WO2012063515A1 - 表面被覆切削工具 - Google Patents
表面被覆切削工具 Download PDFInfo
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- WO2012063515A1 WO2012063515A1 PCT/JP2011/063351 JP2011063351W WO2012063515A1 WO 2012063515 A1 WO2012063515 A1 WO 2012063515A1 JP 2011063351 W JP2011063351 W JP 2011063351W WO 2012063515 A1 WO2012063515 A1 WO 2012063515A1
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- cutting tool
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- residual stress
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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
- B23B27/148—Composition of the cutting inserts
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- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
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- 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/58—After-treatment
- C23C14/5886—Mechanical treatment
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- 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
- C23C16/02—Pretreatment of the material to be coated
- C23C16/0272—Deposition of sub-layers, e.g. to promote the adhesion of the main coating
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- 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
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- 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
- C23C16/56—After-treatment
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- 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
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- 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
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2200/00—Details of cutting inserts
- B23B2200/24—Cross section of the cutting edge
- B23B2200/245—Cross section of the cutting edge rounded
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- 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
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T407/00—Cutters, for shaping
- Y10T407/24—Cutters, for shaping with chip breaker, guide or deflector
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T407/00—Cutters, for shaping
- Y10T407/27—Cutters, for shaping comprising tool of specific chemical composition
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12458—All metal or with adjacent metals having composition, density, or hardness gradient
Definitions
- the present invention relates to a surface-coated cutting tool, and particularly to a surface-coated cutting tool coated with a coating that improves wear resistance and chipping resistance.
- cemented carbides (WC-Co alloys or alloys to which carbonitrides such as Ti (titanium), Ta (tantalum), Nb (niobium), etc. are added) have been used as cutting tools.
- cemented carbide, cermet, cubic boron nitride sintered body, or alumina-based or silicon nitride-based ceramics is used as the base material, and chemical vapor deposition (CVD: Cutting tools coated with one or more coating layers by chemical vapor deposition (PVD) or physical vapor deposition (PVD) have become widespread.
- the coating layer has a thickness of 3 to 20 ⁇ m and one or more first elements selected from IVa group elements, Va group elements, VIa group elements, Al (aluminum), Si or B in the periodic table of elements. And a compound consisting of one or more second elements selected from B, C, N or O (however, when the first element is only B, the second element is other than B).
- Patent No. 3661503, Patent Document 1 As an attempt to increase the service life of a cutting tool, for example, in Japanese Patent Application Laid-Open No. 2001-0662603 (Patent No. 3661503, Patent Document 1), a film composed of a vertically long crystal structure has different residual stresses above and below the film.
- the coating of a coating is disclosed. Specifically, residual compressive stress is applied to the upper layer of the coating, while residual tensile stress is applied to the lower layer of the coating, thereby improving the chipping resistance of the cutting tool.
- Patent Document 2 Japanese Patent Laid-Open No. 2001-096404 (Patent Document 2) describes that a hard coating layer obtained by laminating a Ti compound layer, a titanium carbonitride layer, a titanium carbide layer, and an aluminum oxide layer is coated to provide a high resistance. A technique for improving the chipping property is disclosed.
- JP 2009-0778309 A (Patent Document 3) introduces a compressive stress to the outer layer side by blasting the hard coating layer covering the surface of the surface-coated cutting tool, thereby preventing chipping. Improved.
- Patent Document 4 a first coating made of ⁇ -Al 2 O 3 provided with a second coating made of TiCN imparted with tensile stress on the inner layer side and imparted with compressive stress is disclosed.
- a coating comprising a coating on the surface side is disclosed. This film can improve toughness and wear resistance when the tensile stress of the first film and the compressive stress of the second film satisfy a specific relational expression.
- Patent Documents 1 to 4 described above provide sufficient performance with respect to chipping resistance, they do not sufficiently satisfy the requirements of recent cutting tools with regard to wear resistance.
- the present invention has been made in view of the current situation as described above, and an object of the present invention is to provide a surface-coated cutting tool that is highly compatible with wear resistance and chipping resistance.
- the present inventor has made extensive studies to solve the above-mentioned problems. As a result, the crystal structure of the chamfered portion of the film is different from the crystal structure of the portion other than the chamfered portion of the film, and different residual stresses are applied to each. The inventor has obtained the knowledge that it is the most effective in achieving both wear resistance and chipping resistance, and has finally completed the present invention by further research based on this knowledge.
- the surface-coated cutting tool of the present invention includes a base material and a coating formed on the base material, and the surface-coated cutting tool has a portion where the rake face and the flank face intersect. It is a chamfered portion, and the coating includes at least one first coating layer, and the first coating layer is the outermost surface layer of the coating in the chamfered portion, and the first coating layer in the chamfered portion is the surface thereof.
- the residual stress has a minimum value, and the residual stress increases continuously or stepwise as the depth A further increases in the depth direction.
- the minimum value of the residual stress is -7 GPa to -1 GPa
- the first coating layer other than the chamfered portion has a residual stress larger than the minimum value of the residual stress
- the first coating other than the chamfered portion The layer is in the direction of the rake face center and relief
- the residual stress increases continuously or stepwise as it goes in the center direction, resulting in a residual stress of 0 GPa or more and 2 GPa or less on the base material side, and a region from the surface to the depth A in the first coating layer in the chamfered portion.
- the first coating layer is a region deeper in the depth direction from the depth A in the chamfered portion, and a region other than the chamfered portion.
- it is a coarse crystal structure region including a crystal larger than a crystal in the fine crystal structure region.
- the first coating layer preferably has a layer thickness of 2 ⁇ m or more and 30 ⁇ m or less.
- the first covering layer is preferably the outermost surface layer, but is not necessarily the outermost surface.
