EP0758407B1 - Cermet and process for producing it - Google Patents
Cermet and process for producing it Download PDFInfo
- Publication number
- EP0758407B1 EP0758407B1 EP95913058A EP95913058A EP0758407B1 EP 0758407 B1 EP0758407 B1 EP 0758407B1 EP 95913058 A EP95913058 A EP 95913058A EP 95913058 A EP95913058 A EP 95913058A EP 0758407 B1 EP0758407 B1 EP 0758407B1
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- EP
- European Patent Office
- Prior art keywords
- mass
- cermet
- binder
- content
- pressure
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- 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.)
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- 239000011195 cermet Substances 0.000 title claims abstract description 68
- 238000000034 method Methods 0.000 title claims description 16
- 239000011230 binding agent Substances 0.000 claims abstract description 46
- 239000002344 surface layer Substances 0.000 claims abstract description 30
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 38
- 238000005245 sintering Methods 0.000 claims description 24
- 239000000203 mixture Substances 0.000 claims description 19
- 229910052757 nitrogen Inorganic materials 0.000 claims description 17
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 16
- 238000010438 heat treatment Methods 0.000 claims description 16
- 238000001816 cooling Methods 0.000 claims description 15
- 229910052758 niobium Inorganic materials 0.000 claims description 15
- 239000000463 material Substances 0.000 claims description 14
- 229910052721 tungsten Inorganic materials 0.000 claims description 14
- 229910052715 tantalum Inorganic materials 0.000 claims description 13
- 229910052750 molybdenum Inorganic materials 0.000 claims description 11
- 239000010410 layer Substances 0.000 claims description 10
- 239000007789 gas Substances 0.000 claims description 9
- 230000035515 penetration Effects 0.000 claims description 9
- 229910052786 argon Inorganic materials 0.000 claims description 8
- 229910052720 vanadium Inorganic materials 0.000 claims description 8
- 229910052719 titanium Inorganic materials 0.000 claims description 6
- 238000002844 melting Methods 0.000 claims description 5
- 230000008018 melting Effects 0.000 claims description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 4
- 238000000576 coating method Methods 0.000 claims description 4
- 239000011261 inert gas Substances 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 claims description 4
- 229910052751 metal Inorganic materials 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 4
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 238000000227 grinding Methods 0.000 claims description 3
- 238000002156 mixing Methods 0.000 claims description 3
- 230000003746 surface roughness Effects 0.000 claims description 3
- 239000004020 conductor Substances 0.000 claims description 2
- 229910002804 graphite Inorganic materials 0.000 claims description 2
- 239000010439 graphite Substances 0.000 claims description 2
- 150000001247 metal acetylides Chemical class 0.000 claims description 2
- 150000004767 nitrides Chemical class 0.000 claims description 2
- 238000004452 microanalysis Methods 0.000 claims 2
- 206010026865 Mass Diseases 0.000 claims 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims 1
- 230000006835 compression Effects 0.000 claims 1
- 238000007906 compression Methods 0.000 claims 1
- 229910052593 corundum Inorganic materials 0.000 claims 1
- 239000004615 ingredient Substances 0.000 claims 1
- 239000002356 single layer Substances 0.000 claims 1
- 229910001845 yogo sapphire Inorganic materials 0.000 claims 1
- 239000010936 titanium Substances 0.000 description 14
- 238000005520 cutting process Methods 0.000 description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 7
- 239000012298 atmosphere Substances 0.000 description 6
- 229910002091 carbon monoxide Inorganic materials 0.000 description 5
- 230000000052 comparative effect Effects 0.000 description 5
- 239000000758 substrate Substances 0.000 description 5
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical group [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 239000012299 nitrogen atmosphere Substances 0.000 description 3
- 238000003825 pressing Methods 0.000 description 3
- 238000011282 treatment Methods 0.000 description 3
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 229910001873 dinitrogen Inorganic materials 0.000 description 2
- 238000001513 hot isostatic pressing Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 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 description 2
- 239000002347 wear-protection layer Substances 0.000 description 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Images
Classifications
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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
- C22C29/04—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 carbonitrides
-
- 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
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- 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
Definitions
- the invention relates to a cermet with a hard material content of 95 to 75% by mass and 5 to 25% by mass of binder as the balance Cobalt and / or nickel, the hard material phase consisting of carbonitrides with a cubic B1 crystal structure and 30 to 60 mass% Ti, 5 to 25 mass% W, 5 to 15 mass% Ta, of which up to 70% by mass can be replaced by Nb, 0 to 12 mass% Mo, 0 to 5 mass% V, 0 to 2 mass% Cr, 0 to Contains 1% by mass of Hf and / or Zr, the (C + N) content in the carbonitride phase > 80 mol%, the nitrogen content N / (C + N) is between 0.15 and 0.7 and in the binder phase up to 2% Al and / or metallic W, Ti, Mo, V and / or Cr dissolved are.
- the hard material phases essentially have a core-edge structure.
- the invention further relates to a method of manufacture of such a cermet by mixing, grinding, granulating and Pressing a starting mixture containing corresponding constituents and then sintering.
- EP 0 344 421 A1 proposes a cermet that either an average grain size of the hard material phase in the surface layer compared to a core with a penetration depth of 0.05 mm, which is between 0.8 to 1.2 times the average grain size of the hard material phase in the cermet core is or in the same penetration depth affects a binder phase that is 0.7 up to 1.2 times the average binder content of the cermet core or where the hardness in the aforementioned penetration depth between 0.95 and 1.1 times the average hardness of the Cermet core lies.
- the starting mixture is used to produce this cermet sintered after grinding, mixing and pre-pressing, in a first stage up to 1300 ° C or below is sintered under vacuum or an inert gas atmosphere while in a second stage above 1300 ° C at a nitrogen pressure is sintered from 0.1 to 20 torr, and wherein the Nitrogen pressure also increases with increasing temperature should.
- the cooling is also in the presence of nitrogen performed.
- EP 0 368 336 B1 describes a cermet substrate with a hard surface layer in which the region with the maximum Hardness at a depth between 5 ⁇ m and 50 ⁇ m from the substrate surface is present, and the substrate surface has a hardness of 20 to 90% of the maximum hardness.
- This Cermets becomes the pre-pressed mixture of an initial temperature increase to 1100 ° C in a vacuum, followed by an increase in temperature from 1100 ° C to a temperature range between 1400 ° C and 1500 ° C in a nitrogen atmosphere and one finally subjected to sintering in a vacuum.
