WO2023166900A1 - 超硬合金およびこれを用いた被覆工具、切削工具 - Google Patents

超硬合金およびこれを用いた被覆工具、切削工具 Download PDF

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Publication number
WO2023166900A1
WO2023166900A1 PCT/JP2023/003136 JP2023003136W WO2023166900A1 WO 2023166900 A1 WO2023166900 A1 WO 2023166900A1 JP 2023003136 W JP2023003136 W JP 2023003136W WO 2023166900 A1 WO2023166900 A1 WO 2023166900A1
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WIPO (PCT)
Prior art keywords
cemented carbide
phase
aggregated
coated tool
layer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
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PCT/JP2023/003136
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English (en)
French (fr)
Japanese (ja)
Inventor
匠 橋本
博俊 伊藤
尚久 松田
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Kyocera Corp
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Kyocera Corp
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Priority to KR1020247026890A priority Critical patent/KR20240134957A/ko
Priority to US18/840,495 priority patent/US20250387838A1/en
Priority to JP2024504407A priority patent/JP7851394B2/ja
Priority to CN202380021031.2A priority patent/CN118786233A/zh
Priority to DE112023001249.0T priority patent/DE112023001249T5/de
Publication of WO2023166900A1 publication Critical patent/WO2023166900A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23B—TURNING; BORING
    • B23B27/00—Tools for turning or boring machines; Tools of a similar kind in general; Accessories therefor
    • B23B27/14—Cutting tools of which the bits or tips or cutting inserts are of special material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23B—TURNING; BORING
    • B23B27/00—Tools for turning or boring machines; Tools of a similar kind in general; Accessories therefor
    • B23B27/14—Cutting tools of which the bits or tips or cutting inserts are of special material
    • B23B27/148—Composition of the cutting inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24—After-treatment of workpieces or articles
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/04—Making non-ferrous alloys by powder metallurgy
    • C22C1/05—Mixtures of metal powder with non-metallic powder
    • C22C1/051—Making hard metals based on borides, carbides, nitrides, oxides or silicides; Preparation of the powder mixture used as the starting material therefor
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
    • C22C29/06—Alloys 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
    • C22C29/08—Alloys 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
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
    • C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
    • C23C16/34—Nitrides
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
    • C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
    • C23C16/36—Carbonitrides
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
    • C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
    • C23C16/40—Oxides
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
    • C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
    • C23C16/40—Oxides
    • C23C16/403—Oxides of aluminium, magnesium or beryllium
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/04—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material
    • C23C28/042—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material including a refractory ceramic layer, e.g. refractory metal oxides, ZrO2, rare earth oxides
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/04—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material
    • C23C28/044—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material coatings specially adapted for cutting tools or wear applications
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • C23C30/005—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process on hard metal substrates
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24—After-treatment of workpieces or articles
    • B22F2003/241—Chemical after-treatment on the surface
    • B22F2003/242—Coating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F2005/001—Cutting tools, earth boring or grinding tool other than table ware
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23B—TURNING; BORING
    • B23B2224/00—Materials of tools or workpieces composed of a compound including a metal
    • B23B2224/04—Aluminium oxide
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23B—TURNING; BORING
    • B23B2224/00—Materials of tools or workpieces composed of a compound including a metal
    • B23B2224/32—Titanium carbide nitride (TiCN)
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23B—TURNING; BORING
    • B23B2224/00—Materials of tools or workpieces composed of a compound including a metal
    • B23B2224/36—Titanium nitride
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23B—TURNING; BORING
    • B23B2228/00—Properties of materials of tools or workpieces, materials of tools or workpieces applied in a specific manner
    • B23B2228/10—Coatings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23B—TURNING; BORING
    • B23B2228/00—Properties of materials of tools or workpieces, materials of tools or workpieces applied in a specific manner
    • B23B2228/36—Multi-layered

Definitions

  • the present disclosure relates to cemented carbide and coated tools and cutting tools using the same.
