot sheet rolling.
(b) 熱間静水圧(HIP)法
 図6に示すように、円筒状HIP缶本体部20aに円筒状外層部材11を入れた後、円筒状外層部材11の内側に浸炭処理した鉄系合金製内層部材12を配置し、外層部材11の端面を覆うドーナツ板20b,20bを円筒状HIP缶本体部20aに溶接し、さらにドーナツ板20b,20bに内層部材12を覆うカップ部20c,20cを溶接し、得られたHIP缶内を減圧する。その後、HIP缶をHIP装置に入れ、HIP処理を行う。HIP温度は1100~1300℃が好ましく、HIP圧力は100~140 MPaが好ましい。
(b) Hot isostatic pressure (HIP) method As shown in FIG. 6, an iron-based alloy obtained by putting a cylindrical outer layer member 11 into a cylindrical HIP can body 20 a and then carburizing inside the cylindrical outer layer member 11. The inner layer member 12 is disposed, the donut plates 20b, 20b covering the end surface of the outer layer member 11 are welded to the cylindrical HIP can body 20a, and the cup portions 20c, 20c covering the inner layer member 12 are further attached to the donut plates 20b, 20b. Weld and depressurize the resulting HIP can. Then, the HIP can is put into the HIP device and the HIP process is performed. The HIP temperature is preferably 1100 to 1300 ° C., and the HIP pressure is preferably 100 to 140 MPa.
 HIPにより外層部材11と内層部材12は強固に接合し、外層部材11は外層1となり、内層部材12は内層2となる。また、内層部材12の浸炭層13はC濃化層3になる。冷却後、HIP缶20を機械加工により除去し、外層1と内層2が一体化した超硬合金複合ロール10を得る。この場合も、必要に応じて超硬合金複合ロール10の所望箇所を機械加工しても良い。なお、浸炭層13を設ける代わりに、外層部材11と内層部材12との隙間にC濃度が高い粉末を充填しても良い。このような高C濃度粉末として、WC50-Co50の超硬合金等が挙げられる。 The outer layer member 11 and the inner layer member 12 are firmly joined by HIP, the outer layer member 11 becomes the outer layer 1, and the inner layer member 12 becomes the inner layer 2. Further, the carburized layer 13 of the inner layer member 12 becomes the C concentrated layer 3. After cooling, the HIP can 20 is removed by machining to obtain a cemented carbide composite roll 10 in which the outer layer 1 and the inner layer 2 are integrated. Also in this case, a desired portion of the cemented carbide composite roll 10 may be machined as necessary. Instead of providing the carburized layer 13, the gap between the outer layer member 11 and the inner layer member 12 may be filled with a powder having a high C concentration. Examples of such high C concentration powder include WC 50 -Co 50 cemented carbide.
 本発明の以下の実施例によりさらに詳細に説明するが、本発明はそれらに限定されるものではない。 The present invention will be described in more detail with reference to the following examples, but the present invention is not limited thereto.
実施例1
 表1に示す組成を有する超硬合金を用いて、図7に示す外径20 mm及び厚さ20 mmの円柱状外層試験片31を作製した。また、表2に組成を有する鉄系合金を用いて、図7に示す外径30 mm及び厚さ10 mmの円板状内層試験片32を作製した。内層試験片32にガス浸炭処理を行い、目標深さが4 mmで、表面の目標C濃度が0.75~0.9質量%の浸炭層13を形成した。浸炭層13の表面から内部へのC濃度分布を図9に示す。C濃度の測定は、試験片32から微小サンプルを切り出し、炭素分析装置を用いて行った。測定の結果、浸炭層の厚さは約4 mmであり、C濃度の最大値(表面における濃度)は0.92質量%であった。浸炭層13の表層部を深さ0.2 mmまで機械加工により除去した。
Example 1
Using a cemented carbide having the composition shown in Table 1, a cylindrical outer layer test piece 31 having an outer diameter of 20 mm and a thickness of 20 mm shown in FIG. 7 was produced. Further, a disk-shaped inner layer test piece 32 having an outer diameter of 30 mm and a thickness of 10 mm shown in FIG. 7 was prepared using an iron-based alloy having the composition shown in Table 2. The inner layer test piece 32 was subjected to gas carburizing treatment to form a carburized layer 13 having a target depth of 4 mm and a target C concentration of 0.75 to 0.9% by mass on the surface. FIG. 9 shows the C concentration distribution from the surface to the inside of the carburized layer 13. The C concentration was measured by cutting out a small sample from the test piece 32 and using a carbon analyzer. As a result of the measurement, the thickness of the carburized layer was about 4 mm, and the maximum value of C concentration (concentration on the surface) was 0.92% by mass. The surface layer portion of the carburized layer 13 was removed by machining to a depth of 0.2 mm.
