USRE40005E1 - Coated cutting insert - Google Patents

Coated cutting insert Download PDF

Info

Publication number
USRE40005E1
USRE40005E1 US11/449,887 US44988706A USRE40005E US RE40005 E1 USRE40005 E1 US RE40005E1 US 44988706 A US44988706 A US 44988706A US RE40005 E USRE40005 E US RE40005E
Authority
US
United States
Prior art keywords
layer
tic
thickness
cemented carbide
weight
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.)
Expired - Lifetime
Application number
US11/449,887
Inventor
Asa Kutscher
Kenneth Westergren
Björn Ljungberg
Anders Lenander
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sandvik Intellectual Property AB
Original Assignee
Sandvik Intellectual Property AB
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from SE9603264A external-priority patent/SE509560C2/en
Application filed by Sandvik Intellectual Property AB filed Critical Sandvik Intellectual Property AB
Priority to US11/449,887 priority Critical patent/USRE40005E1/en
Application granted granted Critical
Publication of USRE40005E1 publication Critical patent/USRE40005E1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C16/00Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/22Chemical 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
    • C23C16/30Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C29/00Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/02Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C16/00Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/02Pretreatment of the material to be coated
    • C23C16/0272Deposition of sub-layers, e.g. to promote the adhesion of the main coating
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C16/00Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/22Chemical 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
    • C23C16/30Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
    • C23C16/40Oxides
    • C23C16/403Oxides of aluminium, magnesium or beryllium
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/04Coating 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
    • C23C28/044Coating 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
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T407/00Cutters, for shaping
    • Y10T407/27Cutters, for shaping comprising tool of specific chemical composition
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24942Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24942Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495Thickness [relative or absolute]
    • Y10T428/24967Absolute thicknesses specified
    • Y10T428/24975No layer or component greater than 5 mils thick
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/25Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/25Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
    • Y10T428/252Glass or ceramic [i.e., fired or glazed clay, cement, etc.] [porcelain, quartz, etc.]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/26Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
    • Y10T428/263Coating layer not in excess of 5 mils thick or equivalent
    • Y10T428/264Up to 3 mils
    • Y10T428/2651 mil or less