- the coating comprises at least one element selected from the group consisting of group IVa elements, group Va elements, group VIa elements, Al, Si, Y, B, and S, and a group consisting of boron, carbon, nitrogen, and oxygen. It is preferable to consist of a compound with at least one selected element, and it is preferable to include one or more layers in addition to the first coating layer.
- the total thickness of the coating is preferably 3 ⁇ m or more and 50 ⁇ m or less.
- the first coating layer is preferably made of alumina.
- the surface-coated cutting tool of the present invention has a configuration as described above, so that both wear resistance and chipping resistance can be made highly compatible.
- the layer thickness or film thickness is measured with a scanning electron microscope (SEM).
- the surface-coated cutting tool of the present invention comprises a base material and a film formed thereon.
- the surface-coated cutting tool of the present invention having such a basic configuration includes, for example, a drill, an end mill, a drill tip changeable tip, an end mill tip replacement tip, a milling tip replacement tip, and a turning tip replacement. It can be used very effectively as a die cutting tip, a metal saw, a gear cutting tool, a reamer, a tap and the like.
- FIG. 1 is a schematic view schematically showing a contact state between a surface-coated cutting tool and a work material during cutting.
- the surface-coated cutting tool 1 of the present invention includes a rake face 2 that comes into contact with the chips 6 of the work material 5 and a flank face 3 that comes into contact with the work material itself.
- a chamfered portion 4 is a portion where the cutting edge processing is applied to the ridge where the rake face 2 and the flank 3 intersect.
- the chamfered portion 4 is a portion where the surface-coated cutting tool 1 comes into contact with the work material 5, and is an extremely important portion particularly in a cutting tool.
- FIG. 2 is a schematic view schematically showing a surface-coated cutting tool having a square rake face.
- the surface-coated cutting tool 1 of the present invention is a blade-tip-exchangeable cutting tip, as shown in FIG. 2, a through-hole 20 that passes through the center front and back of the rake face 2 of the blade-tip-exchangeable cutting tip is formed. Also good.
- This through hole 20 is used as a fixing hole attached to the tool. If necessary, another fixing means can be provided in addition to or instead of the fixing hole.
- FIG. 3 is a schematic cross-sectional view showing a chamfered portion chamfered into a curved surface
- FIG. 4 is a schematic cross-sectional view showing a chamfered portion chamfered into a flat shape.
- the chamfered portion 4 is, as shown in FIG. 3, such that the edge corresponding to the ridge where the rake face 2 and the flank 3 intersect is subjected to cutting edge processing to have a radius (R).
- the chamfered part here shown in FIG. 4, the part corresponding to the ridge where the rake face 2 and the flank 3 intersect is cut off in a straight line (negative land part).
- the part processed by combining these chamfering processes shall also be included.
- the chamfered portion 4 is formed by performing grinding, brushing, barreling, blasting, buffing, honing, etc. on the ridge where the rake face 2 and the flank 3 intersect.
- Such a chamfered portion 4 preferably has a width of the chamfered portion of 0.01 mm or more and 0.2 mm or less when the surface-coated cutting tool is viewed in plan view from the rake face direction or the flank direction (FIG. 4). More preferably, it is 0.02 mm or more and 0.1 mm or less.
- a conventionally known material known as such a cutting tool base material can be used without particular limitation.
- cemented carbide for example, WC base cemented carbide, including WC, including Co, or further including carbonitride such as Ti, Ta, Nb, etc.
- cermet TiC, TiN, TiCN, etc.
- High-speed steel ceramics (titanium carbide, silicon carbide, silicon nitride, aluminum nitride, aluminum oxide, and mixtures thereof), cubic boron nitride sintered body, diamond sintered body
- Examples of such a substrate include a boron nitride sintered body or a mixture of aluminum oxide and titanium carbide.
- a cemented carbide (WC-based cemented carbide). This is because the cemented carbide is composed of high-hardness tungsten carbide and contains an iron group metal such as cobalt, so it has both hardness and strength and is extremely balanced.
- a cemented carbide is used as such a base material, the effect of the present invention is exhibited even if such a cemented carbide contains an abnormal phase called free carbon or ⁇ phase in the structure.
- these base materials may have a modified surface.
- a de- ⁇ layer may be formed on the surface, and in the case of cermet, a surface hardened layer may be formed, and even if the surface is modified in this way, The effect is shown.
- the coating formed on the substrate includes at least a first coating layer. That is, the coating of the present invention may be constituted only by the first coating layer (in this case, the first coating layer is formed in contact with the substrate), or such a first coating layer. In addition, one or two or more other layers may be included. Such a layer other than the first coating layer may be formed between the base material and the first coating layer as described later, or may be formed on the first coating layer. However, even if a layer other than the first coating layer is formed on the first coating layer, the first coating layer is the outermost surface layer (the layer constituting the coating surface) in the chamfered portion involved in the cutting process. ). When the first coating layer contains crystals having different average crystal grain sizes depending on the part, the first covering layer has a residual stress suitable for the part, and can achieve both high wear resistance and chipping resistance. The crystal grain size and residual stress of the first coating layer will be described later.
- Such a coating of the present invention includes an embodiment in which the entire surface of the substrate is coated, and also includes an embodiment in which the coating is not partially formed. The aspect which is mentioned is also included.
- the total thickness of the coating of the present invention is preferably 3 ⁇ m or more and 50 ⁇ m or less. If it is less than 3 ⁇ m, the abrasion resistance may be inferior, and if it exceeds 50 ⁇ m, adhesion to the substrate and chipping resistance may be deteriorated.
- a particularly preferable film thickness of such a coating is 5 ⁇ m or more and 25 ⁇ m or less.
- group IVa elements Ti, Zr, Hf, etc.
- group Va elements etc. (From V, Nb, Ta, etc.)
- group VIa elements Cr, Mo, W, etc.