- EP 0 374 358 B1 describes a process for producing a cermet with 7 to 20% by weight binder phase and a hard phase made of titanium carbide, titanium nitride and / or titanium carbonitride with 35 to 59% by weight Ti, 9 to 29% by weight W, 0.4 to 3.5% by weight Mo, 4 to 24% by weight of at least one metal from Ta, Nb, V and zirconium, 5.5 to 9.5% by weight N 2 and 4, 5 to 12 wt .-% C.
- the formulated mixed, dried and pre-pressed mass is sintered in such a way that the temperature is raised to 1350 ° C.
- the nitrogen atmosphere being set to 1 Torr at 1350 ° C.
- the nitrogen partial pressure together with the temperature increase from 1350 ° C. to the sintering temperature is gradually increased, the nitrogen atmosphere being set to 5 torr at the sintering temperature.
- EP 0 492 059 A3 describes a cermet body whose hardness is at a penetration depth of not less than 1 mm higher than in the interior of the cermet, wherein the binder content can be minimized in a layer thickness of 0.5 to 3 ⁇ m compared to the core substrate.
- the cermet should have a hard material coating in a thickness of 0.5 to 20 ⁇ m made of carbides, nitrides, oxides and borides of titanium and Al 2 O 3 .
- a green compact is first heated to a temperature between 1100 ° C. and 1400 ° C. under vacuum, then nitrogen gas is admitted to a pressure at which the partial nitrogen pressure is between 5 and 10 torr, so that the substrate surface is denitrified.
- the sintering and the final cooling are carried out under a non-oxidizing atmosphere, such as a vacuum or an inert gas atmosphere.
- the body is coated using CVD or PVD.
- EP 0 499 223 A1 proposes that the relative concentration of the binder in a 10 ⁇ m thick layer near the surface be 5 to 50% of the average mean content of binder in the cermet core and in the layer below it from 10 ⁇ m to 100 ⁇ m Penetration depth to set the binder content to 70 to 100% relative to the cermet core, whereby compressive stresses of 30 kgf / mm 2 and more exist on the surface.
- the sintering is carried out under nitrogen gas at a constant pressure of 5 to 30 torr and the cooling under vacuum at a cooling rate of 10 to 20 ° C./min.
- EP 0 515 340 A3 describes a cermet with one Binder-enriched zone near the surface.
- EP 0 519 895 A1 discloses a cermet with a three-layered edge zone, in which the first layer is TiN-rich to a depth of 50 ⁇ m, the next layer from 50 to 150 ⁇ m penetration depth with a binder enrichment and the next layer from 150 ⁇ m to 400 ⁇ m is formed with a binder depletion relative to the interior of the cermet core.
- the sintered body is in an atmosphere of N 2 and / or NH 3 , possibly in combination with CH 4 , CO, CO 2 at 1100 ° C to 1350 ° C for one to 25 hours under atmospheric pressure or a pressure above 1.1 bar treated.
- the cermets known from the prior art have the surface either different binder levels what is recognizable by spotty appearance, or tend to stick of the binder with the sinter pad, what because of that related reactions to changes in composition in the Contact zone leads.
- Other disadvantages of the previous one Cermets known in the prior art are sometimes high Surface roughness as well as with increased binder metal contents in poor adhesion to the surface from there Wear protection layers. If nickel content in the Surface is increased, is not a CVD coating at all possible.
- the disadvantages mentioned speak in particular against the use of the cermet as a cutting insert for cutting Editing.
- the core areas under the surface layer mentioned have at least essentially one hard material phase a core edge structure.
- the hard phase in the surface layer only homogeneously or with the core edge structure intended for the core may also be partially available.
- the further preferably low roughness depths R T 6 6 ⁇ m or R Z 5 5 ⁇ m have an effect.
- the hardness HV30 is preferably constant in the surface area.
- the cermet can have one or more wear protection layers, which consist of titanium carbide or nitride and / or Al 2 O 3 , preferably applied by the CVD method.
- the cermet described is produced by the method set out in claim 8. Thereafter, a mixture containing the constituents determined according to claim 1 or 3 to 7 is ground, granulated and pre-pressed and then sintered, preferably in sintering furnaces with graphite heating conductors. After pressing, the green body is first heated to the melting temperature of the binder phase under vacuum with a pressure ⁇ 10 -1 mbar, then further heated to the sintering temperature, which is between 1450 to 1530 ° C, where the temperature is 0.2 to 2 hours held and then the body is cooled to 1200 ° C.
- the last heating, holding and cooling is carried out in a gas mixture of N 2 and CO with an N 2 / (N 2 + CO) ratio between 0.1 and 0.9 under an average pressure of 10% to 80% of the mean alternately in a period between 40 and 240 sec, preferably 40 to 180 sec.
- the sintered Body after sintering under a hot isostatic press Argon at temperatures close to the sintering temperature and pressures be subjected to above 30 bar.
- the respective value x represents the relative nitrogen content in the cermet, namely the ratio N / (C + N) and the value y the setting of the gas mixture N 2 / (N 2 + CO).
- the limit values are specified by cermet nitrogen contents between 0.15 and 0.7, to which settings of the gas mixture of 0.1 and 0.9 are assigned. All values in between can be seen in the graphical representation, whereby fluctuations up or down of 10% are permitted. The same applies to the representation according to FIG. 2, where the ordinate y represents the mean pressure in bar and the abscissa represents the binder content x in mass%.
- the mean pressure to be set is 20 mbar, with a binder content of 5% by mass 6 mbar, with deviations from the mean value of up to 10% being permitted here as well.
- the pressures set in the sintering furnace then fluctuate around a constant mean pressure, alternating upwards and downwards at least 10%.
- step 3 with the proviso that no CO was blown in and the set N 2 pressure was constant at 20 mbar.
- Example 1 Cermet according to the invention Comparative cermet Ti (surface layer) / Ti (core): 1.3 1.4 Binder (surface layer) / Binder (core) 0.12 0.6 Total (W, Mo, Ta, Nb) (surface) / Total (W, Mo, Ta, Nb) (core) 0.9 0.6 Edge layer thickness 0.5 ⁇ m 10 ⁇ m Zone below the surface layer with a porosity ⁇ A02 and ⁇ B02 200 ⁇ m 250 ⁇ m and a porosity in the core ⁇ A06 and ⁇ B02 surface roughness R T 5 ⁇ m 15 ⁇ m R Z 3.8 ⁇ m 11 ⁇ m
- Example 2 Cermet according to the invention Comparative cermet Ti (surface layer) / Ti (core) 1.23 1.00 Binder (surface layer) / Binder (core) 0.15 1.20 Total (W, Mo, Ta, Nb) (surface) / Total (W, Mo, Ta, Nb) (core) 0.98 0.8 Porosity throughout ⁇ A02 and ⁇ B02 all other values as in example 1.