Definitions

  • the present invention relates to a coated cutting tool (cemented carbide insert) particularly useful for the machining of cast iron parts by turning.
  • Cast iron materials may be divided into two main categories, grey cast iron and nodular cast iron. Cast iron materials typically often have an outer layer of cast skin, which may contain various inclusions of sand, rust and other impurities and also a surface zone which is decarburized and contains a larger amount of ferrite than the rest of the material.
  • Adhesive wear occurs when fragments or individual grains of the layer are pulled away from the cutting edge by the work piece chip formed.
  • the surface zone with high amounts of ferrite particularly puts severe demands on the adhesive properties of the coating and in combination with the inclusions in the cast skin on the work piece, causes notch wear at the depth of cut on the main cutting edge.
  • Another feature in the machining of grey cast iron is its sensitivity to excessive amounts of Co binder phase in the interface between the cemented carbide cutting insert and the coating. Excessive amounts of Co binder phase deteriorate the adhesion between coating and cemented carbide and lead to flaking of the coating during machining.
  • Swedish Application 9502640-7 (which corresponds to U.S. Ser. No. 08/675,034, our reference 024444-233) discloses a coated cutting insert tool of a cemented carbide body of a composition 5-11 weight % Co, ⁇ 10 weight %, preferably 1.5-7.5 weight %, cubic carbides of the metals Ti, Ta and/or Nb and balance WC, especially suited for machining of low alloyed steel components by turning.
  • a cutting tool insert comprising a coating and a cemented carbide body, said cemented carbide body comprising WC, 5-10 weight % Co and ⁇ 0.5 weight % cubic carbides of metals from groups IVb, Vb, or VIb of the periodic table with a highly W-alloyed binder phase having a CW-ratio of 0.8-0.9 and a surface composition of the cemented carbide body being well-defined, the amount of Co on the surface being within ⁇ 4 weight % to +4 weight % of the nominal Co content of the body and said coating comprising:
  • a method of making a cutting insert comprising a cemented carbide body and a coating wherein a WC-Co-based cemented carbide body is sintered, said sintering including a cooling step which at least to below 1200° C. is performed in a hydrogen atmosphere of pressure 0.4-0.9 bar and thereafter coating said sintered body with
  • the Figure is a micrograph in 2000 ⁇ magnification of a coated insert according to the present invention in which
  • a cemented carbide body with a highly W-alloyed binder phase a low content of cubic carbides and a well-defined surface composition resulting from a specific sintering process, a columnar TiC x N y O z layer, a textured ⁇ -Al 2 O 3 layer, a TiN layer, fulfilling the demands of easy identification of used edges, and a post-treatment of the coating cutting edge by brushing, an excellent cutting tool for machining of cast iron materials, especially grey cast iron, can be obtained.
  • a cutting tool insert is provided with a cemented carbide body of a composition 5-10 weight % Co, preferably 5-8 weight % Co, ⁇ 2 weight %, preferably ⁇ 0.5 weight %, most preferably 0 weight % cubic carbides of the metals Ti, Ta and/or Nb and balance WC.
  • the grain size of the WC is in the range of 1-2.5 ⁇ m.
  • the cemented carbide body has a CW-ratio of 0.75-0.93, preferably 0.80-0.90.
  • the cemented carbide body may contain small amounts, ⁇ 1 volume %, of eta phase (M 6 C), without any detrimental effect.
  • the surface composition of the cemented carbide insert is well-defined and the amount of Co on the surface is within ⁇ 4 weight % to +4 weight % of the nominal content.
  • the cemented carbide according to the present invention consists of WC and Co and has an about 100-350 ⁇ m wide, preferably 150-300 ⁇ m wide, binder phase depleted surface zone in which the binder phase content increases continuously and in a non-step-wise manner without maximum up to the nominal content of the binder phase in the inner portion of the cemented carbide body.
  • the average binder phase content in a 50 ⁇ m surface zone is 25%-75%, preferably 40%-60%, of the nominal binder phase content.
  • the coating comprises
  • a layer of TiC x N y O z , with x+y+z 1, with z ⁇ 0.5, preferably x>y, most preferably x>0.5 and 0.1 ⁇ z ⁇ 0.4, with a thickness of 0.1-2 ⁇ m and with equiaxed or needle-like grains with size ⁇ 0.5 ⁇ m, this layer being the same as or different from the innermost layer;
  • the edge of the coated insert is subjected to a brushing treatment giving a surface roughness R max ⁇ 0.4 ⁇ m over a length of 10 ⁇ m according to the method described in Swedish Application No. 9402543-4 (which corresponds to U.S. Ser. No. 08/497,934, our reference 024444-144).
  • This treatment removes the top layer of TiC x N y O z along the cutting edge line. It is also within the scope of this invention that the surface might be smoothed by a wet blasting treatment.
  • the ⁇ -Al 2 O 3 layer has a preferred crystal growth orientation in either the (104)-, (012)- or (110)-direction, preferably in the (012)-direction, as determined by X-ray Diffraction (XRD) measurements.
  • XRD X-ray Diffraction
  • TC for the set of (012), (104) or (110) crystal plans should be larger than 1.3, preferably larger than 1.5.
  • a WC-Co-based cemented carbide body having a highly W-alloyed binder phase with a CW-ratio of 0.75-0.93, preferably 0.8-0.9 is subjected to a conventional sintering process and removing the surface cobalt by etching as disclosed in U.S. Pat. No. 5,380,408.
  • cemented carbide consisting of WC and Co cooling at least to below 1200° C. may be performed in a hydrogen atmosphere of pressure 0.4-0.9 bar as disclosed in Swedish Application 9602750-3 (which corresponds to International Application No. PCT/SE97/01231).
  • the insert is coated with
  • edge line of the inserts in smoothed, e.g., by brushing the edges based on, e.g., SiC, as disclosed in Swedish Application 9402543-4.
  • the inserts are tested in a facing operation.
  • the workpiece material is nodular cast iron, SS717.
  • the workpiece shape causes intermittent cutting conditions during each revolution. Cutting speed is 250 m/min, feed 0.10 mm/rev and cutting depth is 2.0 mm.
  • the operation is performed using coolant.
  • This type of operation typically causes severe flaking of the coating.
  • the coating is torn off the insert in fragments.
  • the wear can be measured as the part of the edge line on which the coating has flaked off compared to the total length of the edge line used in the cutting operation.
  • Inserts of type A, B, D and E in Example 1 above are tested in an intermittent cutting operation in grey cast iron, SS0125.
  • the cutting conditions put high demands on the flaking resistance of the coating as well as the chemical and abrasive wear resistance of the coating.
  • the shaping of the work piece is such that for each revolution, two entrances in the work piece will be made giving intermittent cutting conditions.
  • Cutting speed is 300 m/min
  • cutting feed is 0.25 mm/rev
  • cutting depth is 2.0 mm.
  • the machining is made without using any coolant.
  • Example 2 The same cutting conditions is used as in Example 2 with inserts of type A, B, C, D and F from the same batches as in Example 1. In this test, coolant is used during machining.
  • Cemented carbide inserts of type A, B and G in Example 1 are tested in a turning test that causes deformation of the cutting edge leading to flaking of the coating and enhanced wear of the insert.
  • the test is performed in a nodular cast iron SS0737 and for a certain combination of feed and cutting depth in a longitudinal turning operation, the highest possible cutting rate before deformation of the cemented carbide occurs is sought.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Cutting Tools, Boring Holders, And Turrets (AREA)

Abstract

There is disclosed a coated cutting insert particularly useful for cutting in cast iron materials. The insert is characterized by a straight WC-Co cemented carbide body having a highly W-alloyed Co binder phase, a well-defined surface content of Co and a coating including an innermost layer of TiCxNyOz with columnar grains, a layer of a fine-grained, textured Al2O3 layer and a top layer of TiCxNyOz that has been removed along the cutting edge line.