  • Cemented carbide containing WC (tungsten carbide) as a hard phase is used for substrates of coated tools and the like, and is used for cutting tools such as end mills.
  • ZrO 2 phase zirconia phase
  • ZrC 2 phase is scattered on the surface of a substrate made of a cemented carbide, thereby forming a coating layer due to the difference in thermal expansion between the substrate and the coating layer. It is described that the peeling of can be suppressed.
  • a non-limiting aspect of the present disclosure is a cemented carbide containing a hard phase containing W and C, a binder phase consisting of one or more iron group metals, Zr and Nb, and having an atomic ratio of Nb/(Zr+Nb ) of less than 0.38 and a cohesive phase.
  • a non-limiting one-sided coated tool of the present disclosure has the above cemented carbide and a coating layer located on the surface of the cemented carbide.
  • a non-limiting one-sided cutting tool of the present disclosure includes a holder extending from a first end toward a second end and having a pocket on the first end side, and the above-described coated tool located in the pocket.
  • FIG. 1 is a schematic diagram illustrating a cross-section of a non-limiting aspect of a cemented carbide of the present disclosure
  • FIG. 1 is a perspective view of a non-limiting one-sided coated tool of the present disclosure
  • FIG. 1 is a cross-sectional view near the surface of a non-limiting one-sided coated tool of the present disclosure
  • FIG. 1 is a cross-sectional view near the surface of a non-limiting one-sided coated tool of the present disclosure
  • FIG. 1 is a perspective view of a non-limiting one-sided cutting tool of the present disclosure
  • FIG. 1 is a schematic diagram illustrating a cross-section of a non-limiting aspect of a cemented carbide of the present disclosure
  • FIG. 1 is a perspective view of a non-limiting one-sided coated tool of the present disclosure
  • FIG. 1 is a cross-sectional view near the surface of a non-limiting one-sided coated tool of the present disclosure
  • FIG. 1 is a perspective view of a non-limiting one-
  • cemented carbide 1 of the present disclosure
  • the cemented carbide 1 may comprise any constituent members not shown in the referenced figures.
  • the dimensions of the members in the drawings do not faithfully represent the actual dimensions of the constituent members, the dimensional ratios of the respective members, and the like. These points are the same for a coated tool and a cutting tool to be described later.
  • the cemented carbide 1 may contain a hard phase 3, a binder phase 5 and an aggregation phase 7, as in a non-limiting example shown in FIG.
  • the hard phase 3 may contain W (tungsten) and C (carbon). In other words, the hard phase 3 may contain WC.
  • the hard phase 3 may contain WC as a main component. "Main component” may mean the component that has the highest mass % value compared to the other components.
  • the binding phase 5 may consist of one or more iron group metals such as Co (cobalt) and Ni (nickel).
  • the binder phase 5 may consist of at least one of Co and Ni.
  • the binder phase 5 can function as a phase that binds adjacent hard phases 3 together.
  • the binder phase 5 may consist solely of iron group metals or may contain some additives and/or impurities. Specifically, the binder phase 5 only needs to contain 95% by mass or more of the iron group metal, and may contain 5% by mass or less of additives and/or impurities.
  • the aggregation phase 7 can also be called the so-called ⁇ phase.
  • the aggregated phase 7 can function as a phase that imparts heat resistance to the cemented carbide 1 .
  • the aggregation phase 7 may contain Zr (zirconium) and Nb (niobium). That is, the aggregated phase 7 may be a phase in which at least Zr and Nb are aggregated.
  • the aggregated phase 7 may also have an atomic ratio of Nb/(Zr+Nb) of less than 0.38. In the aggregated phase 7, when Zr is present in a larger amount than Nb at such a ratio, the heat resistance of the cemented carbide 1 is likely to be improved. Therefore, the cemented carbide 1 has high heat resistance.
  • the lower limit of Nb/(Zr+Nb) in atomic ratio may be greater than zero. Specifically, this lower limit may be 0.02.
  • Nb is a component that is intentionally added for the purpose of improving heat resistance.
  • the atomic ratio of Nb/(Zr+Nb) may be an average value.
