WO1996021051A1 - Method of coating cutting tool inserts - Google Patents

Method of coating cutting tool inserts Download PDF

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Publication number
WO1996021051A1
WO1996021051A1 PCT/SE1995/001586 SE9501586W WO9621051A1 WO 1996021051 A1 WO1996021051 A1 WO 1996021051A1 SE 9501586 W SE9501586 W SE 9501586W WO 9621051 A1 WO9621051 A1 WO 9621051A1
Authority
WO
WIPO (PCT)
Prior art keywords
inserts
coating
iron group
partly
group metal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/SE1995/001586
Other languages
French (fr)
Inventor
Stefan Ederyd
Enrico Galli
Mats Nygren
Gunnar Westin
Åsa EKSTRAND
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 AB
Original Assignee
Sandvik 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
Application filed by Sandvik AB filed Critical Sandvik AB
Priority to AT95942374T priority Critical patent/ATE190673T1/en
Priority to DE69515683T priority patent/DE69515683T2/en
Priority to US08/849,770 priority patent/US6033735A/en
Priority to EP95942374A priority patent/EP0792387B1/en
Priority to JP8520900A priority patent/JPH10511742A/en
Publication of WO1996021051A1 publication Critical patent/WO1996021051A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • 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
    • C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
    • C23C18/02—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition
    • C23C18/08—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition characterised by the deposition of metallic material

Definitions

  • the present invention relates to a method of coating cutting tool inserts with a layer of an iron group metal. Inserts with a coating applied according to the invention are particularly suitable for brazing.
  • Cemented carbide inserts are generally attached to tool-holders by mechanical means if possible. In case of saw-blades, drills and circular cutters the design does not permit mechanical clamps and/or similar mechanical attachments. In these cases the inserts have to be brazed to the toolholder.
  • Fig 1. shows in 150X the surface structure of the coating of cemented carbide insert coated with the method of the present invention.
  • Fig 2. shows in 1250X the microstructure and the thickness of the coating from the cross section of a T- shape crack in the coating.
  • the network of the coating is observed clearly.
  • the crack has been formed during the cooling step because of difference in thermal expansion coefficient between coating and cemented carbide.
  • a soluble carbon source is added to the solution which is applied onto the cemented carbide inserts.
  • the solvent is evaporated and the coated inserts are heat treated in an inert and/or reducing atmosphere.
  • At least one Me-salt containing organic groups such as carbo-oxylates, acetyl-acetonates, nitrogen containing organic groups such as schiff bases, preferably Me-acetates, is dissolved in at least one polar solvent such as ethanol, acetonitrile, dimetyl- formamide or dimetyl-sulfoxide and combinations of solvent such as methanol-ethanol and water-glycol, preferably ethanol.
  • sugar (Ci2 H 22°ll) or other soluble carbon source such as other types of carbohydrates and/or organic compounds which decompose under formation of carbon in the temperature interval 100-500°C in non- oxidizing atmosphere is added(0.1-2.0 mole C/mole metal, preferably about 0.5 mole C/mole metal), and the solu ⁇ tion is heated to 40°C in order to improve the solubility of the carbon source.
  • the carbon is used to reduce the MeO formed in connection with heat treatment and to regulate the carbon-content in the coating layer.
  • the solution is applied at least onto the surface/surfaces to be brazed by dipping into the solution or by spraying or painting with the solution.
  • the coated inserts obtained in the preceding step are heat treated in nitrogen at about 700-1100°C. To achieve a full reduction a holding temperature might be needed.
  • the time of reduction (5-120 minutes) is influenced by process factors such as coating thickness and reduction temperature. Nitrogen is normally used but argon, hydrogen, NH3, CO and CO2 (or mixtures between them) can be used whereby the composition and micro- structure of the coating can be modulated.
  • cemented carbide inserts coated with Me which e.g. can be brazed to a tool in the conventional way, however, with improved strength of the brazed joint.
  • the thickness of the final coating can be varied by varying the thickness of the initial coating.
  • a thickness of 0.1 - 0.5 ⁇ m is suitable.
  • the coating can be thicker.
  • the method according to this invention can be used to provide coatings also on Ti-based carbonitrides so called cermets, binderless carbide and ceramics.
  • the coating can be tailor-made to form a good wetting to the base material.
  • Ti can be added as soluble salt in the metal salt- solution to form a good adhesion to a Ti containing base material.
  • the inserts were placed onto net trays and heat treated in a furnace with nitrogen atmosphere.
  • the heating rate was 10°C/min to 700°C, no holding temperature, cooling 10°C/min and finally completed with reduction in hydrogen, holding temperature 800°C for 90 minutes .
  • the inserts according to the invention show both higher mean value and lower spread in the force required to remove them than the inserts coated in the conventional way.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Cutting Tools, Boring Holders, And Turrets (AREA)
  • Turning (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
  • Chemical Vapour Deposition (AREA)
  • Chemically Coating (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Ceramic Products (AREA)

