WO2009070107A1 - Coated cutting tool insert - Google Patents

Coated cutting tool insert Download PDF

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Publication number
WO2009070107A1
WO2009070107A1 PCT/SE2008/051354 SE2008051354W WO2009070107A1 WO 2009070107 A1 WO2009070107 A1 WO 2009070107A1 SE 2008051354 W SE2008051354 W SE 2008051354W WO 2009070107 A1 WO2009070107 A1 WO 2009070107A1
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WO
WIPO (PCT)
Prior art keywords
layer
tic
cutting tool
rake face
thickness
Prior art date
Application number
PCT/SE2008/051354
Other languages
French (fr)
Inventor
Rolf Olofsson
Björn Ljungberg
Henrik Nordlund
Gunilla Anderson
Alexandra Kusoffsky
Original Assignee
Sandvik Intellectual Property Ab
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Publication date
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Publication of WO2009070107A1 publication Critical patent/WO2009070107A1/en

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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
    • C23C16/56After-treatment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B27/00Tools for turning or boring machines; Tools of a similar kind in general; Accessories therefor
    • B23B27/14Cutting tools of which the bits or tips or cutting inserts are of special material
    • 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
    • C23C30/00Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • C23C30/005Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process on hard metal substrates
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B2224/00Materials of tools or workpieces composed of a compound including a metal
    • B23B2224/04Aluminium oxide
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B2224/00Materials of tools or workpieces composed of a compound including a metal
    • B23B2224/32Titanium carbide nitride (TiCN)
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B2228/00Properties of materials of tools or workpieces, materials of tools or workpieces applied in a specific manner
    • B23B2228/10Coatings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B2228/00Properties of materials of tools or workpieces, materials of tools or workpieces applied in a specific manner
    • B23B2228/10Coatings
    • B23B2228/105Coatings with specified thickness

