Classifications

• • C—CHEMISTRY; METALLURGY
  • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
  • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
  • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
  • C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
  • C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
  • C23C16/40—Oxides
  • C23C16/403—Oxides of aluminium, magnesium or beryllium
• • C—CHEMISTRY; METALLURGY
  • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
  • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
  • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
  • C23C16/02—Pretreatment of the material to be coated
  • C23C16/0272—Deposition of sub-layers, e.g. to promote the adhesion of the main coating
• • C—CHEMISTRY; METALLURGY
  • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
  • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
  • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
  • C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
  • C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
  • C23C16/32—Carbides
• • C—CHEMISTRY; METALLURGY
  • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
  • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
  • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
  • C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
  • C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
  • C23C16/34—Nitrides
• • C—CHEMISTRY; METALLURGY
  • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
  • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
  • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
  • C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
  • C23C16/455—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for introducing gases into reaction chamber or for modifying gas flows in reaction chamber
• • C—CHEMISTRY; METALLURGY
  • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
  • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
  • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
  • C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
  • C23C16/455—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for introducing gases into reaction chamber or for modifying gas flows in reaction chamber
  • C23C16/45557—Pulsed pressure or control pressure
• • C—CHEMISTRY; METALLURGY
  • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
  • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
  • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
  • C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
  • C23C16/52—Controlling or regulating the coating process
• • C—CHEMISTRY; METALLURGY
  • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
  • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
  • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
  • C23C28/04—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material
  • C23C28/044—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material coatings specially adapted for cutting tools or wear applications

Definitions

• the present invention relates to a surface-coated cutting tool consisting of a substrate body and a hard coating deposited on the substrate by a CVD process, the hard coating comprising at least one dense and hard Al2O3 layer of pure or mainly pure alpha phase ( ⁇ - phase) deposited by a “moderate temperature” CVD (MT-CVD) process within the range from about 600-900°C.
• MT-CVD moderate temperature CVD
• the invention further relates to a process for the deposition of such a ⁇ -Al 2 O 3 layer at moderate temperature by CVD.
• the coating of the cutting tool of the present invention has excellent wear resistance and peeling resistance in continuous and intermittent high-speed metal cutting.
• Cutting tools of various substrate body materials such as cemented carbide, cermet, cubic boron nitride, etc.
• various types of hard layers such as TiC, TiN, TiCN, TiAlN and Al 2 O 3
• Such tool coatings are generally built up by several hard layers in a multi-layer structure. The sequence and the thickness of the individual layers are carefully chosen to suit different cutting applications and workpiece materials.
• Tool coatings are most frequently deposited by Chemical Vapour Deposition (CVD) or Physical Vapour Deposition (PVD) techniques. Both CVD and PVD have advantages and disadvantages over each other, and they result in different microstructural, physical and mechanical coating properties, thus, both techniques provide valuable coatings.
• CVD Chemical Vapour Deposition
• PVD Physical Vapour Deposition
• PVD deposition is carried out at temperatures in the order of about 450-700°C and is performed under ion bombardment leading to high compressive stresses in the coating and no cooling cracks.
• CVD for the deposition of hard tool coatings is carried out at higher temperatures in the order of about 880-1100°C. Due to this high deposition temperature and mismatch in thermal expansion coefficients between the deposited coating materials and the substrate material, such as cemented carbide, CVD produces coatings with cooling cracks and tensile stresses. Because of these process differences CVD coated tools are more brittle and thereby possess inferior toughness behaviour compared to PVD coated tools.
• the CVD technique is suitable and advantageous to deposit many excellent hard and wear resistant coating materials, such as Al 2 O 3 , ZrO 2 , and various Ti and TiAl compounds, e.g. Ti(C,N), TiAl(C,N) etc.
• the microstructure and thereby the properties of these coatings can be altered by varying the deposition conditions. If the standard CVD deposition temperature could be decreased significantly, an increased toughness and improvement of other properties of the coatings would be expected. A noticeable improvement in the toughness behaviour and performance of CVD coated tools came about with the application of the MT-CVD (“moderate temperature” CVD) technique in the tool industry.
• the MT-CVD technique works at deposition temperatures in the range of about 700-900°C and is well established for the deposition of Ti(C,N)-layers from a gas mixture containing TiCl 4 , CH 3 CN and H 2 .