- aluminum Al
- silicon Si
- yttrium Y
- boron B
- sulfur S
- It is preferably composed of a compound of at least one selected element and at least one element selected from the group consisting of boron, carbon, nitrogen, and oxygen (except when both elements are B).
- the compound includes, for example, the above-mentioned group IVa elements (Ti, Zr, Hf, etc.), group Va elements (V, Nb, Ta, etc.), group VIa elements (Cr, Mo, W, etc.), aluminum (Al), silicon ( Si), elements selected from the group consisting of yttrium (Y), carbides, nitrides, oxides, borides, carbonitrides, carbonates, nitrides, carbonitrides, and the like. Solid solutions are also included.
- Examples of such compounds include Ti, Al, (Ti 1-x Al x ), (Al 1-x Zr x ), (Ti 1-x Si x ), (Al 1-x Cr x ), ( Ti 1-xy Si x Al y ) or (Al 1-xy Cr x V y ) nitrides, carbides, oxides, carbonitrides, nitrogen oxides or carbonitrous oxides (in addition to these, B, Cr, etc.) Can be mentioned as a suitable composition thereof (in the formula, x and y represent any number of 1 or less).
- TiCN TiN, TiSiN, TiSiCN , TiAlN, TiAlCrN, TiAlSiN, TiAlSiCrN, AlCrN, AlCrCN, AlCrVN, TiBN, TiAlBN, TiBCN, TiAlBCN, TiSiBCN, AlN, AlCN, AlO, Al 2 O 3, ZrO 2, (AlZr) 2 O 3 and the like.
- the 1st coating layer which comprises a film is demonstrated in detail.
- the first coating layer is characterized in that the residual stress differs greatly between the depth of the chamfered portion and the chamfered portion and a portion other than the chamfered portion, and satisfies all the following conditions (1) to (5).
- the first covering layer in the chamfered portion has a minimum value of the residual stress at the depth A where the depth from the surface is within 2 ⁇ m.
- the minimum value of the residual stress is -7 GPa or more and -1 GPa or less.
- the residual stress increases continuously or stepwise as the depth A further increases in the depth direction.
- the first coating layer other than the chamfered portion has a residual stress larger than the minimum value of the residual stress of the first coating layer in the chamfered portion.
- the residual stress increases continuously or stepwise as it proceeds in the center direction of the rake face and the center direction of the flank face, and the residual stress of 0 GPa to 2 GPa on the base material side. To be.
- FIG. 5 and FIG. 6 show an example of the stress distribution of the first coating layer that satisfies the conditions (1) to (3) among the above (1) to (5).
- FIG. 5 is a graph showing a stress distribution when the residual stress takes a minimum value at the depth A of the first coating layer and the residual stress continuously increases from the depth A toward the depth direction. 6 is the same graph as FIG. 5 except that the manner of increasing the residual stress is stepwise.
- the first coating layer of the present invention has such a stress distribution, in combination with the crystal structure of the first coating layer, which will be described later, the wear resistance and the chipping resistance are highly compatible with each other. The adhesion between the material and the coating is further improved. In addition, since the residual stress has a minimum value in the vicinity of the surface of the coating (first coating layer), it is possible to suppress the progress of cracks generated on the coating surface during cutting.
- first coating layer since the above conditions (1) to (5) and the effects brought about by them will be described.
- the depth A at which the residual stress is a minimum value is preferably at a position where the depth from the surface of the first coating layer is 0.1 ⁇ m or more and 1 ⁇ m or less. When the depth A is greater than 2 ⁇ m from the surface of the first coating layer, the balance between wear resistance and chipping resistance is lost, and the tool life may be reduced.
- the minimum value of such residual stress is preferably -5 GPa or more and -1.5 GPa or less. If it is less than ⁇ 7 GPa, the compressive stress of the first coating layer is too high, so that self-destruction occurs and chipping is likely to occur. On the other hand, if it exceeds ⁇ 1 GPa, the chipping resistance required for the cutting tool cannot be obtained.
- the “minimum value” in the present invention indicates a minimum value in a mathematical sense, and, for example, as shown in FIG. 8 described later, the residual stress is continuous in the thickness direction of the first coating layer. Thus, it is a concept including a case where a certain numerical value is shown.
- the condition (3) is provided to exclude the case where the residual stress includes a locally high value or low value. That is, when the residual stress has a locally high value or low value, chipping is likely to occur from that portion, but this condition (3) is satisfied (the residual stress changes continuously or stepwise). The occurrence of such chipping can be suppressed.
- the first coating layer other than the chamfered portion finally has a residual stress of 0 GPa or more and 2 GPa or less. If the residual stress of the first coating layer other than the chamfered portion exceeds 2 GPa, the coating peels off at the chamfered portion depending on the shape of the cutting tool, which is not preferable. Further, if the residual stress on the substrate side is smaller than 0 GPa, sufficient wear resistance cannot be obtained.
- the rake face center direction means a vector direction from one point of the cutting edge ridge line portion which is a chamfered portion toward the center of the rake face.
- the “flank center direction” means a vector direction from one point of the cutting edge ridge line portion which is a chamfered portion toward the center of the flank surface.
- the compressive stress referred to in the present invention is a kind of internal stress (intrinsic strain) existing in the film, and is represented by a numerical value (unit: GPa) of “ ⁇ ” (minus).
- GPa numerical value
- the expression that the compressive stress (internal stress) is high indicates that the absolute value of the numerical value is large, and the expression that the compressive stress (internal stress) is low indicates that the absolute value of the numerical value is small. I mean.
- what the above numerical value is represented by “+” (plus) is tensile stress.
- the residual stress distribution of the first coating layer of the present invention is measured by the following sin 2 ⁇ method.
