WO1998002394A1 - Sintering method - Google Patents

Sintering method Download PDF

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Publication number
WO1998002394A1
WO1998002394A1 PCT/SE1997/001111 SE9701111W WO9802394A1 WO 1998002394 A1 WO1998002394 A1 WO 1998002394A1 SE 9701111 W SE9701111 W SE 9701111W WO 9802394 A1 WO9802394 A1 WO 9802394A1
Authority
WO
WIPO (PCT)
Prior art keywords
bar
cemented carbide
bodies
weight
sintering
Prior art date
Application number
PCT/SE1997/001111
Other languages
French (fr)
Inventor
Barbro Rohlin
Margareta PÅLSSON
Leif Åkesson
Original Assignee
Sandvik Ab (Publ)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from SE9602752A external-priority patent/SE9602752D0/en
Priority claimed from SE9602751A external-priority patent/SE9602751D0/en
Application filed by Sandvik Ab (Publ) filed Critical Sandvik Ab (Publ)
Priority to AT97932066T priority Critical patent/ATE214044T1/en
Priority to EP97932066A priority patent/EP0912458B1/en
Priority to JP10505907A priority patent/JP2000515110A/en
Priority to DE69710899T priority patent/DE69710899T2/en
Priority to US09/214,594 priority patent/US6071469A/en
Publication of WO1998002394A1 publication Critical patent/WO1998002394A1/en

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C29/00Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/02Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
    • C22C29/06Alloys 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
    • C22C29/08Alloys 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • B22F3/1003Use of special medium during sintering, e.g. sintering aid
    • B22F3/1007Atmosphere
    • B22F3/101Changing atmosphere
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • B22F3/1017Multiple heating or additional steps
    • B22F3/1028Controlled cooling
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/05Mixtures of metal powder with non-metallic powder
    • C22C1/051Making hard metals based on borides, carbides, nitrides, oxides or silicides; Preparation of the powder mixture used as the starting material therefor
    • 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
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2201/00Treatment under specific atmosphere
    • B22F2201/01Reducing atmosphere
    • B22F2201/013Hydrogen
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2201/00Treatment under specific atmosphere
    • B22F2201/10Inert gases
    • B22F2201/11Argon

Definitions

  • the present invention relates to a sintering method for cemented carbide for the purpose of eliminating the 5 binder phase layer from its surface before applying coatings on said surface.
  • Coated cemented carbide inserts have now for many years been commercially available for chip forming machining of metals in the metal cutting industry.
  • inserts are commonly made of a metal carbide, normally WC, generally with addition of carbides of other metals such as Nb, Ti, Ta, etc. and a metallic binder phase of cobalt.
  • a wear resistant material such as TiC, TiN, AI2O3 etc. i'i separately or in combination it has been possible to increase the wear resistance at essentially maintained toughness .
  • binder phase 0 layer generally ⁇ 1 ⁇ m thick on their surface. This particularly applies to inserts with a binder phase enrichment in the surface below the coating, so called cobalt gradient but also to inserts with even distribution of binder phase. In the latter case this
  • the binder phase layer must therefore be removed before carrying out the deposition process.
  • Figure 1 shows in 4000x magnification a top view of the surface of cemented carbide inserts partly covered with a binder phase layer.
  • Figure 2 shows in 4000x magnification a top view of the surface of a cemented carbide insert sintered according to the invention.
  • the dark grey areas are the Co-layer
  • the light grey angular grains are C
  • the grey rounded grains are the so called gamma phase which is (T ⁇ ,Ta,Nb,W)C.
  • the heating and high temperature steps of the sintering is performed in the conventional way.
  • cooling from sintering temperature down to at least below 1200°C is performed in a hydrogen and argon atmosphere of 0.4 to 0.9 bar, preferably 0.5 to 0.8 bar pressure of hydrogen and rest argon.
  • the total pressure shall be 0.5 to 100 bar, preferably 0.5 to 10 bar, most preferably 0.5 to 1 bar, the argon pressure always being >0.1 bar.
  • the best conditions depend on the composition of the cemented carbide, on the sintering conditions and to a certain extent on the design of the equipment used.
  • the sintering should lead to a Co content on the surface of nominal content +6/-4%, preferably +4/-2%.
  • the Co content can be determined e.g. by the use of a SEM (Scanning Electron Microscope) equipped with an EDS (Energy Dispersive Spectrometer) and comparing the intensities of Co from the unknown surface and a reference, e.g. a polished section of a sample of the same nominal composition.
  • the method of the invention can be applied to all kinds of cemented carbides preferably to cemented carbide with a composition of 4 to 15 weight-% Co, up to 20 weight-% cubic carbides such as Tie, TaC, NbC etc. and rest WC .
  • the cemented carbide has a composition 5 to 12 weight-% Co, less than 12 weight-% cubic carbides such as TiC, TaC, NbC etc. and rest WC .
  • the average WC grain size shall be ⁇ 8 ⁇ m, preferably 0.5-5 ⁇ m .
  • Inserts according to the invention are after sintering provided with a thin wear resistant coating including at least one layer by CVD-, MTCVD- or PVD- technique as known in the art.
  • the invention has been described with reference to argon but it is obvious that the same results can also be obtained with the use of other noble gases.
  • Example 1 Cemented carbide inserts of type CNMG 120408 with 5.5 weight-% Co, 8.5 weight-% cubic carbides and 86 weight-% WC of 2 ⁇ m average WC-grain size were sintered in a conventional way at 1450°C and cooled to room temperature in argon. The surface was up to 50% covered with a Co-layer, Fig 1. Inserts of the same composition and type were sintered in the same way but cooled from 1400 to 1200°C temperature in 0.5 bar hydrogen and rest argon and from 1200°C in pure argon atmosphere. The surface was to about 6% covered with Co, which corresponds to the nominal Co content, Fig 2 .

