METHOD OF PREPARING COATED CEMENTED CARBIDE PRODUCT AND RESULTING PRODUCT

Abstract: An improved process for the production of coated cemented carbide products is disclosed. A cemented carbide substrate is treated to form a metal carbide, nitride or carbonitride coating. The coated substrate is heat-treated at a temperature close to the melting point of the binder metal of the cemented carbide to diffuse elements from the substrate into the coating. Thereafter, and without an intermediate oxidation of the coating, a wear-resistant oxide (e. g., aluminium oxide) coating is applied to form the improved coated cemented carbide product. In a modification of the process, an intermediate (second) metal carbide, nitride or carbonitride coating is applied after the heat treatment and a portion of the second coating is oxidized, nitrided or sulfided without detrimentally affecting the adherence of the second coat­ ing. In another modification of the process, a sulfur- and/­ or nitrogen-containing gas is added during the last part of or subsequent to the first treatment of the cemented carbide substrate.

Description: METHOD OF PREPARING COATED CBENED CARBIDE PRODUCTS AND REUDTING PRODUCT The present invention relates to cemented carbide bodies having at least one thin, extremely wear resistant surface layer and to a method of making such products. More particularly, it relates to such coated cemented carbide products in which a layer of aluminum oxide or other wear resistant oxide is firmly bonded to the substrate. It heretofore was known that an improved wear resistance can be obtained in hard metal (cemented carbide) bodies, for example, cutting inserts, by applying a surface layer of wear resistant oxide upon a substrate of conventional sintered hard metal containing at least one carbide together with a binder metal (see, for example, U.S. Patent Nos. 3,736,107 and 3,836,392). Usually, the thin layer has been applied by deposition from a gaseous phase (e.g., Chemical Vapor Deposition or "CVD" technique), but several other methods have been proposed. Disturbances from the substrate (and from the material in the reactor vessel, etc.) may obstruct the formation of layers having a satisfactory structure (morphology) and binding ability to the substrate if an oxide layer is applied directly upon the hard metal. Therefore, further development steps have been performed in order to give the products improved properties, suited for the commercial market. It heretofore was known that desired results could be obtained by the utilization in such composites of different kinds of intermediate layers, for example, one or more layers of carbides, carbonitrides and/or nitrides of Ti, Zr, Rf, V, Nb, Ta, Cr, Mo, W, Si and/or B (see, for example, U.S. Patent No. 3,837,896). In said patent, belonging to the same assignee as the present application, it was noted that neither of the layers contains a binder metal. Other known cemented carbide products consist of laminated layers of different hard metal grades. Such other known cemented carbide products were prepared by conventional pressing and sintering techniques and contained therefore considerable amounts of binder metal (see, for example, British Patent Nos. 1,042,711, 1,115,908 and 1,118,362). Thus, the statement in U.S. Patent 3,837,896 that the coatings should be free from binder metal was not meant to exclude certain inclusions or small contents of mainly Co and W or WC that can be present in the intermediate layer. The essential feature of the invention of U.S. Patent 3,837,896 is that the intermediate layer serves as a barrier to "catch" the mentioned elements, etc., and prevent their diffusion through the layer so that harmful influences upon the oxide layer from these constituents of the substrate can be avoided at the sites of nucleation and/ or the growth of the oxide layer. By these means, a coherent and contiminus carbide or nitride layer free from binder metal can be obtained at least in a zone immediately below the oxide layer. It was also known that improved adherence of oxide coatings on cemented carbide substrates could be obtained by a method comprising certain heat treatment and oxidizing steps (see, for example,U'.S. Patent 4,018,631). In this method there was a combination of essentially four different steps (I)-(IV): (I) Forming on the cemented carbide substrate (containing W and Co.) a coating comprising a material selected from carbide, nitride, carbonitride and mixtures thereof. (II) Diffusing W and Co into said coating by heating the product at a temperature greater than the melting point of the Co phase. (III) Oxidizing said coating. (IV) Applying an oxide layer. All these steps were known, either separately or in certain combinations, in connection with coatings on cemented carbide. Thus, the commercial product covered by the earlier mentioned U.S. Patent 3,837,896 is a combination of the steps (I) and (IV). Furthermore, there is mentioned in the specification of said U.S. patent (see, for example, Column 3, lines 52-57) that also the step (III) may be utilized. Finally, the heat treatment of coated cemented carbide at an increased temperature, i.e., step (it), was disclosed in the earlier