Figure JPOXMLDOC01-appb-T000001
注:(1) WC粒子の平均粒径は5μmであった。
 
Figure JPOXMLDOC01-appb-T000001
Notes: (1) The average particle size of the WC particles was 5 μm.
Figure JPOXMLDOC01-appb-T000002
Figure JPOXMLDOC01-appb-T000002
 外層試験片31及び内層試験片32を図7に示すように積み重ね、黒鉛製治具34に収めた後、真空中で上から加圧し、表3に示す条件で拡散接合し、接合試験片1~5を得た。各接合試験片1~5を切断し、接合界面を観察した。接合試験片4及び5については、接合境界から内層内部へのC濃度分布を調べた。結果を図10に示す。表3においてC濃化層とは、C濃度が0.6質量%以上の範囲のことを言う。 The outer layer test piece 31 and the inner layer test piece 32 are stacked as shown in FIG. 7, and after being placed in a graphite jig 34, they are pressurized from above in a vacuum, diffusion bonded under the conditions shown in Table 3, and bonded test pieces 1 ~ 5 was obtained. Each bonding test piece 1 to 5 was cut and the bonding interface was observed. For the bonding specimens 4 and 5, the C concentration distribution from the bonding boundary to the inner layer was examined. The results are shown in FIG. In Table 3, the C-concentrated layer means that the C concentration is in the range of 0.6% by mass or more.
Figure JPOXMLDOC01-appb-T000003
注:(1) 最表面のC濃度。
  (2) 外層との境界におけるC濃度。
 
Figure JPOXMLDOC01-appb-T000003
Note: (1) C concentration on the outermost surface.
(2) C concentration at the boundary with the outer layer.
 内層試験片32と外層試験片31の接合界面におけるη相については、接合試験片1~4では認められなかったが、接合試験片5では確認された。 The η phase at the bonding interface between the inner layer test piece 32 and the outer layer test piece 31 was not observed in the bonding test pieces 1 to 4, but was confirmed in the bonding test piece 5.
実施例2
 表1に示す組成を有する直径25 mm×長さ75 mmの外層試験片31’、及び表2に示す組成を有する直径25 mm×長さ75 mmの鉄系合金製内層試験片32’(実施例1と同じ条件で浸炭層13を形成した。)を作製した。外層試験片31’及び内層試験片32’を図7に示すように黒鉛製治具34に収めた後、真空中で治具34を上から加圧して、表4に示す条件で拡散接合を行い、接合試験片1’~5’を作製した。
Example 2
An outer layer test piece 31 ′ having a composition shown in Table 1 having a diameter of 25 mm × a length of 75 mm and an inner layer test piece 32 ′ made of an iron-based alloy having a composition shown in Table 2 having a diameter of 25 mm × a length of 75 mm (implemented) A carburized layer 13 was formed under the same conditions as in Example 1.). After placing the outer layer test piece 31 ′ and the inner layer test piece 32 ′ in the graphite jig 34 as shown in FIG. 7, the jig 34 is pressed from above in vacuum, and diffusion bonding is performed under the conditions shown in Table 4. The test specimens 1 ′ to 5 ′ were prepared.