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Powder Metallurgy (AREA)
  • Cutting Tools, Boring Holders, And Turrets (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Chemical Vapour Deposition (AREA)

Abstract

The present invention relates to a method of sintering cemented carbide bodies including heating said bodies to the sintering temperature in a suitable atmosphere and cooling. If said cooling at least to below 1200 °C is performed in a hydrogen atmosphere of pressure 0.4-0.9 bar and ⊃0.1 bar noble gas, preferably argon cemented carbide bodies with no surface layer of binder phase are obtained. This is an advantage when said bodies are to be coated with wear resistant layers by the use of CVD-, MTCVD- or PVD-technique.

Description

Sintering method
The present invention relates to a sintering method for cemented carbide for the purpose of eliminating the 5 binder phase layer from its surface before applying coatings on said surface.
Coated cemented carbide inserts have now for many years been commercially available for chip forming machining of metals in the metal cutting industry. Such
10 inserts are commonly made of a metal carbide, normally WC, generally with addition of carbides of other metals such as Nb, Ti, Ta, etc. and a metallic binder phase of cobalt. By depositing onto said inserts a thin layer of a wear resistant material such as TiC, TiN, AI2O3 etc. i'i separately or in combination it has been possible to increase the wear resistance at essentially maintained toughness .
During sintering cemented carbide inserts often obtain a completely or partly covering binder phase 0 layer generally <1 μm thick on their surface. This particularly applies to inserts with a binder phase enrichment in the surface below the coating, so called cobalt gradient but also to inserts with even distribution of binder phase. In the latter case this
25 layer forms on certain grades but not on other. The reason to this is not understood at present. However, the layer has a negative effect on the process when carrying out CVD- or PVD-deposition, which results in layers with inferior properties and insufficient adhe-
30 rence. The binder phase layer must therefore be removed before carrying out the deposition process.
It is possible to remove such binder phase layer mechanically by blasting. The blasting method is, however, difficult to control. The difficulty resides in
35 the inability to control consistently the blasting depth with necessary accuracy, which leads to an increased scatter in the properties of the final product - the coated insert. It also results in damages to the hard constituent grain of the surface. However, in Swedish patent application 9202142-7 it is disclosed that blasting with fine particles gives an even removal of the binder phase layer without damaging the hard constituent grains.
Chemical or electrolytic methods could be used as alternatives for mechanical methods. US Patent 4,282,289 discloses a method of etching in a gaseous phase by using HC1 in an initial phase of the coating process. In EP-A-337 696 there is proposed a wet chemical method of etching in nitric acid, hydrochloric acid, hydrofluoric acid, sulphuric acid and similar or electro-chemical methods. From JP 88-060279 it is known to use an alkaline solution, NaOH, and from JP 88-060280 to use an acid solution. JP 88-053269 discloses etching in nitric acid prior to diamond deposition. There is one drawback with these methods, namely, that they are incapable of only removing the cobalt layer. They also result in deep penetration, particularly in areas close to the edge. The etching medium not only removes cobalt from the surface but also penetrates areas between the hard consti- tuent grains and as a result an undesired porosity between layer and substrate is obtained at the same time as the cobalt layer may partly remain in other areas of the insert. US 5,380,408 discloses an etching method according to which electrolytic etching is performed in a mixture of sulphuric acid and phosphoric acid. This method gives an even and complete removal of the binder phase layer without depth effect, i.e. reaching zero Co- content on the surface.