mentioned U.S. Patent 3,836,392 (see, for example, Column 2, lines 38-45). The said U.S. Patent 3,836,392 was in turn indirectly referred to in the specification, Column 1, lines 25-47, of U.S. Patent 3,637,896, both patents now belonging to the same assignee. It has now been found that new results can be obtained by a certain combination of some of these known steps. It has now also been found, quite surprisingly, that further, considerable improvements in use and adherence can be achieved if the above mentioned oxidizing step is avoided and the remaining steps (I) + (it) + (IV) are essentially applied. The advantages which might be expected from the earlier mentioned known process which includes oxidation of the surface of the coated cemented carbide, would at first sight appear to be a result of the formation of a compound on that surface which is related to the wear resistant oxide applied afterwards. It has been found, however, that the oxidation of the intermediate layer, for example, in the case of a titanium carbide coating, from TiC to TiO, TiO2 or other oxide or oxycarbide (realising that corresponding compounds containing nitrogen can also be formed if nitrogen is present) causes an expansion of the volume of the layer which can give rise to cracks in the layer. In addition, difficulties arise in the bonding of oxygen in oxides containing titanium to oxygen in oxides containing aluminum. There are, however, different ways of avoiding the mentioned oxidizing step, as will be mentioned in the following, and by these means it is possible to obtain further advantages in the final product. In accordance with the present invention there is provided a method of treating a cemented carbide substrate containing at least one carbide together with binder metal in order to improve its wear resistance and utility, which method consists essentially of treating the substrate in an atmosphere selected from carbide, nitride and carbonitride forming atmospheres to form or apply a coating essentially consisting of at least one coat of at least one member selected from the group consisting of carbides, nitrides and carbonitrides of the elements Ti, Zr, Hf, V, Nb, Tea, Cr, Mo, W, Si and 3; ;'heat treating the coated substrate at a temperature close to or greater than the melting point of the binder phase in order to diffuse elements from the substrate into said coating or from the coating into the substrate; and applying a wear resistant oxide coating on the thus pretreated cemented carbide substrate. The present invention of treating a cemented carbide substrate containing at least one carbide together with binder metal (generally tungsten carbide and cobalt together with other carbides of metals belonging to the groups IVB, VB and VIX of the periodic system if desired as well as possibly other alloying elements) is thus characterized in that as a first step (a) the substrate is treated in a gaseous atmosphere selected from carbide, nitride and carbonitride forming atmospheres in order to form or apply a surface coating essentially comprising a material selected from carbide, nitride, carbonitride and mixtures thereof of elements selected from Ti, Zr, Ef, V, Nb, Ta, Cr, Mo, W, Si and B. After that, in a second step (b) the product, i.e., the substrate provided with a coating according to (a), is heat-treated at a temperature close to or exceeding the melting point of a binder metal phase. Then, in a third step (c), a wear resistant oxide layer is applied on the heat-treated (previously coated) substrate of step (b) without any interfening oxidation of the substrate. The first step (a), by which surface coatings of carbide, nitride or carbonitride (preferably titanium carbide, titanium nitride) are formed or applied, can be performed in several different ways. Besides a usual method which is deposition from a gaseous phase containing metal halide, hydrogen, hydrocarbon and possibly nitrogen (CVD technique), a layer can be applied by pack-eementing and/or resintering. In the last instance, the metal or the hard element (for example TiC) is taken from the substrate. This latter instance is equivalent to the treatment of the substrate according to the steps (a) + (b) as one operation in which the metal or metals forming the actual carbide, nitride and/or carbonitride are diffused from the interior of the substrate to the surface where they are being enriched by using a reactive gvs. In this case, the cemented carbide in the substrate has to contain at least some Y (ga:nma)-phase carbide, i.e. , it has to contain at least some oi the carbide in the form of a cubic carbide such as TiC, TaC, NbC, etc. Thus, there is obtained a Y (gamma)-phase zone at the surface of the substrate and the application of X surface layer (according to the step (a) and the recrystallization and growth of the grains of the layer (being obtained in the process according to the step (b)) can be substituted by a single process step. Because of said grain growth which is normally obtained, the amount of grain boundaries in the surface layer is reduced and the diffusion of metals as W and Co from the substrate is impeded to a great extent as this diffusion takes place essentially along