• Modern tool coatings should include at least one polycrystalline layer of Al 2 O 3 in order to achieve high wear resistance, hardness etc. It is well known that Al 2 O 3 crystallises in several different phases: ⁇ , ⁇ , ⁇ , ⁇ , ⁇ etc.
• the most common CVD deposition temperature for Al 2 O 3 is in the range 980-1050°C. At these temperatures both metastable ⁇ -Al 2 O 3 and stable ⁇ -Al 2 O 3 or mixtures thereof can be produced.
• the ⁇ -phase can be present in smaller amounts.
• the high temperature commonly used for the deposition of Al 2 O 3 may lead to embrittlement of the substrate and/or decomposition of thermodynamically metastable materials in the layers underneath the Al 2 O 3 deposition, such as TiAlN etc. Therefore, to avoid the disadvantages going along with high temperature CVD depositions to the deposited Al 2 O 3 layer itself, but also to the layers and the substrate underneath, it would be desirable if also high quality Al 2 O 3 layers, especially single phase stable ⁇ -Al 2 O 3 layers, could be deposited by a CVD process at lower temperatures in the range similar to that of the MT- CVD process. Various attempts have been made to deposit Al 2 O 3 by CVD at low temperature.
• EP 1947213 B1 describes a process to deposit ⁇ -Al 2 O 3 at a temperature in the range from about 625-800°C.
• the Al 2 O 3 deposition requires pre-deposition of an underlying oxygen rich TiCNO layer, which further has to be treated with an oxygen containing gas mixture before the subsequent Al 2 O 3 deposition can be carried out.
• the Al 2 O 3 deposition process requires high concentration of CO 2 and a sulfur dopant, such as H 2 S. If the oxygen treatment step is excluded, then mainly amorphous or metastable phases of Al 2 O 3 are formed.
• the deposition of the underlying TiCNO layer can either be deposited at 450-600°C using PVD technique or at 1000-1050°C using CVD technique. If CVD is used, the required oxygen treatment step to the TiCNO layer, prior to the start of the Al 2 O 3 deposition, is also carried out at high temperature around 1000°C or above. Thus, either two different deposition techniques have to be applied, PVD and CVD, going along with the need to provide double equipment and to transfer the samples between completely different coating devices. And, if one or more additional CVD layers are deposited underneath the TiCNO layer, as it is described for some embodiments of EP 1947213, even more than only one transfer of the samples from CVD to PVD and back to CVD equipment are required.
• high temperature CVD has to be applied to deposit the TiCNO layer and to carry out the oxidation step, going along with all the disadvantages of high temperature treatment to the substrate and/or any further underlying layers of the multi-layer coating.
• the subsequent Al 2 O 3 deposition process is carried out by CVD at a process pressure of 40- 300 mbar and a temperature of 625-800°C, and using a reaction gas composition of AlCl 3 , CO 2 , H 2 , H 2 S and preferably HCl, whereby the CO 2 concentration is very high in the order of 16-40 vol.-% of the reaction gas composition.
• EP 3505282 A1 describes a cutting tool with a multi-layer hard CVD coating comprising a lower layer of a complex nitride or complex carbonitride of Ti and Al, (Ti, Al)(C,N), an adhesion layer, and an upper layer of ⁇ -Al 2 O 3 .
• the authors have found that, in a case where an ⁇ -Al 2 O 3 layer is deposited directly on a (Ti,Al)(C,N) lower layer under typical CVD conditions at about 1000°C, phase separation of AlN occurs in the (Ti,Al)(C,N) layer, and a sufficient hardness for the (Ti,Al)(C,N) layer is not obtained.
• adhesion strength between the (Ti,Al)(C,N) layer and the ⁇ - Al 2 O 3 layer can be improved by providing an adhesion layer of TiCN with an increased oxygen content in the vicinity of the surface being in contact with the ⁇ -Al 2 O 3 upper layer, which can then be formed under relatively low temperature conditions in the range from 800- 900°C at a process pressure of 5-15 kPa, and using a reaction gas composition of AlCl 3 , CO 2 , H 2 and HCl in the nucleation step and an additional amount of H 2 S during layer growth.
• thermodynamic calculations have identified NO + H 2 and HCOOH systems as the most potential sources of oxygen donors to form alumina in the moderate temperature range of 700-950°C.
