USRE40873E1 - Method of making grooving or parting insert - Google Patents
Method of making grooving or parting insert Download PDFInfo
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- USRE40873E1 USRE40873E1 US11/484,830 US48483006A USRE40873E US RE40873 E1 USRE40873 E1 US RE40873E1 US 48483006 A US48483006 A US 48483006A US RE40873 E USRE40873 E US RE40873E
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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
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
- C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
- C22C29/08—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds based on tungsten carbide
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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
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/0641—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
- 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
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F2005/001—Cutting tools, earth boring or grinding tool other than table ware
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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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
- Y10T428/2495—Thickness [relative or absolute]
- Y10T428/24967—Absolute thicknesses specified
- Y10T428/24975—No layer or component greater than 5 mils thick
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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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/25—Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
- Y10T428/252—Glass or ceramic [i.e., fired or glazed clay, cement, etc.] [porcelain, quartz, etc.]
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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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
- Y10T428/264—Up to 3 mils
- Y10T428/265—1 mil or less
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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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer
Definitions
- the present invention relates to a coated cutting tool (cemented carbide insert) useful for grooving or parting of steel components, such as bars or tubes, not only of stainless steels of different compositions and micostructures but also of non-stainless steels such as low carbon steels and low and medium alloyed steels.
- the cutting edge When machining low and medium alloyed steels and stainless steels with cemented carbide tools, the cutting edge is worn according to different wear mechanisms. Examples of such mechanisms include chemical wear, abrasive wear, adhesive wear and edge chipping. In bad cutting conditions problems with bulk and edge line breakage commonly occur. Furthermore, different cutting variables, such as cutting speed and cutting feed rate, and external conditions, such as dry or wet machining and heavy vibrations of the work piece, require a plurality of different properties of the cutting edge.
- U.S. Pat. No. 6,062,776 discloses a coated cutting insert particularly useful for dry and wet machining in low and medium alloyed steels and stainless steels, with or without raw surface zones, under severe conditions such as vibration, long overhang, and recutting of chips.
- the insert is characterized by a WC—Co cemented carbide with a low content of cubic carbides, a rather low W-alloyed binder phase, and a coating including an innermost layer of TiC x N y O z with columnar grains and a top layer of TiN and an inner layer of ⁇ -Al 2 O 3 .
- Swedish patent application SE 9901149-6 discloses a coated cutting insert, particularly useful at high cutting speeds, for use on stainless steels of different compositions and microstructures.
- the insert is also useful for the milling of non-stainless steels such as low carbon steels and low and medium alloyed steels.
- the coated WC—Co based cemented carbide insert is characterized by a specific composition range of WC/Co without any addition of cubic carbides, a low W-alloyed Co binder, a narrowly defined range of average WC grainsizes, and a hard and wear resistant coating including a multilayered structure of sub-layers of the composition (Ti x Al 1-x )N with repeated variation of the Ti/Al ratio.
- a cutting tool insert for parting of steel and stainless steel, and a method of making the same is provided.
- the cutting tool insert is comprised of a cemented carbide body and a coating wherein the cemented carbide body consists of WC with an average grain size of about 1.4 mm, 12-13 wt-% Co, 0.4-1.8 wt-% TaC+NbC, and a low W-alloyed binder phase with a CW-ratio of 0.82-0.91.
- the coating is comprised of a multiple layer.
- the first (innermost) layer is 0.1-0.5 ⁇ m of TiN.
- a second layer is comprised of a multilayered structure of 0.05-0.2 ⁇ m thick sublayers.
- the sublayers are of a composition (Ti x Al 1-x )N in which x varies repeatedly between the two ranges 0.45 ⁇ x ⁇ 0.55 and 0.70 ⁇ x ⁇ 0.80.
- a first sublayer, adjacent to the TiN bonding layer, is of a composition (Ti x Al 1-x )N having an x-value of 0.45 ⁇ x ⁇ 0.55.
- a second sublayer is of a composition (Ti x Al 1-x )N having an x-value of 0.70 ⁇ x ⁇ 0.80 and a third sublayer is of a composition (Ti x Al 1-x )N having x of 0.45 ⁇ x ⁇ 0.55.
- the sequence of sublayers alternates and repeats until 12-25 sublayers are built up.
- the total coating thickness is 1-8 mm and the thickness of the second layer constitutes 75-95% of the total coating thickness.