On the other hand it is in some cases not desirable to reach zero Co-content on the surface from coating adhesive point of view, but rather a Co surface content close to nominal content.
The above mentioned methods require additional production steps and are for that reason less attractive for production in a large scale. It would be desirable if sintering could be performed in such a way that no binder phase layer is formed or alternatively can be removed during cooling.
It is therefore an object of the present invention to provide a method of sintering cemented carbide in such a way that no binder phase layer is present on the surface after the sintering process but a well defined Co content .
Figure 1 shows in 4000x magnification a top view of the surface of cemented carbide inserts partly covered with a binder phase layer. Figure 2 shows in 4000x magnification a top view of the surface of a cemented carbide insert sintered according to the invention. In these figures the dark grey areas are the Co-layer, the light grey angular grains are C and the grey rounded grains are the so called gamma phase which is (Tι,Ta,Nb,W)C.
According to the method of the present invention the heating and high temperature steps of the sintering is performed in the conventional way. However, cooling from sintering temperature down to at least below 1200°C is performed in a hydrogen and argon atmosphere of 0.4 to 0.9 bar, preferably 0.5 to 0.8 bar pressure of hydrogen and rest argon. The total pressure shall be 0.5 to 100 bar, preferably 0.5 to 10 bar, most preferably 0.5 to 1 bar, the argon pressure always being >0.1 bar. The best conditions depend on the composition of the cemented carbide, on the sintering conditions and to a certain extent on the design of the equipment used. It is within the purview of the skilled artisan to determine by experiments the optimum hydrogen pressure for which no binder phase layer is obtained and no undesired carburization of the cemented carbide is obtained. The sintering should lead to a Co content on the surface of nominal content +6/-4%, preferably +4/-2%. The Co content can be determined e.g. by the use of a SEM (Scanning Electron Microscope) equipped with an EDS (Energy Dispersive Spectrometer) and comparing the intensities of Co from the unknown surface and a reference, e.g. a polished section of a sample of the same nominal composition.
The method of the invention can be applied to all kinds of cemented carbides preferably to cemented carbide with a composition of 4 to 15 weight-% Co, up to 20 weight-% cubic carbides such as Tie, TaC, NbC etc. and rest WC . Most preferably the cemented carbide has a composition 5 to 12 weight-% Co, less than 12 weight-% cubic carbides such as TiC, TaC, NbC etc. and rest WC . The average WC grain size shall be <8 μm, preferably 0.5-5 μm .
Inserts according to the invention are after sintering provided with a thin wear resistant coating including at least one layer by CVD-, MTCVD- or PVD- technique as known in the art. The invention has been described with reference to argon but it is obvious that the same results can also be obtained with the use of other noble gases.
Example 1 Cemented carbide inserts of type CNMG 120408 with 5.5 weight-% Co, 8.5 weight-% cubic carbides and 86 weight-% WC of 2 μm average WC-grain size were sintered in a conventional way at 1450°C and cooled to room temperature in argon. The surface was up to 50% covered with a Co-layer, Fig 1. Inserts of the same composition and type were sintered in the same way but cooled from 1400 to 1200°C temperature in 0.5 bar hydrogen and rest argon and from 1200°C in pure argon atmosphere. The surface was to about 6% covered with Co, which corresponds to the nominal Co content, Fig 2 .