- the sin 2 ⁇ method using X-rays is widely used as a method for measuring the residual stress of a polycrystalline material. This measurement method is described in detail in pages 54 to 66 of “X-ray stress measurement method” (Japan Society for Materials Science, published by Yokendo Co., Ltd. in 1981).
- the X-ray penetration depth is first fixed by combining the parallel tilt method and the side tilt method, and various ⁇ directions are measured in the plane including the stress direction to be measured and the sample surface normal set at the measurement position.
- the diffraction angle 2 ⁇ is measured to create a 2 ⁇ -sin 2 ⁇ diagram, and the compressive stress from the gradient to the depth (distance from the coating surface) is obtained.
- X-rays from an X-ray source are incident on the first coating layer at a predetermined angle, and X-rays diffracted by the first coating layer are detected by an X-ray detector, The internal stress is measured based on the detected value.
- synchrotron radiation in terms of the quality of the X-ray source (high brightness, high parallelism, wavelength variability, etc.)
- SR synchrotron radiation
- the Young's modulus and Poisson's ratio of the coating are preferable to use.
- the Young's modulus can be measured using a dynamic hardness meter, and since the Poisson's ratio does not vary greatly depending on the material, a value of around 0.2 may be used.
- the Young's modulus is not necessarily used, and the compressive stress may be calculated by substituting the lattice constant and the lattice spacing.
- the first covering layer is composed of an IVa group element (Ti, Zr, Hf, etc.), a Va group element (V, Nb, Ta, etc.), a VIa group element (Cr, Mo, W, etc.), aluminum ( At least one element selected from the group consisting of Al), silicon (Si), yttrium (Y), boron (B), and sulfur (S), and a group consisting of boron, carbon, nitrogen, and oxygen It is preferably composed of a compound with at least one element (except when both elements are B), more preferably composed of alumina, and further preferably alumina having an ⁇ -type crystal structure.
- ⁇ Crystal structure of the first coating layer> 7 and 8 are cross-sectional views schematically showing the crystal structure of the first coating layer in the vicinity of the chamfered portion. 7 and 8 show that the coating consists only of the first coating layer.
- the first coating layer 8 of the present invention is a layer that includes a fine crystal structure region 10 in which an average crystal grain size of a compound constituting the first cover layer 8 is minute and a coarse crystal structure region 9 in which the average crystal grain size is coarse.
- Such a first coating layer is formed by aggregating crystal grains of a compound, and a region where the crystal grains having an average crystal grain size of 10 to 200 nm are aggregated is a fine crystal structure region. And a region where crystal grains larger than crystals in the fine crystal structure region are aggregated is defined as a coarse crystal structure region.
- the fine crystal structure region occupies a region from the surface of the first coating layer 8 to the depth A in the chamfered portion 4 as shown in FIGS. That is, the first coating layer 8 in the chamfered portion 4 is composed of two regions in the thickness direction, the coarse crystal structure region 9 is present on the substrate 7 side, and the fine crystal structure region 10 is present on the surface side.
- the thickness of the fine crystal structure region 10 occupies a region from the surface of the first coating layer 8 to the depth A.
- the present invention succeeds in achieving both high wear resistance and chipping resistance at the same time by using the first coating layer 8 having such a configuration. That is, by forming the fine crystal structure region 10 on the surface of the first coating layer 8, the unit in which the coating is destroyed is reduced, thereby improving the wear resistance.
- the crystal grain boundaries increase as the crystal grains are miniaturized, whereby cracks generated on the coating surface side do not progress toward the base material side, and chipping resistance is improved.
- the progress of cracks is suppressed at the interface between the fine crystal structure region and the coarse crystal structure region, and an improvement in toughness can be expected.
- the 1st coating layer 8 of this invention has the effect
- the average crystal grain size of the crystal grains in the fine crystal structure region needs to be 10 nm or more and 200 nm or less, and more preferably 15 nm or more and 80 nm or less. If it is less than 10 nm, the bonding strength between the particles constituting the crystal structure constituting the first coating layer 8 becomes weak, so that the wear resistance is lowered. On the other hand, if it exceeds 200 nm, the crystal structure of the coating on the cutting surface is too rough, and adhesive wear occurs on the work material, resulting in a decrease in wear resistance.
- the average crystal grain size of the crystal grains in the coarse texture region varies depending on the average crystal grain size of the crystal grains in the fine crystal texture region. Larger than the average crystal grain size, more preferably 200 nm or more, and still more preferably 300 nm or more and 1500 nm or less.
- the average crystal grain size of crystal grains can be determined as follows. That is, the base material and the coating (first coating layer) formed on the base material are processed with a FIB processed material so that the cross section can be seen, and the cross section is processed by FE-SEM (electrolytic emission scanning electron microscope). Observe. At that time, by observing as a reflected electron image, portions having the same crystal orientation are observed with the same contrast, and the same contrast portion is regarded as one crystal particle.
- a straight line having an arbitrary length (preferably corresponding to 400 ⁇ m) parallel to the surface of the base material is drawn at an arbitrary position of the first coating layer with respect to the image thus obtained.
- the number of crystal grains included in the straight line is measured, and the length obtained by dividing the length of the straight line by the number of crystal grains is defined as the average crystal grain diameter in that portion of the first coating layer.
- the interface between the fine crystal structure region and the coarse crystal structure region is perpendicular to the substrate surface by observing the cross section of the coating (first coating layer) using, for example, a transmission electron microscope (TEM).
- TEM transmission electron microscope
- the first coating layer when the coating is composed of a plurality of layers, the first coating layer may be formed on the substrate side of the coating or may be formed on the surface side of the coating. It is preferable that This is because the first coating layer comes into contact with the work material, and the chipping at the initial stage of cutting can be suppressed to improve the cutting performance and extend the life. In the chamfered portion, it is essential that the first coating layer is the outermost surface layer of the coating.