Definitions

  • the present invention relates to a high performance coated cutting tool insert particularly useful for turning at stable conditions in unalloyed and low alloyed steels in wet and dry conditions, having the ability to withstand high temperatures, resulting from, e.g., extended times in cut or high metal removal.
  • the majority of today's cutting tools are based on a cemented carbide insert coated with several hard layers like TiC, TiC x N y , TiN, TiC ⁇ N y O z and Al 2 O 3 .
  • the sequence and the thickness of the individual layers are carefully chosen to suit different cutting application areas and work-piece materials.
  • the most frequent employed coating techniques are Chemical Vapour Deposition (CVD) and Physical Vapour Deposition (PVD) .
  • the CVD technique is conducted at a rather high temperature range, conventionally 950-1050 0 C. Due to this high deposition temperature and to a mismatch in the coefficients of thermal expansion between the deposited coating materials and the cemented carbide tool insert, CVD can lead to coatings with cooling cracks and high tensile stresses (sometimes up to 1000 MPa) .
  • the high tensile stresses can under some cutting conditions be a disadvantage as it may cause the cooling cracks to propagate further into the cemented carbide body and cause breakage of the cutting edge.
  • Every post treatment technique that exposes a surface, e.g., a coating surface to a mechanical impact as, e.g., wet or dry blasting will influence the surface finish and the stress state ( ⁇ ) of the coating.
  • a very intensive treatment may even lead to a big change in the stress state, e.g., from highly tensile to highly compressive as disclosed in EP-A-I 311 712, in which a dry blasting technique is used.
  • the blasting media e.g., AI2O3 grits, have to strike the coating surface with a high impulse.
  • a post treatment comprising intensive wet blasting with a sufficiently high energy can give the coating a favourable tensile stress level, i.e., create tensile stress relaxation, and give the Al 2 ⁇ 3 -layer a top surface with an excellent surface finish.
  • a coated cutting tool insert of cemented carbide comprising a body having at least one rake face and at least one clearance face wherein said insert has a composition of 4.0-5.3, preferably 4.4-5.25, most preferably 4.8-5.2, wt-% Co, 4.6-8.1 wt-% cubic carbides, balance WC and a hardness HV3 of 1590-1650.
  • the cobalt binder phase is highly alloyed with W.
  • a low CW- ratio corresponds to a high W-content in the Co binder phase.
  • the CW-ratio is in the range 0.80-0.88, and the body has a surface zone of a thickness of 10-16 ⁇ m, preferably 10-15 ⁇ m, depleted from the cubic carbides TiC, TaC and/or NbC.
  • the TiC ⁇ N y -layer has a thickness of from 4 to 12 ⁇ m, preferably from 5 to 7 ⁇ m or from 9 to 11 ⁇ m, and a tensile stress level of 50-500, preferably 50-450, MPa and
  • the ⁇ -Al 2 ⁇ 3-layer has a thickness of from 8 to 12 ⁇ m, preferably from 9 to 11 ⁇ m and a mean Ra value
  • MRa ⁇ 0.12 ⁇ m, preferably ⁇ 10 ⁇ m, at least in the chip contact zone on the rake face, and on said at least one clearance face
  • the TiC ⁇ N y -layer has a tensile stress in the range 500-700 MPa and
  • the ⁇ -Al 2 O 3 -layer is covered with a thin 0.1-1 ⁇ m TiN, TiC x N ⁇ ZrC x Ny or TiC layer giving the insert a different colour on this face .
  • the coating on the rake face and along the cutting edge line is intensively wet blasted with a sufficiently high energy to create tensile stress relaxation in both the A1 2 C>3- and the TiC x N y - layers.
  • the outermost A1 2 C>3 layer has a very smooth surface at least in the chip contact zone on the rake face.
  • additional layers can be incorporated into the coating structure between the substrate and the layers, composed of metal nitrides and/or carbides and/or oxides with the metal elements selected from Ti, Nb, Hf, V, Ta, Mo, Zr, Cr, W and Al to a total coating thickness of ⁇ 5 ⁇ m.
  • the cutting tool insert is, thus, provided with a CVD-coating comprising a penultimate TiC x N y - layer and an outer ⁇ -Al 2 ⁇ 3 -layer .
