EP1360343A1 - Device for ceramic-type coating of a substrate - Google Patents
Device for ceramic-type coating of a substrateInfo
- Publication number
- EP1360343A1 EP1360343A1 EP02701200A EP02701200A EP1360343A1 EP 1360343 A1 EP1360343 A1 EP 1360343A1 EP 02701200 A EP02701200 A EP 02701200A EP 02701200 A EP02701200 A EP 02701200A EP 1360343 A1 EP1360343 A1 EP 1360343A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- substrate
- coating
- layer
- ceramic
- source
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
- 239000000758 substrate Substances 0.000 title claims abstract description 50
- 238000000576 coating method Methods 0.000 title claims abstract description 28
- 239000011248 coating agent Substances 0.000 title claims abstract description 27
- 239000000463 material Substances 0.000 claims abstract description 36
- 239000002245 particle Substances 0.000 claims description 11
- 238000009792 diffusion process Methods 0.000 claims description 9
- 238000001816 cooling Methods 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 5
- 230000015572 biosynthetic process Effects 0.000 claims description 4
- 230000005684 electric field Effects 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 238000005524 ceramic coating Methods 0.000 abstract 1
- 239000010410 layer Substances 0.000 description 56
- 239000007789 gas Substances 0.000 description 10
- 150000002500 ions Chemical class 0.000 description 9
- 239000000919 ceramic Substances 0.000 description 8
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 6
- 235000019589 hardness Nutrition 0.000 description 6
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 5
- 239000002318 adhesion promoter Substances 0.000 description 5
- 229910044991 metal oxide Inorganic materials 0.000 description 5
- 150000004706 metal oxides Chemical class 0.000 description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- 230000005284 excitation Effects 0.000 description 4
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 4
- 238000004544 sputter deposition Methods 0.000 description 4
- 239000010936 titanium Substances 0.000 description 4
- 229910052719 titanium Inorganic materials 0.000 description 4
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- 229910003481 amorphous carbon Inorganic materials 0.000 description 3
- 229910021417 amorphous silicon Inorganic materials 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 230000005855 radiation Effects 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- 229910052581 Si3N4 Inorganic materials 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 150000004767 nitrides Chemical class 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000002347 wear-protection layer Substances 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910019923 CrOx Inorganic materials 0.000 description 1
- 229910004205 SiNX Inorganic materials 0.000 description 1
- 229910010037 TiAlN Inorganic materials 0.000 description 1
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 1
- 239000012790 adhesive layer Substances 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- 229910000423 chromium oxide Inorganic materials 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000002103 nanocoating Substances 0.000 description 1
- 239000002114 nanocomposite Substances 0.000 description 1
- 239000002105 nanoparticle Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000004886 process control Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 150000003377 silicon compounds Chemical class 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
- -1 transition metal nitride Chemical class 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J37/00—Discharge tubes with provision for introducing objects or material to be exposed to the discharge, e.g. for the purpose of examination or processing thereof
- H01J37/32—Gas-filled discharge tubes
- H01J37/32009—Arrangements for generation of plasma specially adapted for examination or treatment of objects, e.g. plasma sources
- H01J37/32192—Microwave generated discharge
-
- 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
-
- 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/3471—Introduction of auxiliary energy into the plasma
-
- 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/35—Sputtering by application of a magnetic field, e.g. magnetron sputtering
- C23C14/354—Introduction of auxiliary energy into the plasma
-
- 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/35—Sputtering by application of a magnetic field, e.g. magnetron sputtering
- C23C14/354—Introduction of auxiliary energy into the plasma
- C23C14/357—Microwaves, e.g. electron cyclotron resonance enhanced sputtering
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J2237/00—Discharge tubes exposing object to beam, e.g. for analysis treatment, etching, imaging
- H01J2237/32—Processing objects by plasma generation
- H01J2237/33—Processing objects by plasma generation characterised by the type of processing
- H01J2237/339—Synthesising components
Definitions
- the invention relates to a device for ceramic-like coating of a substrate according to the preamble of claim 1.
- ceramic-like layers with excellent mechanical, electrical, optical and chemical properties can be produced.
- Appropriate methods have long been used for the coating of tools to extend the service life or to increase the life of mechanically stressed components or machine elements, such as. B. shafts, bearing components, pistons, gears or the like, and used for the decorative design of surfaces.
- metallic compounds such as. B. high-melting oxides, nitrides and carbides of aluminum, titanium, zirconium, chromium or silicon are used.
- the titanium-based coating systems such as TiN, TiCN or TiAlN coating systems, are mainly used as wear protection on cutting tools.
- Superhard materials are also known which represent a combination of a nanocrystalline (nc), hard transition metal nitride Me n N with amorphous (a) Si 3 N 4 .