- the first coating layer preferably has a layer thickness of 2 ⁇ m or more and 30 ⁇ m or less. Furthermore, the upper limit of the thickness is 20 ⁇ m, more preferably 10 ⁇ m, and the lower limit is 3 ⁇ m, more preferably 5 ⁇ m. If the thickness is less than 2 ⁇ m, the effect is not sufficient when compressive residual stress is applied, so there is not much effect in improving chipping resistance, and if it exceeds 30 ⁇ m, it is located inside the substrate or the first coating layer. Adhesiveness with the layer to perform may fall.
- the coating film of the present invention can contain one layer or two or more layers in addition to the first coating layer.
- Examples of such a layer include an intermediate layer formed between the base material and the first coating layer and an outermost surface layer formed on the first coating layer. These layers are formed to provide other effects such as oxidation resistance and lubricity, while the first covering layer exhibits the effects as described above.
- the intermediate layer is formed for the purpose of improving wear resistance or improving adhesion to the substrate, and can be formed in one layer or two or more layers.
- Such an intermediate layer can be made of, for example, TiC, TiN, TiCN, TiCNO, TiSiN, TiAlN, TiZrCN, TiAlCrN, TiAlSiN, TiAlCrSiN, or the like. In these compositions, conventionally known atomic ratios can be adopted without any particular limitation.
- Such an intermediate layer is preferably formed with a thickness of 0.2 ⁇ m or more and 1 ⁇ m or less, and preferably has a residual stress of ⁇ 1 GPa or more and ⁇ 0.1 GPa or less.
- the outermost surface layer is formed for the purpose of coloring and the like for identifying used blade edges, and can be formed in one layer or two or more layers.
- Such an outermost surface layer can be made of, for example, Cr, CrN, TiN, TiCN, or the like. In these compositions, conventionally known atomic ratios can be adopted without any particular limitation.
- Such an outermost surface layer is preferably formed with a thickness of 0.1 ⁇ m or more and 0.3 ⁇ m or less.
- a chamfered portion is formed by performing grinding treatment, brush treatment, barrel treatment, blast treatment, and the like on the ridge where the rake face and flank face of the substrate intersect. And a film is formed with respect to the base material in which the chamfered part was formed.
- the method for producing a coating film of the present invention can be employed without any particular limitation on a conventionally known method, but is preferably formed by a chemical vapor deposition method (CVD method).
- CVD method chemical vapor deposition method
- each layer of the film has a tensile residual stress, and the adhesion to the substrate can be very high.
- a blasting process is locally performed on the chamfered portion of the coating film formed above, particularly the first coating layer.
- compressive stress is applied to the surface side of the first coating layer in the chamfered portion, and the average crystal grain size of the crystal particles from the surface of the first coating layer in the chamfered portion to the position of the depth A is 10 nm or more and 200 nm or less.
- the blast treatment is carried out by preparing a dispersion solvent in which abrasive grains are dispersed directly or in a solvent such as water and colliding it with the surface of the first coating layer.
- concentration of the liquid contained in the dispersion solvent is increased continuously or stepwise to gradually reduce the abrasive concentration, and the volume ratio of the abrasive grains in the dispersion solvent is 5% by volume to 40% by volume.
- the blasting process is performed in the range of.
- blasting process may be divided into two stages, and the process may be performed using different powders.
- the condition of the collision of the abrasive grains can be appropriately adjusted depending on the composition of the coating film, the magnitude of the compressive residual stress to be applied, etc., but the projection pressure is 0.01 MPa or more and 0.5 MPa or less and the projection distance is 0. It is preferable that the projection angle is 5 mm or more and 50 mm or less, and the projection angle is projected at right angles to the chamfered portion. If the impact strength of the particles is not sufficient, the desired compressive residual stress cannot be applied, and therefore it is preferable to cause the impact to occur with an appropriate strength.
- the present invention is characterized in that the residual stress and the crystal grain size of the first coating layer in the chamfered portion are changed by performing the blasting process, but the first coating layer other than the chamfered portion is used. Part of the chamfered portion has the same residual stress and crystal grain size as the first covering layer, or the first covering layer in the chamfered portion partially satisfies the above residual stress and crystal grain size. It goes without saying that even if it is not present, it does not depart from the scope of the present invention as long as the effects of the present invention are not impaired.
- the cutting edge of the base material was chamfered with a nylon brush containing SiC abrasive grains to form a round honing as a chamfered portion. Thereafter, the surface of the substrate was washed.
- each layer of the coating film shown in the column of “Layer structure” in Table 1 was formed on the surface of the substrate using a conventionally known thermal CVD method (“Layer structure” in Table 1).
- Layer structure in Table 1
- a TiN layer having a thickness of 0.3 ⁇ m in order from the substrate side
- a TiCN layer having a thickness of 10 ⁇ m
- a TiCNO layer having a thickness of 0.5 ⁇ m
- a ⁇ having a thickness of 4 ⁇ m An Al 2 O 3 layer was formed.
- the 1st coating layer in each Example is an outermost surface layer.
- the chamfered portion of the first coating layer was subjected to blasting using zirconia having a hardness lower than that of the coating and a high specific gravity and diamond abrasive grains having a high hardness and a low specific gravity.
- the abrasive concentration is gradually reduced while increasing the liquid concentration continuously or stepwise, and adjusted at a projection distance of 0.5 to 50 mm with a projection pressure of 0.01 to 0.5 MPa.
- the chamfered portion of the coating was blasted.
- it processed with two types of different media so that the 1st coating layer might become the residual stress shown in the following Table 1, and a fine structure.
- the column of “increase mode” in Table 1 indicates whether the mode of increase in the residual stress is “continuous” or “stepwise”. In the comparative example, since the state of increase in the residual stress of the first coating layer is constant, it is described as “constant”.
- the surface-coated cutting tool of each example was also produced by the same method.