 各接合試験片1’~5’から、図8に示す形状の引張試験片40(外層試験片部41及び内層試験片部42からなり、標点間の中央に境界を有する。)を作製した。外層試験片部41は外層試験片31’から形成し、内層試験片部42は内層試験片32’から形成した。引張試験片40の直径は6.3 mmで、標点距離は19 mmであった。 A tensile test piece 40 having a shape shown in FIG. 8 (consisting of an outer layer test piece part 41 and an inner layer test piece part 42 having a boundary in the center between the gauge points) was prepared from each of the joining test pieces 1 ′ to 5 ′. . The outer layer test piece portion 41 was formed from the outer layer test piece 31 ', and the inner layer test piece portion 42 was formed from the inner layer test piece 32'. The diameter of the tensile test piece 40 was 6.3 mm, and the gauge distance was 19 mm.
 得られた各引張試験片1~5(接合試験片1’~5’に相当する)に対して、引張試験により接合境界の引張強度を測定した。結果を表4に示す。表4から明らかなように、外層試験片部41と内層試験片部42との接合境界の引張強度は、引張試験片1~4では600 MPa以上であったが、引張試験片5では530 MPaと低かった。これは、接合試験片5’では接合界面にη相が形成されたためであると考えられる。 For each of the obtained tensile test pieces 1 to 5 (corresponding to the joining test pieces 1 'to 5'), the tensile strength at the joining boundary was measured by a tensile test. The results are shown in Table 4. As is apparent from Table 4, the tensile strength at the boundary between the outer layer test piece portion 41 and the inner layer test piece portion 42 was 600 MPa or more for the tensile test pieces 1 to 4, but 530 MPa for the tensile test piece 5 It was low. This is considered to be because the η phase was formed at the bonding interface in the bonding test piece 5 '.
Figure JPOXMLDOC01-appb-T000004
Figure JPOXMLDOC01-appb-T000004
実施例3
 表2に示す組成を有する鉄系合金を用いて、外径276 mm及び全長1930 mmのロール軸状の内層部材12を作製した。内層部材12の表面に目標厚さ4 mm及び目標C濃度0.75~0.9質量%の浸炭層13をガス浸炭法により形成した。内層部材12の端部から試験片を採取し、浸炭層13の深さ方向にC濃度を測定した結果、図9と同様のC濃度分布であることが分った。その後、浸炭層13を深さ0.5 mmだけ機械加工により除去した。
Example 3
Using a ferrous alloy having the composition shown in Table 2, a roll shaft-shaped inner layer member 12 having an outer diameter of 276 mm and a total length of 1930 mm was produced. A carburized layer 13 having a target thickness of 4 mm and a target C concentration of 0.75 to 0.9% by mass was formed on the surface of the inner layer member 12 by a gas carburizing method. A test piece was collected from the end of the inner layer member 12, and the C concentration was measured in the depth direction of the carburized layer 13. As a result, it was found that the C concentration distribution was the same as in FIG. Thereafter, the carburized layer 13 was removed by machining by a depth of 0.5 mm.
 また、表1に示す組成を有する超硬合金を用いて、外径364 mm、内径276 mm及び全長680 mmの中空円筒状外層部材11を作製した。さらに、外径600 mm、内径365.5 mm及び全長800 mmの黒鉛製中空円筒状拘束部材16を作製した。 Further, a hollow cylindrical outer layer member 11 having an outer diameter of 364 mm, an inner diameter of 276 mm, and a total length of 680 mm was manufactured using a cemented carbide having the composition shown in Table 1. Further, a graphite hollow cylindrical restraining member 16 having an outer diameter of 600 mm, an inner diameter of 365.5 mm, and a total length of 800 mm was produced.