- a comparison body was subjected to the same process steps 1, 2 and 4, but process step 3 with the proviso that no CO was blown in and the N 2 pressure was constant at 20 mbar.
- Example 3 Cermet according to the invention Comparative cermet Ti (surface layer) / Ti (core) 1.32 1.00 Binder (surface layer) / Binder (core) 0.27 0.50 Total (W, Ta, Nb) (surface) / Total (W, Ta, Nb) (core) 0.82 1.5 Edge layer thickness 0.3 ⁇ m 5 ⁇ m Zone below the surface layer with a porosity ⁇ A02 and ⁇ B02 100 ⁇ m 120 ⁇ m Porosity in the core ⁇ A08 and ⁇ B02 roughness depth R T 3.5 ⁇ m 13 ⁇ m R Z 2.8 ⁇ m 9 ⁇ m
- Example 4 Cermet according to the invention Comparative cermet Ti surface layer / Ti core 1.21 1.00 Binder surface layer / binder core 0.69 1.60 Total amount (W, Ta, Nb) surface / total amount (W, Ta, Nb) core 0.78 0.4 Porosity throughout ⁇ A02 and ⁇ B02 all other values as in example 3.
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Abstract
Description
Die Erfindung betrifft ein Cermet mit einem Hartstoffanteil von 95 bis 75 Massen-% und 5 bis 25 Massen-% Binder als Rest aus Cobalt und/oder Nickel, wobei die Hartstoffphase aus Carbonitriden mit kubischer B1 Kristallstruktur besteht und 30 bis 60 Massen-% Ti, 5 bis 25 Massen-% W, 5 bis 15 Massen-% Ta, wovon bis zu 70 Massen-% durch Nb ersetzt sein können, 0 bis 12 Massen-% Mo, 0 bis 5 Massen-% V, 0 bis 2 Massen-% Cr, 0 bis 1 Massen-% Hf und/oder Zr enthält, der (C+N)-Gehalt in der Carbonitridphase >80 Mol% beträgt, der Stickstoffanteil N/(C+N) zwischen 0,15 und 0,7 liegt und in der Binderphase bis zu 2 % Al und/oder metallisches W, Ti, Mo, V und/oder Cr gelöst sind. Die Hartstoffphasen besitzen im wesentlichen eine Kern-Rand-Struktur.The invention relates to a cermet with a hard material content of 95 to 75% by mass and 5 to 25% by mass of binder as the balance Cobalt and / or nickel, the hard material phase consisting of carbonitrides with a cubic B1 crystal structure and 30 to 60 mass% Ti, 5 to 25 mass% W, 5 to 15 mass% Ta, of which up to 70% by mass can be replaced by Nb, 0 to 12 mass% Mo, 0 to 5 mass% V, 0 to 2 mass% Cr, 0 to Contains 1% by mass of Hf and / or Zr, the (C + N) content in the carbonitride phase > 80 mol%, the nitrogen content N / (C + N) is between 0.15 and 0.7 and in the binder phase up to 2% Al and / or metallic W, Ti, Mo, V and / or Cr dissolved are. The hard material phases essentially have a core-edge structure.
Die Erfindung betrifft ferner ein Verfahren zur Herstellung eines solchen Cermets durch Mischen, Mahlen, Granulieren und Pressen einer entsprechende Bestandteile enthaltenden Ausgangsmischung und anschließendem Sintern.The invention further relates to a method of manufacture of such a cermet by mixing, grinding, granulating and Pressing a starting mixture containing corresponding constituents and then sintering.
In der EP 0 344 421 A1 wird ein Cermet vorgeschlagen, das entweder eine mittlere Korngröße der Hartstoffphase in der Oberflächenschicht gegenüber einem Kern mit einer Eindringtiefe von 0,05 mm haben soll, die zwischen dem 0,8 bis 1,2fachen der mittleren Korngröße der Hartstoffphase im Cermetkern liegt oder in derselben Eindringtiefe eine Binderphase betrifft, die 0,7 bis 1,2mal dem mittleren Bindergehalt des Cermetkerns entspricht oder bei dem die Härte in der vorgenannten Eindringtiefe zwischen dem 0,95 und 1,1fachen der mittleren Härte des Cermetkerns liegt. Zur Herstellung dieses Cermets wird die Ausgangsmischung nach dem Mahlen, Mischen und Vorpressen gesintert, wobei in einer ersten Stufe bis 1300°C oder darunter unter Vakuum oder einer Inertgasatmosphäre gesintert wird, während in einer zweiten Stufe oberhalb 1300°C bei einem Stickstoffdruck von 0,1 bis 20 Torr gesintert wird, und wobei der Stickstoffdruck mit steigender Temperatur ebenfalls steigen soll. Die Abkühlung wird ebenfalls in Anwesenheit von Stickstoff vorgenommen.EP 0 344 421 A1 proposes a cermet that either an average grain size of the hard material phase in the surface layer compared to a core with a penetration depth of 0.05 mm, which is between 0.8 to 1.2 times the average grain size of the hard material phase in the cermet core is or in the same penetration depth affects a binder phase that is 0.7 up to 1.2 times the average binder content of the cermet core or where the hardness in the aforementioned penetration depth between 0.95 and 1.1 times the average hardness of the Cermet core lies. The starting mixture is used to produce this cermet sintered after grinding, mixing and pre-pressing, in a first stage up to 1300 ° C or below is sintered under vacuum or an inert gas atmosphere while in a second stage above 1300 ° C at a nitrogen pressure is sintered from 0.1 to 20 torr, and wherein the Nitrogen pressure also increases with increasing temperature should. The cooling is also in the presence of nitrogen performed.