- Each comparative example was manufactured by the same method as each example except that the blasting process was not performed.
- the residual stress distribution of the first coating layer was measured by the above-described sin 2 ⁇ method. Moreover, about the average crystal grain diameter of the 1st coating layer, it implemented by observing the cross section of a film with the method mentioned above.
- the X-ray energy used was 10 keV, and the peak of the diffraction line was the (166) plane of ⁇ -type Al 2 O 3 .
- the measured diffraction peak position is determined by fitting a Gaussian function, the slope of the 2 ⁇ -sin 2 ⁇ diagram is obtained, and the value obtained using a dynamic hardness meter (MST nanoindenter) is adopted as the Young's modulus.
- MST nanoindenter dynamic hardness meter
- a value of Al 2 O 3 (0.2) was used.
- the “film thickness” of each layer in Table 1 indicates the film thickness of the coating, and the layer thickness of each layer constituting the coating is shown in parentheses next to each layer in Table 1.
- values obtained by cutting with a plane including a normal to the surface of the surface-coated cutting tool and observing the cut surface with an SEM were adopted.
- the distance from the surface of the first coating layer to the minimum value of the residual stress is shown, and the minimum value of the residual stress is shown as “Minimum value” in Table 1. It is shown in the column.
- the column of “increase mode” indicates whether the mode of the residual stress that increases as it proceeds toward the rake face center direction and the flank center direction is “continuous” or “stepwise”.
- the “fine” column of “average particle size” indicates the average crystal particle size of the crystal particle size (fine crystal structure region) from the surface of the first coating layer to the depth A in the chamfered portion.
- the average crystal grain size of the crystal grain size (coarse crystal structure region) of the first coating layer in the part other than the fine crystal structure region is shown.
- the wear reduction width of the flank is calculated, and the time until the wear reduction width exceeds 0.25 mm on average is calculated. It is shown in the column of “Tool life” in Table 2. The longer the tool life, the longer the life of the surface-coated cutting tool.
- the surface-coated cutting tool of each example has less flank wear and less chipping than that of each comparative example. From this result, it can be said that the surface-coated cutting tool of each example is excellent in wear resistance and chipping resistance as compared with that of each comparative example. As described above, the wear resistance and chipping resistance of the surface-coated cutting tool of each example were improved because the crystal of the first coating layer in the chamfered portion was refined and the residual stress in that portion was locally reduced. It is thought to be due to.
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Abstract
Description
本発明の表面被覆切削工具は、基材とその上に形成された被膜とを備えたものである。このような基本的構成を有する本発明の表面被覆切削工具は、たとえばドリル、エンドミル、ドリル用刃先交換型チップ、エンドミル用刃先交換型チップ、フライス加工用刃先交換型切削チップ、旋削加工用刃先交換型切削チップ、メタルソー、歯切工具、リーマ、タップ等として極めて有用に用いることができる。
図3は、曲面状に面取り加工された面取り部を示す概略断面図であり、図4は、平面状に面取り加工された面取り部を示す概略断面図である。本発明において、面取り部4とは、図3に示されるように、すくい面2と逃げ面3とが交差する稜に相当する部分に対し、刃先処理がされてアール(R)を有するように面取り加工された部分(ホーニング部)の他、図4に示されるように、すくい面2と逃げ面3とが交差する稜に相当する部分を直線状に切り落として面取り加工された部分(ネガランド部)を意味することもある。さらに、これらの面取り加工が組み合わされて処理された部分も含むものとする。
本発明の表面被覆切削工具の基材としては、このような切削工具の基材として知られる従来公知のものを特に限定なく使用することができる。たとえば、超硬合金(たとえばWC基超硬合金、WCの他、Coを含み、あるいはさらにTi、Ta、Nb等の炭窒化物等を添加したものも含む)、サーメット(TiC、TiN、TiCN等を主成分とするもの)、高速度鋼、セラミックス(炭化チタン、炭化硅素、窒化硅素、窒化アルミニウム、酸化アルミニウム、およびこれらの混合体など)、立方晶型窒化硼素焼結体、ダイヤモンド焼結体、窒化硼素焼結体、または酸化アルミニウムと炭化チタンとからなる混合体等をこのような基材の例として挙げることができる。