  • the aggregation phase 7 may contain Zr at a rate of 1 to 10 atomic % (at %). Also, the aggregation phase 7 may contain Nb in a proportion of 0.5 to 3 atomic %.
  • the aggregation phase 7 may further contain C, Ti (titanium), Co, Ta (tantalum), W, etc. in addition to Zr and Nb.
  • the aggregation phase 7 may have the highest C content ratio in terms of atomic ratio.
  • Elemental analysis for calculating atomic ratios may be performed, for example, by Energy Dispersive X-ray Spectroscopy (EDS). Elemental analysis may be performed by cross-sectional observation using an EDS attached to an electron microscope. Electron microscopes can include, for example, Scanning Electron Microscopy (SEM) and Transmission Electron Microscopy (TEM).
  • the aggregated phase 7 may contain the first aggregated phase 9.
  • the first aggregated phase 9 may have an atomic ratio of Nb/(Zr+Nb) of 0.25 or less. In this case, the heat resistance of the cemented carbide 1 is likely to be improved.
  • the first aggregated phase 9 may have an atomic ratio of Nb/(Zr+Nb) of 0.2 or less. In this case, an improvement in heat resistance can be expected. Moreover, if it is in the form of a coated tool, wear resistance is likely to be improved.
  • the first aggregated phase 9 may have an atomic ratio of Nb/(Zr+Nb) of 0.05 or more.
  • the aggregated phase 7 may further contain the second aggregated phase 11 and the third aggregated phase 13 .
  • the second aggregated phase 11 may have an atomic ratio of Nb/(Zr+Nb) greater than 0.3 and less than or equal to 0.34.
  • the third aggregated phase 13 may have an atomic ratio of Nb/(Zr+Nb) greater than 0.34 and less than 0.38. In these cases, the heat resistance of the cemented carbide 1 is likely to be improved.
  • the average particle size of the first aggregated phase 9 may be smaller than the average particle size of the second aggregated phase 11 and the average particle size of the third aggregated phase 13 . In this case, the heat resistance of the cemented carbide 1 is likely to be improved.
  • the average particle size of the third aggregated phase 13 may be smaller than the average particle size of the second aggregated phase 11. In this case, the heat resistance of the cemented carbide 1 is likely to be improved.
  • the average particle size of the second aggregated phase 11 may be larger than the average particle size of the first aggregated phase 9 and the average particle size of the third aggregated phase 13 . In this case, the heat resistance of the cemented carbide 1 is likely to be improved.
  • the average particle size of the first aggregated phase 9 is not limited to a specific size. This point is the same for the average particle size of the second aggregated phase 11 and the average particle size of the third aggregated phase 13 .
  • the average particle size of the first aggregated phase 9 may be 0.5-4 ⁇ m.
  • the average particle size of the second aggregated phase 11 may be 1.5-5 ⁇ m.
  • the average particle size of the third aggregated phase 13 may be 1-4.5 ⁇ m.
  • the measurement of the average particle size of the first aggregated phase 9 may be performed by image analysis.
  • the equivalent circle diameter may be the average particle diameter of the first aggregated phase 9 .
  • the measurement of the average particle size of the first aggregated phase 9 may be performed by the following procedure. First, a SEM image may be obtained by observing a cross section of the cemented carbide 1 at a magnification of 3000 to 5000 times. At least 50 or more first aggregation phases 9 in this SEM image may be specified and extracted. After that, the average particle size of the first aggregated phase 9 may be obtained by calculating the equivalent circle diameter using image analysis software ImageJ (1.52). The average particle size of the second aggregated phase 11 and the average particle size of the third aggregated phase 13 may be measured in the same procedure as the average particle size of the first aggregated phase 9 .
  • WC powder, Co powder, TiC powder, ZrC powder, NbC powder, TaC powder, and the like may be prepared as raw material powders.
  • the ratio of Co powder may be 4 to 15% by mass (wt%).
  • the proportion of TiC powder may be between 0.5 and 5% by weight.