Description

CROSS-REFERENCES TO RELATED APPLICATIONS
The present application is a reissue of U.S. Pat. No. 5,945,207, which claims the benefit of priority to Swedish Application No. 9603264-4 filed Sep. 6, 1996.
BACKGROUND OF THE INVENTION
The present invention relates to a coated cutting tool (cemented carbide insert) particularly useful for the machining of cast iron parts by turning.
Cast iron materials may be divided into two main categories, grey cast iron and nodular cast iron. Cast iron materials typically often have an outer layer of cast skin, which may contain various inclusions of sand, rust and other impurities and also a surface zone which is decarburized and contains a larger amount of ferrite than the rest of the material.
The wear when machining grey cast iron materials with Al2O3-coated cutting tools is dominated by chemical, abrasive and so-called adhesive wear. In order to protect the cutting tool against chemical wear, it is desirable to use as thick Al2O3 layers as possible. This is contradicted by the properties regarding adhesive wear that this type of layer generally possesses. Adhesive wear occurs when fragments or individual grains of the layer are pulled away from the cutting edge by the work piece chip formed. The surface zone with high amounts of ferrite particularly puts severe demands on the adhesive properties of the coating and in combination with the inclusions in the cast skin on the work piece, causes notch wear at the depth of cut on the main cutting edge.
Another feature in the machining of grey cast iron is its sensitivity to excessive amounts of Co binder phase in the interface between the cemented carbide cutting insert and the coating. Excessive amounts of Co binder phase deteriorate the adhesion between coating and cemented carbide and lead to flaking of the coating during machining.
Swedish Application 9502640-7 (which corresponds to U.S. Ser. No. 08/675,034, our reference 024444-233) discloses a coated cutting insert tool of a cemented carbide body of a composition 5-11 weight % Co, <10 weight %, preferably 1.5-7.5 weight %, cubic carbides of the metals Ti, Ta and/or Nb and balance WC, especially suited for machining of low alloyed steel components by turning.
OBJECTS AND SUMMARY OF THE INVENTION
It is an object of this invention to avoid or alleviate the problems of the prior art.
It is further an object of this invention to provide a coated cutting tool particularly useful for the machining of cast iron parts by turning.
In one aspect of the invention there is provided a cutting tool insert comprising a coating and a cemented carbide body, said cemented carbide body comprising WC, 5-10 weight % Co and <0.5 weight % cubic carbides of metals from groups IVb, Vb, or VIb of the periodic table with a highly W-alloyed binder phase having a CW-ratio of 0.8-0.9 and a surface composition of the cemented carbide body being well-defined, the amount of Co on the surface being within −4 weight % to +4 weight % of the nominal Co content of the body and said coating comprising:
    • a first, innermost, layer of TiCxNyOz with x+y+z=1 and y>x and z<0.1 with a thickness of 0.1-2 μm, and with equiaxed grains having a size <0.5
    • a layer of TiCxNyOz where x+y+z=1, and z=0, x>0.3 and y>0.3, with a thickness of 5-10 μm with columnar grains having a diameter of <2 μm;
    • a layer of TiCxNyOz where x+y+z=1, z<0.5 and x>y with a thickness of 0.1-2 μm and with equiaxed or needle-like grains having a size <0.5 μm;
    • a layer of smooth, texture, fine-grained α-Al2O3 having a grain size of 0.5-2 μm with a thickness of 3-6 μm; and
    • an outer layer of TiCxNyOz where x+y+z=1, z<0.05 with a thickness of 0.5-3 μm and a grain size <1 μm, the outer coating layer having been removed in at least the edge line so that the Al2O3 layer is on top along the cutting edge line and the outer layer of TiCxNyOz is the top layer on the clearance side.
In another aspect of the invention there is provided a method of making a cutting insert comprising a cemented carbide body and a coating wherein a WC-Co-based cemented carbide body is sintered, said sintering including a cooling step which at least to below 1200° C. is performed in a hydrogen atmosphere of pressure 0.4-0.9 bar and thereafter coating said sintered body with
    • a first, innermost, layer of TiCxNyOz with a thickness of 0.1-2 μm, with equiaxed grains with size <0.5 μm by CVD;
    • a layer of TiCxNyOz with a thickness of 4-12 μm with columnar grains and with a diameter of <5 μm deposited by MTCVD technique, using acetonitrile as the carbon and nitrogen source for forming the layer in a temperature range of 850°-900° C.;
    • a layer of TiCxNyOz with a thickness of 0.1-2 μm with equiaxed or needle-like grains with size <0.5 μm, using CVD;
    • a layer of a smooth textured α-Al2O3 textured in the direction (012), (104) or (110) with a thickness of 3-8 μm using CVD; and
    • an outer layer of TiCxNyOz with a thickness of 0.5-3 μm, using CVD and thereafter removing the outer layer of TiCxNyOz on at least the cutting edge line so that the Al2O3 layer is on top along the cutting edge line and the outer layer of TiCxNyOz is the top layer on the clearance side of the cutting insert.
BRIEF DESCRIPTION OF THE DRAWINGS