the grain boundaries. It has also been found that a surface having a great,micro-rougbness can be obtained in the last mentioned treatment because of the grain growth and/or the recrystallization, which means an enlarged area of contact and possibilities of nhook-bindingn or otherwise adhering the following oxide layer applied according to the step (c) to the substrate. A method of enriching titanium carbide to the surface of cemented carbide containing (gamma)-phase by packing processes at sintering temperature was, however, known per se (see, for example, U.S. Patent No. 3,564,683, Example 5, in which packing of cemented carbide in TiO2 and graphite at 13500C is described). Also other similar processes were known (see, for example, British patent specification 1,506,915) in which a surface layer of carbide was obtained on a cemented carbide body by treatment of the body with carbon monoxide. By said treatment, the concentration of carbide was caused to be greater in the surface layer than within the remainder of the body, As mentioned earlier, however, it is the special combination of various steps that is essential for obtaining new results, and unexpected, in the final product. Also the heat treatment, erg., in a carbon containing furnace, according to step (b) which is generally conducted in an atmosphere such as vacuum, argon, hydrogen, nitrogen and the like at a temperature above the melting point of the matrix binder metal (in the case of cobalt, a temperature of from about 12000 to 16000C) for a time sufficient to diffuse the metal from the substrate to the coating (usually from about 5 minutes up to about 3 hours or longer) can preferably be performed at a high temperature within that range such that a certain conversion of the crystals in the coating of carbide, etc., is obtained. This increased temperature of diffusion will cause a formation of a micro-rough surface offering the same possibil- ities and advantages as mentioned in the foregoing. The surface coating of carbide, etc., according to step (a) can be applied under such circumstances and at such a supersaturation that short whiskers, coarse grains, ellipsoidal plates, etc., of the carbide, etc. are formed. Suitable conditions for formation of whiskers can be obtained at a carefully adjusted, relatively low supersaturation. ("Supersaturation" or over-saturation is present when the initial concentrations or reactants (including reactants (e.g., carbon) coming from the substrate) and products, ordered as in an ,equilibrium equation, are smaller than the equilibrium concentrations ordered in an analogous way). (See for example 1:Proceedings of the Conference on Chem. Vap. Dep. of Refr. Metals, Alloys and Compounds (1967) USA, Page 3). The whiskers should not be so long, however, that the surface of the subsequent oxide layer will be too rough. Oxidizing is avoided by applying the oxide layer at sufficiently reducing condi- tions. If the oxide layer is applied by means of.CVI)- technique with H20 and H2 present in the gaseous phase, the E20/E2-ratio in the reaction gas shall be relatively low, generally lower than 0.02 and preferably lower than 0.01 so that all of the oxidizing materials take part in the formation of the oxide layer and do not oxidize the substrate. In order to clean the hard metal bodies or if a certain amount of the binder metal such as cobalt, or if a tungsten phase has penetrated to the outermost part of the surface layer during the heat treatment, an etching operation can be efficiently utilized. 3y etching as for example with HC1, possibly in a gaseous phase (in E2), the binder metal is removed. Furthermore, the etching can be effective in the formation of a micro-rough surface. Tungsten and/or tungsten carbide can be removed in a similar way by selec tive etchants. By the concurrent addition of R2 to the etching gas there is also obtained a reduction of cobalt oxide and tungsten oxide which may possibly be present and whose formation can cause cracking. In other cases, it may be advantageous to apply by CVD-technique a very thin layer of carbide, nitride and/or carbonitride or the earlier mentioned elements upon the substrate heated according to the steps (a) + (b). The layer can, if desired, be of the same material as applied in the step (a) and the treatment is. of special interest if this layer and/or layer according to the step (a) has been applied at conditions which produce short whiskers, ellipsoidal plates or coarse grains at the surface which results in an enlarged area of bonding between the carbide, nitride and/or carbonitride and the following oxide layer. In some cases, in a third step, the treatment of step (a) is repeated to provide a second coating. The resulting substrate is then contacted with an atmosphere containing an oxygen nitrogen- or sulfur-containing gas to oxide, nitride and/or sulfide a portion of the second coating (without oxidizing, etc., the whole of the second coating which causes the said coating to have poor adherence). Thereafter, a wear, resistant oxide layers applied on the substrate. The oxide (e.g., aluminum or zirconium oxide) may be applied to the substrate in accordance with known tech -niques such as, for