- FIG. 1 is a micrograph of a polished cross section of a coated insert according to the present invention.
- FIG. 1 shows a micrograph of 1200 ⁇ magnification of a polished cross section of a coated insert according to the present invention in which the layers of the cross section are visible.
- the layers are a cemented carbide body A, an innermost TiN layer B, a layer of several TiAlN sublayers C, a layer of TiAlN D, and an outermost TiN layer E.
- a coated cutting tool insert that satisfies the toughness demands of machining operations such as the grooving and parting of stainless steels.
- the coated cutting tool insert comprises a WC—Co based cemented carbide body with a composition of 11.5-13.6 wt % Co, preferably 12.0-13.0 wt % Co, most preferably 12.3-12.9 wt % Co, 0.2-1.8 wt % cubic carbides, preferably 0.4-1.8 wt % cubic carbides, most preferably 0.5-1.7 wt % cubic carbides of the metals Ta, Nb and Ti and balance WC.
- the cemented carbide may also contain other carbides from elements from group IVb, Vb or VIb of the periodic table.
- the content of Ti is preferably on a level corresponding to a technical impurity.
- the average grain size of the WC is about 1.1-2.1 ⁇ m, preferably about 1.4 ⁇ m.
- the cobalt binder phase is rather low and alloyed with W.
- the CW-value is a function of the W content in the Co binder phase. A high CW-value corresponds to a low W-content in the binder phase.
- the cemented carbide body has a CW-ratio of 0.80-0.92, preferably 0.82-0.91, and most preferably 0.85-0.90.
- the cemented carbide may contain small amounts, ⁇ 1 volume %, of ⁇ -phase (M 6 C), without any detrimental effect. From the CW-value it follows that no free graphite is allowed in the cemented carbide body according to the present invention.
- the hard and wear resistant refractory coating deposited on the cemented carbide substrate A according to the present invention comprises a first (innermost) thin 0.1-0.5 ⁇ m bonding layer of TiN B.
- the coating includes a second layer comprising a multi-layered structure of sublayers C of the composition (Ti x Al 1-x )N in which x varies repeatedly between the two ranges 0.45 ⁇ x ⁇ 0.55 and 0.70 ⁇ x ⁇ 0.80.
- the second sublayer of (Ti x Al 1-x )N having an x-value of 0.70 ⁇ x ⁇ 0.80
- the third sublayer having x of 0.45 ⁇ x ⁇ 0.55 and so forth repeated until 12-25 sublayers, preferably 22-24 sublayers, are built up.
- this second layer comprising a multilayered structure of sublayers constitutes 75-95% of the total coating thickness.
- the individual sublayers of (Ti x Al 1-x )N are essentially of the same thickness but their thickness may also vary in a regular or irregular way and said sublayer thickness is 0.05-0.2 ⁇ m.
- the coating further includes a third 0.1-0.5 ⁇ m layer of (Ti x Al 1-x )N D having an x-value of 0.45 ⁇ x ⁇ 0.55, and a fourth (innermost) thin 0.1-0.2 ⁇ m layer of TiN E.
- the total thickness of the coating is 1-8 ⁇ m, preferably 2-5 ⁇ m.
- the layer thickness, the sublayer thickness and the coating thickness quoted above refer to measurements made close to the cutting edge, i.e.—the functional part of the cutting tool.
- the insert was coated with an innermost 0.5 ⁇ m equiaxed TiCN-layer.
- a 1.5 ⁇ m TiN layer was deposited, during the same cycle, on top of the TiCN-layer. No post treatment was applied.
- a competitive cemented carbide parting tool insert in style similar to previously mentioned inserts was obtained from an external leading cemented carbide procedure.
- the carbide had a composition of 12.5 wt-% Co, 0.1 wt-% TiC, 1.8 wt-% TaC, 0.2 wt-% NbC, and balance WC with a CW-ratio of 0.87.
- the insert had a coating consisting of 1.4 ⁇ m TiN, and, outermost, 1.4 ⁇ m TiCN. Examination under a high optical microscope revealed no edge treatment subsequent to coating.
- Inserts A, B and C were tested in a parting off to center in stainless steel SS2321 with OD 26 mm.
- the cutting speed was varied from 86 to 0 m/min with a feed rate of 0.05 mm/r.
- the wear mechanism was uneven flank wear and chipping.