 図4に示すように、浸炭層13を形成した内層部材12を黒鉛製基台8の上に配置し、内層部材12の外周に間隙G1(=1.0 mm)で外層部材11を配置し、外層部材11の外周に間隙G2(=1.5 mm)で拘束部材16を配置した。この配置で真空炉の中に入れ、1250℃の温度に60分間保持して拡散接合を行い、超硬合金複合ロール10を作製した。 As shown in FIG. 4, the inner layer member 12 on which the carburized layer 13 is formed is disposed on the graphite base 8, and the outer layer member 11 is disposed on the outer periphery of the inner layer member 12 with a gap G 1 (= 1.0 mm). A restraining member 16 was disposed on the outer periphery of the outer layer member 11 with a gap G 2 (= 1.5 mm). In this arrangement, it was placed in a vacuum furnace and held at 1250 ° C. for 60 minutes for diffusion bonding to produce a cemented carbide composite roll 10.
 超硬合金複合ロール10中の外層1及び内層2の端部を目視検査し、かつ接合面全域を浸透探傷検査した。その結果、接合面全域にわたって境界の欠陥は観察されなかった。また、外層1と内層2の剥離も認められなかった。 The end portions of the outer layer 1 and the inner layer 2 in the cemented carbide composite roll 10 were visually inspected, and the entire bonding surface was inspected. As a result, no boundary defect was observed over the entire bonding surface. Further, no peeling between the outer layer 1 and the inner layer 2 was observed.
1:外層
2:内層
3:C濃化層
8:基台
9:受台
10:超硬合金複合ロール
11:外層部材
12:内層部材
13:浸炭層
16:拘束部材
20:HIP缶
31:外層試験片
32:内層試験片
34:黒鉛製治具
61~66:拘束部材用リング部材
L1:外層部材の長さ
L2:内層部材の長さ
L3:拘束部材の長さ
D:外層部材の各端部から延びる拘束部材の長さ
T1:外層部材の厚さ
T2:内層部材の直径
T3:拘束部材の厚さ
G1:外層部材と内層部材との間隙
G2:外層部材と拘束部材との間隙
1: Outer layer
2: Inner layer
3: C thickened layer
8: Base
9: cradle
10: Cemented carbide composite roll
11: Outer layer member
12: Inner layer member
13: Carburized layer
16: Restraint member
20: HIP can
31: Outer layer specimen
32: Inner layer specimen
34: Graphite jig
61-66: Ring member for restraint member
L 1 : Length of outer layer member
L 2 : Length of inner layer member
L 3 : Length of restraint member
D: Length of the restraining member extending from each end of the outer layer member
T 1 : Thickness of outer layer member
T 2 : Diameter of inner layer member
T 3 : Thickness of restraining member
G 1 : Gap between the outer layer member and the inner layer member
G 2 : Gap between the outer layer member and the restraining member

Claims (17)

  1. 超硬合金製外層と鉄系合金製内層とが拡散接合した超硬合金複合ロールにおいて、前記外層との接合境界に隣接する前記内層の表層域に、前記内層本体よりC濃度が高い鉄系合金からなるC濃化層を有することを特徴とする超硬合金複合ロール。 In a cemented carbide composite roll in which a cemented carbide outer layer and an iron-based alloy inner layer are diffusion-bonded, an iron-based alloy having a C concentration higher than that of the inner layer main body in a surface layer region of the inner layer adjacent to a bonding boundary with the outer layer A cemented carbide composite roll having a C-concentrated layer made of
  2. 請求項1に記載の超硬合金複合ロールにおいて、前記C濃化層の厚さが0.5~6 mmであることを特徴とする超硬合金複合ロール。 2. The cemented carbide composite roll according to claim 1, wherein the C concentrated layer has a thickness of 0.5 to 6 mm.
  3. 請求項1又は2に記載の超硬合金複合ロールにおいて、前記C濃化層の前記接合境界におけるC濃度が0.7~1.2質量%であることを特徴とする超硬合金複合ロール。 3. The cemented carbide composite roll according to claim 1, wherein the C concentration at the joining boundary of the C concentrated layer is 0.7 to 1.2% by mass.