example, those set forth in U.S. Patents 3,836,392 and 3,837,896. In certain instances, an extra strong adherence between the substrate and coating cvn be obtained by heattreating the product after applying the aluminum oxide coating, i.e.r the substrate, treated according to the steps (a) + (b) + (c) , is treated in a further step (d) at a temperature close to or exceeding the melting point of the binder metal phase in the same manner as set forth above for step (b). When a sufficiently effective bond has been obtained between the substrate,heated according to the steps (a) + (b), and the very thin layer of carbide, nitride and/ or carbonitride, for example, between an (inner) TiC-enriched zone of the substrate and a second, outer TiC coating, the substrate is contacted with an oxygen-, nitrogen- or sulfurcontaining gas to partially oxidize, nitride or sulfide the outer (or second) layer. It has been found that if all of the second layer is oxidized, for example, its adherence to the underlying substrate is poor and the layer may fall off in normal usage. It is therefore important the treatment of the composite be conducted such that the entirety of the. second layer is not oxidized, nitrided or sulfided. Although the reasons for the improved results obtained when only a portion (that is, less than about 70% of the thickness of this surface is oxidized, etc.) it appears that the treatment of step (b) changes the relatively fine-grained surface of the first layer into a relatively coarse-grained surface. It also appears that the fine-grained surface gives a more complete, continuous oxide layer (as compared with the coarse-grained surface) so that less cobalt diffuses through. The presence of cobalt has been found to be detrimental in Awl203 coated carbides. The treatment of the substrate with an oxygen-, nitrogen- or sulfur-containing gas may be conducted in accordance with conventional techniques. For example, if the treatment of the substrate to provide the second layer is performed in a gaseous phase by CVD-technique, a gas containing one or more of oxygen, nitrogen or sulfur or their compounds can be added at the end of or at a period during the coating process and in this way cause said elements to be taken up in the layer in a natural order and without the type of problems obtained when' sepa- rate layers are applied in succeeding, discrete steps. For example, this structure can be obtained without the kind of cracking found when the layer is oxidized by CO2 + E2 after the coating as proposed in U.S. Patent 4,018,631. The addition of the mentioned elements to the intermediate layer causes an improved adherence to the outer oxide layer. In particular, very interesting and beneficial results are obtained when the treatment to form the first or second layers is performed without using any chlorine or chlorine compounds in the gaseous phase. The oxide, nitride and,/or sulfide partial outer layer may also be applied by oxidizing, nitriding and/or sulfiding the substrate by conventional techniques known in the art, e.g., utilizing mixtures of CO2 (or CO) + H20 'This method is especially efficient when especially good protection is sought to prevent cobalt diffusion from the substrate. Instead of using CO2 + H2, to oxidize the outer layer it is also possible to treat the coating with a mix'- ture containing sulfur, e.g., CS2 + E2 which forms a sulfide on the outer layer or a mixture containing nitrogen, e.g., a nitrogen oxide and B2, which forms a nitride on the outer layer. In addition, the last-mentioned oxidizing, nitrid ing and/or sulfiding treatment may be applied to the substrate treated as mentioned above in which an ogen-, nitrogen- or sulfur-containing gas is added to the CVI) depositing gas of the second layer. Optionally, another thin coating of carbide, nitride and/or carbonitride can be deposited on top of the last mentioned coating prior to the last alumina coating step and, if desired, an oxygen- or sulfur-containing gas may be added to the CVI) depositing gas in the same manner as described below. It is also advantageous to apply by further step a wear resistant aluminum oxide iayer, suitably a relatively thin layer by means of CVD-technique at a temperature around 1000 C. By this step there is obtained a bonding of oxide during the critical CVI) nucleation stage, which is particular- ly desirable in regard to adherence. A CVD-layer (not heat treated) is also more wear resistant than a heat treated CVI) layer. In certain instances, extra strong adherence between the substrate and a coating can be obtained by heat treating the product after applying the second layer (before andfor after it is oxidized, nitrided or sulfided) in a further step at a temperature close to or exceeding the melting point of the binder metal phase in the same manner as set forth above for step (b). If desired, the substrate, after application of the aluminum oxide coating may also be heat-treated in a similar manner. It may also be advantageous to apply to the aluminum oxide-coated substrate another layer of a carbide, nitride or carbonitride as described 'above in regard to the first step and thereafter to,Åapply another aluminum oxide as wear resistant