  • the AI2O3 can be produced according to patent EP 603 144 giving the Al 2 ⁇ 3 -layer a crystallographic texture in 012-direction with a texture coefficient TC (012) >1.3, preferably >1.5, or produced according to patents US 5,851,687 and US 5,702,808 giving a texture in the 110-direction with texture coefficient TC(110)>1.5.
  • the AI2O3 is produced according to patent EP 738 336 giving the Al 2 ⁇ 3-layer a crystallographic texture in 104-direction with a texture coefficient TC (104) > 2.0, preferably TC(104)>2.5.
  • the insert has a different colour on the clearance side than on the black rake face.
  • the insert is then blasted removing the top layer exposing the black Al 2 U 3 -layer.
  • the coating is subjected to a wet blasting operation with a slurry consisting of F150 grits (FEPA-standard) of AI2O3 in water at an air pressure of 2.2-2.6 bar for about 10-20 sec/insert.
  • the spray guns are placed approximately 100 mm from the inserts with a 90° spray angle.
  • the coating on the rake face will have the low desired tensile stress 50-500 MPa while the clearance side will have high tensile stresses in the range 500-700 MPa, the tensile stress on the rake face being lower than the tensile stress on the clearance face, dependent on the choice of coating and the coefficient of Thermal Expansion (CTE) of the used cemented carbide insert.
  • CTE Thermal Expansion
  • Example 1 The following sample was prepared: A) Cemented carbide cutting inserts with the composition 5.0 wt-% Co, 2.9 wt-% TaC, 0.5 wt-% NbC, 1.9 wt-% TiC, 0.35 wt-% TiN, balance WC, a hardness HV3 of 1620, measured according to ISO 3878- 1983 (E), Hardmetals-Vickers test, and with a surface zone, 14 ⁇ m thick, depleted from cubic carbides.
  • the saturation magnetization, M 3 was measured to be 0.068 hAm 2 /kg giving a CW-ratio of 0.84.
  • the inserts were coated with a 0.5 ⁇ m thick layer of TiN using conventional CVD-technique followed by a 10 ⁇ m TiC x N y -layer employing the MTCVD-technique .
  • a layer of TiC x O z about 0.5 ⁇ m thick was deposited, and then the Al 2 ⁇ 3-process was started up by flushing the reactor with a mixture of 2.0 CO 2 3.0 HCl and 95 % N 2 for 2 min before a 10 ⁇ m thick layer of CC-Al 2 ⁇ 3 was deposited.
  • On top was a thin, approximately 0.5 ⁇ m, TiN layer deposited.
  • the process conditions during the deposition steps were as below:
  • I (hkl) measured intensity of the (hkl) reflection
  • I o (hkl) standard intensity of Powder Diffraction File JCPDS No 43-1484.
  • n number of reflections used in the calculation (hkl) reflections used are: (012), (104), (110), (113), (024), (116) .
  • the coated inserts according to A) and B) were post treated by the earlier mentioned blasting method, blasting the rake face of the inserts, using a blasting pressure of 2.4 bar and an exposure time of 20 seconds.
  • the smoothness of the coating surface was measured by AFM on an equipment from Surface Imaging System AG (SIS) .
  • the roughness was measured on ten randomly selected plane surface areas (lO ⁇ mxlO ⁇ m) in the chip contact zone on the rake face.
  • the resulting mean value from these ten Ra values, MRa was 0.10 ⁇ m.
  • the residual stress, ⁇ , of the inner TiC x N y -layer was determined by XRD measurements using the well known sin 2 ⁇ method as described by I.C. Noyan, J. B. Cohen, Residual Stress Measurement by Diffraction and Interpretation, Springer-Verlag, New York, 1987 (pp 117-130), and the measurements were performed according to WO 2006/135330 with the following specifics:
  • the residual stress was determined using ⁇ -geometry on an X- ray diffractometer Bruker D8 Discover-GADDS equipped with laser- video positioning, Euler 1/4-cradle, rotating anode as X-ray source (CuK ⁇ -radiation) and an area detector (Hi-star) .
  • a collimator of size 0.5 mm was used to focus the beam.
  • insert B) according to the invention had a better edge line security than the high performance P05 grade and a better wear resistance than the competitive P05 grade.
  • insert A) according to the invention has an improved wear resistance and a more secure performance compared to the commercially available grades .