Die EP 0 368 336 B1 beschreibt ein Cermet-Substrat mit einer harten Oberflächenschicht, in der die Region mit der maximalen Härte in einer Tiefe zwischen 5 µm und 50 µm von der Substratoberfläche vorliegt, und die Substratoberfläche eine Härte von 20 bis 90 % der maximalen Härte hat. Zur Herstellung dieses Cermets wird die vorgepreßte Mischung einer anfänglichen Temperaturerhöhung auf 1100°C im Vakuum, einer anschließenden Temperaturerhöhung von 1100°C auf einen Temperaturbereich zwischen 1400°C und 1500°C in einer Stickstoffatmosphäre und einem schließlichen Sintern im Vakuum unterzogen.EP 0 368 336 B1 describes a cermet substrate with a hard surface layer in which the region with the maximum Hardness at a depth between 5 µm and 50 µm from the substrate surface is present, and the substrate surface has a hardness of 20 to 90% of the maximum hardness. To make this Cermets becomes the pre-pressed mixture of an initial temperature increase to 1100 ° C in a vacuum, followed by an increase in temperature from 1100 ° C to a temperature range between 1400 ° C and 1500 ° C in a nitrogen atmosphere and one finally subjected to sintering in a vacuum.
Die EP 0 374 358 B1 beschreibt ein Verfahren zur Herstellung eines Cermets mit 7 bis 20 Gew.-% Binderphase und einer Hartphase aus Titancarbid, Titannitrid und/oder Titancarbonitrid mit 35 bis 59 Gew.-% Ti, 9 bis 29 Gew.-% W, 0,4 bis 3,5 Gew.-% Mo, 4 bis 24 Gew.-% mindestens eines Metalles aus Ta, Nb, V und Zirkonium, 5,5 bis 9,5 Gew.-% N2 und 4,5 bis 12 Gew.-% C. Die formulierte gemischte, getrocknete und vorgepreßte Masse wird derart gesintert, daß die Temperatur auf 1350°C im Vakuum erhöht wird, wobei die Stickstoffatmosphäre zu 1 Torr bei 1350°C eingestellt wird, der Stickstoffpartialdruck zusammen mit der Temperaturerhöhung von 1350°C bis zur Sintertemperatur allmählich erhöht wird, wobei die Stickstoffatmosphäre zu 5 Torr bei Sintertemperatur eingestellt wird.EP 0 374 358 B1 describes a process for producing a cermet with 7 to 20% by weight binder phase and a hard phase made of titanium carbide, titanium nitride and / or titanium carbonitride with 35 to 59% by weight Ti, 9 to 29% by weight W, 0.4 to 3.5% by weight Mo, 4 to 24% by weight of at least one metal from Ta, Nb, V and zirconium, 5.5 to 9.5% by weight N 2 and 4, 5 to 12 wt .-% C. The formulated mixed, dried and pre-pressed mass is sintered in such a way that the temperature is raised to 1350 ° C. in vacuo, the nitrogen atmosphere being set to 1 Torr at 1350 ° C., the nitrogen partial pressure together with the temperature increase from 1350 ° C. to the sintering temperature is gradually increased, the nitrogen atmosphere being set to 5 torr at the sintering temperature.
Die EP 0 492 059 A3 beschreibt einen Cermetkörper, dessen Härte in einer Eindringtiefe von nicht weniger als 1 mm höher ist als im Cermet-Inneren, wobei der Bindergehalt in einer Schichtdicke von 0,5 bis 3 µm gegenüber dem Kernsubstrat minimiert sein kann. Das Cermet soll eine Hartstoffbeschichtung in einer Dicke von 0,5 bis 20 µm aus Carbiden, Nitriden, Oxiden und Boriden des Titans und Al2O3 aufweisen. Zur Herstellung dieses Körpers wird ein Grünling unter Vakuum zunächst auf eine Temperatur zwischen 1100°C und 1400°C erwärmt, anschließend Stickstoffgas eingelassen bis zu einem Druck, bei dem der Partialstickstoffdruck zwischen 5 und 10 Torr liegt, so daß die Substratoberfläche entstickt wird. Die Sinterung und die abschließende Abkühlung werden unter einer nichtoxidierenden Atmosphäre, wie dem Vakuum oder einer Inertgasatmosphäre durchgeführt. Abschließend wird der Körper mittels CVD oder PVD beschichtet.EP 0 492 059 A3 describes a cermet body whose hardness is at a penetration depth of not less than 1 mm higher than in the interior of the cermet, wherein the binder content can be minimized in a layer thickness of 0.5 to 3 μm compared to the core substrate. The cermet should have a hard material coating in a thickness of 0.5 to 20 μm made of carbides, nitrides, oxides and borides of titanium and Al 2 O 3 . To produce this body, a green compact is first heated to a temperature between 1100 ° C. and 1400 ° C. under vacuum, then nitrogen gas is admitted to a pressure at which the partial nitrogen pressure is between 5 and 10 torr, so that the substrate surface is denitrified. The sintering and the final cooling are carried out under a non-oxidizing atmosphere, such as a vacuum or an inert gas atmosphere. Finally, the body is coated using CVD or PVD.
Zur Herstellung eines hochzähen Cermets schlägt die EP 0 499 223 Al vor, die relative Konzentration des Binders in einer 10 µm dicken oberflächennahen Schicht auf 5 bis 50 % des durchschnittlichen mittleren Gehaltes an Binder im Cermetkern und in der darunterliegenden Schicht von 10 µm bis 100 µm Eindringtiefe den Bindergehalt auf 70 bis 100 % relativ zum Cermetkern einzustellen, wobei Druckspannungen von 30 kgf/mm2 und mehr an der Oberfläche bestehen. Bei dem hierzu angewendeten Verfahren wird die Sinterung unter Stickstoffgas mit einem konstanten Druck von 5 bis 30 Torr und die Abkühlung unter Vakuum mit einer Kühlrate von 10 bis 20°C/min durchgeführt.To produce a high-viscosity cermet, EP 0 499 223 A1 proposes that the relative concentration of the binder in a 10 μm thick layer near the surface be 5 to 50% of the average mean content of binder in the cermet core and in the layer below it from 10 μm to 100 μm Penetration depth to set the binder content to 70 to 100% relative to the cermet core, whereby compressive stresses of 30 kgf / mm 2 and more exist on the surface. In the process used for this purpose, the sintering is carried out under nitrogen gas at a constant pressure of 5 to 30 torr and the cooling under vacuum at a cooling rate of 10 to 20 ° C./min.
Die EP 0 515 340 A3 beschreibt hingegen ein Cermet mit einer an Binder angereicherten oberflächennahen Zone.EP 0 515 340 A3, however, describes a cermet with one Binder-enriched zone near the surface.