• the authors describe that dense, uniform and adherent alumina coatings can be deposited on TiC and TiCN coated cemented carbide cutting tools at 870°C using the AlCl 3 + CHOOH + H 2 system. XRD analyses showed that the deposited Al 2 O 3 coatings contained alpha and kappa phases. Funk, R.
• the authors could show that in the H 2 O process at 5 Torr the alumina deposition rate decreased within increasing deposition temperature (from 600-1000°C), whereas in the H 2 -CO 2 process at 50 Torr the deposition rate increased within increasing deposition temperature (from 750-1100°C). It was found that adherence of the TiC and TiN pre-coated substrates was better than on uncoated cemented carbide, and on Cr pre-coated substrates non-adherent deposits were formed. For the standard H 2 -CO 2 process the coatings contained ⁇ -Al 2 O 3 over the temperature range from 850-1100°C, whereas nothing is said about modification, quality, phase purity or any microstructural, physical or mechanical properties of the deposition produced by the H 2 O process.
• the present invention provides a new process for manufacturing a coated cutting tool for hip-forming metal machining consisting of a substrate of cemented carbide, cermet or cubic oron nitride based or other ceramic material and a single-layered or multi-layered wear esistant hard coating, the layers of the hard coating comprise at least one alpha ( ⁇ ) phase Al 2 O 3 coating layer being deposited by chemical vapour deposition (CVD) at an averagehickness in the range from 1 ⁇ m to 20 ⁇ m, wherein the deposition of the alpha phase Al 2 O 3 oating layer is carried out at a temperature in the temperature range from 600 to 900°C, using a process gas composition, as introduced into the CVD reactor, comprising or consisting of AlCl 3 , H 2 O, H 2 and optionally HCl and/or a sulfur source, selected from H 2 S, SF 6 , SO 2 and SO 3 , wherein in the process gas composition, as introduced into the CVD reactor, -
• the process of the present invention overcomes several deficiencies of the prior art and it llows for the deposition and controlled growth of a Al 2 O 3 coating layer of pure or almost pure lpha phase of good crystallinity, high hardness and density at comparably low temperature.
• the standard H 2 -CO 2 process for the deposition of ⁇ -Al 2 O 3 requires high temperature in the rder of 1000°C and above, which may lead to embrittlement of the substrate and ecomposition of thermodynamically metastable materials in the layers underneath the Al 2 O 3 eposition.
• the process of the present invention overcomes this deficiency of highemperature deposition.
• the also known H 2 O process may deposit Al 2 O 3 at temperatures asow as 250°C, however, none of the prior art H 2 O processes was suitable to deposit pure or lmost pure alpha phase Al 2 O 3 of the quality obtained by the process of the presentnvention. In the prior art H 2 O processes either no alpha phase Al 2 O 3 at all was obtained or nly a certain amount of ⁇ -Al 2 O 3 in admixture with significant amounts of other isadvantageous phases, such as gamma or theta phase, and/or amorphous Al 2 O 3 .
• the process of the present invention allows for the deposition of pure or almost pure high quality ⁇ -Al 2 O 3 without the deteriorating effect of a too high deposition temperature on the material underneath.
• the deposition of the alpha phase Al 2 O 3 coating layer is carried out at a temperature in the temperature range from 600 to 900°C. If the temperature is less than 600°C, no alpha phase Al 2 O 3 or alpha phase in admixture with significant amounts of other disadvantageous phases was observed, and layers of poor crystallinity and bad adhesion were obtained. If the temperature is higher than 900°C, the deteriorating effect on instable or metastable material underneath is too high. In an embodiment of the invention the deposition of the alpha phase Al 2 O 3 coating layer is carried out at a temperature in the temperature range from 600 to 850°C.
• the temperature of 850°C or less further reduces the risk of phase transformation of underlying material and the risk of depositing porous Al 2 O 3 layers due to gas phase reactions. It has surprisingly been found that this is achieved in a H 2 O process at comparably low deposition temperature, if the ratio of H 2 O / AlCl 3 is in the range from 0.5 to 2.5, and at the same time, the ratio of H 2 / AlCl 3 is in the range from 200 to 3000 in the process gas composition, as introduced into the CVD reactor. If the ratio of H 2 O / AlCl 3 is too low, lower than 0.5, no pure or almost pure alpha phase is obtained and/or the deposition rate would be extremely low that the process would no longer be economically feasible.