Abstract

The present invention relates to a CVD-coated cutting tool insert with improved toughness properties having the ability to withstand high temperatures resulting from, e.g., extended times in cut or high metal removal. The insert has a cemented carbide body with composition of 4.0-5.3 wt-% Co, 6.4-8.1 wt-% cubic carbides, balance WC, a hardness HV3 of 1590-1650, a CW-ratio in the range 0.78-0.92 and having a surface zone of a thickness of 10 to 16 mm depleted from the cubic carbides TiC, TaC and/or NbC, the insert being at least partly coated with a 11-19 mm thick coating including at least one layer of TiC xN y and an a-Al 2O 3 layer being the outer layer on the rake face and on the cutting edge line, and that on said at least one rake face the TiC xN y-layer has a thickness of from 4 to 12 mm and a tensile stress level of 50-500 MPa and the a-Al 2O 3-layer having a thickness of from 8 mm to 12 mm and has a mean Ra value MRa < 0.12 mm, at least in the chip contact zone on the rake face, and on said at least one clearance face the TiC xN y-layer has a tensile stress in the range 500-700 MPa and the a-Al 2O 3-layer is covered with a thin 0.1-1 mm TiN, TiC xN y,ZrC xN y or TiC layer giving the insert a different colour on this face.

Description

COATED CUTTING TOOL INSERT
The present invention relates to a high performance coated cutting tool insert particularly useful for turning at stable conditions in unalloyed and low alloyed steels in wet and dry conditions, having the ability to withstand high temperatures, resulting from, e.g., extended times in cut or high metal removal.
The majority of today's cutting tools are based on a cemented carbide insert coated with several hard layers like TiC, TiCxNy, TiN, TiCχNyOz and Al2O3. The sequence and the thickness of the individual layers are carefully chosen to suit different cutting application areas and work-piece materials. The most frequent employed coating techniques are Chemical Vapour Deposition (CVD) and Physical Vapour Deposition (PVD) .
The CVD technique is conducted at a rather high temperature range, conventionally 950-1050 0C. Due to this high deposition temperature and to a mismatch in the coefficients of thermal expansion between the deposited coating materials and the cemented carbide tool insert, CVD can lead to coatings with cooling cracks and high tensile stresses (sometimes up to 1000 MPa) . The high tensile stresses can under some cutting conditions be a disadvantage as it may cause the cooling cracks to propagate further into the cemented carbide body and cause breakage of the cutting edge.
In the metal cutting industry there is a constant striving to increase productivity, wherein turning operations involving high metal removal have an important role. Such operations generally place high demands on the cutting insert in respect of ability to withstand high temperatures, often during extended times in cut, as well as high demands on wear resistance. Important improvements in this area have been achieved by combining inserts with a binder phase enriched surface zone and optimized, thicker coatings. However, with an increasing coating thickness, a positive effect on wear resistance is out-balanced by an increasing negative effect in the form of an increased risk of coating delamination and reduced toughness making the cutting tool less reliable. Further, thick coatings generally have a more uneven surface, negatively affecting the cutting performance. These problems can, however, largely be remedied by applying a post treatment of the coating.
Smoothing operation of the coating by brushing or by wet blasting are disclosed in several patents, e.g., EP 0 298 729, EP 1 306 150 and EP 0 736 615. In US 5,861,210 the purpose has, e.g., been to achieve a smooth cutting edge and to expose the AI2O3 as the outermost layer on the rake face leaving the TiN on the clearance side to be used as a wear detection layer.