  4. 請求項1~3のいずれかに記載の超硬合金複合ロールにおいて、前記C濃化層内におけるC濃度が前記接合境界から前記内層本体に向けて徐々に減少していることを特徴とする超硬合金複合ロール。 The cemented carbide composite roll according to any one of claims 1 to 3, wherein the C concentration in the C concentrated layer gradually decreases from the joining boundary toward the inner layer main body. Hard alloy composite roll.
  5. 請求項4に記載の超硬合金複合ロールにおいて、前記C濃化層内の深さ方向のC濃度の減少率が0.01%/mm以上であることを特徴とする超硬合金複合ロール。 5. The cemented carbide composite roll according to claim 4, wherein a reduction rate of the C concentration in the depth direction in the C concentrated layer is 0.01% / mm or more.
  6. 請求項1~5のいずれかに記載の超硬合金複合ロールにおいて、前記外層と前記内層との境界の引張強度が600 MPa以上であることを特徴とする超硬合金複合ロール。 6. The cemented carbide composite roll according to claim 1, wherein a tensile strength at a boundary between the outer layer and the inner layer is 600 層 MPa or more.
  7. 請求項1~6のいずれかに記載の超硬合金複合ロールにおいて、前記超硬合金製外層が70~88質量%のWC粒子を含有することを特徴とする超硬合金複合ロール。 7. The cemented carbide composite roll according to claim 1, wherein the cemented carbide outer layer contains 70 to 88% by mass of WC particles.
  8. 請求項1~7のいずれかに記載の超硬合金複合ロールにおいて、前記鉄系合金製内層本体のC濃度が0.2~0.5質量%であることを特徴とする超硬合金複合ロール。 8. The cemented carbide composite roll according to claim 1, wherein the iron-based alloy inner layer body has a C concentration of 0.2 to 0.5 mass%.
  9. 請求項1~8のいずれかに記載の超硬合金複合ロールにおいて、前記鉄系合金製内層がCr、Ni、Mo、V、W、Ti及びNbからなる群から選ばれた少なくとも一種を合計で1.0質量%以上含有することを特徴とする超硬合金複合ロール。 The cemented carbide composite roll according to any one of claims 1 to 8, wherein the iron-based alloy inner layer includes at least one selected from the group consisting of Cr, Ni, Mo, V, W, Ti and Nb in total. A cemented carbide composite roll containing 1.0% by mass or more.
  10. 超硬合金からなる円筒状外層部材と鉄系合金からなる内層部材とが接合した超硬合金複合ロールを製造する方法において、前記内層部材の外面に浸炭処理を施した後に、前記外層部材と前記内層部材を拡散接合することを特徴とする方法。 In a method of manufacturing a cemented carbide composite roll in which a cylindrical outer layer member made of cemented carbide and an inner layer member made of an iron-based alloy are joined, after carburizing the outer surface of the inner layer member, the outer layer member and the A method comprising diffusion bonding an inner layer member.
  11. 請求項10に記載の超硬合金複合ロールの製造方法において、前記浸炭処理により形成された浸炭層の厚さが0.5~10 mmであることを特徴とする方法。 11. The method for producing a cemented carbide composite roll according to claim 10, wherein a thickness of the carburized layer formed by the carburizing treatment is 0.5 to 10 mm.
  12. 請求項10又は11に記載の超硬合金複合ロールの製造方法において、前記浸炭処理をガス浸炭処理法により行うことを特徴とする方法。 12. The method for producing a cemented carbide composite roll according to claim 10, wherein the carburizing treatment is performed by a gas carburizing treatment method.