Claims

Claims
1. Method of sintering cemented carbide bodies including heating said bodies to the sintering temperature in a suitable atmosphere and cooling c h a r a c t e r i s e d in that said cooling at least to below 1200 °C is performed in a hydrogen atmosphere of pressure 0.4-0.9 bar and rest a noble gas, preferably argon, with a pressure of >0.1 bar with a total pressure of 0.5 to 100 bar, preferably 0.5 to 10 bar.
2. Method according to claim 1 c h a r a c t e r i s e d n that said hydrogen pressure
Figure imgf000008_0001
3. Method according to any of the preceding claims c h a r a c t e r i s e d in that said cemented carbide has the composition of 4 to 15 weight-% Co, up to 20 weight-% cubic carbides such as TiC, TaC, NbC etc. and rest WC.
4. Method according to any of the preceding claims c h a r a c t e r i s e d in that said cemented carbide has the composition 5 to 12 weight-% Co, less than 12 weight-% cubic carbides such as TiC, TaC, NbC etc. and rest WC.
5. Method according to any of the preceding claims c h a r a c t e r i s e d in that said bodies are provided with a thin wear resistant coating including at least one layer by CVD-, MTCVD- or PVD-techmque .
PCT/SE1997/001111 1996-07-11 1997-06-23 Sintering method WO1998002394A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
AT97932066T ATE214044T1 (en) 1996-07-11 1997-06-23 SINTERING PROCESS
EP97932066A EP0912458B1 (en) 1996-07-11 1997-06-23 Sintering method
JP10505907A JP2000515110A (en) 1996-07-11 1997-06-23 Sintering method
DE69710899T DE69710899T2 (en) 1996-07-11 1997-06-23 SINTER PROCESS
US09/214,594 US6071469A (en) 1997-06-23 1997-07-23 Sintering method with cooling from sintering temperature to below 1200° C. in a hydrogen and noble gas atmosphere

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
SE9602752A SE9602752D0 (en) 1996-07-11 1996-07-11 Sintering method
SE9602751A SE9602751D0 (en) 1996-07-11 1996-07-11 Sintering method
SE9602752-9 1996-07-11
SE9602751-1 1996-07-11

Publications (1)

Publication Number Publication Date
WO1998002394A1 true WO1998002394A1 (en) 1998-01-22

Family

ID=26662713

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/SE1997/001111 WO1998002394A1 (en) 1996-07-11 1997-06-23 Sintering method

Country Status (5)

Country Link
EP (1) EP0912458B1 (en)
JP (1) JP2000515110A (en)
AT (1) ATE214044T1 (en)
DE (1) DE69710899T2 (en)
WO (1) WO1998002394A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0910558B1 (en) * 1996-07-11 2002-02-13 Sandvik Aktiebolag (publ) Sintering method
US6638474B2 (en) 2000-03-24 2003-10-28 Kennametal Inc. method of making cemented carbide tool
US6998173B2 (en) 2000-03-24 2006-02-14 Kennametal Inc. Cemented carbide tool and method of making

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990005200A1 (en) * 1988-10-31 1990-05-17 Krupp Widia Gmbh Hard-metal body

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60110838A (en) * 1983-11-16 1985-06-17 Sumitomo Electric Ind Ltd Sintered hard alloy and its production
JP2600359B2 (en) * 1989-01-19 1997-04-16 三菱マテリアル株式会社 Manufacturing method of surface coated tungsten carbide based cemented carbide cutting tool
SE500049C2 (en) * 1991-02-05 1994-03-28 Sandvik Ab Cemented carbide body with increased toughness for mineral felling and ways of making it

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990005200A1 (en) * 1988-10-31 1990-05-17 Krupp Widia Gmbh Hard-metal body

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0910558B1 (en) * 1996-07-11 2002-02-13 Sandvik Aktiebolag (publ) Sintering method
US6638474B2 (en) 2000-03-24 2003-10-28 Kennametal Inc. method of making cemented carbide tool
US6998173B2 (en) 2000-03-24 2006-02-14 Kennametal Inc. Cemented carbide tool and method of making

Also Published As

Publication number Publication date
JP2000515110A (en) 2000-11-14
EP0912458B1 (en) 2002-03-06
DE69710899T2 (en) 2002-11-28
ATE214044T1 (en) 2002-03-15
EP0912458A1 (en) 1999-05-06
DE69710899D1 (en) 2002-04-11

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