The Figure is a micrograph in 2000× magnification of a coated insert according to the present invention in which
    • A—cemented carbide body
    • B—TiCxNyOz layer with equiaxed grains
    • C—TiCxNyOz layer with columnar grains
    • D—TiCxNyOz layer with equiaxed or needle-like grains
    • E—textured Al2O3 layer with columnar-like grains
    • F—TiN layer
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS OF THE INVENTION
It has surprisingly been found that by combining the following features: a cemented carbide body with a highly W-alloyed binder phase, a low content of cubic carbides and a well-defined surface composition resulting from a specific sintering process, a columnar TiCxNyOz layer, a textured α-Al2O3 layer, a TiN layer, fulfilling the demands of easy identification of used edges, and a post-treatment of the coating cutting edge by brushing, an excellent cutting tool for machining of cast iron materials, especially grey cast iron, can be obtained.
According to the present invention, a cutting tool insert is provided with a cemented carbide body of a composition 5-10 weight % Co, preferably 5-8 weight % Co, <2 weight %, preferably <0.5 weight %, most preferably 0 weight % cubic carbides of the metals Ti, Ta and/or Nb and balance WC. The grain size of the WC is in the range of 1-2.5 μm. The cobalt binder phase is highly alloyed with W. The content of W in the binder phase can be expressed as the
CW-ratio=Ms/(weight % Co×0.0161),
    • where Ms is the measured saturation magnetization of the cemented carbide body in kA/m hAm2 /kg and
    • weight % Co is the weight percentage of Co in the cemented carbide. The CW-value is a function of the W content in the Co binder phase. A low CW-value corresponds to a high W-content in the binder phase.
It has now been found according to the present invention that improved cutting performance is achieved, if the cemented carbide body has a CW-ratio of 0.75-0.93, preferably 0.80-0.90. The cemented carbide body may contain small amounts, <1 volume %, of eta phase (M6C), without any detrimental effect.
The surface composition of the cemented carbide insert is well-defined and the amount of Co on the surface is within −4 weight % to +4 weight % of the nominal content.
Alternatively, the cemented carbide according to the present invention consists of WC and Co and has an about 100-350 μm wide, preferably 150-300 μm wide, binder phase depleted surface zone in which the binder phase content increases continuously and in a non-step-wise manner without maximum up to the nominal content of the binder phase in the inner portion of the cemented carbide body. The average binder phase content in a 50 μm surface zone is 25%-75%, preferably 40%-60%, of the nominal binder phase content.
The coating comprises
    • a first, innermost, layer of TiCxNyOz with x+y+z=1, preferably y>x and z<0.1, most preferably y>0.8 and z=0, with a thickness of 0.1-2 μm, and with equiaxed grains with size <0.5 μm. In an alternative embodiment, the TiCxNyOz layer preferably has the composition z<0.5 and y<0.1, most preferably 0.1<z<0.5 and y=0;
    • a layer of TiCxNyOz with x+y+z=1, preferably with z=0, x>0.3 and y>0.3, most preferably x>0.5, with a thickness of 4-12 μm, preferably 5-10 μm, most preferably 6-9 μm with columnar grains and with a diameter of <5 μm, preferably <2 μm;
a layer of TiCxNyOz, with x+y+z=1, with z<0.5, preferably x>y, most preferably x>0.5 and 0.1<z<0.4, with a thickness of 0.1-2 μm and with equiaxed or needle-like grains with size <0.5 μm, this layer being the same as or different from the innermost layer;
    • a layer of textured, fine-grained (with average grain size 0.5-2 μm) α-Al2O3 layer with a thickness of 3-8 μm, preferably 3-6 μm; and
    • an outer layer of TiCxNyOz. This TiCxNyOz layer comprises one or more layers with the composition x+y+z=1, z<0.05, preferably y>x. Alternatively, this outer layer can be a multilayer of TiN/TiC/TiN in one or several sequences and a total thickness of 0.5-3 μm, preferably 1-2 μm. This layer exhibits a grain size <1 μm.
In order to obtain a smooth cutting edge line suitable for machining, the edge of the coated insert is subjected to a brushing treatment giving a surface roughness Rmax≦0.4 μm over a length of 10 μm according to the method described in Swedish Application No. 9402543-4 (which corresponds to U.S. Ser. No. 08/497,934, our reference 024444-144). This treatment removes the top layer of TiCxNyOz along the cutting edge line. It is also within the scope of this invention that the surface might be smoothed by a wet blasting treatment.
Furthermore, as disclosed in U.S. Pat. No. 5,654,035 or Swedish Applications 9304283-6 (which corresponds to U.S. Ser. No. 08/348,084, our reference 024444-092) or 9400089-0 (which corresponds to U.S. Ser. No. 08/366,107, our reference 024444-093), the α-Al2O3 layer has a preferred crystal growth orientation in either the (104)-, (012)- or (110)-direction, preferably in the (012)-direction, as determined by X-ray Diffraction (XRD) measurements. A Texture Coefficient (TC) can be defined as: TC ( hkl ) = I ( hkl ) I o ( hkl ) { 1 n I ( hkl ) I o ( hkl ) } - 1
where
    • I(hkl)=measured intensity of the (hkl) reflection
    • Io(hkl)=standard intensity of the ASTM standard powder pattern diffraction data