Every post treatment technique that exposes a surface, e.g., a coating surface to a mechanical impact as, e.g., wet or dry blasting will influence the surface finish and the stress state (σ) of the coating. A very intensive treatment may even lead to a big change in the stress state, e.g., from highly tensile to highly compressive as disclosed in EP-A-I 311 712, in which a dry blasting technique is used. To significantly change the stress state of a coating by blasting, the blasting media, e.g., AI2O3 grits, have to strike the coating surface with a high impulse. As disclosed in, e.g., WO 2006/135330 and EP 1 734 155, a post treatment comprising intensive wet blasting with a sufficiently high energy can give the coating a favourable tensile stress level, i.e., create tensile stress relaxation, and give the Al2θ3-layer a top surface with an excellent surface finish.
It is an object of the present invention to provide a CVD- coated tool insert having the ability to withstand high temperatures, resulting from, e.g., extended times in cut or high metal removal .
It has surprisingly been found that by finely tuning the balance between the hardness of a WC-Co based substrate and the depth of a toughness inducing Co enriched surface zone of the substrate in combination with a thick and partly stress relaxed coating has a significant effect on an inserts ability to withstand high temperatures.
According to the present invention there is provided a coated cutting tool insert of cemented carbide comprising a body having at least one rake face and at least one clearance face wherein said insert has a composition of 4.0-5.3, preferably 4.4-5.25, most preferably 4.8-5.2, wt-% Co, 4.6-8.1 wt-% cubic carbides, balance WC and a hardness HV3 of 1590-1650.
The cobalt binder phase is highly alloyed with W. The content of W in the binder phase can be expressed as the CW-ratio: CW-ratio = M3/ (wt-%Co*0.0161) wherein M3 = measured saturation magnetization in hAm2/kg and wt-% Co is the cobalt content in the cemented carbide. A low CW- ratio corresponds to a high W-content in the Co binder phase.
The CW-ratio is in the range 0.80-0.88, and the body has a surface zone of a thickness of 10-16 μm, preferably 10-15 μm, depleted from the cubic carbides TiC, TaC and/or NbC.
The insert is at least partly coated with a 10-25 μm thick coating including at least one layer of TiCxNy, where x≥O, y≥O and x+y=l, preferably MTCVD-TiCxNy, and a well crystalline CC-Al2O3- layer, preferably 100 % α-Al2θ3-layer, being the outermost visible layer on the rake face and on the cutting edge line, and on the at least one rake face of the insert
- the TiCχNy-layer has a thickness of from 4 to 12 μm, preferably from 5 to 7 μm or from 9 to 11 μm, and a tensile stress level of 50-500, preferably 50-450, MPa and
- the α-Al2θ3-layer has a thickness of from 8 to 12 μm, preferably from 9 to 11 μm and a mean Ra value
MRa < 0.12 μm, preferably < 10 μm, at least in the chip contact zone on the rake face, and on said at least one clearance face
- the TiCχNy-layer has a tensile stress in the range 500-700 MPa and
- the α-Al2O3-layer is covered with a thin 0.1-1 μm TiN, TiCxN^ ZrCxNy or TiC layer giving the insert a different colour on this face .
The coating on the rake face and along the cutting edge line is intensively wet blasted with a sufficiently high energy to create tensile stress relaxation in both the A12C>3- and the TiCxNy- layers. The outermost A12C>3 layer has a very smooth surface at least in the chip contact zone on the rake face.
Preferably there is a thin 0.2-1 μm bonding layer of TiCxNyOz, x≥O, z>0 and y≥O between the TiCxNy-layer and the CC-Al2O3-layer . Also according to the present invention, additional layers can be incorporated into the coating structure between the substrate and the layers, composed of metal nitrides and/or carbides and/or oxides with the metal elements selected from Ti, Nb, Hf, V, Ta, Mo, Zr, Cr, W and Al to a total coating thickness of <5 μm.
According to the present invention the cutting tool insert is, thus, provided with a CVD-coating comprising a penultimate TiCxNy- layer and an outer α-Al2θ3-layer . The AI2O3 can be produced according to patent EP 603 144 giving the Al2θ3-layer a crystallographic texture in 012-direction with a texture coefficient TC (012) >1.3, preferably >1.5, or produced according to patents US 5,851,687 and US 5,702,808 giving a texture in the 110-direction with texture coefficient TC(110)>1.5. However, in another embodiment, the AI2O3 is produced according to patent EP 738 336 giving the Al2θ3-layer a crystallographic texture in 104-direction with a texture coefficient TC (104) > 2.0, preferably TC(104)>2.5.