Abstract

The present invention relates to a method of coating cemented carbide inserts at least partly with a layer of at least one iron group metal. When inserts coated with such a layer are brazed to a holder or similar, a joint with improved strength is obtained. According to the method of the invention one or more metal salts of at least one iron group metal containing organic groups are dissolved and complex bound in at least one polar solvent with at least one complex former comprising functional groups in the form of OH or NR3, (R=H or alkyl). A soluble carbon source is added to the solution which is subsequently at least partly applied to the cemented carbide inserts by dipping, spraying or painting. The inserts are dried and heat treated in an inert and/or reducing atmosphere. As a result, cemented carbide inserts are obtained at least partly coated with a layer of an iron group metal.

Description

Method of coatinσ cutting tool inserts
The present invention relates to a method of coating cutting tool inserts with a layer of an iron group metal. Inserts with a coating applied according to the invention are particularly suitable for brazing.
Cemented carbide inserts are generally attached to tool-holders by mechanical means if possible. In case of saw-blades, drills and circular cutters the design does not permit mechanical clamps and/or similar mechanical attachments. In these cases the inserts have to be brazed to the toolholder.
When brazing cemented carbide with a low binder content there are problems with the wetting of the braze and therefore the inserts have to be coated with cobalt prior to the brazing procedure. For coating on industrial scale this cobalt coating is generally made electrolytically. However, such coating generally has poor adherence and in order to improve the adhesion the inserts are heat treated in a subsequent production step. This coating method is rather complex and expensive and the resultant coating adhesion is still not always satisfactory.
It has now surprisingly been found that using a technique related to the SOL-GEL technique cemented carbide inserts can be provided with a cobalt layer with improved bond to the tool.
Fig 1. shows in 150X the surface structure of the coating of cemented carbide insert coated with the method of the present invention.
Fig 2. shows in 1250X the microstructure and the thickness of the coating from the cross section of a T- shape crack in the coating. The network of the coating is observed clearly. The crack has been formed during the cooling step because of difference in thermal expansion coefficient between coating and cemented carbide.
According to the method of the present invention one or more metal salts of at least one iron group metal containing organic groups are dissolved and complex bound in at least one polar solvent with at least one complex former comprising functional groups in the form of OH or NR3, (R=H or alkyl) . Optionally, a soluble carbon source is added to the solution which is applied onto the cemented carbide inserts. The solvent is evaporated and the coated inserts are heat treated in an inert and/or reducing atmosphere. As a result coated cemented carbide inserts are obtained which can be brazed to a tool according to standard practice. The process according to the invention comprises the following steps where Me= Co, Ni and/or Fe, preferably Co:
1. At least one Me-salt containing organic groups such as carbo-oxylates, acetyl-acetonates, nitrogen containing organic groups such as schiff bases, preferably Me-acetates, is dissolved in at least one polar solvent such as ethanol, acetonitrile, dimetyl- formamide or dimetyl-sulfoxide and combinations of solvent such as methanol-ethanol and water-glycol, preferably ethanol. Triethanolainine or other complex former especially molecules containing more than two functional groups, i. e. OH or NR3 with R = H or alkyl(0.1-2.0 mole complex former/mole metal, preferably about 0.5 mole complex former/mole metal) is added under stirring.
2. Optionally, sugar (Ci2H22°ll) or other soluble carbon source such as other types of carbohydrates and/or organic compounds which decompose under formation of carbon in the temperature interval 100-500°C in non- oxidizing atmosphere is added(0.1-2.0 mole C/mole metal, preferably about 0.5 mole C/mole metal), and the solu¬ tion is heated to 40°C in order to improve the solubility of the carbon source. The carbon is used to reduce the MeO formed in connection with heat treatment and to regulate the carbon-content in the coating layer.
3. The solution is applied at least onto the surface/surfaces to be brazed by dipping into the solution or by spraying or painting with the solution.