- Inserts A and B were tested at an end user's machine shop in a parting of a stainless steel component (AISI 316 OD 42 mm).
- the cutting speed was varied from 110 to 0 m/min with a feed rate varying from 0.08 to 003 mm/r.
- the low feed rate was used close to the center of the bar.
- the wear mechanism was fracture in the cutting zone.
- Inserts A and B were tested at an end user's machine shop in a parting of a steel component (SS2172 OD 47 mm).
- the rotating speed was 1800 rpm with a feed rate of 0.1 mm/r.
- the wear mechanism was flank wear and flaking.
- Inserts A and C were tested at an end user's machine shop in a parting of a stainless steel component (AISI 316 OD 31 mm).
- the cutting speed was varied from 60 to 0 m/min with a feed rate varying from 0.06 to 0.03 mm/r.
- the low feed rate was used close to the center of the bar.
- the wear mechanism was flank wear and chipping.
- the present invention also relates to a method of making a coating cutting tool insert consisting of a cemented carbide body with a composition of 11.5-13.6 wt % Co, preferably 12.0-13.0 wt % Co, most preferably 12.3-12.9 wt % Co, 0.2-1.8 wt % cubic carbides, preferably 0.4-1.8 wt % cubic carbides, most preferably 0.5-1.7 wt % cubic carbides of the metals Ta, Nb and Ti and balance WC.
- the cemented carbide may also contain other carbides from elements from group IVb, Vb or VIb of the periodic table.
- the content of Ti is preferably on a level corresponding to a technical impurity.
- the average grain size of the WC is about 1.1-2.1 ⁇ m, preferably about 1.4 ⁇ m.
- the hard and wear resistant refractory coating is deposited onto the cemented carbide substrate by applying conventional PVD (Physical Vapor Deposition) or CVD (Chemical Vapor Deposition) methods and, according to the present invention, said coating comprises a first (innermost) thin 0.1-0.5 ⁇ m bonding layer of TiN, a second layer comprising a multilayered structure of sublayers of the composition (Ti x Al 1-x )N in which x varies repeatedly between the two range 0.45 ⁇ x ⁇ 0.55 and 0.70 ⁇ x ⁇ 0.80.
- PVD Physical Vapor Deposition
- CVD Chemical Vapor Deposition
- the thickness of this second layer comprising a multilayered structure of sublayers constitutes 74-95% of the total coating thickness.
- the individual sublayers of (Ti x Al 1-x )N are essentially of the same thickness but their thickness may also vary in a regular or irregular way and said sublayer thickness is 0.05-0.2 ⁇ m, a third thin 0.1-0.5 ⁇ m layer of (Ti x Al 1-x )N having an x-value of 0.45 ⁇ x ⁇ 0.55 and a fourth (outermost) 0.1-0.2 ⁇ layer of TiN.
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- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Inorganic Chemistry (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
- Physical Vapour Deposition (AREA)
- Clamps And Clips (AREA)
- Scissors And Nippers (AREA)
- Powder Metallurgy (AREA)
- Chemical Vapour Deposition (AREA)
Abstract
A method of making a cutting tool, the cutting tool having a WC—Co based cemented carbide body and a multi-layer coating, the method including: applying a first innermost bonding layer TiN to the body; applying a second layer in the form of a mutlilayered structure having sublayers of (TixAl1-x)N were x varies according to 0.45<x<0.55 and 0.70<x<0.80; applying a third layer of (TixAl1-x)N where x is 0.45<x<0.55; and applying a forth outermost layer on TiN.
Description
The present application is a reissue of U.S. Pat. No. 6,627,049 B2, filed Oct. 30, 2001, which is a divisional application of U.S. Pat. No. 6,342,291, filed Aug. 31, 2000, which claims the benefit of priority of Swedish Application No. 9903089 - 2 filed Sep. 1, 1999.
This application is a divisional of U.S. application Ser. No. 09/652,026 filed on Aug. 31, 2000, now U.S. Pat. No. 6,342,291.
1. Field of the Invention
The present invention relates to a coated cutting tool (cemented carbide insert) useful for grooving or parting of steel components, such as bars or tubes, not only of stainless steels of different compositions and micostructures but also of non-stainless steels such as low carbon steels and low and medium alloyed steels.