The insert has a different colour on the clearance side than on the black rake face. Preferably, an outermost thin 0.1-1 μm colouring layer of TiN (yellow) , TiCxNy (grey or bronze) , ZrCxNy (reddish or bronze), where x≥O, y≥O and x+y=l, or TiC (grey) is deposited. The insert is then blasted removing the top layer exposing the black Al2U3-layer.
In order to obtain a high surface smoothness and low tensile stress level the coating is subjected to a wet blasting operation with a slurry consisting of F150 grits (FEPA-standard) of AI2O3 in water at an air pressure of 2.2-2.6 bar for about 10-20 sec/insert. The spray guns are placed approximately 100 mm from the inserts with a 90° spray angle.
The coating on the rake face will have the low desired tensile stress 50-500 MPa while the clearance side will have high tensile stresses in the range 500-700 MPa, the tensile stress on the rake face being lower than the tensile stress on the clearance face, dependent on the choice of coating and the coefficient of Thermal Expansion (CTE) of the used cemented carbide insert.
Example 1 The following sample was prepared: A) Cemented carbide cutting inserts with the composition 5.0 wt-% Co, 2.9 wt-% TaC, 0.5 wt-% NbC, 1.9 wt-% TiC, 0.35 wt-% TiN, balance WC, a hardness HV3 of 1620, measured according to ISO 3878- 1983 (E), Hardmetals-Vickers test, and with a surface zone, 14 μm thick, depleted from cubic carbides.
The saturation magnetization, M3, was measured to be 0.068 hAm2/kg giving a CW-ratio of 0.84. The inserts were coated with a 0.5 μm thick layer of TiN using conventional CVD-technique followed by a 10 μm TiCxNy-layer employing the MTCVD-technique . In subsequent process steps during the same coating cycle a layer of TiCxOz about 0.5 μm thick was deposited, and then the Al2θ3-process was started up by flushing the reactor with a mixture of 2.0 CO2 3.0 HCl and 95 % N2 for 2 min before a 10 μm thick layer of CC-Al2θ3 was deposited. On top was a thin, approximately 0.5 μm, TiN layer deposited. The process conditions during the deposition steps were as below:
TiN TlCxNy TiCxOz Al2O3-start Al2O3
Step 1 and 6 2 3 4 5
TiCl4 1.5 % 1.4 % 2 %
N2 38 % 38 % balance
CO2: 2.0 % 4.4 %
CO 6 %
AlCl3: 3.2 %
H2S - 0.3 %
HCl 3.0 % 3.0 %
H2: balance balance balance - balance
CH3CN - 0.6 %
Pressure : 160 mbar 60 mbar 60 mbar 60 mbar 70 mbar
Temp. : 9300C 885°C 10000C 10000C 10000C
Time: 30 mm 6 h 20 mm 2 mm 10 h
Additional insert was:
B) Cemented carbide cutting inserts of the same type as in A) differing only in TiCxNy- and 0C-Al2O3-layer thickness, being 6 μm and 10 μm thick respectively, were manufactured using the same processing conditions except for the TiCxNy and Al2O3 depositing times being 4 h and 10 h, respectively. X-ray Diffraction Analysis (Bragg-Brentano diffractometer, Siemens D5000, Cu KCC-radiation) of the deposited Al2O3-layer of the inserts according to A) and B) showed that it consisted only of the α-phase with a texture coefficient TC (104) =2.6 defined as below:
- 1
TCdOD - I(104) I 1 V I (hkl )
( } Io(104) t n 2^° (hkl ) where
I (hkl) = measured intensity of the (hkl) reflection Io(hkl) = standard intensity of Powder Diffraction File JCPDS No 43-1484. n = number of reflections used in the calculation (hkl) reflections used are: (012), (104), (110), (113), (024), (116) .
The coated inserts according to A) and B) were post treated by the earlier mentioned blasting method, blasting the rake face of the inserts, using a blasting pressure of 2.4 bar and an exposure time of 20 seconds.
The smoothness of the coating surface, expressed as a well known roughness value Ra, was measured by AFM on an equipment from Surface Imaging System AG (SIS) . The roughness was measured on ten randomly selected plane surface areas (lOμmxlOμm) in the chip contact zone on the rake face. The resulting mean value from these ten Ra values, MRa, was 0.10 μm. The residual stress, σ, of the inner TiCxNy-layer was determined by XRD measurements using the well known sin2ψ method as described by I.C. Noyan, J. B. Cohen, Residual Stress Measurement by Diffraction and Interpretation, Springer-Verlag, New York, 1987 (pp 117-130), and the measurements were performed according to WO 2006/135330 with the following specifics:
