EP0083043B1 - Pièce d'usure - Google Patents
Pièce d'usure Download PDFInfo
- Publication number
- EP0083043B1 EP0083043B1 EP82111762A EP82111762A EP0083043B1 EP 0083043 B1 EP0083043 B1 EP 0083043B1 EP 82111762 A EP82111762 A EP 82111762A EP 82111762 A EP82111762 A EP 82111762A EP 0083043 B1 EP0083043 B1 EP 0083043B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- layer
- layers
- range
- titanium
- wearing part
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000010936 titanium Substances 0.000 claims description 52
- 229910052757 nitrogen Inorganic materials 0.000 claims description 37
- 238000000576 coating method Methods 0.000 claims description 31
- 239000011248 coating agent Substances 0.000 claims description 28
- 229910052799 carbon Inorganic materials 0.000 claims description 26
- 229910052719 titanium Inorganic materials 0.000 claims description 24
- 239000000203 mixture Substances 0.000 claims description 23
- 239000007789 gas Substances 0.000 claims description 19
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 18
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 18
- 229910052796 boron Inorganic materials 0.000 claims description 18
- 229910052760 oxygen Inorganic materials 0.000 claims description 18
- 238000005520 cutting process Methods 0.000 claims description 16
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 14
- 239000000463 material Substances 0.000 claims description 14
- 239000001301 oxygen Substances 0.000 claims description 14
- 238000003754 machining Methods 0.000 claims description 12
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 11
- 229910052751 metal Inorganic materials 0.000 claims description 11
- 239000002184 metal Substances 0.000 claims description 11
- 150000004767 nitrides Chemical class 0.000 claims description 11
- 229910052710 silicon Inorganic materials 0.000 claims description 8
- 229910052735 hafnium Inorganic materials 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 5
- 229910052726 zirconium Inorganic materials 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- 238000000151 deposition Methods 0.000 claims description 4
- 230000008021 deposition Effects 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 claims description 4
- 150000001247 metal acetylides Chemical class 0.000 claims description 4
- 239000000126 substance Substances 0.000 claims description 4
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 claims description 3
- 229910052582 BN Inorganic materials 0.000 claims description 2
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 claims description 2
- 230000000737 periodic effect Effects 0.000 claims description 2
- FGUJWQZQKHUJMW-UHFFFAOYSA-N [AlH3].[B] Chemical compound [AlH3].[B] FGUJWQZQKHUJMW-UHFFFAOYSA-N 0.000 claims 4
- -1 carbon nitrides Chemical class 0.000 claims 2
- CYKMNKXPYXUVPR-UHFFFAOYSA-N [C].[Ti] Chemical compound [C].[Ti] CYKMNKXPYXUVPR-UHFFFAOYSA-N 0.000 claims 1
- 239000010410 layer Substances 0.000 description 113
- DJPURDPSZFLWGC-UHFFFAOYSA-N alumanylidyneborane Chemical compound [Al]#B DJPURDPSZFLWGC-UHFFFAOYSA-N 0.000 description 24
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 11
- 229910052739 hydrogen Inorganic materials 0.000 description 11
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 9
- 229910002091 carbon monoxide Inorganic materials 0.000 description 7
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 6
- 239000000853 adhesive Substances 0.000 description 5
- 230000001070 adhesive effect Effects 0.000 description 5
- 239000012159 carrier gas Substances 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- 238000010348 incorporation Methods 0.000 description 4
- 229910052748 manganese Inorganic materials 0.000 description 4
- 229910052758 niobium Inorganic materials 0.000 description 4
- 239000010955 niobium Substances 0.000 description 4
- 229910001060 Gray iron Inorganic materials 0.000 description 3
- 229910000746 Structural steel Inorganic materials 0.000 description 3
- 229910052786 argon Inorganic materials 0.000 description 3
- 239000002356 single layer Substances 0.000 description 3
- 229910052715 tantalum Inorganic materials 0.000 description 3
- 229910052720 vanadium Inorganic materials 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 229910015844 BCl3 Inorganic materials 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 229910052698 phosphorus Inorganic materials 0.000 description 2
- 229910052717 sulfur Inorganic materials 0.000 description 2
- FAQYAMRNWDIXMY-UHFFFAOYSA-N trichloroborane Chemical compound ClB(Cl)Cl FAQYAMRNWDIXMY-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910000997 High-speed steel Inorganic materials 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 229910001347 Stellite Inorganic materials 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052810 boron oxide Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- AHICWQREWHDHHF-UHFFFAOYSA-N chromium;cobalt;iron;manganese;methane;molybdenum;nickel;silicon;tungsten Chemical compound C.[Si].[Cr].[Mn].[Fe].[Co].[Ni].[Mo].[W] AHICWQREWHDHHF-UHFFFAOYSA-N 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- JKWMSGQKBLHBQQ-UHFFFAOYSA-N diboron trioxide Chemical compound O=BOB=O JKWMSGQKBLHBQQ-UHFFFAOYSA-N 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- 235000012245 magnesium oxide Nutrition 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical class [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 229910052706 scandium Inorganic materials 0.000 description 1
- 239000002347 wear-protection layer Substances 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 0.000 description 1
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
- 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
Definitions
- the invention relates to a wearing part, in particular a hard metal cutting insert for machining, with a multilayer hard material coating, at least one layer being embodied as an oxide layer.