2. Description of Related Art
In the discussion of the state of the art that follows, reference is made to certain structures and/or methods. However, the following references should not be construed as an admission that these structures and/or methods constitute prior art. Applicant expressly reserves the right to demonstrate that such structures and/or methods do not qualify as prior art against the present invention.
When machining low and medium alloyed steels and stainless steels with cemented carbide tools, the cutting edge is worn according to different wear mechanisms. Examples of such mechanisms include chemical wear, abrasive wear, adhesive wear and edge chipping. In bad cutting conditions problems with bulk and edge line breakage commonly occur. Furthermore, different cutting variables, such as cutting speed and cutting feed rate, and external conditions, such as dry or wet machining and heavy vibrations of the work piece, require a plurality of different properties of the cutting edge.
It has been very difficult to improve all of the plurality of preferred tool properties simultaneously. Therefore, commercial cemented carbide grades have been optimized with respect to one or only a few of these wear types and, hence, to specific application areas.
U.S. Pat. No. 6,062,776 discloses a coated cutting insert particularly useful for dry and wet machining in low and medium alloyed steels and stainless steels, with or without raw surface zones, under severe conditions such as vibration, long overhang, and recutting of chips. The insert is characterized by a WC—Co cemented carbide with a low content of cubic carbides, a rather low W-alloyed binder phase, and a coating including an innermost layer of TiCxNyOz with columnar grains and a top layer of TiN and an inner layer of κ-Al2O3.
Swedish patent application SE 9901149-6 discloses a coated cutting insert, particularly useful at high cutting speeds, for use on stainless steels of different compositions and microstructures. The insert is also useful for the milling of non-stainless steels such as low carbon steels and low and medium alloyed steels. The coated WC—Co based cemented carbide insert is characterized by a specific composition range of WC/Co without any addition of cubic carbides, a low W-alloyed Co binder, a narrowly defined range of average WC grainsizes, and a hard and wear resistant coating including a multilayered structure of sub-layers of the composition (TixAl1-x)N with repeated variation of the Ti/Al ratio.
It has now surprisingly been found that a combination of a modified cemented carbide substrate described in the above mentioned U.S. Pat. No. 6,062,776 and the coating described in the above mentioned SE 9901149-6 results in excellent cutting performance in grooving or, in particular, parting of steel, including stainless steel.
A cutting tool insert, for parting of steel and stainless steel, and a method of making the same is provided. The cutting tool insert is comprised of a cemented carbide body and a coating wherein the cemented carbide body consists of WC with an average grain size of about 1.4 mm, 12-13 wt-% Co, 0.4-1.8 wt-% TaC+NbC, and a low W-alloyed binder phase with a CW-ratio of 0.82-0.91. The coating is comprised of a multiple layer. The first (innermost) layer is 0.1-0.5 μm of TiN. A second layer is comprised of a multilayered structure of 0.05-0.2 μm thick sublayers. The sublayers are of a composition (TixAl1-x)N in which x varies repeatedly between the two ranges 0.45<x<0.55 and 0.70<x<0.80. A first sublayer, adjacent to the TiN bonding layer, is of a composition (TixAl1-x)N having an x-value of 0.45<x<0.55. A second sublayer is of a composition (TixAl1-x)N having an x-value of 0.70<x<0.80 and a third sublayer is of a composition (TixAl1-x)N having x of 0.45<x<0.55. The sequence of sublayers alternates and repeats until 12-25 sublayers are built up. After the multilayered structure, a third layer of (TixAl1-x)N, where x is 0.45<x<0.55, is deposited to a thickness of 0.1-0.5 μm. A fourth and outermost layer of TiN is deposited to a thickness of 0.1-0.2 μm. The total coating thickness is 1-8 mm and the thickness of the second layer constitutes 75-95% of the total coating thickness.
The objects and advantages of the invention will become apparent from the following detailed description of preferred embodiments thereof in connection with the accompanying drawings in which like numerals designate like elements and in which:
According to the present invention, there is provided a coated cutting tool insert that satisfies the toughness demands of machining operations such as the grooving and parting of stainless steels. The coated cutting tool insert comprises a WC—Co based cemented carbide body with a composition of 11.5-13.6 wt % Co, preferably 12.0-13.0 wt % Co, most preferably 12.3-12.9 wt % Co, 0.2-1.8 wt % cubic carbides, preferably 0.4-1.8 wt % cubic carbides, most preferably 0.5-1.7 wt % cubic carbides of the metals Ta, Nb and Ti and balance WC. The cemented carbide may also contain other carbides from elements from group IVb, Vb or VIb of the periodic table. The content of Ti is preferably on a level corresponding to a technical impurity. The average grain size of the WC is about 1.1-2.1 μm, preferably about 1.4 μm.