4. The coated inserts obtained in the preceding step are heat treated in nitrogen at about 700-1100°C. To achieve a full reduction a holding temperature might be needed. The time of reduction (5-120 minutes) is influenced by process factors such as coating thickness and reduction temperature. Nitrogen is normally used but argon, hydrogen, NH3, CO and CO2 (or mixtures between them) can be used whereby the composition and micro- structure of the coating can be modulated.
5. As a result of the heat treatment cemented carbide inserts coated with Me are obtained which e.g. can be brazed to a tool in the conventional way, however, with improved strength of the brazed joint.
The thickness of the final coating can be varied by varying the thickness of the initial coating. For brazing purposes a thickness of 0.1 - 0.5 μm is suitable. For other purposes, however, the coating can be thicker.
Because of the difference in thermal expansion the coating generally shows cracks. These cracks however, do not affect the brazing properties of the coating. The method according to this invention can be used to provide coatings also on Ti-based carbonitrides so called cermets, binderless carbide and ceramics.
In these applications the coating can be tailor-made to form a good wetting to the base material. In addition to or instead of the carbon source mentioned above e.g. Ti can be added as soluble salt in the metal salt- solution to form a good adhesion to a Ti containing base material.
Most of the solvent can be recovered which is of great importance on an industrial production scale.
Example 1
134.89 g cobalt acetate-tetrahydrate (Co (C2H3O2) 2 *4H2°) was dissolved in 800 ml methanol (CH3OH) . 36.1 ml triethanol-amine ((C2H5θ)3N (0.5 mole TEA/mole Co) was added during stirring and after that 7.724 g sugar (0.5 mole C/mole Co) was added. The solution was heated to about 40°C in order to dissolve all the sugar added. About 100 cemented carbide, grade SANDVIK DC03 , saw tooth inserts were dipped into the solution and dried in a drying cabinet at a temperature of about 70°C.
The inserts were placed onto net trays and heat treated in a furnace with nitrogen atmosphere. The heating rate was 10°C/min to 700°C, no holding temperature, cooling 10°C/min and finally completed with reduction in hydrogen, holding temperature 800°C for 90 minutes .
As a result the cemented carbide inserts had been coated with a 0.3 μm coating of cobalt.
Example 2
The inserts from Example 1 were brazed onto a saw blade according to the following: Steel DIN75Crl
Brazing material Degussa 49 Cu Flux Degussa Special H
Brazing temperature 690°C
As a reference a saw blade was manufactured using the same materials, but the inserts had been coated with cobalt in the conventional way, i.e. by electrochemical deposition. The strength of the brazing joint was determined on both saw blades by pushing off the inserts in a compression tester, using a special fixture to support the steel blade in the interface between the brazing joint and the steel. The force needed to remove (push off) the inserts was measured with the following results:
Conventional 1 Coating ace coating to the invention
Number of inserts 100 100 Force N per mπ.2, mean 246 287 standard dev 19 11
The inserts according to the invention show both higher mean value and lower spread in the force required to remove them than the inserts coated in the conventional way.

Claims

a m
1. Method of coating metal composites bodies formed by carbides, nitrides, carbonitrides with a binder phase consisting of Co and/or Ni at least partly with a layer of at least one iron group metal preferably Co c h a r a c t e r i s e d in comprising the following steps
- dissolving and complex binding at least one salt of at least one iron group metal containing organic groups in at least one polar solvent with at least one complex former comprising functional groups in the form of OH or NR3, (R=H or alkyl)
- optionally adding a soluble carbon source and/or other soluble agents to improve the wetting properties into the solution
- applying the solution at least partly on said bodies by dipping, spraying or painting
- drying the inserts to evaporate the solvent
- heat treating the dried bodies in inert and/or reducing atmosphere to obtain said bodies at least partly coated with said at least one iron group metal.
PCT/SE1995/001586 1994-12-30 1995-12-27 Method of coating cutting tool inserts Ceased WO1996021051A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
AT95942374T ATE190673T1 (en) 1994-12-30 1995-12-27 METHOD FOR COATING CUTTING INSERTS
DE69515683T DE69515683T2 (en) 1994-12-30 1995-12-27 METHOD FOR COATING CUTTING INSERTS
US08/849,770 US6033735A (en) 1994-12-30 1995-12-27 Method of coating cutting inserts
EP95942374A EP0792387B1 (en) 1994-12-30 1995-12-27 Method of coating cutting tool inserts
JP8520900A JPH10511742A (en) 1994-12-30 1995-12-27 Cutting tool insert coating method