- Such a wear part is known from DE-AS 2253745, the inner layer of the carbide base body which is initially located and consists of one or more carbides and / or nitrides of the elements Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W, Si and / or B and the outer layer of which consists of one or more extremely wear-resistant deposits made of aluminum oxide and / or zirconium oxide.
- a disadvantage of this wearing part is that cracks can occur in the pure oxide top layers and that in many cases the oxide layers have insufficient adhesive strength and flake off.
- the brittleness of the oxide layer increases rapidly with increasing layer thickness.
- the structure changes very disadvantageously, so that in practice such wear parts are limited to the use of a comparatively very thin layer of a few micrometers or a thicker layer does not bring any additional advantages. This in turn limits the service life of wearing parts, e.g. from indexable inserts to machining, crucial.
- DE-OS 2317447 which represents an additional application to the aforementioned E-AS 2253745, describes a wearing part, the outer cover layer of which consists of one or more deposits of ceramic oxides, the oxides of the elements Si in particular being in addition to the oxides mentioned in the main patent , B, Ca, Mg, Ti and / or Hf are listed and the formation of mixed oxides is generally included in the application. Individual mixed oxides are not particularly emphasized.
- DE-AS 2851584 discloses a composite body, preferably with a hard metal base body, in which on the base body one or more layers of one or more carbides and / or nitrides of the elements Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W, Si, B and on this layer or layers one or more layers of a mixture of at least one oxide and at least one nitride and / or of at least one oxynitride of the elements Cr, Al, Ca, Mg, Th , Sc, Y, La, Ti, Hf, V, Nb, Ta are arranged, the nitrogen content of the outermost layer being 0.1 to 30 atom%, preferably 0.2 to 15 atom%.
- the only example describes the following layer structure on hard metal: TiC, 4 Jl m + Al 2 O 2.8 N 0.2 , 2-3 Jlm.
- carbide wear parts in particular have been known, in which the outer layer consists of a large number of layers of alternating Ti (C, N) and Al 2 (O, N), this embodiment also being within the scope of protection of DE-AS 2917348 falls.
- the object on which the invention is based is to create a wearing part, in particular a hard metal cutting insert for machining with a multi-layer hard material coating, at least one layer being designed as an oxide layer, which has improved wear resistance and improved wear resistance compared to known wearing parts Has adhesive strength of the hard material coating.
- the wearing part according to the invention has a significantly increased wear resistance as well as an excellent adhesive strength of the hard material coating compared to known multi-layer coated wearing parts, so that there is a considerably longer service life of the wearing part.
- These unexpectedly good properties are achieved by the incorporation of boron in the aluminum oxide layers with the simultaneous incorporation of oxygen components in the oxycarbide, oxycarbonitride, oxynitride, oxiboride, oxibornitride and oxiborocarbonitride intermediate layers.
- oxygen and boron contents of the individual layers are within the specified limits.