本発明の表面被覆切削工具において、基材上に形成される被膜は、少なくとも第1被覆層を含むことを特徴とする。すなわち、本発明の被膜は、第1被覆層のみによって構成されていてもよいし(この場合は第1被覆層が基材に接して形成されることになる)、このような第1被覆層以外に1層または2層以上の他の層を含んでいてもよい。このような第1被覆層以外の層は、後述のように基材と第1被覆層との間に形成されていてもよいし、第1被覆層上に形成されていてもよい。ただし、第1被覆層以外の層が第1被覆層上に形成される場合であっても、切削加工に関与する面取り部においては、第1被覆層が最表面層(被膜表面を構成する層)であることを特徴とする。かかる第1被覆層が、部位によって異なる平均結晶粒径の結晶を含むことにより、その部位に適した残留応力を有し、耐摩耗性および耐チッピング性を高度に両立させることができる。なお、第1被覆層の結晶粒径および残留応力に関しては後述する。
本発明において、第1被覆層は、その残留応力が面取り部の深度ならびに面取り部と、面取り部以外の部分とで大きく異なり、以下の(1)~(5)の条件を全て満たすことを特徴とする。
(3)深さAからさらに深さ方向に深くなるにつれて、連続的または段階的に残留応力が増加すること。
上記第1被覆層は、元素周期律表のIVa族元素(Ti、Zr、Hf等)、Va族元素(V、Nb、Ta等)、VIa族元素(Cr、Mo、W等)、アルミニウム(Al)、ケイ素(Si)、イットリウム(Y)、ホウ素(B)、および硫黄(S)からなる群から選ばれる少なくとも1種の元素と、ホウ素、炭素、窒素、および酸素からなる群より選ばれる少なくとも1種の元素との化合物(ただし、両元素がBの場合を除く)からなることが好ましく、より好ましくはアルミナからなることであり、さらに好ましくはα型の結晶構造を有するアルミナである。
図7および図8は、面取り部の近郊における第1被覆層の結晶構造を模式的に示す断面図である。なお、図7および図8は、被膜が第1被覆層のみからなるものを示している。本発明の第1被覆層8は、それを構成する化合物の平均結晶粒径が微小である微細結晶組織領域10と該平均結晶粒径が粗大である粗大結晶組織領域9とを含む層である。このような第1被覆層は、化合物の結晶粒子が集合して構成されるものであるが、その結晶粒子の平均結晶粒径が10~200nmとなる結晶粒子が集合した領域を微細結晶組織領域とし、該微細結晶組織領域における結晶よりも大きい結晶粒子が集合した領域を粗大結晶組織領域とする。
本発明において、被膜が複数層からなる場合には、第1被覆層は、被膜の基材側に形成されていてもよいし、被膜の表面側に形成されていてもよいが、最表面層であることが好ましい。これにより第1被覆層が被削材と接することとなり、切削初期における欠損を抑制し、切削性能の向上と長寿命化を図ることができるからである。なお、面取り部においては、第1被覆層が被膜の最表面層であることが必須である。
本発明において、第1被覆層は、2μm以上30μm以下の層厚を有することが好ましい。さらにその厚みの上限は20μm、より好ましくは10μmであり、その下限は3μm、より好ましくは5μmである。その厚みが2μm未満であると、圧縮残留応力が付与される場合その効果が十分ではないため、耐チッピング性向上にあまり効果がなく、30μmを超えると基材または第1被覆層の内側に位置する層との密着性が低下する場合がある。
本発明の被膜は、上記第1被覆層以外に1層または2層以上の層を含むことができる。このような層としては、基材と第1被覆層との間に形成される中間層や第1被覆層上に形成される最外表面層を挙げることができる。これらの層は、上記第1被覆層が上記のような効果を示すのに対して、耐酸化性や潤滑性等の他の作用を付与するために形成する。
まず、基材のすくい面と逃げ面とが交差する稜に対し、研削処理、ブラシ処理、バレル処理、ブラスト処理などを施すことにより、面取り部を形成する。そして、面取り部を形成した基材に対し、被膜を成膜する。
各実施例および各比較例の表面被覆切削工具を用いて、以下の条件で旋削切削加工試験を行なった。
切削速度:230m/min
送り速度:0.15mm/rev
切り込み:1.0mm
切削油:あり
切削試験を開始してから表面被覆切削工具にチッピングが生じるまでの時間を表2の「チッピング発生時間」の欄に示した。チッピング発生時間が長いほど、切削工具にチッピングが生じにくいことを示している。
Claims (6)
- 基材(7)と、該基材(7)上に形成された被膜とを備える表面被覆切削工具(1)であって、
前記表面被覆切削工具(1)は、すくい面(2)と逃げ面(3)とが交差する部分が面取り部(4)となっており、
前記被膜は、少なくとも1層の第1被覆層(8)を含み、
前記第1被覆層(8)は、前記面取り部(4)における前記被膜の最表面層であり、
前記面取り部(4)における前記第1被覆層(8)は、その表面からの深さが2μm以内の深さとなる深さAにおいて、残留応力の極小値を有し、かつ前記深さAからさらに深さ方向に深くなるにつれて、連続的または段階的に残留応力が増加し、
前記残留応力の極小値は、-7GPa以上-1GPa以下であり、
前記面取り部(4)以外における第1被覆層(8)は、前記残留応力の極小値よりも大きい残留応力を有し、
前記面取り部(4)以外における第1被覆層(8)は、すくい面中心方向および逃げ面中心方向に進むにつれて、連続的または段階的に残留応力が増加して、前記基材(7)側で0GPa以上2GPa以下の残留応力となり、
前記面取り部(4)における第1被覆層(8)において、その表面から前記深さAまでの領域は、10nm以上200nm以下の平均結晶粒径の結晶を含む微細結晶組織領域(10)であり、
前記第1被覆層(8)は、前記面取り部(4)における前記深さAからさらに深さ方向に深くなる領域、および前記面取り部(4)以外における領域において、前記微細結晶組織領域(10)における結晶よりも大きい結晶を含む粗大結晶組織領域(9)である、表面被覆切削工具(1)。 - 前記第1被覆層(8)は、2μm以上30μm以下の層厚である、請求項1に記載の表面被覆切削工具(1)。
- 前記被膜は、IVa族元素、Va族元素、VIa族元素、Al、Si、Y、B、およびSからなる群から選ばれる少なくとも1種の元素と、ホウ素、炭素、窒素、および酸素からなる群より選ばれる少なくとも1種の元素との化合物からなる、請求項1に記載の表面被覆切削工具(1)。
- 前記被膜は、前記第1被覆層(8)以外に1層以上の層を含む、請求項1に記載の表面被覆切削工具(1)。
- 前記被膜は、その全厚が3μm以上50μm以下である、請求項1に記載の表面被覆切削工具(1)。
- 前記第1被覆層(8)は、アルミナからなる、請求項1に記載の表面被覆切削工具(1)。
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP11818965.3A EP2638993B1 (en) | 2010-11-10 | 2011-06-10 | Surface-coated cutting tool |
US13/393,473 US8715838B2 (en) | 2010-11-10 | 2011-06-10 | Surface-coated cutting tool |
KR1020127006046A KR101386856B1 (ko) | 2010-11-10 | 2011-06-10 | 표면 피복 절삭 공구 |
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Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001062603A (ja) | 1999-06-23 | 2001-03-13 | Mitsubishi Materials Corp | 断続重切削で硬質被覆層がすぐれた耐チッピング性を発揮する表面被覆炭化タングステン基超硬合金製切削工具 |