• the ratio of H2O / AlCl3 is higher than 2.5, no alpha phase, but only gamma phase Al2O3 is deposited, even if the ratio of H 2 / AlCl 3 is in the range from 200 to 3000. If the ratio of H 2 / AlCl 3 is too low, lower than 200, no alpha phase Al 2 O 3 is deposited, but only gamma phase or mixtures of gamma and theta phase, and in some cases a powdery layer is obtained with bad or no adherence, even if the ratio of H 2 O / AlCl 3 is in the range from 0.5 to 2.5.
• both reaction gas conditions must be met at the same time, i.e. the ratio of H 2 O / AlCl 3 from 0.5 to 2.5 and the ratio of H 2 / AlCl 3 from 200 to 3000, to allow for the deposition and controlled growth of a ⁇ -Al2O3 coating layer of good crystallinity, high hardness and density at the comparably low deposition temperature of the present invention.
• the process of the present invention allows for the deposition of the ⁇ -Al 2 O 3 coating layer even on top of substrates and/or further layers underneath, which are instable or less stable or are susceptible to embrittlement or any other disadvantageous changes at higher temperatures.
• the process of the present invention provides a sufficiently high deposition rate to make the production of several micrometre thick wear resistant layers economically feasible.
• the process of the present invention is suitable for commonly used industrial CVD equipment designs, and the deposition of the ⁇ -Al2O3 coating layer can be carried out in the same deposition run as further coating layers of a multi-layer coating structure, which is cost and time effective in the mass production of coated cutting tools. No separate manufacturing steps, such as intermediate PVD depositions, are required.
• the ⁇ -Al 2 O 3 coating layers produced by the process of the present invention provide good wear resistance and mechanical properties, as they exhibit high crystallinity, high hardness and density. In comparison to conventional processes for the deposition of ⁇ -Al 2 O 3 coating layers at high temperature, the process of the present invention runs at significantly lower temperatures leading to lower energy consumption and potentially lower production costs.
• the deposition of the alpha phase Al 2 O 3 coating layer is carried out at a total pressure in the range from 3 to 50 mbar, or from 3 to 30 mbar, or from 3 to 20 mbar, or from 3 to 15 mbar. If the total pressure is too low, the deposition rate may decrease.
• the generation of process vacuum while evacuating corrosive precursors and by-products may require exceedingly high technical and financial resources. If the total pressure is too high, no pure or almost pure alpha phase is obtained. Furthermore, the higher reactive gas partial pressures may lead to undesired gas phase reactions and may not result in compact layers.
• the ratio of H 2 O / AlCl 3 in the range from 0.7 to 2.0, or in the range from 0.8 to 1.5. It was observed that ratios of H 2 O / AlCl 3 in this range may improve the homogeneity of coating thickness distribution within the reactor.
• the ratio of H2 / AICI3 is > 500, or > 800, or > 1200, or > 1400, or > 1600.
• the process gas composition in the deposition of the alpha phase AI2O3 coating layer, consists of AICI3, H 2 O and H 2 , or the process gas composition additionally contains a sulfur source, preferably H2S, in an amount of up to 2 vol.-% of the process gas.
• the process gas composition, as introduced into the CVD reactor contains no additional HCI.
• the invention includes embodiments, wherein in the deposition of the alpha phase AI2O3 coating layer the process gas composition, as introduced into the CVD reactor, additionally contains HCI in an amount of not more than 10 times the volume amount of AICI3 in the process gas.
• the deposition process includes the deposition of further layers underneath the alpha phase AI2O3 coating layer, i.e. the deposition of a multi-layer structure.
• the further layers preferably include one or more Ti and/or Ti+AI compound layers being selected from carbides, nitrides, oxides, carbonitrides and oxicarbonitrides.
• the further layers, including the further Ti and/or Ti+AI compound layers may be suitable to improve adhesion of the coating and/or promote a preferred crystallographic orientation or texture of the 0AI2O3 coating layer and/or of further layers and/or contribute and improve the wear resistance of the entire coating structure.
• the layers deposited underneath the alpha phase AI2O3 coating layer include a layer sequence of a titanium nitride (TiN) lower layer, followed by one or more subsequent layers selected from titanium carbonitride (TiCN), titanium aluminium carbonitride (TiAICN) and titanium aluminium nitride (TiAIN), optionally followed by a bonding layer immediately underneath the alpha phase AI2O3 coating layer according to the invention, which bonding layer preferably includes titanium carbonitride (TiCN) or titanium aluminium carbonitride (TiAICN).