- the influence of oxygen can practically no longer be determined below 0.1% by weight.
- the hardness of the intermediate layers drops very quickly and does not increase the wear resistance of the layer structure according to the invention.
- an underlayer between the base body and the coating according to the invention.
- This underlayer preferably has a single or multi-layer structure consisting of one or more carbides, nitrides, carbonitrides, borides or boron nitrides of the elements of IV. To VI. Group of the periodic table.
- titanium oxycarbonitride and / or titanium oxynitride with a layer thickness of 0.05 to 1 ⁇ m directly on a base body made of hard metal or over a base layer and then a single aluminum-boron mixed oxide layer with a layer thickness from 2 to 10 ⁇ m.
- a particularly preferred embodiment of the invention provides that directly on a base body made of hard metal or over an underlayer of a coating, consisting of a layer of titanium oxycarbonitride and / or titanium oxynitride with a layer thickness of 0.1 to 1 ⁇ m and subsequently of 2 to 8 aluminum-boron mixed oxide layers having layer thicknesses of 0.3 to 2 microns, respectively, alternating with 1 to 7 layers of Titanoxikarbonitrid and / or titanium oxynitride of the layer thicknesses of 0.05 to 0.5 m Jl are applied.
- the titanium oxycarbonitride and / or titanium oxynitride layers preferably have an oxygen content of 0.5 to 3% by weight, while the aluminum-boron mixed oxide layers preferably have a boron content of 0.04-0.4% by weight. -% exhibit.
- this multilayered layer structure according to the invention results in a further increase in the toughness of the coating with an excellent adhesive strength of the individual layers and thus in an unexpected increase in the wear resistance under impact stress compared to a layer structure according to the invention which contains only one aluminum-boron mixed oxide layer of the wearing part.
- a particularly preferred underlayer starting from a base body made of hard metal, has the layer sequence titanium carbide and / or titanium carbonitride and / or titanium nitride with a total layer thickness of 1 to 8 ⁇ m .
- the aluminum-boron mixed oxides partially contain titanium, zirconium, hafnium, niobium, chromium and / or magnesium oxides.
- the mixed oxides can also have a nitrogen content of 0.14-2.76% by weight (0.2 to 4 atomic%).
- the hard material coating of the wearing part according to the invention is preferably carried out by the CVD process, the chemical composition of the individual layers being determined by appropriate mixing ratios of the reaction gases.
- Another preferred method for producing the wearing part according to the invention is that the individual layers of appropriate chemical composition are produced both by deposition using the CVD method and by interdiffusion between adjacent layers.
- the introduction of the oxygen fractions into the oxycarbide, oxycarbonitride, oxynitride, oxiboride, oxibornitride and / or oxiborocarbonitride layers can take place both via an appropriate gas mixture composition, for example CO 2 H z O vapor, air, O 2 or contain other oxidizing gases, as well as by interdiffusion from the adjacent aluminum-boron mixed oxide layers.
- This interdiffusion can be carried out, for example, by a temperature treatment between or after the individual coating runs at a temperature which is above the coating temperature, or during the coating travel of the aluminum-boron mixed oxide layers by means of an increased supply of oxygen in the gas mixture.
- indexable inserts made of carbide of the UIOT grade / composition 6% Co, 5% TiC, 5% (TaC + NbC), 84% WC coatings corresponded to the USO application group MIO / and the shape SPGN 120308 EN in 5 different layer construction variants applied according to the table below.
- the indexable inserts were cleaned, installed in the coating chamber of a prototype system from the applicant, heated to the coating temperature under protective gas and coated under the following coating conditions.
- Variants 4 and 5 are provided with a layer structure according to the invention. These variants are compared with variants 1 to 3, which have a layer structure which differs from the invention and is known in one case, in a machining test.
- the wear mark width v B of the open area wear was measured after a rotation time of 5 min.
- the single-layer Al 2 O 3 or aluminum-boron mixed oxide layer is replaced by 4 layers, that by 3 Ti (C, N) or 3 Ti (C, N, 0) intermediate layers are connected.
- a Ti (C 0.6 , N 0.4 ) layer was deposited on indexable inserts of the same type as in Example 1 and a TiN layer was deposited thereon.