The cobalt binder phase is rather low and alloyed with W. The content of W in the binder phase can be expressed as the CW-ratio:
CW-ratio=MS/(wt % Co-0.0161)
where MS is the saturation magnetization of the cemented carbide body in kA/m hAm2 /kg and wt % 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 high CW-value corresponds to a low W-content in the binder phase.
CW-ratio=MS/(wt % Co-0.0161)
where MS is the saturation magnetization of the cemented carbide body in kA/m hAm2 /kg and wt % 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 high CW-value corresponds to a low 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 0.80-0.92, preferably 0.82-0.91, and most preferably 0.85-0.90. The cemented carbide may contain small amounts, <1 volume %, of η-phase (M6C), without any detrimental effect. From the CW-value it follows that no free graphite is allowed in the cemented carbide body according to the present invention.
The hard and wear resistant refractory coating deposited on the cemented carbide substrate A according to the present invention comprises a first (innermost) thin 0.1-0.5 μm bonding layer of TiN B.
The coating includes a second layer comprising a multi-layered structure of sublayers C of the composition (TixAl1-x)N in which x varies repeatedly between the two ranges 0.45<x<0.55 and 0.70<x<0.80. The first sublayer of (TixAl1-x)N adjacent to the TiN bonding layer having an x-value of 0.45<x<0.55, the second sublayer of (TixAl1-x)N having an x-value of 0.70<x<0.80 and the third sublayer having x of 0.45<x<0.55 and so forth repeated until 12-25 sublayers, preferably 22-24 sublayers, are built up. The thickness of this second layer comprising a multilayered structure of sublayers constitutes 75-95% of the total coating thickness. The individual sublayers of (TixAl1-x)N are essentially of the same thickness but their thickness may also vary in a regular or irregular way and said sublayer thickness is 0.05-0.2 μm.
The coating further includes a third 0.1-0.5 μm layer of (TixAl1-x)N D having an x-value of 0.45<x<0.55, and a fourth (innermost) thin 0.1-0.2 μm layer of TiN E.
The total thickness of the coating is 1-8 μm, preferably 2-5 μm. The layer thickness, the sublayer thickness and the coating thickness quoted above refer to measurements made close to the cutting edge, i.e.—the functional part of the cutting tool.
The present invention will now be further described by reference to the following examples, which are intended to be illustrative rather restrictive.
A. A cemented carbide parting tool insert in accordance with the present invention with a composition of 12.6 wt-% Co, 1.25 wt-% TaC, 0.30 wt-% NbC and balance WC with a 1.4 μm grain size and with a binder phase alloyed with W corresponding to a CW-ratio of 0.91 was coated with a 4 μm thick coating by applying a conventional PVD cathodic arc technique. The coating considered of a first (innermost) 0.2 μm layer of TiN followed by a 3.2 μm thick second layer comprising 23 alternating sublayers (TixAl1-x)N, where x alternatively varied between 0.55 and 0.75, a third layer 0.2 μm (TixAl1-x)N, where x=0.55, and, finally, an outermost 0.4 μm layer of TiN.
B. A cemented carbide parting tool insert not of the present invention with a composition of 8.0 wt-% Co, no cubic carbides, balance WC and a CW-ratio of 0.94. The insert was coated with an innermost 0.5 μm equiaxed TiCN-layer. A 1.5 μm TiN layer was deposited, during the same cycle, on top of the TiCN-layer. No post treatment was applied.
C. For comparison, a competitive cemented carbide parting tool insert in style similar to previously mentioned inserts was obtained from an external leading cemented carbide procedure. The carbide had a composition of 12.5 wt-% Co, 0.1 wt-% TiC, 1.8 wt-% TaC, 0.2 wt-% NbC, and balance WC with a CW-ratio of 0.87. The insert had a coating consisting of 1.4 μm TiN, and, outermost, 1.4 μm TiCN. Examination under a high optical microscope revealed no edge treatment subsequent to coating.