    • n=number of reflections used in the calculation, (hkl)
    • reflections used are: (012), (104), (110), (113), (024), (116)
TC for the set of (012), (104) or (110) crystal plans should be larger than 1.3, preferably larger than 1.5.
According to the method of the present invention, a WC-Co-based cemented carbide body having a highly W-alloyed binder phase with a CW-ratio of 0.75-0.93, preferably 0.8-0.9, is subjected to a conventional sintering process and removing the surface cobalt by etching as disclosed in U.S. Pat. No. 5,380,408. Alternatively, for cemented carbide consisting of WC and Co cooling at least to below 1200° C. may be performed in a hydrogen atmosphere of pressure 0.4-0.9 bar as disclosed in Swedish Application 9602750-3 (which corresponds to International Application No. PCT/SE97/01231).
The insert is coated with
    • a first, innermost, layer of TiCxNyOz with x+y+z=1, preferably y>x and z<0.1, most preferably y>0.8 and z=0, with a thickness of 0.1-2 μm, and with equiaxed grains with size <0.5 μm. In an alternative embodiment, the TiCxNyOz layer preferably has the composition z<0.5 and y<0.1, most preferably 0.1<z<0.5 and y=0;
    • a layer of TiCxNyOz, with x+y+z=1, preferably with z0, x>0.3 and y>0.3, most preferably x>0.5, with a thickness of 4-12 μm, preferably 5-10 μm, with columnar grains and with a diameter of <5 μm, preferably <2 μm, deposited preferably by MTCVD technique (using acetonitrile as the carbon and nitrogen source for forming the layer in the temperature range of 700-900° C.). The exact conditions, however, depend to a certain extent on the design of the equipment used;
    • a layer of TiCxNyOz, with x+y+z=1, with z<0.5, preferably x>y, most preferably x>0.5 and 0.1<z<0.4, with a thickness of 0.1-2 μm and with equiaxed or needle-like grains with size <0.5 μm, using known CVD methods, this layer being the same as or different from the innermost layer;
    • an intermediate layer of a smooth textured α-Al2O3 according to U.S. Pat. No. 5,654,035 or Swedish Applications 9304283-6 or 9400089-0 with a thickness of 3-8 μm, preferably 3-6 μm; and
    • an outer layer of TiCxNyOz, comprising one or several individual layers each with composition x+y+z=1 and z<0.05, preferably y>x. Alternatively, this outer layer comprises a multilayer of TiN/TiC/TiN in one or several sequences. The total coating thickness of these outer layers is 0.5-3.0 μm, preferably 0.5-2 μm. The grain size in this outer layer is <1.0 μm.
The edge line of the inserts in smoothed, e.g., by brushing the edges based on, e.g., SiC, as disclosed in Swedish Application 9402543-4.
When a TiCxNyOz layer with z>0 is desired, CO2 and/or CO are/is added to the reaction gas mixture.
The invention is additionally illustrated in connection with the following Examples which are to be considered as illustrative of the present invention. It should be understood, however, that the invention is not limited to the specific details of the Examples.
EXAMPLE 1
Inserts are made as follows:
    • A. Cemented carbide cutting tool inserts of style CNMG 120412-KM with the composition 6.0 weight % Co and balance WC are sintered in a conventional way at 1410° C. and cooled down to 1200° C. in 0.6 bar H2 giving inserts with a binder phase highly alloyed with W, corresponding to a CW-ratio of 0.085 and a Co-content on the surface corresponding to 7 weight % as measured with Energy Dispersive Spectroscopy. After conventional ER-treating, the inserts are coated with a 0.5 μm equiaxed TiCxNyOz layer, x=0.1, y=0.9, z=0 and an average grain size of about 0.2 μm, followed by a 8.0 μm thick TiCxNyOz layer, x=0.55, y=0.45, with columnar grains with an average grain size of 2.5 μm, by using MTCVD technique (process temperature 850° C. and CH3CN as the carbon/nitrogen source). In subsequent process steps during the same coating cycle, a 1 μm thick layer of TiCxNyOz (about x=0.6, y=0.2 and z=0.2) with equiaxed grains and an average grain size of 0.2 μm is deposited followed by a 5.0 μm thick layer of (012)-textured α-Al2O3, with average grain size of about 1.2 μm, deposited according to conditions given in U.S. Pat. No. 5,654,035. On top of the α-Al2O3 layer, TiN/TiC/TiN/TiC/TiN is deposited in a multilayer structure with a total coating thickness of 1.5 μm, the average grain size <0.3 μm in each individual layer. Finally, the inserts are subjected to a brushing treatment in which the cutting edge lines are smoothed with a 320 mesh brush containing SiC as grinding material, the outer TiN/TiC multilayer is removed by the brushing treatment along the cutting edge line.
    • B. Cemented carbide cutting tool inserts of style CNMG 120412-KM with the composition 6.0 weight % Co and balance WC are coated under the procedure described for insert A. The cemented carbide body has a CW-ratio of 0.88 and is subjected to a conventional sintering without H2 during the cooling step. Prior to the coating process, the inserts are subjected to surface cleaning involving an electrolytic etching process according to U.S. Pat. No. 5,380,408. The Co content on the insert surface is about 5 weight % as measured with Energy Dispersive Spectroscopy. The cemented carbide has an about 250 μm wide binder phase depleted surface zone in which the binder phase content increased continuously and in a non-step-wise manner without maximum up to the nominal content of the binder phase in the inner portion of the cemented carbide. The average binder phase content in a 25 μm surface zone is 3 weight %. The inserts are subjected to the same final brushing treatment as for insert A.