  • the proportion of ZrC powder may be 0.2-5% by weight.
  • the proportion of NbC powder may be between 0.1 and 3% by weight.
  • the proportion of TaC powder may be 0.1 to 5% by weight.
  • the remainder may be WC powder.
  • the proportion of ZrC powder may be set higher than the proportion of NbC powder.
  • the average particle size of the raw material powder may be appropriately selected within the range of 0.1 to 10 ⁇ m.
  • the average particle size of the raw material powder may be a value measured by the Microtrac method.
  • a compact may be obtained by mixing and molding prepared raw material powders.
  • Forming methods may include, for example, press molding, casting, extrusion, and cold isostatic pressing.
  • the obtained compact may be subjected to binder removal treatment and then fired. Firing may be performed in a non-oxidizing atmosphere such as vacuum, argon atmosphere and nitrogen atmosphere.
  • the firing temperature may be 1450-1600°C.
  • the firing time may be 0.5-3 hours.
  • the cemented carbide 1 may be obtained by cooling after firing.
  • the cooling process may be provided with a condition that the temperature is kept in the range of 900 to 1400° C. for 0.25 to 2 hours. If such a keep (keeping temperature and keeping time) is provided in the cooling process, the aggregated phase 7 having an atomic ratio of Nb/(Zr+Nb) of less than 0.38 is likely to be formed. Also, the aggregated phase 7 containing the first aggregated phase 9, the second aggregated phase 11 and the third aggregated phase 13 is likely to be formed.
  • the above manufacturing method is an example of a method for manufacturing the cemented carbide 1. Therefore, it goes without saying that the cemented carbide 1 is not limited to those produced by the above manufacturing method.
  • the coated tool 101 may have a cemented carbide 1 and a coating layer 103 located on the surface 15 of the cemented carbide 1, as in one non-limiting example shown in FIGS.
  • the coated tool 101 may have cemented carbide 1 as a substrate.
  • the cemented carbide 1 since the heat resistance of the cemented carbide 1 is high, wear due to heat is suppressed. Therefore, the cemented carbide 1 (substrate) has high wear resistance, and combined with the wear resistance of the coating layer 103, the durability of the coated tool 101 is high.
  • the coating layer 103 may be positioned over the entire surface 15 of the cemented carbide 1, or may be positioned only partially. That is, the coating layer 103 may be located on at least part of the surface 15 of the cemented carbide 1 .
  • the coating layer 103 may be deposited by a chemical vapor deposition (CVD) method.
  • the covering layer 103 may be a CVD film.
  • the coating layer 103 may be a PVD film formed by a physical vapor deposition (PVD) method.
  • the covering layer 103 may have a single-layer structure, or may have a structure in which a plurality of layers are laminated.
  • the composition of the coating layer 103 may include, for example, TiCN (titanium carbonitride), Al 2 O 3 (alumina), and TiN (titanium nitride).
  • the coating layer 103 may have a TiCN layer 105 and an Al 2 O 3 layer 107 in order from the cemented carbide 1 side, as a non-limiting example shown in FIG.
  • the TiCN layer 105 may contact the cemented carbide 1 .
  • Al 2 O 3 layer 107 may contact TiCN layer 105 .
  • the coating layer 103 may have a TiN layer 109, a TiCN layer 105 and an Al 2 O 3 layer 107 in order from the cemented carbide 1, as in a non-limiting example shown in FIG.
  • the TiN layer 109 may contact the cemented carbide 1 .
  • TiCN layer 105 may contact TiN layer 109 .
  • Al 2 O 3 layer 107 may contact TiCN layer 105 .
  • the covering layer 103 is not limited to a specific thickness.
  • the thickness of the TiCN layer 105 may be set to approximately 1 to 15 ⁇ m.
  • the thickness of the Al 2 O 3 layer 107 may be set to approximately 1 to 15 ⁇ m.
  • the thickness of the TiN layer 109 may be set to approximately 0.1 to 5 ⁇ m.
  • the thickness of the coating layer 103 may be measured by cross-sectional observation using an electron microscope.