layer in the same manner described above. It can also be advantageous to add a sulfur- and/ or a nitrogen-containing gas at the end of or at a period during the treatment .,of step (a) to form a sulfide and/or a nitride portion on or in said coating. Thus, when the treatment of the substrate according to thestep (a) is performed in a gaseous phase by svs-technique, a gas containing one or more sulfur- and/or nitrogen-containing compounds is added at the end of or at a period during the coating process and in this way cause the sulfur and/or nitrogen to be taken up in the layer in a natural order. The addition of these elements to the intermediate layer causes a further improved adherence to the outer oxide layer particularly, when the step (a) treatment was performed without using any chlorine or chlorine compounds in the gaseous phase, The nitride and or sulfide partial outer layer may also be applied by nitriding and/or sulfiding the substrate by conventional techniques known in the art, e.g., utilizing mixtures of CS2 + H2 which forms a sulfide on the outer layer or a mixture containing nitrogen, e.g., a nitrogen oxide and H2, which forms a nitride on the outer layer. This method is especially efficient when especially good protection is sought to prevent cobalt diffusion from the substrate. In any event, the nitriding or sulfiding of the first layer is performed such that no more than about 70% of the first layer is sulfided or nitrided. The invention is additionally illustrated in connection with the following Examples which are to be considered as illustrative of the present invention. It should be understood, however, that the invention is not limited to the specific details of the Examples. Example 1 300 cemented carbide cutting inserts (type SPES 120308) are coated with a thin n layer of TiC in a conven- tional CVD pilot plant The composition of the cemented carbide is in % by weight: 86% WC, 5.5% Co and the remainder cubic carbides (TaC, NbC and TiC). The deposition process is performed at lO3O0C and 20 torr; the deposition time is 4 hours. The gas contains 4% CH4 and 4% TiCl4, the remainder being essentially H2. There is obtained a coating of TiC with a thickness of 2 /ume The coated inserts are then heat treated at 13500C to 15000C in a tunnel furnace in hydrogen atmosphere for a time in the heat zone of from about 1 to 3 hours (the shorter times being used for the inserts treated at the higher temperatures). In a final step the inserts are coated with Al203 by treatment in a gaseous phase at a temperature of 1O3O0C and a pressure of 50 torr. In the gaseous phase 3% AlC13 is added to a H2/C02-mixture adjusted so that the content of H2O at the inserts is about 0.002 of the content of H2. The product obtained has the following characteristics according to light microscope examinations: A 4-5 /um. thick.21203 coating (mean average thickness) has been deposited on a micro-rough surface consisting of a 1-2 /Um thick zone. Said zone or layer consists essentially of cubic carbides which have a grain size of about 1 /um and contain crystals protruding about 1 /um and having about the same grain size as in the substrate. The bonding between the substrate and the zone of cubic carbides as well as the bonding between said zone and the Al2O3 coating is excellent. No crack formation between the 1205 coating and the carbide zone can be found. Comparative Example A number of cemented carbide cutting inserts are treated in the same way as in Example 1 - except that the inserts are oxidized for about 0.2 hr in a CO2 + H2-mixture (about 10 CO2) at about 11000C and atmospheric pressure before the coating with Al2O3 is performed. The inserts are examined in a light microscope after the Al203 coating treatment. In the inspections, it is found that the interface between the Al203 layer and the oxidized surface of the heat treated substrate is relatively uniform in com- parison with the results obtained in example 1. In a comparative test using hardness indentations at varying loads the following results are obtained; (Each example gives the result of 3 separate tests. The figure "O" means that no cracking appears and the figure "1" means that cracking is observed). Comparative 'load Example 1 sample (E kg) 60 000 000' too 000 010 150 100 111 The results show that an improved adherence of the Al203 coating was obtained by means of the present invention (Example 1). Example 2 300 hard metal cutting inserts of different batches (type SPUN 120308) are heated in a EF-heated graphite crucible furnace. The composition of the hard metal is (in % by weight) 86% WC, 5.5% Co and the remainder cubic carbides (TaC, NbC and TiC). The temperature is 1350-15500C and as protecting gas is used hydrogen, nitrogen or mixtures of hydrogen and nitrogen with varying amounts of (0-70%) of oxygen and nitrogen-containing gases (up to 1% of oxygen). One batch is treated without any oxygen containing compounds being added to the gas mixture. The flow of gas is lower than in normal sintering. A treatment time at 14000C of 30 minutes is used. In a further step the cutting inserts are coated with Al2O3 in the same way as in the Example 1. Examinations in a light microscope and in a