Die EP 0 519 895 A1 offenbart ein Cermet mit einer dreischichtigen Randzone, bei der die erste Schicht bis zu einer Tiefe von 50 µm TiN-reich, die nächste Schicht von 50 bis 150 µm Eindringtiefe mit einer Binderanreicherung und die nächste Schicht von 150 µm bis 400 µm mit einer Binderverarmung relativ zum Cermetkerninneren ausgebildet ist. Der Sinterkörper wird hierzu in einer Atmospähre aus N2 und/oder NH3, ggf. in Kombination mit CH4, CO, CO2 bei 1100°C bis 1350°C eine bis 25 Stunden unter Atmosphärendruck oder einem Druck oberhalb 1,1 bar behandelt.EP 0 519 895 A1 discloses a cermet with a three-layered edge zone, in which the first layer is TiN-rich to a depth of 50 μm, the next layer from 50 to 150 μm penetration depth with a binder enrichment and the next layer from 150 μm to 400 µm is formed with a binder depletion relative to the interior of the cermet core. For this purpose, the sintered body is in an atmosphere of N 2 and / or NH 3 , possibly in combination with CH 4 , CO, CO 2 at 1100 ° C to 1350 ° C for one to 25 hours under atmospheric pressure or a pressure above 1.1 bar treated.
Die nach dem Stand der Technik bekannten Cermets besitzen an der Oberfläche entweder unterschiedliche Bindergehalte, was durch fleckiges Aussehen erkennbar ist, oder neigen zu Anhaftungen des Binders mit der Sinterunterlage, was wegen der damit verbundenen Reaktionen zu Änderungen der Zusammensetzung in der Kontaktzone führt. Weitere Nachteile der nach dem bisherigen Stand der Technik bekannten Cermets sind eine teilweise hohe Oberflächenrauhigkeit sowie bei erhöhten Bindemetallgehalten in der Oberfläche eine schlechte Haftung von dort aufgebrachten Verschleißschutzschichten. Sofern Nickelanteile in der Oberfläche erhöht auftreten, ist erst gar keine CVD-Beschichtung möglich. Die genannten Nachteile sprechen insbesondere gegen die Verwendung des Cermets als Schneideinsatz zur spanenden Bearbeitung.The cermets known from the prior art have the surface either different binder levels what is recognizable by spotty appearance, or tend to stick of the binder with the sinter pad, what because of that related reactions to changes in composition in the Contact zone leads. Other disadvantages of the previous one Cermets known in the prior art are sometimes high Surface roughness as well as with increased binder metal contents in poor adhesion to the surface from there Wear protection layers. If nickel content in the Surface is increased, is not a CVD coating at all possible. The disadvantages mentioned speak in particular against the use of the cermet as a cutting insert for cutting Editing.
Es ist daher Aufgabe der Erfindung, das eingangs genannte Cermet durch Beeinflussung der oberflächennahen Zone dahingehend zu verbessern, daß es für Zerspanungsoperationen besser geeignet ist, gleichgültig, ob es unbeschichtet oder mit einer Ein- oder Viellagenbeschichtung eingesetzt werden soll.It is therefore an object of the invention, the cermet mentioned by influencing the near-surface zone to improve that it is more suitable for cutting operations regardless of whether it is uncoated or with a single or multi-layer coating is to be used.
Diese Aufgabe wird durch das im Anspruch 1 genannte Cermet gelöst. Abgesehen von der im Anspruch 1 definierten, extrem dünnen Randzone liegt demnach das Cermet in einer homogenen Struktur vor, was das Vorliegen von Kern-Randstrukturen der Hartstoffphase nicht ausschließen soll.This object is achieved by the cermet mentioned in claim 1 solved. Apart from the extreme defined in claim 1 thin edge zone, the cermet lies in a homogeneous Structure before what the presence of core-edge structures of the Hard phase should not rule out.
Die Aufgabe wird ferner durch das im Anspruch 2 beschriebene Cermet gelöst.The object is further described by that described in claim 2 Solved cermet.
Weiterbildungen der Erfindung sind in den Unteransprüchen 3 bis 7 beschrieben. Further developments of the invention are in the subclaims 3 to 7 described.
Die unter der genannten Oberflächenschicht liegenden Kernbereiche besitzen zumindest im wesentlichen eine Hartstoffphase mit einer Kern-Randstruktur. Demgegenüber kann die Hartstoffphase in der Oberflächenschicht ausschließlich homogen oder mit der für den Kern bestimmten Kernrandstruktur ggf. auch teilweise vorliegen.The core areas under the surface layer mentioned have at least essentially one hard material phase a core edge structure. In contrast, the hard phase in the surface layer only homogeneously or with the core edge structure intended for the core may also be partially available.
Nach einer weiteren Ausgestaltung der Erfindung besitzt das Cermet eine Zone unmittelbar unter der Oberflächenschicht bis zu einer Tiefe von mindestens 50 µm, maximal 600 µm, die eine Porosität nach IS04505 von ≤A02 und <B02 und im darunterliegenden Kern <A08 und <B04 aufweist.According to a further embodiment of the invention Cermet up a zone just below the surface layer to a depth of at least 50 µm, maximum 600 µm, the one Porosity according to IS04505 of ≤A02 and <B02 and below Core <A08 and <B04.
Insbesondere für den Fall der Verwendung der Cermets zu Schneidoperationen wirken sich die weiterhin vorzugsweise geringen Rauhtiefen RT ≤ 6 µm oder RZ ≤ 5 µm aus. Vorzugsweise ist die Härte HV30 im Oberflächenbereich konstant. Particularly when the cermets are used for cutting operations, the further preferably low roughness depths R T 6 6 μm or R Z 5 5 μm have an effect. The hardness HV30 is preferably constant in the surface area.
Nach einer alternativen Ausführungsform besitzt das Cermet in der Oberflächenschicht mit einer Tiefe zwischen 0,01 und 3 µm einen Co- und/oder Ni-Bindergehalt <90 Massen-% bei einem Ti-Gehalt zwischen 100 % bis 120 % relativ zum Kernbereich und die Summe der Gehalte an W, Ta sowie ggf. Mo, Nb, V, Cr beträgt 80 bis 100 Massen-%.According to an alternative embodiment, the cermet in the surface layer with a depth between 0.01 and 3 µm a Co and / or Ni binder content <90 mass% in one Ti content between 100% and 120% relative to the core area and the sum of the contents of W, Ta and possibly Mo, Nb, V, Cr is 80 to 100 mass%.