• TiN titanium nitride
• TiAICN titanium aluminium carbonitride
• TiAIN titanium aluminium nitride
• the bonding layer includes an oxidized state of the TiCN or TiAICN near the transition region to or immediately underneath the alpha phase AI2O3 coating layer, which either depositing a TiCNO or TiAICNO sub-layer or by carrying out an oxidation step to the TiCN or TiAICN of the bonding layer prior to the deposition of the alpha phase AI2O3 coating layer.
• the provision of the oxidized state may further improve the adhesion of the alpha phase AI2O3 coating layer.
• the deposition process includes an oxidation step prior to the deposition of the alpha phase AI2O3 coating layer.
• the oxidation step is applied to a Ti and/or Ti+AI compound layer deposited underneath the AI2O3 coating layer. It was found that the application of an oxidation step may be suitable to improve the adhesion of the subsequently deposited alpha phase AI2O3 coating layer.
• the oxidation step is carried out in the presence of H 2 O as oxidizing agent for a time of about 2 to 20 min, preferably, about 3 to 15 min.
• the temperature of the oxidation step is about the same as or plus/minus 50°C of the temperature applied for the deposition of the alpha phase AI2O3 coating layer.
• the present invention also includes the surface-coated cutting tool for chip-forming metal machining consisting of a substrate of cemented carbide, cermet or cubic boron nitride based ceramic material and a single-layered or multi-layered wear resistant hard coating, wherein the layers of the hard coating comprising at least one alpha (a) phase AI2O3 coating layer being deposited by the chemical vapour deposition (CVD) process as defined herein.
• CVD chemical vapour deposition
• the inventive cutting tool of the present invention distinguishes from cutting tools having at least one conventionally produced alpha (a) phase AI2O3 coating layer at high temperature in that the substrate and/or further layers underneath the AI2O3 coating layer have not undergone structural changes and deteriorations due to a high temperature deposition or treatment step. Therefore, the inventive cutting tool may, due to the inventive deposition process, exhibit improved mechanical properties and wear resistance. Furthermore, since the process of the present invention is carried out at significantly lower temperatures, the cutting tool of the present invention can be produced at lower costs and less consumption of resources than comparable cutting tools having at least one a-ALOs coating layer conventionally produced at high temperature.
• the at least one alpha phase AI 2 C>3 coating layer deposited by the inventive process has a Vickers hardness HV0.01 of > 2000 HV, or > 2300 HV.
• the wear resistant hard coating of the surface-coated cutting tool further comprises one or more Ti and/or Ti+AI compound layers underneath the alpha phase AI2O3 coating layer, the Ti and/or Ti+AI compound layers being selected from carbides, nitrides, oxides, carbonitrides and oxicarbonitrides.
• X-ray diffraction measurements were performed in a XRD3003 PTS diffractometer of GE Sensing and Inspection Technologies using CuKa-radiation.
• the X-ray tube was run in point focus at 40 kV and 40 mA.
• a parallel beam optic using a polycapillary collimating lens with a measuring aperture of fixed size was used on the primary side whereby the irradiated area of the sample was defined in such manner that a spillover of the X-ray beam over the coated face of the sample was avoided.
• a parallel plate collimator with a divergence of 0.4° and a 25 pm thick NiK0 filter was used.
• the microhardness was measured with the Vickers hardness test.
• a diamond pyramid (with interfacial angle of 136°, Vickers pyramid) was pressed into the layer with a defined test load.
• DIN EN ISO 4516 a smooth calotte grind was used for the test. A smooth surface is necessary to minimize surface effects on measurement.
• the indenter is placed in the outer area of the coating to ensure that the indention depth is lower than 1/10 of the layer thickness.
• the diagonals of the indenter’s remaining impression were measured optically.
• An MHT-10 (Anton Paar) installed on a light microscope was used to perform the indentation and measurements. The hardness was calculated by software using the average of the two diagonal lengths according to following equation (F is the test load and d is the average of diagonal lengths):
• Calotte grinding was used to assess coating thickness and adhesion.
• the insert was placed on an inclined magnetic holder of the ball cratering set-up.
• a spherical calotte was ground in the coating and substrate material by a rotating 30 mm steel ball wetted with a drop of 3 pm water-based diamond suspension (Struers, DP-Lubricant Green) and driven by a driving shaft at > 500 rpm.