scanning electron microscope give results analogous to those in the Example 1. Compared to the results in said Example the,amount of binder phase enclosed in the surface zone of (gamma)-phase is still lower. Tests with hardness indentations give the following results, being added to the results given in the table of Example 1. Comparative load trample 1 , xwamDle R le 2 (HR & kg) 60 000 000 000000 100 - - 000 010 000000 150 100 111 000000 The greater number of tests in Example 2 is due to the varied partial pressures of oxygen and nitrogen compounds which results in a greater number of samples. The results show that the concurrent performance of steps (a) and (b), besides facilitating the operating of the process, produce coated products having at least as good adherence of the oxide layer as the one obtained by the treatments according to Example 1. Example 3 300 sintered hard metal cutting inserts are coated with a thin layer of TiC. The composition of the hard metal and the process conditions are the same as those described in Example 1. After that, the gas composition is changed to 10% TiCl4, 30% N2 and 60% H2 and a thin layer of iN is applied.on the TiC-coated bodies. The thickness of the TiC (2 /um) + TiN (3 /um) layer is about 5 /um. The coated inserts are then heat treated at 12500 - 14500C in a tunnel furnace in an atmosphere of nitrogen + hydrogen for 0.5 - 3 hours, after which a coating of Al203 is applied by CVD-technique in a treatment similar.so that described in Example 1. It is found by examnations in microscopes that the diffusion of tungsten and cobalt from the substrate has been effectively prevented by the resulting kind of intermediate layer. ExamPle 4 One batch of 300 sintered hard metal cutting inserts is coated with a thin layer of TiC and then heattreated under conditions similar to those described in the sample 1. Another batch of 300 sintered hard metal cutting inserts is heat treated according to the conditions described in Example 2. All cutting inserts are then coated with successive layers of (TC + TiN) and a further TiC layer at the conditions mentioned in Example 3. The coating time is shortened, however, so that a total thickness of 0.5 - 2 /um of the (TiC + iN) and the further TiC layer is obtained. Finally, a coating of A1203 is applied on the inserts. The resulting products in both instances of performing steps (a) and (b) concurrently show excellent adherence of the oxide coating0 Example 5 100 hard metal cutting inserts of the type SPUN 120308 with the composition (in s by weight) 84*9 WC, 5.5 Co and 9.6 cubic carbides (eia, rba, EaC) in a first method ("variant a") are coated with a TiC layer, 4 /um thick, by means of the CED-technique mentioned in Example 1 (except a longer coating time). After that, the coated inserts are heat-treated at 14100C in a muffle furnace in hydrogen atmosphere for about 2 hours'. In a final step, the cutting inserts are coated with a surface layer of Al2O3, about 4 thick, using the same conditions as in the Example 1. For a comparison, 100 hard metal cutting inserts of the same composition as before are processed by a second method ("variant b"), in which the inserts are coated with TiC and heat-treated at about the same conditions for variant a. After the heat-treatment, however, the inserts are oxidized for about 0.2 hr in a C02 + H2-mixture (about 10% C 2) at about 11000C and atmospheric pressure. In a final step, the cutting inserts are coated with a surface layer of Al2O3, about 4 /um thick, using the same conditions as mentioned earlier. The thickness of the zone enriched in cubic carbides is about 2-3 /um. Cutting tests, in which the mentioned two groups of inserts (variant a and b, respectively) are compared, are performed by turning a steel with the following analysis ( by weight): 0.4 C, 0.3 Si, 0.7 Bdn, 1.4 Cr, 1.4 Ni, 0.2 Mo and the remainder Fe, using the following cutting data: Cutting speed 200 m/min Feed 0.4 mm/rev. Cutting depth 2 mm As a result there is obtained the following life of the inserts: Cutting insert life, mean value, in min, Variant a) 22 Variant b) 14 (Comparative Sample) Example 6 A batch of inserts treated in accordance with hnaples 1 and 2 are treated with HCl to remove most of the cobalt present in the surface zone by etching the inserts with a H2 + HCl-mixture containing 0.1-10 HCl prior to the final Al2O3 deposition. It is observed that the substance became more irregular and rough because of the treatment. The adherence of the aluminum oxide layer is further improved in comparison with Example 1 and 2. The principles, preferred embodiments and modes of operation of the present invention have been described in the foregoing specification. The invention which is intended to be protected herein, however, is not to be construed as limited to the particular forms disclosed, since these are to be regarded as illustrative rather than restrictive. Variations and changes may be made by those skilled in the art without departing from the spirit of the invention. Ex.ample-7 100 cemented carbide cutting inserts (type SPUN 120308) are coated with a thin layer of TiC in a conventional CVI) pilot plant. The composition of the cemented carbide is in % by