  • the thickness of the coating layer 103 may be an average value.
  • the thickness may be measured at 10 or more measurement points at intervals of 1 ⁇ m over a width of 10 ⁇ m or more at any position on each layer, and the average value thereof may be calculated.
  • FIG. 2 shows a cutting insert as a non-limiting example of the coated tool 101.
  • the coated tool 101 is not limited to a cutting insert.
  • the coated tool 101 includes a first surface 111 (upper surface), a second surface 113 (side surface) adjacent to the first surface 111, and cuts positioned on at least a part of the ridge between the first surface 111 and the second surface 113. and a blade 115 .
  • the first surface 111 may be a rake surface.
  • the entire surface of the first surface 111 may be a rake face, or a part thereof may be a rake face.
  • the region of the first surface 111 along the cutting edge 115 may be a rake face.
  • the second surface 113 may be a flank surface.
  • the second surface 113 may be entirely a flank surface, or a part thereof may be a flank surface.
  • the area of the second surface 113 along the cutting edge 115 may be a flank.
  • the cutting edge 115 may be positioned on a part of the ridge line, or may be positioned on the entire ridge line.
  • the cutting edge 115 can be used for cutting a work material.
  • the coated tool 101 may have through holes 117 .
  • the through-holes 117 can be used to attach fixing screws, clamping members, or the like when holding the coated tool 101 to the holder.
  • the through hole 117 may be formed from the first surface 111 to a surface (lower surface) located on the opposite side of the first surface 111, or may be opened on these surfaces. It should be noted that there is no problem even if the through-holes 117 are configured so as to open in mutually opposing regions on the second surface 113 .
  • the coated tool 101 may have a rectangular plate shape. Note that the shape of the coated tool 101 is not limited to a rectangular plate shape.
  • first surface 111 may be triangular, pentagonal, hexagonal, or circular.
  • the coated tool 101 is not limited to a specific size.
  • the length of one side of the first surface 111 may be set to approximately 3 to 20 mm.
  • the height from the first surface 111 to the surface (lower surface) located on the opposite side of the first surface 111 may be set to approximately 5 to 20 mm.
  • the coated tool 101 may be obtained by forming a coating layer 103 on the surface 15 of the cemented carbide 1 by CVD.
  • the TiCN layer 105 may be deposited as follows. First, as the reaction gas composition, 0.1 to 10% by volume of titanium tetrachloride (TiCl 4 ) gas, 10 to 60% by volume of nitrogen (N 2 ) gas, and 0.1 to 15% by volume of methane (CH 4 ) gas. % and the rest being hydrogen (H 2 ) gas. Then, the TiCN layer 105 may be formed by introducing this mixed gas into the chamber, setting the temperature to 800 to 1100° C. and the pressure to 5 to 30 kPa.
  • TiCl 4 titanium tetrachloride
  • N 2 nitrogen
  • CH 4 methane
  • H 2 hydrogen
  • the Al 2 O 3 layer 107 may be deposited as follows. First, as the reaction gas composition, 0.5 to 5% by volume of aluminum trichloride (AlCl 3 ) gas, 0.5 to 3.5% by volume of hydrogen chloride (HCl) gas, and 0% of carbon dioxide (CO 2 ) gas. A mixed gas containing 0.5% by volume or less of hydrogen sulfide (H 2 S) gas and the balance of hydrogen (H 2 ) gas may be prepared. Then, this mixed gas is introduced into the chamber, and the temperature is set to 930 to 1010° C. and the pressure is set to 5 to 10 kPa to form the Al 2 O 3 layer 107 .
  • AlCl 3 aluminum trichloride
  • HCl hydrogen chloride
  • CO 2 carbon dioxide
  • the TiN layer 109 may be deposited as follows. First, as a reaction gas composition, a mixed gas composed of 0.1 to 10% by volume of titanium tetrachloride (TiCl 4 ) gas, 10 to 60% by volume of nitrogen (N 2 ) gas, and the balance of hydrogen (H 2 ) gas was used. may be adjusted. Then, the TiN layer 109 may be formed by introducing this mixed gas into the chamber, setting the temperature to 800 to 1010° C. and the pressure to 10 to 85 kPa.