    • C. Cemented carbide cutting tool inserts of style CNMG 120412-KM from the same batch as in insert A are coated with a 4 μm equiaxed layer of TiC with grain size <2.0 μm, followed by a 6 μm thick layer of Al2O3 according to prior art technique. XRD analysis shows that the Al2O3 layer consists of a mixture of α- and κ-Al2O3, in the ratio of about 60/40, the α-Al2O3 showing no preferred growth orientation as measured by XRD. The grain size of the κ-Al2O3 is 2.0 μm while the α-Al2O3 exhibited grains up to 5.5 μm.
    • D. Cemented carbide cutting tool inserts from the same batch as insert C. The inserts are subjected to a wet blasting treatment after coating.
    • E. Cemented carbide cutting tool inserts of style CNMG 120412-KM from the same batch as insert A are coated with a 2 μm equiaxed layer of TiCxNyOz, the average grain size of this layer is 0.2 μm, followed by a 8 μm thick columnar TiCN deposited according to prior art technique, the grain size in this coating being about 3.0 μm and a 6 μm thick layer of (012)-textured α-Al2O3 deposited according to the same process conditions as for insert A. The inserts are subjected to the same brushing treatment as insert A prior to machining.
    • F. Cemented carbide cutting tool inserts of style CNMG 120412-KM with the composition of 6 weight % Co, 4 weight % cubic carbides and balance WC are subjected to the same coating process as in insert A. The CW-ratio of the inserts is 0.88, they are subjected to a sintering process using H2 during the cooling step, and the Co content on the surface is 9% as measured by Energy Dispersive Spectroscopy. The inserts are subjected to the same final brushing treatment as insert A.
    • G. Cemented carbide cutting inserts of style CNMG 120412-KM with the composition of 6.0 weight % Co and balance WC are coated under the procedure described for insert E. The cemented carbide has a CW-ratio of 0.98 and the inserts are subjected to a conventional sintering without H2 during the cooling step. The inserts are ER-treated and cleaned in conventional processes. The Co content on the surface prior to coating is 30 weight % as measured with Energy Dispersive Spectroscopy. The inserts are subjected to the same final brushing treatment as in insert A.
The inserts are tested in a facing operation. The workpiece material is nodular cast iron, SS717. The workpiece shape causes intermittent cutting conditions during each revolution. Cutting speed is 250 m/min, feed 0.10 mm/rev and cutting depth is 2.0 mm. The operation is performed using coolant.
This type of operation typically causes severe flaking of the coating. The coating is torn off the insert in fragments. The wear can be measured as the part of the edge line on which the coating has flaked off compared to the total length of the edge line used in the cutting operation.
Insert Type % of Edge Line with Flaking
A <5
B <5
C 100
D 70
E 25
F 20
G 50
EXAMPLE 2
Inserts of type A, B, D and E in Example 1 above are tested in an intermittent cutting operation in grey cast iron, SS0125. The cutting conditions put high demands on the flaking resistance of the coating as well as the chemical and abrasive wear resistance of the coating. The shaping of the work piece is such that for each revolution, two entrances in the work piece will be made giving intermittent cutting conditions. Cutting speed is 300 m/min, cutting feed is 0.25 mm/rev and cutting depth is 2.0 mm. The machining is made without using any coolant.
Number of Passes Before
Insert Type the Edge Was Worn Out
A 60
B 55
D 48
E 48
EXAMPLE 3
The same cutting conditions is used as in Example 2 with inserts of type A, B, C, D and F from the same batches as in Example 1. In this test, coolant is used during machining.
Insert Type Number of Passes State of the Edge
A 60 minor chipping of edge line
not worn out
B 60 undamaged edge line
not worn out
C 48 fracture in cutting edge
insert worn out
D 24 fracture in cutting edge
insert worn out
F 24 fracture in cutting edge
insert worn out
EXAMPLE 4
Cemented carbide inserts of type A, B and G in Example 1 are tested in a turning test that causes deformation of the cutting edge leading to flaking of the coating and enhanced wear of the insert. The test is performed in a nodular cast iron SS0737 and for a certain combination of feed and cutting depth in a longitudinal turning operation, the highest possible cutting rate before deformation of the cemented carbide occurs is sought.
Insert Type Highest Possible Cutting Speed
A 475 m/min
B 450 m/min
G 400 m/min
The principles, preferred embodiments and modes of operation of the present invention have been described in the foregoing specification. The invention which is intended to be protected herein, however, is not to be construed as limited to the particular forms disclosed, since these are to be regarded as illustrative rather than restrictive. Variations and changes may be made by those skilled in the art without departing from the spirit of the invention.