Das Cermet kann eine oder mehrere Verschleißschutzschichten aufweisen, die aus Carbiden oder Nitriden des Titan und/oder aus Al2O3 bestehen, vorzugsweise aufgetragen nach dem CVD-Verfahren.The cermet can have one or more wear protection layers, which consist of titanium carbide or nitride and / or Al 2 O 3 , preferably applied by the CVD method.
Das beschriebene Cermet wird durch das im Anspruch 8 dargelegte
Verfahren hergestellt. Hiernach wird eine die nach Anspruch 1
oder 3 bis 7 bestimmten Bestandteile enthaltende Mischung
gemahlen, granuliert und vorgepreßt sowie anschließend
gesintert, vorzugsweise in Sinteröfen mit Graphitheizleitern.
Nach dem Pressen wird der Grünling zunächst bis zu der Schmelztemperatur
der Binderphase unter Vakuum mit einem Druck ≤
10-1 mbar aufgeheizt, anschließend weiterhin aufgeheizt bis zur
Sintertemperatur, die zwischen 1450 bis 1530°C liegt, wo die
Temperatur 0,2 bis 2 Stunden gehalten und anschließend der
Körper auf 1200°C abgekühlt wird. Das letzte Aufheizen, Halten
und Abkühlen wird in einem Gasgemisch aus N2 und CO mit
N2/(N2+CO)-Verhältnis zwischen 0,1 und 0,9 unter einem um einen
mittleren Druck um 10 % bis 80 % des Mittelwertes alternierend
in einer Periodendauer zwischen 40 und 240 sec, vorzugsweise 40
bis 180 sec, durchgeführt. Das N2/(N2+CO)-Verhältnis wird
bestimmt durch die Gleichung
Der mittlere Druck bestimmt sich durch den linearen Zusammenhang y = ( 7 / 10 x + 2,5) ± 10 %, wobei y der mittlere Druck (mbar) und x der Bindegehalt in Massen-% ist. Dies bedeutet für einen Bindergehalt von 5 Massen-% einen Druck von 6 mbar ± 0,6 mbar als Druckmittelwert und bei 25 Massen-% einen Druck von 20 mbar ± 2 mbar.The mean pressure is determined by the linear relationship y = (7/10 x + 2.5) ± 10%, where y is the mean pressure (mbar) and x is the binding content in mass%. This means for one Binder content of 5 mass% a pressure of 6 mbar ± 0.6 mbar as pressure average and at 25 mass% a pressure of 20 mbar ± 2 mbar.
Die vorbeschriebene Verfahrensführung ist so zu verstehen, daß ein Druckmittelwert über den gesamten Ablauf des Aufheizens ab dem Schmelzpunkt der Bindephase, Sinterns und Abkühlens bis 1200°C konstant bleibt, jedoch um diesen Druckmittelwert der Druck periodisch schwankt, insbesondere durch eine gleichförmige Auslenkung zu höheren und niedrigeren Werten. Die Schwankungsamplitude kann sinusförmig oder sägezahnförmig sein oder hiervon abgeleitete Formen besitzen. Im Gegensatz zu den nach dem Stand der Technik bekannten Druckbehandlungen führen nur die geschilderten Druckschwankungen zu einer dünnen gleichmäßigen Oberflächenschichtbeeinflussung der vorbeschriebenen Art.The procedure described above is to be understood such that a pressure average over the entire heating process the melting point of the binding phase, sintering and cooling to 1200 ° C remains constant, but around this pressure average Pressure fluctuates periodically, especially due to a uniform one Deflection to higher and lower values. The fluctuation amplitude can be sinusoidal or sawtoothed or have forms derived from them. In contrast to the after state of the art pressure treatments only lead the pressure fluctuations described to a thin uniform Surface layer influence of the type described above.
Nach einer Ausführungsvariante zur Herstellung eines Cermets
nach einem der Ansprüche 2, 3, 5, 6 oder 7 kann der gesinterte
Körper nach dem Sintern einem heißisostatischen Pressen unter
Argon bei Temperaturen nahe der Sintertemperatur und Drücken
oberhalb von 30 bar unterzogen werden. Während der ohne das
nachfolgende heißisostatische Pressen hergestellte Körper einen
erheblich verminderten Bindergehalt von weniger als 30 Massen-%
in der Oberflächenschicht bis zu einer Eindringtiefe von maximal
3 µm zeigt, hat der anschließend heißisostatisch gepreßte
Körper zum Teil höhere Bindergehalte, die jedoch noch unter
90 % relativ zum Bindergehalt im Cermet-Kern liegen.According to a variant for the production of a cermet
according to one of
In einer ersten Ausführungsvariante werden Cermet-Körper nur einem Sintern unterzogen. Die Einstellung der Gasatmosphäre beim Sintern ist aus Fig. 1 und 2 ersichtlich. Es zeigen
- Fig. 1
- den linearen Zusammenhang zwischen dem Verhältnis N/(C+N) im Cermet und der Einstellung des Gehaltes N2/(N2+CO) im Gasgemisch und
- Fig. 2
- die Abhängigkeit der Einstellung des mittleren Druckes vom Bindemetallgehalt in der Ausgangsmischung bzw. im Cermet.
- Fig. 1
- the linear relationship between the ratio N / (C + N) in the cermet and the setting of the content N 2 / (N 2 + CO) in the gas mixture and
- Fig. 2
- the dependence of the setting of the mean pressure on the binder metal content in the starting mixture or in the cermet.
Wie aus Fig. 1 zu entnehmen, stellt der jeweilige Wert
In einem ersten Ausführungsbeispiel der Erfindung ist von folgender
Ausgangsmischung ausgegangen worden (Angaben in Massen-%):
Die Pulverteilchendurchmesser lagen zwischen 1 bis 2 µm. Hieraus
ergibt sich ein Stickstoffgehalt von 3,4 Massen-% und ein
Kohlenstoffgehalt von 9,3 Massen-%, so daß das Verhältnis
N/(N+C) = 0,27 ist. Der Gesamtbindergehalt liegt bei
13,4 Massen-%. Die Ausgangsmischung wurde, wie nach dem Stand
der Technik bekannt, gemahlen, gemischt und vorgepreßt.
Anschließend wurden folgende Verfahrensschritte angewendet:
Bei einem Vergleichskörper wurden dieselben Verfahrensschritte 1, 2 und 4 durchgeführt, aber Schritt 3 mit der Maßgabe, daß kein CO eingeblasen wurde und der eingestellte N2-Druck konstant bei 20 mbar lag.The same process steps 1, 2 and 4 were carried out for a reference body, but step 3 with the proviso that no CO was blown in and the set N 2 pressure was constant at 20 mbar.