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE9404588-7 1994-12-30
SE9404588A SE513959C2 (en) 1994-12-30 1994-12-30 Method of coating cemented carbide tool cutters

Publications (1)

Publication Number Publication Date
WO1996021051A1 true WO1996021051A1 (en) 1996-07-11

Family

ID=20396540

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/SE1995/001586 Ceased WO1996021051A1 (en) 1994-12-30 1995-12-27 Method of coating cutting tool inserts

Country Status (8)

Country Link
US (1) US6033735A (en)
EP (1) EP0792387B1 (en)
JP (1) JPH10511742A (en)
KR (1) KR100383701B1 (en)
AT (1) ATE190673T1 (en)
DE (1) DE69515683T2 (en)
SE (1) SE513959C2 (en)
WO (1) WO1996021051A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6315945B1 (en) * 1997-07-16 2001-11-13 The Dow Chemical Company Method to form dense complex shaped articles
SE0101241D0 (en) * 2001-04-05 2001-04-05 Sandvik Ab Tool for turning of titanium alloys
SE531439C2 (en) * 2005-01-07 2009-04-07 Gunnar Westin Method for making composite materials including metal particles in ceramic matrix and composite materials
JP5977673B2 (en) * 2009-11-09 2016-08-24 カーネギー メロン ユニバーシティ Metal ink composition, conductive pattern, method and device

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3011920A (en) * 1959-06-08 1961-12-05 Shipley Co Method of electroless deposition on a substrate and catalyst solution therefor
US3620834A (en) * 1968-07-18 1971-11-16 Hooker Chemical Corp Metal plating of substrates
US3947616A (en) * 1973-09-27 1976-03-30 Gte Sylvania Incorporated Process for producing cobalt coated refractory metal carbides
US3915665A (en) * 1974-01-23 1975-10-28 Adamas Carbide Corp Coated cemented carbides for brazing
JPS5151908A (en) * 1974-11-01 1976-05-07 Fuji Photo Film Co Ltd
US4907665A (en) * 1984-09-27 1990-03-13 Smith International, Inc. Cast steel rock bit cutter cones having metallurgically bonded cutter inserts
US5134039A (en) * 1988-04-11 1992-07-28 Leach & Garner Company Metal articles having a plurality of ultrafine particles dispersed therein
US4914813A (en) * 1988-11-25 1990-04-10 Innovative Packing Technology Refurbishing of prior used laminated ceramic packages

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
CHEMICAL ABSTRACTS, Volume 121, No. 10, 5 Sept. 1994, (Columbus, Ohio, USA), page 438, Abstract No. 115335x; & JP,A,06 049 651 (NIPPON ALUMINIUM MFG), 22 February 1994. *
PATENT ABSTRACTS OF JAPAN, Vol. 13, No. 501, C-652; & JP,A,01 201 091 (IBIDEN CO LTD), 14 August 1989. *
PATENT ABSTRACTS OF JAPAN, Vol. 8, No. 99, E-243; & JP,A,59 017 223 (NIPPON DENKI K.K.), 28 January 1984. *

Also Published As

Publication number Publication date
SE513959C2 (en) 2000-12-04
DE69515683T2 (en) 2000-07-06
ATE190673T1 (en) 2000-04-15
KR100383701B1 (en) 2003-07-18
EP0792387B1 (en) 2000-03-15
US6033735A (en) 2000-03-07
SE9404588D0 (en) 1994-12-30
SE9404588L (en) 1996-07-01
JPH10511742A (en) 1998-11-10
DE69515683D1 (en) 2000-04-20
EP0792387A1 (en) 1997-09-03

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