The residual stress was determined using ψ-geometry on an X- ray diffractometer Bruker D8 Discover-GADDS equipped with laser- video positioning, Euler 1/4-cradle, rotating anode as X-ray source (CuKα-radiation) and an area detector (Hi-star) . A collimator of size 0.5 mm was used to focus the beam. The analysis was performed on the TiCxNy (422) reflection using the goniometer settings 2Θ=126°, ω=63° and Φ=0°, 90°, 180°, 270°, Eight ψ tilts between 0° and 70° were performed for each Φ-angle. The sin2ψ method was used to evaluate the residual stress using the software DIFFRACplus Stress32 v. 1.04 from Bruker AXS with the constants Young's modulus, E=480 GPa and Poisson's ratio, V=O.20 and locating the reflection using the Pseudo-Voigt-Fit function. A biaxial stress state was confirmed and the average value was used as the residual stress value. Measurements were carried out both on the rake face and the clearance side. The obtained tensile stress on the clearance side was about 640 MPa for the inserts according to A) and B) . A corresponding measurement on the rake face showed that a tensile stress of about 318 MPa was obtained for the inserts according to A) and a tensile stress of about 420 MPa was obtained for the inserts according to B) .
Example 2
Inserts A) from Example 1 were tested and compared with commercially available inserts (high performance inserts in the P05 and P15 area, respectively) in a roughing turning operation. Roughing of axle diameter, Φ=70 mm and length=300 mm, of tough- hardened steel.
Material: 42CrMoS4V (290 HB) . Cutting data: vc = 180 m/min fn = 0.35 mm/ rev ap = 2 mm Coolant
Inserts style: CNMG120412-PR
Results: No. of axles before failure of insert
Figure imgf000008_0001
Examination of the inserts showed that the P15 grade had obtained plastic deformation/crater wear and the P05 grade had obtained chipping/breakage. The grade A) according to the invention showed only flank wear. It can be concluded from the test that insert A) according to the invention had a better edge line security than the P05 grade and a better resistance to plastic deformation than the P15 grade.
Example 3
Inserts B) from Example 1 were tested and compared with commercially available inserts (high performance inserts and competitive grade in the P05 area, respectively) in a roughing turning operation. Facing and turning of inner diameter of a CV- joint, Φ=70 mm, of unalloyed steel.
Material: Cf53 (220 HB) . Cutting data: vc = 280 m/min fn = 0.35 mm/rev ap = 2 mm
Dry
Inserts style: WNMG080412-PR
Results: No. of CV-joints before failure of insert
Figure imgf000009_0001
Examination of the inserts showed that the high performance P05 grade had obtained chipping/breakage and the competitive P05 grade had obtained flank wear. The grade B) according to the invention showed only flank wear.
It can be concluded from the test that insert B) according to the invention had a better edge line security than the high performance P05 grade and a better wear resistance than the competitive P05 grade.
Example 4
Inserts A) from Example 1 were tested and compared with commercially available inserts (high performance inserts and competitive grade in the P15 area, respectively) in a roughing turning operation. Facing and turning of outer diameter of a ring, Φ=1250 mm, of ball bearing steel.
Material: 827B (190 HB) . Cutting data: vc = 170 m/min fn = 0.95 mm/rev ap = 7 mm Coolant
Inserts style: SNMM 190624
Results: Time before failure of insert
Figure imgf000010_0001
Examination of the inserts showed that the high performance P15 grade had obtained flank wear and plastic deformation, and the competitive P15 grade had obtained flank wear, chipping and crater wear. The grade A) according to the invention showed only flank wear . It can be concluded from the test that insert A) according to the invention had a better deformation resistance and crater wear resistance than the high performance P15 grade and the competitive P15 grade.
From the tests in Example 2-4 it is evident that insert A) according to the invention has an improved wear resistance and a more secure performance compared to the commercially available grades .