Inserts A, B and C were tested in a parting off to center in stainless steel SS2321 with OD 26 mm. The cutting speed was varied from 86 to 0 m/min with a feed rate of 0.05 mm/r. The wear mechanism was uneven flank wear and chipping.
Insert | Number of components | ||
A | 50 | ||
B | 13 | ||
C | 41 | ||
Inserts A and B were tested at an end user's machine shop in a parting of a stainless steel component (AISI 316 OD 42 mm). The cutting speed was varied from 110 to 0 m/min with a feed rate varying from 0.08 to 003 mm/r. The low feed rate was used close to the center of the bar. The wear mechanism was fracture in the cutting zone.
Insert | Number of components | ||
A | 201 | ||
B | 224 | ||
Inserts A and B were tested at an end user's machine shop in a parting of a steel component (SS2172 OD 47 mm). The rotating speed was 1800 rpm with a feed rate of 0.1 mm/r. The wear mechanism was flank wear and flaking.
Insert | Number of components | ||
A | 163 | ||
B | 50 | ||
Inserts A and C were tested at an end user's machine shop in a parting of a stainless steel component (AISI 316 OD 31 mm). The cutting speed was varied from 60 to 0 m/min with a feed rate varying from 0.06 to 0.03 mm/r. The low feed rate was used close to the center of the bar. The wear mechanism was flank wear and chipping.
Insert | Number of components | ||
A | 182 | ||
C | 43 | ||
The present invention also relates to a method of making a coating cutting tool insert consisting of a cemented carbide body with a composition of 11.5-13.6 wt % Co, preferably 12.0-13.0 wt % Co, most preferably 12.3-12.9 wt % Co, 0.2-1.8 wt % cubic carbides, preferably 0.4-1.8 wt % cubic carbides, most preferably 0.5-1.7 wt % cubic carbides of the metals Ta, Nb and Ti and balance WC. The cemented carbide may also contain other carbides from elements from group IVb, Vb or VIb of the periodic table. The content of Ti is preferably on a level corresponding to a technical impurity. The average grain size of the WC is about 1.1-2.1 μm, preferably about 1.4 μm.
The hard and wear resistant refractory coating is deposited onto the cemented carbide substrate by applying conventional PVD (Physical Vapor Deposition) or CVD (Chemical Vapor Deposition) methods and, according to the present invention, said coating comprises a first (innermost) thin 0.1-0.5 μm bonding layer of TiN, a second layer comprising a multilayered structure of sublayers of the composition (TixAl1-x)N in which x varies repeatedly between the two range 0.45<x<0.55 and 0.70<x<0.80. The first sublayer of (TixAl1-x)N adjacent to the TiN bonding layer having an x-value of 0.45<x<0.55, the second sublayer of (TixAl1-x)N having an x-value of 0.70<x<0.80 and the third sublayer having x of 0.45<x<0.55 and so forth repeated until 12-25 sublayers, preferably 22-24 sublayers, are built up. The thickness of this second layer comprising a multilayered structure of sublayers constitutes 74-95% of the total coating thickness. The individual sublayers of (TixAl1-x)N are essentially of the same thickness but their thickness may also vary in a regular or irregular way and said sublayer thickness is 0.05-0.2 μm, a third thin 0.1-0.5 μm layer of (TixAl1-x)N having an x-value of 0.45<x<0.55 and a fourth (outermost) 0.1-0.2 μlayer of TiN.
Although the present invention has been described in connection with preferred embodiments thereof, it will be appreciated by those skilled in the art that additions, deletions, modifications, and substitutions not specifically described may be made without department from the spirit and scope of the invention as defined in the appended claims.
Claims (5)
1. A method of making a cutting tool, the cutting tool comprising a WC—Co based cemented carbide body comprising WC with an average grain size of about 1.4 μm, 12-13 wt-% Co and 0.4-1.8 wt-% TaC+NbC, and a W-alloyed binder phase with a CW-ratio of 0.82-0.91, the method comprising:
applying a first innermost 0.1-0.5 μm bonding layer of TiN to the body;
applying a second layer comprising a mutlilayered structure comprising a plurality of 0.05-0.2 μm thick sublayers of a composition (TixAl1-x)N in which x varies repeatedly between the two ranges 0.45<x<0.55 and 0.70<x<0.80, a first sublayer of (TixAl1-x)N adjacent to the TiN bonding layer having an x-value of 0.45<x<0.55, a second sublayer of (TixAl1-x)N having an x-value of 0.70<x<0.80 and a third sublayer having x in the range 0.45<x<0.55, the sequence of sublayers alternating and repeating until 12-25 sublayers are built up;
applying a third 0.1-0.5 μm thick layer of (TixAl1-x)N, where x is 0.45<x<0.55; and
applying a fourth outermost 0.1-0.2 μm layer of TiN;
wherein the total coating thickness close to a cutting edge of the tool is in the range of 1-8 μm and the thickness of the second layer constitutes 75-95% of the total coating thickness.