weight: 86% WC, 5.5% Co and the remainder cubic carbides (TaC, NbC and TiC). The deposition process is performed at 10300C and 20 torr; the deposition time is 4 hours. The gas contains 4% CH4 and 4% TiCl4, the remainder being essentially H2. There is obtained a coating of TiC with a thickness of 2 /um. The coated inserts are then heat-treated at 13500C to 1500 C in a tunnel furnace in hydrogen atmosphere for a time in the heat zone of from about 1 to 3 hours (the shorter times being used for the inserts treated at the higher temperatures). - The cutting inserts are then coated with successive layers of (TiC + DiN) and TiC under process conditions including a gas composition of 4% CH4, 4% TiCl4, remainder H2 applied as before. After that, the gas composition is changed to 10% TiCl4, 30% N2 and 60% H2 and a thin layer of iN is applied on the iC-coated bodies. The total thickness of the (TiC + TiN) and TiC layers was about 0.5-2 /um. Prior to the final Al203 coating, however, the top TiC coating - being 0.5 m thick - is surface oxidized by a C02 and H2 mixture (8% CO2) by which a 0.2 /um thick oxidized layer is formed. The remainder of the 0.5 /um TiC layer remains unoxidized. The resulting product shows excellent adherence of the oxide coating in comparison tests. Example 8 100 cemented carbide inserts are treated in accordance with Example 7. Prior to the final Al203 coating, however, another iC-coating is added on top of the oxidized coating. This coating is obtained in accordance with the first deposition step of Example 7 and its thickness is 1/2 /um. The resulting product shows superior life in comparison cutting tests. Example 9 A batch of 100 cemented carbide inserts is treated in accordance with Example 7. However, instead of the CO2 + E2 mixture used for surface oxidation, a mixture of CO (1%), TiCl4 (0.5%) balance H2 is used. A 0.2 /um thick Ti(C,O) layer is obtained immediately below the aluminum oxide coating. The adherence of A1203 coating is improved. Example 10 A batch of 100 cemented carbide inserts is treated in accordance with Example 9. Prior to the final A1203 coating, another iC-coating is added on top of the oxidized coating in accordance with the first deposition step of Example 7 and its thickness is about 1/2 /um. The resulting product shows superior life in ,comparison cutting tests. Example 11 Two batches of 100 cemented carbide inserts are treated in accordance with Examples 7 and 8, respectively. Prior to the final Al203 deposition, a TiC coating designed to yield coarse grains is added. The added TiC coating is formed by coating with CVD-technique as in the first deposition step of Example 7 with a relatively short (about 1 hour) coating time. During the last 20 minutes of the deposition time, 1% propane and 2,5 HCl are added to obtain a coarse grain size in the surface of the 'coating. Improved adherence of the coating is achieved. Example 12 A batch of inserts treated in accordance with Examples 7 and 8 is treated with HCl prior to the final 8120, coating. It is found that as a result of the heat treatments utilized in these processes of Examples 7 and 8, some of the cutting inserts show an enrichment of.the binder metal (e.g., cobalt) on the surface of the inserts where the cobalt has diffused from the interior of the substrate As the presence of the cobalt will negatively affect the adherence to the surface layer of the later applied oxide coating, most of the cobalt present in the surface zone is efficiently removed by etching the inserts with an H2 + RCl mixture containing 0.1 to 10% HClo It is found that the substrate (including the TiC layer) becomes more rough and irregular because of this treatment. This irregular surface gives an improved adherence of the oxide layer. ExamPle 13 A batch of 300 cemented carbide cutting inserts (type SPUN 120308), having a composition in ffi by weight: 86% WC, 5.5% Co and the remainder cubic carbides (TaC, NbC and TiC) is heated to 1C)300C and treated for about 30 minutes with mixtures of CO2 + H2 containing from 1 to 10% CO2. After this treatment, the inserts are coated with TiC by CVD-teclinique in a conventional CVD-pilot plant. The deposition process was performed at 103OOC and 20 torr. The gas contained 4% CH4 and 4% TiCl4, the remainder being essentially H2. There was obtained a coating of TiC with a thickness of 1-2 /um. The coating time was relatively short, about 1 hour. During the last 15 minutes of the coating time, a sulfur-containing gas (CS2) is added in an amount of 1 percent by volume to form a solid solution of titanium carbide and titanium sulfide. The inserts are then coated with awl203 by treatment in a gaseous phase at a temperature of 10300C and a pressure of 50 torr. In the gaseous phase, 3% AlC13 is added to a H2/C02-mixture adjusted so that the content of H20 at the inserts was about 0.002% of the content of H2. Examinations in a light microscope show that the 4-5 /um thick awl203 coating is reinforced to the substrate by small outgrowths of TiC and the solid solution with excellent bonding and no signs of crack formations. As a result of the heat treatment mentioned above, some of the cutting inserts showed an enrichment of the binder metal (e.g., cobalt) on