Claims (14)

1. A cutting tool insert comprising a coating and a cemented carbide body, said cemented carbide body comprising WC, 5-10 weight % Co and <0.5 weight % cubic carbides of metals from groups IVb, Vb, or VIb of the periodic table with a highly W-alloyed binder phase having a CW-ratio of 0.75-0.93 and a surface composition of the cemented carbide body being well-defined, the amount of Co on the surface being within −4 weight % to +4 weight % of the nominal Co content of the body and said coating comprising:
a first, innermost, layer of TiCxNyOz with x+y+z=1 and y>x and z<0.1, with a thickness of 0.1-2 μm, and with equiaxed grains having a size <0.5 μm;
a layer of TiCxNyOz where x+y+z=1, and z=0, x>0.3 and y>0.3, with a thickness of 5-10 μm with columnar grains having a diameter of <2 μm;
a layer of TiCxNyOz where x+y+z=1, z<0.5 and x>y with a thickness of 0.1-2 μm and with equiaxed or needle-like grains having a size <0.5 μm;
a layer of smooth, textured, fine-grained α-Al2O3 having a grain size of 0.5-2 μm with a thickness of 3-6 μm; and
an outer layer of TiCxNyOz where x+y+z=1, z<0.05 with a thickness of 0.5-3 μm and a grain size <1 μm, the outer coating layer having been removed in at least the edge line so that the Al2O3 layer is on top along the cutting edge line and the outer layer of TiCxNyOz is the top layer on the clearance side.
2. The cutting tool insert of claim 1 wherein the α-Al2O3 layer has a texture in (012)-direction and a texture coefficient TC(012) larger than 1.3.
3. A cutting tool insert comprising a coating and a cemented carbide body, said cemented carbide body comprising WC, 5-10 weight % Co and <0.5 weight % cubic carbides of metals from groups IVb, Vb, or VIb of the periodic table with a highly W-alloyed binder phase having a CW-ratio of 0.75-0.93 and a surface composition of the cemented carbide body being well-defined, the amount of Co on the surface being within −4 weight % to +4 weight % of the nominal Co content of the body and said coating comprising:
a first, innermost, layer of TiCxNyOz with x+y+z=1 and z<0.5 and y<0.1 with a thickness of 0.1-2 μm, and with equiaxed grains having a size <0.5 μm;
a layer of TiCxNyOz where x+y+z=1, and z=0, x>0.3 and y>0.3, with a thickness of 5-10 μm with columnar grains having a diameter of <2 μm;
a layer of TiCxNyOz where x+y+z=1, z<0.5 and x>y with a thickness of 0.1-2 μm and with equiaxed or needle-like grains having a size <0.5 μm;
a layer of smooth, textured, fine-grained α-Al2O3 having a grain size of 0.5-2 μm with a thickness of 3-6 μm; and
an outer layer of TiCxNyOz where x+y+z=1, z<0.05 with a thickness of 0.5-3 μm and a grain size <1 μm, the outer coating layer having been removed in at least the edge line so that the Al2O3 layer is on top along the cutting edge line and the outer layer of TiCxNyOz is the top layer on the clearance side.
4. The cutting tool insert of claim 1 wherein the outer TiCxNyOz layer comprises a multilayer of TiN/TiC/TiN.
5. The cutting tool insert of claim 1 wherein the binder phase has a CW ratio of from 0.8-0.9.
6. The cutting tool insert of claim 1 wherein the cobalt content of the cemented carbide body is 5-8 weight %.
7. A method of making a cutting insert comprising a cemented carbide body and a coating wherein a WC-Co-based cemented carbide body is sintered, said sintering including a cooling step which at least to below 1200° C. is performed in a hydrogen atmosphere of pressure 0.4-0.9 bar and thereafter coating said sintered body with
a first, innermost, layer of TiCxNyOz with a thickness of 0.1-2 μm, with equiaxed grains with size <0.5 μm by CVD;
a layer of TiCxNyOz with a thickness of 4-12 μm with columnar grains and with a diameter of <5 μm deposited by MTCVD technique, using acetonitrile as the carbon and nitrogen source for forming the layer in a temperature range of 850-900° C.;
a layer of TiCxNyOz with a thickness of 0.1-2 μm with equiaxed or needle-like grains with size <0.5 μm, using CVD;
a layer of a smooth textured α-Al2O3 textured in the direction (012), (104) or (110) with a thickness of 3-8 μm using CVD; and
an outer layer of TiCxNyOz with a thickness of 0.5-3 μm, using CVD and thereafter removing the outer layer of TiCxNyOz on at least the cutting edge line so that the Al2O3 layer is on top along the cutting edge line and the outer layer of TiCxNyOz is the top layer on the clearance side of the cutting insert.
8. The cutting tool insert of claim 3 wherein the α-Al2 O 3 layer has a texture in (012)-direction and a texture coefficient TC(012) larger than 1.3.
9. The cutting tool insert of claim 3 wherein the outer TiCx N y O z layer comprises a multilayer of TiN/TiC/TiN.
10. The cutting tool insert of claim 3 wherein the binder phase has a CW ratio of from 0.8-0.9.
11. The cutting tool insert of claim 3 wherein the cobalt content of the cemented carbide body is 5-8 weight %.
12. The cutting tool insert of claim 7 wherein the outer TiCx N y O z layer comprises a multilayer of TiN/TiC/TiN.
13. The cutting tool insert of claim 7 wherein the binder phase has a CW ratio of from 0.8-0.9.
14. The cutting tool insert of claim 7 wherein the cobalt content of the cemented carbide body is 5-8 weight %.
US11/449,887 1996-09-06 2006-06-09 Coated cutting insert Expired - Lifetime USRE40005E1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US11/449,887 USRE40005E1 (en) 1996-09-06 2006-06-09 Coated cutting insert