- the further layer structure was carried out in two variants, variant 2 representing a layer structure according to the invention.
- the coating was carried out under reduced pressure. The wear resistance of the individual variants was again compared with one another in a machining test.
- Oxygen content of the Ti (C, N, O) layers approx. 2% by weight.
- the end of the service life was given by scour wear in both variants.
- the end of the service life was 32 minutes for variant 1 and 41 minutes for variant 2 according to the invention.
- the invention is not limited to hard metal base bodies.
- the layer structure according to the invention also leads to other base materials such as e.g. with high-speed steel, stellite or other heat-resistant alloys, this leads to an unexpectedly large increase in wear resistance.
- the invention is not limited to machining tools. Rather, it also extends to tools for non-cutting machining such as drawing dies and the like. As well as to tools that are mainly exposed to eroding wear, such as. B. rock drilling.
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
- Laminated Bodies (AREA)
- Chemical Vapour Deposition (AREA)
Claims (10)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT0555781A AT377786B (de) | 1981-12-24 | 1981-12-24 | Verschleissteil, insbesondere hartmetall -schneideinsatz zur spanabhebenden bearbeitung |
AT5557/81 | 1981-12-24 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0083043A1 EP0083043A1 (fr) | 1983-07-06 |
EP0083043B1 true EP0083043B1 (fr) | 1985-07-03 |
Family
ID=3577093
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP82111762A Expired EP0083043B1 (fr) | 1981-12-24 | 1982-12-17 | Pièce d'usure |
Country Status (5)
Country | Link |
---|---|
US (1) | US4599281A (fr) |
EP (1) | EP0083043B1 (fr) |
JP (1) | JPS58115081A (fr) |
AT (1) | AT377786B (fr) |
DE (1) | DE3264591D1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6726987B2 (en) | 2001-02-09 | 2004-04-27 | Plansee Tizit Aktiengesellschaft | Hard metal wearing part with mixed oxide coating |
Families Citing this family (49)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IL72728A (en) * | 1983-08-22 | 1988-02-29 | Ovonic Synthetic Materials | Adherence wear resistant coatings |
DE3434616C2 (de) * | 1983-12-19 | 1997-06-19 | Hartmetall Beteiligungsgesells | Verfahren zur Herstellung von Titan-Bor-Oxinitridschichten auf Sinterhartmetallkörpern |
AT385947B (de) * | 1983-12-22 | 1988-06-10 | Ver Edelstahlwerke Ag | Hartmetallkoerper, insbesondere hartmetall-schneidwerkzeug |
US4574459A (en) * | 1983-12-23 | 1986-03-11 | Corning Glass Works | Extrusion die manufacture |
JPS60141406A (ja) * | 1983-12-27 | 1985-07-26 | Fuji Die Kk | 皮剥ダイス |
JPS60238481A (ja) * | 1984-05-14 | 1985-11-27 | Sumitomo Electric Ind Ltd | 多重層被覆超硬合金 |
US4568614A (en) * | 1984-06-27 | 1986-02-04 | Energy Conversion Devices, Inc. | Steel article having a disordered silicon oxide coating thereon and method of preparing the coating |
JPS61221369A (ja) * | 1985-03-27 | 1986-10-01 | Sumitomo Electric Ind Ltd | 被覆超硬合金部材 |
US4774151A (en) * | 1986-05-23 | 1988-09-27 | International Business Machines Corporation | Low contact electrical resistant composition, substrates coated therewith, and process for preparing such |
US5310603A (en) * | 1986-10-01 | 1994-05-10 | Canon Kabushiki Kaisha | Multi-layer reflection mirror for soft X-ray to vacuum ultraviolet ray |