Bei der Analyse der Oberflächenschichten nach dem Sintern wurden
folgende Werte festgestellt:
Die entsprechenden Analysen der Oberflächenschicht nach einem
heißisostatischen Pressen ergaben folgende Werte:
In einem weiteren Beispiel der Erfindung ist von folgender Ausgangsmischung
ausgegangen worden (Angaben in Massen-%):
Die Pulverteilchendurchmesser lagen zwischen 1 bis 2 µm. Hieraus
ergibt sich ein Stickstoffgehalt von 6,1 Massen-% und ein
Kohlenstoffgehalt von 7,2 Massen-%, so daß das Verhältnis
N/(N+C) = 0,46 ist. Der Gesamtbindergehalt liegt bei
16,9 Massen-%. Die Ausgangsmischung wurde, wie nach dem Stand
der Technik bekannt, gemahlen, gemischt und vorgepreßt.
Anschließend wurden folgende Verfahrensschritte angewendet:
Ein Vergleichskörper wurde denselben Verfahrensschritten 1, 2 und 4, Verfahrensschritt 3 jedoch mit der Maßgabe unterzogen, daß kein CO eingeblasen wurde und der N2-Druck konstant 20 mbar betrug.A comparison body was subjected to the same process steps 1, 2 and 4, but process step 3 with the proviso that no CO was blown in and the N 2 pressure was constant at 20 mbar.
Bei der Analyse der Oberflächenschichten nach dem Sintern wurden
folgende Werte festgestellt:
Die entsprechenden Analysen der Oberflächenschicht nach einem
heißisostatischen Pressen ergaben folgende Werte:
Die nach obengenannten Beispielen hergestellten Cermets sind
folgenden Zerspanungsuntersuchungen unterzogen worden:
Drehen im glatten Schnitt, trocken
Schnittgeschwindigkeit Vc = 140 m/min
Schnittiefe ap = 2 mm
Vorschub f = 0,3 mm
Turning in a smooth cut, dry
Cutting speed V c = 140 m / min
Depth of cut a p = 2 mm
Feed f = 0.3 mm
Claims (10)
- Cermet with a hard material content of 95 to 75 % by mass and 5 to 25 % by mass Co- and/or Ni-binder, whereby the hard material phase consists of carbonitrides with cubic B1 crystalline structure and contains 30 to 60 % by mass Ti, 5 to 25 % by mass W, 5 to 15 % by mass Ta, of which up to 70 % by mass can be replaced by Nb, 0 to 12 % by mass Mo, 0 to 5 % by mass V, 0 to 2 % by mass Cr, 0 to 1 % by mass Hf and/or Zr, the (C+N) content in the carbonitride phase is >80 mol %, the nitrogen content N/(C+N) ranges between 0.15 and 0.7 and in the binder phase up to 2 % by mass Al is contained and/or metallic W, Ti, Mo, V and/or Cr are dissolved, whereby only in a surface layer defined by a penetration depth of 0.01 to 3 µm, measurable through an energy dispersive microanalysis on a measuring surface >(0.5 x 0.5)mm2,1. the content of Co- and/or Ni-binder in relation to the underlying cermet core zones amounts to ≤30 % by mass2. the Ti-content amounts to 110 to 130 % in relation to the underlying cermet core zones, whereby each time in the cermet core on the one hand and in the surface layer on the other hand an even distribution of the binder metal exists and3. the sum of contents in W, Ta, as well as possible contents of Mo, Nb, V and/or Cr in the surface layer with a thickness of 0.01 to 3 µm amounts to 70 to 100 % by mass in relation to the underlying cermet core zones.
- Cermet with a hard material content of 95 to 75 % by mass and 5 to 25 % by mass Co- and/or Ni-binder, whereby the hard material phase consists of carbonitrides with cubic B1 crystalline structure and contains 30 to 60 % by mass Ti, 5 to 25 % by mass W, 5 to 15 % by mass Ta, 70 % by mass of which can be replaced by Nb, 0 to 12 % by mass Mo, 0 to 5 % by mass V, 0 to 2 % by mass Cr, 0 to 1 % by mass Hf and/or Zr, the (C+N) content in the carbonitride phase amounts to > 80 mol %, the nitrogen content N/(C+N) ranges between 0.15 and 0.7 and in the binder phase up to 2 % by mass Al is contained and/or metallic W, Ti, Mo, V and/or Cr are dissolved, whereby the Co- and/or Ni-binder content in the surface layer with a penetration depth of 0.01 to 3 µm, measurable by an energy dispersive microanalysis, in relation to the underlying layers <90 % by masss at a Ti-content between 100 % to 120 % in relation to the core zone and the sum of the contents of W, Ta, as well as optionally Mo, Nb, V, Cr ranges between 80 % by mass and 110 % by mass.
- Cermet according to claim 1 or 2, characterized in that the core zones underlying the surface layer have at least in essence a hard material phase with a core-rim structure and/or that in the surface layer the hard material phase is exclusively homogeneous.
- Cermet according to one of claims 1 or 3, characterized in that the zone immediately under the surface layer down to a depth of al least 50 µm, maximum 600 µm, has a porosity ≤A02 and <B02 (according to ISO4505) and <A08 and <B04 in the underlying core.
- Cermet according to claim 2 or 2, characterized in that throughout the body the porosity is ≤A02 and <B02.
- Cermet according to one of claim 1 to 5, characterized in that the depth of surface roughness equals RT ≤6 µm or RZ ≤5 µm and/or that the hardness HV 30 is constant in the surface area.
- Cermet according to one of claims 1 to 6, characterized by a single or multiple layer coating of carbides or nitrides of Ti and/or Al2O3, preferably applied through the CVD process.