the surface of the inserts where the cobalt diffused from the interior of the substrate. As the presence of cobalt will negatively affect the adherence to the surface layer of oxide applied later on, most of the cobalt present in the surface zone is efficiently removed by etching the inserts with a H2 + HOl-mLxture containing 0.1 - 10% HCl. It is found that the substrate (including the TiC-layer) becomes more rough and irregular because of the treatment. It is observed in similar tests that this irregular surface of the substrate gives an improved adherence of the oxide layer. Example 14 Another batch of the cemented carbide cutting inserts of Example 13 is coated with TiC by CVD-technique as in Example 13 except that the inserts are not heattreated prior to coating. During the last part (i.e., last 15 minutes) of the coating time, a sulfur-containing gas is added as-in Example 13 td form on the surface a solid solution of titanium carbide and titanium sulfide. The inserts are then coated with A1203. The bonding between the substrate and the A1203 coating is excellent. No crack formation between the Al203 coating and the substrate can be found. Example 15 The procedure of Example 14 is repeated except that a nitrogen-containing gas is added to the CVD-atmosphere during the last 15 minutes of the coating time instead of the sulfur-containing gas to form a titanium carbide and titanium nitride solid solution. Example 16 A batch of 300 cemented carbide cutting inserts (type SPUN 120308) having the same composition as in Example 13 is coated with TiC by CVD-techniques in the same way as in Example 13. The coating time is relatively short,. about 1 hour. During the last 20 minutes of the deposition time, 1 v/o propane and 2.5 v/o HCl are added to obtain a coarse grain size in the coating surface. Daring the last 10 minutes of the deposition time, carbon disulfide in an amount of 0.3 v/o is added to form titanium carbide and titanium sulfide coating. The inserts are then coated with Al203 as in Example 13. The resulting inserts show excellent adherence of the coatings with no crack formation between coating and substrate.

Claims: CLAIMS 1. Method of treating a cemented carbide substrate containing at least one carbide together with binder metal in order to improve its wear resistance and utility, which method consists essentially of: (a) treating the substrate in an atmosphere selected from carbide, nitride and carbonitride forming atmospheres to form or apply a coating essentially comprising at least one coat of at least one member selected from the group consisting of carbides, nitrides and carbonitrides of the elements Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W, Si and B; (b) heat treating the coated substrate at a t.em- perature close to or greater than the melting point of the binder phase in order to diffuse elements from the substrate into said coating or from the coating into the substrate; and (c) applying a wear resistant oxide coating on the thus pretreated cemented carbide substrate. 2. The method of claim 1, wherein a second coating of at least one member selected from the group consisting of carbides, nitrides and carbonitrides of the elements Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W, Si and B is applied to the substrate treated according to the steps (a) + (b) prior to step (c). 3. The method of claim 2, wherein the resulting substrate is treated with an oxygen-, nitrogen- or sulfur-containing gas to oxidize, nitride or sulfide a portion of the second coating without detrimentally affecting the adherence of the second coating to the said substrate. 4. The method of claim 3, wherein a further coating of at least one member selected from the group consisting of carbides, nitrides and carbonitrides of the elements Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W, Si and B is applied to the substrate treated. 5. The method of claim 4, wherein an 'oxygen-, nitrogenand/or sulfur-containng gas is added at the end of or at a period during the treatment.6. The method of claim 1, wherein at least part of the binder metal which has diffused to the outermost part of the surface coating during the heat treatment step is removed by menus of selective enchants. 7. The method of claim 1, wherein the treatment of the substrate according to the steps (a) + (b) is performed as one operation, in which the member of the metals of the substrate forming the carbide, nitride and carbonitride is brought to diffuse from the interior of the substrate out to the surface. 8. The method of claim 1, wherein a sulfur- and/or nitrogen-containing gas is added at the end of or at a period during the treatment of step (a) to form a sulfide and/or nitride portion on said coating. 9o The method of any of the preceding claims, wherein the cemented carbide substrate is heat treated by a further step at a temperature close to or greater than the melting point of the binder metal phase. 10. The product of the process of claim 1.

Inventors: CHATFIELD, CHRISTOPHER GEORGE, KULLANDER, GREGOR HENRIK, MIKUS, MARIAN, WESTERGREN, BO KENNETH
Applicants: SANDVIK AKTIEBOLAG
Application year: 1981
Main classification: C23C16
IPC codes: C23C16, C23C30