  13. 請求項10~12のいずれかに記載の超硬合金複合ロールの製造方法において、
     前記外層部材の内側に前記内層部材を配置し、
     前記外層部材の外側に、室温から接合温度までの温度範囲において前記外層部材より熱膨張率が小さい中空円筒状の拘束部材を配置し、
     加熱により最も熱膨張した前記内層部材の外面が前記外層部材の内面を押圧するとともに、最も熱膨張しない前記拘束部材の内面が前記外層部材の外面を押圧するように、前記外層部材と前記内層部材及び前記拘束部材との間隙を設定し、
     加熱により前記外層部材の内面と前記内層部材の外面とを密接させ、もって前記外層部材と前記内層部材とを拡散接合することを特徴とする方法。
    The method for producing a cemented carbide composite roll according to any one of claims 10 to 12,
    Arranging the inner layer member inside the outer layer member,
    A hollow cylindrical restraining member having a smaller coefficient of thermal expansion than the outer layer member in a temperature range from room temperature to a bonding temperature is disposed outside the outer layer member,
    The outer layer member and the inner layer member are configured such that the outer surface of the inner layer member that is most thermally expanded by heating presses the inner surface of the outer layer member, and the inner surface of the restraining member that is not thermally expanded presses the outer surface of the outer layer member. And setting a gap with the restraining member,
    A method wherein the inner surface of the outer layer member and the outer surface of the inner layer member are brought into close contact with each other by heating, whereby the outer layer member and the inner layer member are diffusion bonded.
  14. 請求項13に記載の超硬合金複合ロールの製造方法において、前記拘束部材の軸線方向両端部が前記外層部材の軸線方向両端面より突出していることを特徴とする方法。 14. The method for producing a cemented carbide composite roll according to claim 13, wherein both end portions in the axial direction of the restraining member protrude from both end surfaces in the axial direction of the outer layer member.
  15. 請求項13又は14に記載の超硬合金複合ロールの製造方法において、前記拘束部材が前記外層部材より厚いことを特徴とする方法。 15. The method for producing a cemented carbide composite roll according to claim 13, wherein the restraining member is thicker than the outer layer member.
  16. 請求項13~15のいずれかに記載の超硬合金複合ロールの製造方法において、前記拘束部材が黒鉛又はセラミックスからなることを特徴とする方法。 16. The method for producing a cemented carbide composite roll according to claim 13, wherein the restraining member is made of graphite or ceramics.
  17. 請求項13~16のいずれかに記載の超硬合金複合ロールの製造方法において、前記拘束部材と前記外層部材との間に反応防止材を介在させることを特徴とする方法。 The method for producing a cemented carbide composite roll according to any one of claims 13 to 16, wherein a reaction preventing material is interposed between the restraining member and the outer layer member.
PCT/JP2014/076214 2013-10-09 2014-09-30 Superhard alloy composite roll and production method therefor WO2015053137A1 (en)

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5838683A (en) * 1982-07-05 1983-03-07 Sumitomo Electric Ind Ltd Manufacture of composite abrasion resistance member
JPH105825A (en) * 1996-06-19 1998-01-13 Hitachi Metals Ltd Composite roll made of sintered hard alloy
JP2002224715A (en) * 2001-02-05 2002-08-13 Kawasaki Steel Corp Method for rolling thick steel plate
JP2003275809A (en) * 2002-03-18 2003-09-30 Hitachi Metals Ltd Composite roll for rolling

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006181628A (en) * 2004-12-28 2006-07-13 Jfe Steel Kk Method for rolling thick steel plate and method for producing thick steel plate

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5838683A (en) * 1982-07-05 1983-03-07 Sumitomo Electric Ind Ltd Manufacture of composite abrasion resistance member
JPH105825A (en) * 1996-06-19 1998-01-13 Hitachi Metals Ltd Composite roll made of sintered hard alloy
JP2002224715A (en) * 2001-02-05 2002-08-13 Kawasaki Steel Corp Method for rolling thick steel plate
JP2003275809A (en) * 2002-03-18 2003-09-30 Hitachi Metals Ltd Composite roll for rolling

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