  • TiCl 4 titanium tetrachloride
  • N 2 nitrogen
  • H 2 hydrogen
  • the manufacturing method described above is an example of a method for manufacturing the coated tool 101. Therefore, it cannot be overemphasized that the coated tool 101 is not limited to what was produced by said manufacturing method.
  • a cutting tool 201 extends from a first end 203a toward a second end 203b and has a pocket 205 on the side of the first end 203a, and a holder 203 located in the pocket 205, as in one non-limiting example shown in FIG.
  • a coated tool 101 may be provided. When the cutting tool 201 is provided with the coated tool 101, stable cutting is possible because the coated tool 101 has high durability.
  • the pocket 205 may be a portion to which the covered tool 101 is attached.
  • the pocket 205 may be open on the outer peripheral surface of the holder 203 and the end surface on the side of the first end 203a.
  • the covered tool 101 may be attached to the pocket 205 so that the cutting edge 115 protrudes outward from the holder 203 .
  • Shielded tool 101 may also be attached to pocket 205 by set screw 207 . That is, by inserting the fixing screw 207 into the through-hole 117 of the coated tool 101, inserting the tip of the fixing screw 207 into the screw hole formed in the pocket 205, and screwing the threaded portions together, the coated tool 101 can be secured. It may be attached to pocket 205 . At this time, the lower surface of the covering tool 101 may directly contact the pocket 205 , or a sheet may be sandwiched between the covering tool 101 and the pocket 205 .
  • Examples of materials for the holder 203 include steel and cast iron. When the material of the holder 203 is steel, the toughness of the holder 203 is high.
  • FIG. 5 illustrates a cutting tool 201 used for so-called turning.
  • Turning operations may include, for example, internal diameter machining, external diameter machining, grooving, and the like.
  • the application of the cutting tool 201 is not limited to turning. For example, there is no problem even if the cutting tool 201 is used for milling.
  • the cemented carbide 1, the coated tool 101, and the cutting tool 201 which are not limited to the present disclosure, have been exemplified, but the present disclosure is not limited to the above-described embodiments, and can be arbitrary as long as it does not deviate from the gist of the present disclosure. It goes without saying that it is possible.
  • cemented carbide 1 is used for the coated tool 101 and the cutting tool 201 has been described as an example, but the cemented carbide 1 can be applied to other uses.
  • Other applications may include, for example, wear-resistant parts such as sliding parts and molds, tools such as drilling tools and knives, and shock-resistant parts.
  • raw material powders were mixed so that the composition of the agglomerated phase in the sintered body became the composition shown in Table 1, and press-molded into a cutting tool shape (CNMG120408) to obtain a molded body.
  • the obtained compact was subjected to a binder removal treatment, and then fired at a temperature of 1450 to 1600° C. for 0.5 to 2 hours. After sintering, the sintered body was cooled under the cooling conditions shown in Table 2 to obtain a cemented carbide composed of a sintered body containing an agglomerated phase having the composition shown in Table 1.
  • Elemental analysis was performed with EDS. Specifically, cross-sectional observation was performed using an EDS attached to the SEM. Measurements were taken at arbitrary three points at a magnification of 5,000 to 20,000 times, and the average value was calculated. Also, the atomic ratio Nb/(Zr+Nb) was calculated from the average value.
  • cemented carbides contained a hard phase containing W and C as main components and a binder phase made of ferrous metal (Co). Moreover, sample no. 3 to 4 contained aggregated phases in which the value of Nb/(Zr+Nb) in atomic ratio differed from the numerical range of the first to third aggregated phases, but for convenience, the first described in the column of ⁇ 3rd aggregation phase.