- Process for the production of a cermet according to one of claims 1 or 3 to 7, by blending, grinding, granulating and compressing a corresponding initial mixture containing the ingredients and sintering it afterwards, preferably in sintering furnaces with graphite heat conductors,
characterized by a heating up to the melting point of the binder phase under vacuum with a pressure of ≤10-1 mbar, a further heating from the melting temperature of the binder phase up to the sintering temperature and holding the sintering temperature for 0.2 - 2 hours and a subsequent cooling down to 1220°C, whereby the further heating, holding and cooling takes place in a gas mixture of N2 and CO with a N2/(N2+CO) ratio between 0.1 and 0.9 under a average pressure alternating by 10 % to 80 % about the middle pressure in a period of time between 40 and 240 seconds, preferably 40 to 180 seconds, with an average pressure which is determined by the linear relation
y = ( 7 / 10 x + 2,5) ± 10 %, whereby y = the average pressure (mbar) and x = the binder content in % by mass, and a N2/(N2 + CO) ratio y, which is determined by
y = ( 16 / 11 x - 0,12) ± 10 % with x = N/(C+N) in the cermet, and subsequent cooling under inert gas, such as argon, nitrogen or under vacuum. - Process according to claim 8, characterized in that during the heating within the melting point range (TS ± 80°C) with the introduction of nitrogen a pressure of 0.2 mbar is set, whereby preferably the compressed body is at first heated up to 1020°C under vacuum with a pressure of ≤0.1 mbar, before a pressure of 0.2 mbar is set during the heating from 1020°C to 1370°C with the introduction of nitrogen.
- Precess for the production of a cermet according to one of claims 2, 3, 5 or 6 or 8, 9, characterized in that after sintering a hot isostatic compression under argon is performed, at temperatures close to the sintering temperature and pressure and pressure above 30 bar.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
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DE4415454 | 1994-05-03 | ||
DE4415454 | 1994-05-03 | ||
DE4423451 | 1994-07-05 | ||
DE4423451A DE4423451A1 (en) | 1994-05-03 | 1994-07-05 | Cermet and process for its manufacture |
PCT/DE1995/000434 WO1995030030A1 (en) | 1994-05-03 | 1995-03-29 | Cermet and process for producing it |
Publications (2)
Publication Number | Publication Date |
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EP0758407A1 EP0758407A1 (en) | 1997-02-19 |
EP0758407B1 true EP0758407B1 (en) | 1998-02-11 |
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US (1) | US5856032A (en) |
EP (1) | EP0758407B1 (en) |
JP (1) | JPH09512308A (en) |
AT (1) | ATE163203T1 (en) |
ES (1) | ES2112053T3 (en) |
WO (1) | WO1995030030A1 (en) |
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SE9701859D0 (en) * | 1997-05-15 | 1997-05-15 | Sandvik Ab | Titanium based carbonitride alloy with nitrogen enriched surface zone |
SE511846C2 (en) * | 1997-05-15 | 1999-12-06 | Sandvik Ab | Ways to melt phase a titanium-based carbonitride alloy |
SE512133C2 (en) * | 1997-07-10 | 2000-01-31 | Sandvik Ab | Method of making titanium-based carbonitride alloys free from binder surface layers |
JP2948803B1 (en) * | 1998-03-31 | 1999-09-13 | 日本特殊陶業株式会社 | Cermet tool and its manufacturing method |
SE514053C2 (en) * | 1999-05-03 | 2000-12-18 | Sandvik Ab | Method of Manufacturing Ti (C, N) - (Ti, Ta, W) (C, N) -Co alloys for cutting tool applications |
SE525745C2 (en) * | 2002-11-19 | 2005-04-19 | Sandvik Ab | Ti (C- (Ti, Nb, W) (C, N) -Co alloy for lathe cutting applications for fine machining and medium machining |
DE10342364A1 (en) * | 2003-09-12 | 2005-04-14 | Kennametal Widia Gmbh & Co.Kg | Carbide or cermet body and process for its preparation |
DE102008048967A1 (en) * | 2008-09-25 | 2010-04-01 | Kennametal Inc. | Carbide body and process for its production |
US8834594B2 (en) | 2011-12-21 | 2014-09-16 | Kennametal Inc. | Cemented carbide body and applications thereof |
CN116162838B (en) * | 2023-04-26 | 2023-06-30 | 崇义章源钨业股份有限公司 | Metal ceramic and preparation method thereof |
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JPS61281835A (en) * | 1985-06-07 | 1986-12-12 | Sumitomo Electric Ind Ltd | Sintering method for cermet |
JPH0643622B2 (en) * | 1985-12-04 | 1994-06-08 | 住友電気工業株式会社 | Method for producing nitrogen-containing cermet |
JPH01152228A (en) * | 1987-12-10 | 1989-06-14 | Sumitomo Electric Ind Ltd | Manufacture of nitrogen-containing cermet |
JPH02131803A (en) * | 1988-11-11 | 1990-05-21 | Mitsubishi Metal Corp | Cutting tool made of abrasion resistant cermet excelling in chipping resistance |
SE467257B (en) * | 1989-06-26 | 1992-06-22 | Sandvik Ab | SINTRAD TITAN-BASED CARBON Nitride Alloy with DUPLEX STRUCTURES |
SE500047C2 (en) * | 1991-05-24 | 1994-03-28 | Sandvik Ab | Sintered carbonitride alloy with high alloy binder phase and method of making it |
SE9101865D0 (en) * | 1991-06-17 | 1991-06-17 | Sandvik Ab | Titanium-based carbonate alloy with durable surface layer |
SE9201928D0 (en) * | 1992-06-22 | 1992-06-22 | Sandvik Ab | SINTERED EXTREMELY FINE-GRAINED TITANIUM BASED CARBONITRIDE ALLOY WITH IMPROVED TOUGHNESS AND / OR WEAR RESISTANCE |
SE470481B (en) * | 1992-09-30 | 1994-05-24 | Sandvik Ab | Sintered titanium-based carbonitride alloy with core-core structure hardeners and ways to manufacture it |
JPH1152228A (en) * | 1997-08-05 | 1999-02-26 | Nikon Corp | Wide angle lens |
-
1995
- 1995-03-29 US US08/716,340 patent/US5856032A/en not_active Expired - Fee Related
- 1995-03-29 JP JP7527925A patent/JPH09512308A/en active Pending
- 1995-03-29 EP EP95913058A patent/EP0758407B1/en not_active Expired - Lifetime
- 1995-03-29 ES ES95913058T patent/ES2112053T3/en not_active Expired - Lifetime
- 1995-03-29 AT AT95913058T patent/ATE163203T1/en not_active IP Right Cessation
- 1995-03-29 WO PCT/DE1995/000434 patent/WO1995030030A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
JPH09512308A (en) | 1997-12-09 |
WO1995030030A1 (en) | 1995-11-09 |
US5856032A (en) | 1999-01-05 |
ES2112053T3 (en) | 1998-03-16 |
EP0758407A1 (en) | 1997-02-19 |
ATE163203T1 (en) | 1998-02-15 |
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