US5433988A (en) * | 1986-10-01 | 1995-07-18 | Canon Kabushiki Kaisha | Multi-layer reflection mirror for soft X-ray to vacuum ultraviolet ray |
US4855264A (en) * | 1986-11-20 | 1989-08-08 | Minnesota Mining And Manufacturing Company | Aluminum oxide/aluminum oxynitride/group IVB metal nitride abrasive particles derived from a sol-gel process |
US4957886A (en) * | 1986-11-20 | 1990-09-18 | Minnesota Mining And Manufacturing Company | Aluminum oxide/aluminum oxynitride/group IVB metal nitride abrasive particles derived from a sol-gel process |
CA1333270C (fr) * | 1987-03-26 | 1994-11-29 | Ppg Industries Ohio, Inc. | Pellicules d'oxynitrure de titane obtenues par pulverisation cathodique |
AT387186B (de) * | 1987-05-04 | 1988-12-12 | Ver Edelstahlwerke Ag | Beschichteter hartmetallkoerper |
AT387988B (de) * | 1987-08-31 | 1989-04-10 | Plansee Tizit Gmbh | Verfahren zur herstellung mehrlagig beschichteter hartmetallteile |
US4950558A (en) * | 1987-10-01 | 1990-08-21 | Gte Laboratories Incorporated | Oxidation resistant high temperature thermal cycling resistant coatings on silicon-based substrates and process for the production thereof |
AT390228B (de) * | 1987-12-24 | 1990-04-10 | Boehler Gmbh | Verschleissteil und verfahren zu seiner herstellung |
GB8801366D0 (en) * | 1988-01-21 | 1988-02-17 | Secr Defence | Infra red transparent materials |
US5304417A (en) * | 1989-06-02 | 1994-04-19 | Air Products And Chemicals, Inc. | Graphite/carbon articles for elevated temperature service and method of manufacture |
FR2649974B1 (fr) * | 1989-07-21 | 1991-09-27 | Aerospatiale | Materiau carbone protege contre l'oxydation par du carbonitrure de bore |
US5266389A (en) * | 1989-09-29 | 1993-11-30 | Sumitomo Electric Industries, Ltd. | Surface-coated hard material for cutting tools or wear resistance tools |
SE9101953D0 (sv) * | 1991-06-25 | 1991-06-25 | Sandvik Ab | A1203 coated sintered body |
DE4340652C2 (de) * | 1993-11-30 | 2003-10-16 | Widia Gmbh | Verbundwerkstoff und Verfahren zu seiner Herstellung |
JP2793773B2 (ja) * | 1994-05-13 | 1998-09-03 | 神鋼コベルコツール株式会社 | 耐摩耗性に優れた硬質皮膜、硬質皮膜被覆工具及び硬質皮膜被覆部材 |
JP3866305B2 (ja) * | 1994-10-27 | 2007-01-10 | 住友電工ハードメタル株式会社 | 工具用複合高硬度材料 |
GB2310218B (en) * | 1996-02-13 | 1999-12-22 | Marconi Gec Ltd | Coatings |
SE510778C2 (sv) * | 1996-07-11 | 1999-06-21 | Sandvik Ab | Belagt skär för finfräsning av grått gjutjärn |
SE518145C2 (sv) * | 1997-04-18 | 2002-09-03 | Sandvik Ab | Multiskiktbelagt skärverktyg |
JP4185172B2 (ja) * | 1997-06-19 | 2008-11-26 | 住友電工ハードメタル株式会社 | 被覆硬質工具 |
US6492011B1 (en) * | 1998-09-02 | 2002-12-10 | Unaxis Trading Ag | Wear-resistant workpiece and method for producing same |
US6432480B1 (en) * | 1999-09-27 | 2002-08-13 | Caterpillar Inc. | Modified boron containing coating for improved wear and pitting resistance |
US6593015B1 (en) | 1999-11-18 | 2003-07-15 | Kennametal Pc Inc. | Tool with a hard coating containing an aluminum-nitrogen compound and a boron-nitrogen compound and method of making the same |
ES2304918T3 (es) * | 2000-03-09 | 2008-11-01 | Sulzer Metaplas Gmbh | Partes recubiertas con una capa dura. |
US7264668B2 (en) * | 2001-10-16 | 2007-09-04 | The Chinese University Of Hong Kong | Decorative hard coating and method for manufacture |