  • the obtained cemented carbide was evaluated for cutting. Specifically, a TiN layer with a thickness of 1 ⁇ m, a TiCN layer with a thickness of 10 ⁇ m, and an Al 2 O 3 layer with a thickness of 5 ⁇ m are formed in order from the cemented carbide (substrate) by the CVD method. , cutting evaluation was performed under the following conditions. In addition, the thickness of each layer is an average value.
  • Table 2 shows the evaluation results.
  • the "flank wear amount” in the evaluation results in Table 2 represents the amount of wear on the flank face of the cutting edge during cutting.
  • Sample No. 1 and 2 are sample Nos. Compared to 3-4, the stability was clearly improved.
  • sample No. 1 As a result of measuring the average particle size of the first to third aggregated phases in 1 and 2 by the image analysis described above, the average particle size of the first to third aggregated phases is: 2nd aggregated phase > 3rd aggregated phase > 1st It had an aggregation phase relationship.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Ceramic Engineering (AREA)
  • Cutting Tools, Boring Holders, And Turrets (AREA)
  • Powder Metallurgy (AREA)
PCT/JP2023/003136 2022-03-03 2023-02-01 超硬合金およびこれを用いた被覆工具、切削工具 Ceased WO2023166900A1 (ja)

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KR1020247026890A KR20240134957A (ko) 2022-03-03 2023-02-01 초경합금 및 이것을 사용한 피복 공구, 절삭 공구
US18/840,495 US20250387838A1 (en) 2022-03-03 2023-02-01 Cemented carbide and coated tool and cutting tool each using the same
JP2024504407A JP7851394B2 (ja) 2022-03-03 2023-02-01 超硬合金およびこれを用いた被覆工具、切削工具
CN202380021031.2A CN118786233A (zh) 2022-03-03 2023-02-01 硬质合金及使用其的涂层刀具、切削刀具
DE112023001249.0T DE112023001249T5 (de) 2022-03-03 2023-02-01 Hartmetall sowie beschichtetes werkzeug und schneidwerkzeug, die dieses jeweils verwenden

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WO2024203158A1 (ja) * 2023-03-30 2024-10-03 三菱マテリアル株式会社 切削工具用超硬合金と該合金を用いた切削工具

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JP2001502249A (ja) * 1996-10-11 2001-02-20 サンドビック アクティエボラーグ 結合相富化した表面領域を有する超硬合金の製造方法
JP2002356734A (ja) * 2001-05-30 2002-12-13 Kyocera Corp 超硬合金およびそれを用いた切削工具
JP2003105477A (ja) * 2001-09-26 2003-04-09 Kyocera Corp 超硬合金およびそれを用いた切削工具
JP2019042830A (ja) * 2017-08-30 2019-03-22 三菱マテリアル株式会社 複合焼結体切削工具
WO2019189775A1 (ja) * 2018-03-29 2019-10-03 京セラ株式会社 超硬合金、被覆工具及び切削工具

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JP7235199B2 (ja) 2019-02-22 2023-03-08 三菱マテリアル株式会社 超硬合金および切削工具
WO2021193159A1 (ja) 2020-03-26 2021-09-30 三菱マテリアル株式会社 Ｗｃ基超硬合金製切削工具
JP7553939B2 (ja) 2020-08-12 2024-09-19 株式会社Ｖｒバンク 広告管理システム、広告管理方法及びプログラム

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JP2001502249A (ja) * 1996-10-11 2001-02-20 サンドビック アクティエボラーグ 結合相富化した表面領域を有する超硬合金の製造方法
JP2002356734A (ja) * 2001-05-30 2002-12-13 Kyocera Corp 超硬合金およびそれを用いた切削工具
JP2003105477A (ja) * 2001-09-26 2003-04-09 Kyocera Corp 超硬合金およびそれを用いた切削工具
JP2019042830A (ja) * 2017-08-30 2019-03-22 三菱マテリアル株式会社 複合焼結体切削工具
WO2019189775A1 (ja) * 2018-03-29 2019-10-03 京セラ株式会社 超硬合金、被覆工具及び切削工具

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CN118786233A (zh) 2024-10-15
JP7851394B2 (ja) 2026-04-24

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