2. The method according to claim 1 , wherein the cemented carbide body comprises a WC—Co composition of WC with an average grain size of about 1.4 μm, 12-13 wt-% Co and 0.4-1.8 wt-% TaC+NbC, and a W-alloyed binder phase with a CW-ratio of 0.82-0.91.
3. The method according to claim 1 , wherein the coating is deposited by CVD techniques.
4. The method according to claim 1 , the coating is deposited by PVD techniques.
5. A method according to claim 1 wherein the CW-i ratio is 0.85-0.90.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/484,830 USRE40873E1 (en) | 1999-09-01 | 2006-07-12 | Method of making grooving or parting insert |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9903089A SE9903089D0 (en) | 1999-09-01 | 1999-09-01 | Coated grooving or parting insert |
US09/652,026 US6342291B1 (en) | 1999-09-01 | 2000-08-31 | Coated grooving or parting insert and method of making same |
US09/984,612 US6627049B2 (en) | 1999-09-01 | 2001-10-30 | Method of making grooving or parting insert |
US11/484,830 USRE40873E1 (en) | 1999-09-01 | 2006-07-12 | Method of making grooving or parting insert |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/984,612 Reissue US6627049B2 (en) | 1999-09-01 | 2001-10-30 | Method of making grooving or parting insert |
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Publication Number | Publication Date |
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USRE40873E1 true USRE40873E1 (en) | 2009-08-18 |
Family
ID=20416823
Family Applications (4)
Application Number | Title | Priority Date | Filing Date |
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US09/652,026 Ceased US6342291B1 (en) | 1999-09-01 | 2000-08-31 | Coated grooving or parting insert and method of making same |
US09/984,612 Ceased US6627049B2 (en) | 1999-09-01 | 2001-10-30 | Method of making grooving or parting insert |
US11/449,012 Expired - Fee Related USRE40025E1 (en) | 1999-09-01 | 2006-06-08 | Coated grooving or parting insert and method of making same |
US11/484,830 Expired - Fee Related USRE40873E1 (en) | 1999-09-01 | 2006-07-12 | Method of making grooving or parting insert |
Family Applications Before (3)
Application Number | Title | Priority Date | Filing Date |
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US09/652,026 Ceased US6342291B1 (en) | 1999-09-01 | 2000-08-31 | Coated grooving or parting insert and method of making same |
US09/984,612 Ceased US6627049B2 (en) | 1999-09-01 | 2001-10-30 | Method of making grooving or parting insert |
US11/449,012 Expired - Fee Related USRE40025E1 (en) | 1999-09-01 | 2006-06-08 | Coated grooving or parting insert and method of making same |
Country Status (8)
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US (4) | US6342291B1 (en) |
EP (1) | EP1218557B1 (en) |
JP (1) | JP2003508242A (en) |
AT (1) | ATE269425T1 (en) |
DE (1) | DE60011644T2 (en) |
IL (1) | IL147779A (en) |
SE (1) | SE9903089D0 (en) |
WO (1) | WO2001016388A1 (en) |
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Also Published As
Publication number | Publication date |
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ATE269425T1 (en) | 2004-07-15 |
USRE40025E1 (en) | 2008-01-22 |
EP1218557B1 (en) | 2004-06-16 |
EP1218557A1 (en) | 2002-07-03 |
IL147779A0 (en) | 2002-08-14 |
US6342291B1 (en) | 2002-01-29 |
SE9903089D0 (en) | 1999-09-01 |
IL147779A (en) | 2005-07-25 |
JP2003508242A (en) | 2003-03-04 |
WO2001016388A1 (en) | 2001-03-08 |
US6627049B2 (en) | 2003-09-30 |
DE60011644T2 (en) | 2004-09-30 |
DE60011644D1 (en) | 2004-07-22 |
US20020051887A1 (en) | 2002-05-02 |
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