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE9603264A SE509560C2 (en) 1996-09-06 1996-09-06 Coated cemented carbide inserts for machining cast iron
US08/923,922 US5945207A (en) 1996-09-06 1997-09-05 Coated cutting insert
US11/449,887 USRE40005E1 (en) 1996-09-06 2006-06-09 Coated cutting insert

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US08/923,922 Reissue US5945207A (en) 1996-09-06 1997-09-05 Coated cutting insert

Publications (1)

Publication Number Publication Date
USRE40005E1 true USRE40005E1 (en) 2008-01-15

Family

ID=38921122

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/449,887 Expired - Lifetime USRE40005E1 (en) 1996-09-06 2006-06-09 Coated cutting insert

Country Status (1)

Country Link
US (1) USRE40005E1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070283554A1 (en) * 2004-07-12 2007-12-13 Sandvik Intellectual Property Ab Cutting tool insert
US8080323B2 (en) 2007-06-28 2011-12-20 Kennametal Inc. Cutting insert with a wear-resistant coating scheme exhibiting wear indication and method of making the same

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5135801A (en) 1988-06-13 1992-08-04 Sandvik Ab Diffusion barrier coating material
JPH06108254A (en) 1992-09-28 1994-04-19 Mitsubishi Materials Corp Cutting tool made of surface-coated wc-base sintered hard alloy
EP0594875A1 (en) 1992-10-22 1994-05-04 Mitsubishi Materials Corporation Multilayer coated hard alloy cutting tool
US5310605A (en) 1992-08-25 1994-05-10 Valenite Inc. Surface-toughened cemented carbide bodies and method of manufacture
US5380408A (en) 1991-05-15 1995-01-10 Sandvik Ab Etching process
EP0653499A1 (en) 1993-05-31 1995-05-17 Sumitomo Electric Industries, Ltd. Coated cutting tool and method for producing the same
US5453241A (en) 1991-02-05 1995-09-26 Sandvik Ab Cemented carbide body with extra tough behavior
EP0685572A2 (en) 1994-05-31 1995-12-06 Mitsubishi Materials Corporation Coated hard-alloy blade member
EP0693574A1 (en) 1994-07-20 1996-01-24 Sandvik Aktiebolag Aluminium oxide coated tool
US5487625A (en) 1992-12-18 1996-01-30 Sandvik Ab Oxide coated cutting tool
EP0709484A1 (en) 1994-10-20 1996-05-01 Mitsubishi Materials Corporation Coated tungsten carbide-based cemented carbide blade member
US5674564A (en) 1991-06-25 1997-10-07 Sandvik Ab Alumina-coated sintered body
US5766782A (en) 1994-01-14 1998-06-16 Sandvik Ab Aluminum oxide coated cutting tool and method of manufacturing thereof

Patent Citations (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5135801A (en) 1988-06-13 1992-08-04 Sandvik Ab Diffusion barrier coating material
US5453241A (en) 1991-02-05 1995-09-26 Sandvik Ab Cemented carbide body with extra tough behavior
US5380408A (en) 1991-05-15 1995-01-10 Sandvik Ab Etching process
US5674564A (en) 1991-06-25 1997-10-07 Sandvik Ab Alumina-coated sintered body
US5310605A (en) 1992-08-25 1994-05-10 Valenite Inc. Surface-toughened cemented carbide bodies and method of manufacture
JPH06108254A (en) 1992-09-28 1994-04-19 Mitsubishi Materials Corp Cutting tool made of surface-coated wc-base sintered hard alloy
EP0594875A1 (en) 1992-10-22 1994-05-04 Mitsubishi Materials Corporation Multilayer coated hard alloy cutting tool
US5487625A (en) 1992-12-18 1996-01-30 Sandvik Ab Oxide coated cutting tool
US5654035A (en) 1992-12-18 1997-08-05 Sandvik Ab Method of coating a body with an α-alumina coating
EP0653499A1 (en) 1993-05-31 1995-05-17 Sumitomo Electric Industries, Ltd. Coated cutting tool and method for producing the same
US5766782A (en) 1994-01-14 1998-06-16 Sandvik Ab Aluminum oxide coated cutting tool and method of manufacturing thereof
EP0685572A2 (en) 1994-05-31 1995-12-06 Mitsubishi Materials Corporation Coated hard-alloy blade member
EP0693574A1 (en) 1994-07-20 1996-01-24 Sandvik Aktiebolag Aluminium oxide coated tool
EP0709484A1 (en) 1994-10-20 1996-05-01 Mitsubishi Materials Corporation Coated tungsten carbide-based cemented carbide blade member
US5652045A (en) 1994-10-20 1997-07-29 Mitsubishi Materials Corporation Coated tungsten carbide-based cemented carbide blade member

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
English Translation of JP 25282-1978.
Patent Abstracts of Japan, abstract of JP, A, 60110840, published Jun. 17, 1985.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070283554A1 (en) * 2004-07-12 2007-12-13 Sandvik Intellectual Property Ab Cutting tool insert
US8080323B2 (en) 2007-06-28 2011-12-20 Kennametal Inc. Cutting insert with a wear-resistant coating scheme exhibiting wear indication and method of making the same

Similar Documents

Publication Publication Date Title
US5945207A (en) Coated cutting insert
EP1788123B1 (en) Coated cutting tool insert
US6333098B1 (en) Coated cutting insert
EP0753603B1 (en) Coated cutting insert
USRE39987E1 (en) Coated turning insert
EP0870073B1 (en) Coated cutting insert and method of making it
US6638609B2 (en) Coated inserts for rough milling
USRE39884E1 (en) Coated milling insert and method of making it
US7135221B2 (en) Coated cutting insert for rough turning
US8043729B2 (en) Coated cutting tool insert
USRE39999E1 (en) Coated turning insert and method of making it
EP2014789A1 (en) Coated cutting tool
US20070292672A1 (en) Coated inserts
EP1218558B1 (en) Coated milling insert
EP1997938A2 (en) Coated cutting tool insert
JP2000514370A (en) Coated cutting inserts
EP1676939A1 (en) Coated cutting insert
US7150772B2 (en) CVD coated cutting tool insert
US20060188748A1 (en) Cemented carbide insert for wear resistance demanding short hole drilling operations
EP1352697B1 (en) Coated cutting tool insert
USRE40005E1 (en) Coated cutting insert

Legal Events

Date Code Title Description
FPAY Fee payment

Year of fee payment: 12