JP2001096404A (ja) | 1999-07-23 | 2001-04-10 | Mitsubishi Materials Corp | 断続重切削で硬質被覆層がすぐれた耐チッピング性を発揮する表面被覆炭化タングステン基超硬合金製切削工具 |
JP2002062603A (ja) | 2000-08-18 | 2002-02-28 | Fuji Photo Film Co Ltd | 画像読み取り装置 |
JP2006035383A (ja) * | 2004-07-28 | 2006-02-09 | Sumitomo Electric Hardmetal Corp | 表面被覆切削工具 |
WO2006064724A1 (ja) | 2004-12-14 | 2006-06-22 | Sumitomo Electric Hardmetal Corp. | 表面被覆切削工具 |
JP2009078309A (ja) | 2007-09-25 | 2009-04-16 | Mitsubishi Materials Corp | 表面被覆切削工具 |
WO2009081026A2 (fr) * | 2007-12-20 | 2009-07-02 | Saint-Gobain Centre De Recherches Et D'etudes Europeen | Particules de grenaillage |
JP2010137315A (ja) * | 2008-12-10 | 2010-06-24 | Sumitomo Electric Hardmetal Corp | 表面被覆切削工具 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003061885A1 (fr) | 2002-01-18 | 2003-07-31 | Sumitomo Electric Industries, Ltd. | Outil de coupe presentant un revetement de surface |
CN100479955C (zh) * | 2003-12-05 | 2009-04-22 | 住友电工硬质合金株式会社 | 表面被覆切削工具 |
JP2005271190A (ja) | 2003-12-05 | 2005-10-06 | Sumitomo Electric Hardmetal Corp | 表面被覆切削工具 |
WO2006009121A1 (ja) * | 2004-07-23 | 2006-01-26 | Sumitomo Electric Hardmetal Corp. | 圧縮応力の強度分布を有する被膜を備えた表面被覆切削工具 |
CN100496824C (zh) * | 2004-10-29 | 2009-06-10 | 住友电工硬质合金株式会社 | 表面被覆切削工具 |
EP2000237A1 (en) | 2006-03-28 | 2008-12-10 | Kyocera Corporation | Surface-coated tool |
-
2011
- 2011-06-10 US US13/393,473 patent/US8715838B2/en active Active
- 2011-06-10 EP EP11818965.3A patent/EP2638993B1/en active Active
- 2011-06-10 WO PCT/JP2011/063351 patent/WO2012063515A1/ja active Application Filing
- 2011-06-10 KR KR1020127006046A patent/KR101386856B1/ko active IP Right Grant
- 2011-06-10 CN CN201180004081.7A patent/CN102625737B/zh active Active
- 2011-06-10 JP JP2012509406A patent/JP5866650B2/ja active Active
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001062603A (ja) | 1999-06-23 | 2001-03-13 | Mitsubishi Materials Corp | 断続重切削で硬質被覆層がすぐれた耐チッピング性を発揮する表面被覆炭化タングステン基超硬合金製切削工具 |
JP3661503B2 (ja) | 1999-06-23 | 2005-06-15 | 三菱マテリアル株式会社 | 断続重切削で硬質被覆層がすぐれた耐チッピング性を発揮する表面被覆炭化タングステン基超硬合金製切削工具 |
JP2001096404A (ja) | 1999-07-23 | 2001-04-10 | Mitsubishi Materials Corp | 断続重切削で硬質被覆層がすぐれた耐チッピング性を発揮する表面被覆炭化タングステン基超硬合金製切削工具 |
JP2002062603A (ja) | 2000-08-18 | 2002-02-28 | Fuji Photo Film Co Ltd | 画像読み取り装置 |
JP2006035383A (ja) * | 2004-07-28 | 2006-02-09 | Sumitomo Electric Hardmetal Corp | 表面被覆切削工具 |
WO2006064724A1 (ja) | 2004-12-14 | 2006-06-22 | Sumitomo Electric Hardmetal Corp. | 表面被覆切削工具 |
JP2009078309A (ja) | 2007-09-25 | 2009-04-16 | Mitsubishi Materials Corp | 表面被覆切削工具 |
WO2009081026A2 (fr) * | 2007-12-20 | 2009-07-02 | Saint-Gobain Centre De Recherches Et D'etudes Europeen | Particules de grenaillage |
JP2010137315A (ja) * | 2008-12-10 | 2010-06-24 | Sumitomo Electric Hardmetal Corp | 表面被覆切削工具 |
Non-Patent Citations (2)
Title |
---|
"The Society of Materials Science, Japan", 1981, YOKENDO CO., LTD., article "X-ray Stress Measurement Method", pages: 54 - 66 |
C. BARBATTI ET AL.: "Influence of micro-blasting on the microstructure and residual stresses of CVD K-A1203 coatings", SURFACE AND COATINGS TECHNOLOGY, vol. 203, no. 24, September 2009 (2009-09-01), pages 3708 - 3717, XP026284336 * |
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Also Published As
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CN102625737A (zh) | 2012-08-01 |
EP2638993B1 (en) | 2019-07-24 |
JPWO2012063515A1 (ja) | 2014-05-12 |
EP2638993A1 (en) | 2013-09-18 |
JP5866650B2 (ja) | 2016-02-17 |
KR101386856B1 (ko) | 2014-04-17 |
CN102625737B (zh) | 2014-12-17 |
US20120282049A1 (en) | 2012-11-08 |
EP2638993A4 (en) | 2017-12-20 |
KR20120094467A (ko) | 2012-08-24 |
US8715838B2 (en) | 2014-05-06 |
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