Claims

Claims
1. A coated cutting tool insert of cemented carbide comprising a body having at least one rake face and at least one clearance face c h a r a c t e r i z e d in said insert having a composition of 4.0-5.3 wt-% Co, 4.6-8.1 wt-% cubic carbides, balance WC, a hardness HV3 of 1590-1650, a CW-ratio in the range 0.80-0.88 and having a surface zone of a thickness of 10 to 16 μm depleted from the cubic carbides TiC, TaC and/or NbC, said insert being at least partly coated with a 10-25 μm thick coating including at least one layer of TiCxNy, where x>0, y>0 and x+y=l, and an α-Al2O3-layer being the outer layer on the rake face and on the cutting edge line, and that on said at least one rake face
- the TiCχNy-layer having a thickness of from 4 to 12 μm and a tensile stress level of 50-500 MPa and - the α-Al2θ3-layer having a thickness of from 8 to 12 μm and having a mean Ra value MRa < 0.12 μm, at least in the chip contact zone on the rake face, and on said at least one clearance face
- the TiCχNy-layer having a tensile stress in the range 500-700 MPa and that
- the α-Al2O3-layer is covered with a thin 0.1-1 μm TiN, TiCxN^ ZrCxNy or TiC layer giving the insert a different colour on this face.
2. A cutting tool insert according to claim 1 c h a r a c t e r i z e d in having 4.4-5.25, preferably 4.8-5.2, wt-% Co and a surface zone of a thickness of 10 to 15 μm, depleted from the cubic carbides TiC, TaC and/or NbC.
3. A cutting tool insert according to any of the preceding claims c h a r a c t e r i z e d in said at least one layer of TiCxNy is MTCVD-TiCxNy.
4. A cutting tool insert according to any of the preceding claims c h a r a c t e r i z e d in that on said at least one rake face the TiCxNy-layer having a thickness of from 5 to 7 μm, or from 9 to 11 μm, and having a tensile stress level of 50-450 MPa.
5. A cutting tool insert according to any of the preceding claims c h a r a c t e r i z e d in that on said at least one rake face the α-Al2θ3-layer having a thickness of 9 to 11 μm and having a mean Ra value MRa ≤ 0.10 μm, at least in the chip contact zone on the rake face.
6. A cutting tool insert according to the preceding claim c h a r a c t e r i z e d in having a thin 0.2-1 μm TiCxNyOz bonding layer, x≥O, z>0 and y≥O, between the TiCxNy- and the Al2O3-layer.
7. A cutting tool insert according to any of the preceding claims c h a r a c t e r i z e d in the 0C-Al2θ3-layer having a texture in the 104-direction with a texture coefficient TC(104)>2.0, preferably >2.5.
8. A cutting tool insert according to any of the preceding claims c h a r a c t e r i z e d in the α-Al2θ3-layer having a texture in the 012-direction with a texture coefficient TC(012)>1.3, preferably TC(012)> 1.5.
9. A cutting tool insert according to any of the preceding claims c h a r a c t e r i z e d in the 0C-Al2θ3-layer having a texture in the 110-direction with a texture coefficient TC(110)>1.5.
PCT/SE2008/051354 2007-11-28 2008-11-26 Coated cutting tool insert WO2009070107A1 (en)

Applications Claiming Priority (2)

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SE0702646 2007-11-28
SE0702646-1 2007-11-28

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011011331A (en) * 2009-07-03 2011-01-20 Sandvik Intellectual Property Ab Coated cutting tool insert
US20160326641A1 (en) * 2013-12-17 2016-11-10 Kyocera Corporation Coated tool

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WO1995019457A1 (en) * 1994-01-14 1995-07-20 Sandvik Ab Oxide coated cutting tool
EP1696051A1 (en) * 2005-02-25 2006-08-30 Sandvik Intellectual Property AB Coated cutting tool insert
WO2006135330A1 (en) * 2005-06-17 2006-12-21 Sandvik Intellectual Property Ab Coated cutting tool insert
EP1867755A2 (en) * 2006-06-16 2007-12-19 Sandvik Intellectual Property AB Coated cutting tool insert
EP1918423A2 (en) * 2006-10-18 2008-05-07 Sandvik Intellectual Property AB Coated cutting tool insert

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WO1995019457A1 (en) * 1994-01-14 1995-07-20 Sandvik Ab Oxide coated cutting tool
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WO2006135330A1 (en) * 2005-06-17 2006-12-21 Sandvik Intellectual Property Ab Coated cutting tool insert
EP1867755A2 (en) * 2006-06-16 2007-12-19 Sandvik Intellectual Property AB Coated cutting tool insert
EP1918423A2 (en) * 2006-10-18 2008-05-07 Sandvik Intellectual Property AB Coated cutting tool insert

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011011331A (en) * 2009-07-03 2011-01-20 Sandvik Intellectual Property Ab Coated cutting tool insert
US20160326641A1 (en) * 2013-12-17 2016-11-10 Kyocera Corporation Coated tool
US10174421B2 (en) * 2013-12-17 2019-01-08 Kyocera Corporation Coated tool

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