• the grinding process was stopped when the calotte diameter in the substrate material reached approx. 600-1100 pm.
• the thickness measurements taking into account the geometry of the calottes were done by a dedicated software using light optical microscopy (LOM).
• LOM light optical microscopy
• Cutting tests Coated cutting tools were tested herein in a milling operation in 42CrMo4 steel having a tensile strength of 785 N/mm 2 using the following cutting data: Cutting speed v c : 180 m/min Cutting feed, f: 0.2 mm/revolution Depth of cut, a p : 3 mm Width of cut, a e : 98 mm Radial overhang, ue: 5 mm No. of teeth: 1 Insert geometry: SPHW120408 (no cutting fluid) CVD coatings The CVD coatings of the examples given herein below were done on WC-Co-based cemented carbide cutting tool substrates.
• Equipment “A” is a lab-scale horizontal flow hot wall CVD reactor made of Inconel and having an inner diameter of 79 mm, a horizontal length of 800 mm and an inner volume of approximately 6 litres.
• the substrate temperature is controlled by a type K thermocouple. Reaction gases are introduced by separate gas inlets into the reaction zone.
• Equipment A was used for the preparation of CVD Al 2 O 3 coatings of some of the inventive working examples and comparative examples described below.
• H 2 O evaporator of this equipment water was evaporated by bubbling H2 carrier gas through liquid water at controlled pressure and temperature.
• the reaction gas was fed into the reactor through a central gas inlet ipe and introduced into the reaction zone through openings distributed along the inlet pipeo provide an essentially radial gas flow over the substrate bodies.
• Equipment B was used forhe preparation of CVD Al 2 O 3 coatings of some of the inventive working examples and omparative examples described below.
• H 2 O evaporator of this equipment water was vaporated by spraying liquid water into a H 2 carrier gas stream at 100 °C under reduced ressure.
• the evaporated amount was controlled by a liquid mass flow controller calibratedo units of g/h from which the gas volume flow in sccm is calculated using the molar mass of H 2 O and ideal gas volume at normal conditions 0°C and 1.013 bar(abs.).
• olume ratios of the process gas composition as introduced into the reactor refer to the forementioned gas flows in sccm. not otherwise indicated, in the examples herein, the reactor was filled with inserts up to bout its full capacity, whereby sample inserts to be investigated were distributed at various ifferent positions within the reactor, and the remaining sample positions within the reactor were filled with “scrap” inserts to simulate, as close as possible, full scale deposition onditions and volume usage within the respective reactor.
• inventive examples 11 to 116 and comparative examples C1 to C13 and CWG1 are indicated in table 2.
• an oxidation step was applied to the TiCN layer prior to the deposition of the AI2O3.
• Oxidations in equipment A were carried out at fixed H 2 O flows of 12 seem and in equipment B at fixed H 2 O flows of 1333 seem for a time and at a temperature as indicated in table 2 under “Ox-Time” and “Ox- Temp”, respectively.
• the AI2O3 layer was deposited applying the the water-gas shift reaction from H2 + CO2 --> H2O + CO.
• the layer sequences, process parameters and reaction gases introduced into the reactor for comparative example CWG1 are included in tables 1 and 2, whereas layer sequences, process parameters and reaction gases for comparative example CWG2 (prepared in equipment B) are indicated in table 3.
• Table 4 shows the measured parameters of the AI2O3 layer of the inventive examples (11 to 116) and the comparative examples (C1 to C13, CWG1 and CWG2).
• Table 5 shows cutting test results of inventive and comparative examples. For each example, four cutting edges were used in the milling test. The milling operation was interrupted after milling paths of 800 mm, 1600 mm, 3200 mm, 4800 mm and 5600 mm to evaluate the wear marks, which were flank wear width (Vb), maximum flank wear width (Vb max ) and number of comb cracks (comb cracks). Each cutting edge was used until a maximum flank wear width Vbmax of > 0.30 mm was reached. Table 5 lists the wear data for the cutting edge of each variant, which showed the poorest wear resistance, i.e. with the shortest milling length to reach Vb max* 0.30 mm, and had the largest wear width in case several edges exceeded 0.3 mm at the same interval of measurement.
• Vb flank wear width
• Vb max maximum flank wear width
• comb cracks number of comb cracks

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• 2022
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