EP1310580B1 (fr) * | 2001-11-07 | 2007-06-13 | Hitachi Tool Engineering, Ltd. | Outil revêtu d'une couche dure |
US6660133B2 (en) * | 2002-03-14 | 2003-12-09 | Kennametal Inc. | Nanolayered coated cutting tool and method for making the same |
SE526603C3 (sv) | 2003-01-24 | 2005-11-16 | Sandvik Intellectual Property | Belagt hårdmetallskär |
JP4569861B2 (ja) * | 2004-03-02 | 2010-10-27 | 三菱マテリアル株式会社 | 硬質被覆層がすぐれた耐チッピング性を発揮する表面被覆サーメット製切削工具 |
AT7663U1 (de) * | 2004-04-16 | 2005-07-25 | Ceratizit Austria Gmbh | Werkzeug mit verschleissfester beschichtung |
SE528108C2 (sv) * | 2004-07-13 | 2006-09-05 | Sandvik Intellectual Property | Belagt hårdmetallskär, speciellt för svarvning av stål, samt sätt att tillverka detsamma |
DE102004063816B3 (de) * | 2004-12-30 | 2006-05-18 | Walter Ag | Al2O3-Multilagenplatte |
JP2009035784A (ja) * | 2007-08-02 | 2009-02-19 | Kobe Steel Ltd | 酸化物皮膜、酸化物皮膜被覆材および酸化物皮膜の形成方法 |
EP2409798B1 (fr) | 2009-03-18 | 2017-04-19 | Mitsubishi Materials Corporation | Outil de coupe à revêtement de surface |
AT12293U1 (de) * | 2009-10-05 | 2012-03-15 | Ceratizit Austria Gmbh | Schneidwerkzeug zur bearbeitung metallischer werkstoffe |
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JPS5022572B1 (fr) * | 1970-07-29 | 1975-07-31 | ||
SE357984B (fr) * | 1971-11-12 | 1973-07-16 | Sandvik Ab | |
US4055451A (en) * | 1973-08-31 | 1977-10-25 | Alan Gray Cockbain | Composite materials |
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US4035541A (en) * | 1975-11-17 | 1977-07-12 | Kennametal Inc. | Sintered cemented carbide body coated with three layers |
JPS5819626B2 (ja) * | 1977-03-17 | 1983-04-19 | セントラル硝子株式会社 | 酸化硼素アルミナ質耐火物 |
US4169913A (en) * | 1978-03-01 | 1979-10-02 | Sumitomo Electric Industries, Ltd. | Coated tool steel and machining tool formed therefrom |
DE2851584B2 (de) * | 1978-11-29 | 1980-09-04 | Fried. Krupp Gmbh, 4300 Essen | Verbundkörper |
DE2917348C2 (de) * | 1979-04-28 | 1984-07-12 | Fried. Krupp Gmbh, 4300 Essen | Verschleißfester Verbundkörper |
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JPS55154562A (en) * | 1979-05-18 | 1980-12-02 | Sumitomo Electric Ind Ltd | Sintered hard alloy part for base material of surface-covered tool material and their manufacture |
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1982
- 1982-12-17 DE DE8282111762T patent/DE3264591D1/de not_active Expired
- 1982-12-17 EP EP82111762A patent/EP0083043B1/fr not_active Expired
- 1982-12-22 JP JP57234983A patent/JPS58115081A/ja active Granted
- 1982-12-23 US US06/452,445 patent/US4599281A/en not_active Expired - Lifetime
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PATENT ABSTRACTS OF JAPAN, unexamined applications, C Field, vol. 5, no. 195, 11. Dezember 1981, THE PATENT OFFICE JAPANESE GOVERNMENT, page 26 C 83 * |
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Cited By (1)
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US6726987B2 (en) | 2001-02-09 | 2004-04-27 | Plansee Tizit Aktiengesellschaft | Hard metal wearing part with mixed oxide coating |
Also Published As
Publication number | Publication date |
---|---|
JPS6154114B2 (fr) | 1986-11-20 |
JPS58115081A (ja) | 1983-07-08 |
ATA555781A (de) | 1984-09-15 |
EP0083043A1 (fr) | 1983-07-06 |
US4599281A (en) | 1986-07-08 |
AT377786B (de) | 1985-04-25 |
DE3264591D1 (en) | 1985-08-08 |
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