- nc-MeN / a-SI 3 N 4 composite materials for example, the hardness increases sharply with decreasing crystallite size below about 4 to 5 nanometers and approximates that of the diaantes at 2 to 3 nanometers.
- the multi-phase structure of the coating leads, for example, to layers with a hardness> 2500 HV with comparatively low brittleness.
- Corresponding layers are produced in particular by plasma-activated chemical vapor deposition (PACVD) processes at temperatures of approximately 500 to 600 ° C.
- PSVD plasma-activated chemical vapor deposition
- the comparatively high temperature of the substrate and consequently the coating enable diffusion of correspondingly amorphously deposited coating components and thus the formation of nanocrystallites in an amorphous matrix.
- the object of the invention is to propose a device for ceramic-like coating of a substrate, means for applying a material, in particular by means of a plasma, to a surface of the substrate being provided which, compared to the prior art, also include a ceramic-like coating of comparatively temperature-sensitive Allows substrates.
- This object is achieved on the basis of a device of the type mentioned in the introduction by the characterizing features of claim 1.
- a device is characterized in that an energy source that is different from a material source of the material provided for coating is provided for locally defined energy input into the material located in front of and / or on the surface.
- this enables, in particular, a nanostructured ceramic, high-quality layer system to be implemented within a layer, the nanostructured metal crystallites with a crystal size of up to approximately 100 nm, for example consisting of MeO, MeN or MeC, in a further structure which is amorphous, crystalline or metallic and e.g. consists of amorphous silicon compounds or the like.
- the nanostructured layer contains at least one crystalline hard material phase.
- the layer hardness is significantly increased, for example hardnesses of over 4000 HV can be achieved when TiO crystallites are embedded.
- the brittleness of the ceramic layers is reduced, in particular by the nanostructuring.
- the entire layer system can be one or more layers, chemically and partially graded and / or ungraded.
- a run-in layer can be realized by a carbon-containing cover layer.
- corresponding nanocomposites can advantageously be deposited, for example at substrate temperatures T ⁇ 400 ° C., preferably at temperatures T ⁇ 250 ° C., so that comparatively temperature-sensitive substrates can also be coated.
- the supply of kinetic energy for increasing the surface mobility and thus for the diffusion of the deposited material components preferably takes place via an additional plasma excitation, so that compared to the prior art in particular much higher ion densities can be achieved, which is also due to a corresponding change in the color and the brightness of the Plasma is made clear.
- the plasma excitation or higher ion density and thus higher energy density the initially amorphously deposited particles on the substrate receive enough energy for diffusion to be able to form, for example, nanometer-sized TiO crystallites on the substrate.
- Further plasma sources are also conceivable for this purpose, which in particular at lower pressure, e.g. be operated in a fine vacuum.
- the high ion energy or ion density preferably prevents the build-up of microcrystallites which have already formed, and at the same time favors the advantageous nanocrystalline growth.
- This can include various three-dimensional components can be coated accordingly.
- the energy is introduced into the material located on the surface, so that the initially amorphously deposited particles on the substrate again have enough energy available for diffusion, in turn, for example, cubic, hexagonal, metallic or on the substrate to be able to form other nanometer-sized crystallites.
- a microwave unit is advantageously provided for the energy input, so that, for example, the ion density of the material can be increased by additional ionization during sputtering.
- advantageous ionization densities of approximately 10 10 to 10 13 ions per cm 3 can be achieved, so that the material which is initially amorphously deposited on the substrate has sufficient energy available for diffusion.
- microwave radiation for so-called electron cyclotron resonance excitation (ECR) is preferably provided.
- an ion source unit is provided for the energy input, so that in turn advantageous plasma excitation or an increase in the ionization density is realized, thereby permitting the diffusion of the initially amorphously deposited material on the substrate.
- a DC or RF excited hollow cathode unit or the like can also be provided for the energy input according to the invention.
- Common to these units is the locally defined energy input according to the invention, preferably into the material located in front of the surface of the substrate.
- UV unit or the like is advantageously provided. These units are preferably used to introduce additional kinetic energy for the diffusion of the particles initially deposited amorphously on the substrate into the material on the surface of the substrate.
- a cooling device for cooling the substrate is provided. This advantageously ensures that the substrate temperature is reduced as far as possible. In particular, this measure makes it possible to coat more temperature-sensitive substrates.
- the cooling device is preferably implemented by means of a metallic or other highly thermally conductive substrate carrier.
- an advantageous coolant can also flow through the cooling device, so that a further reduction in the substrate temperature can be achieved.
- a voltage source for generating an electrical field is provided between the material source and the substrate. This ensures that, for example, an advantageous potential profile is generated between the material source and the substrate and that charging of the substrate, in particular by means of an RF substrate or bias voltage, is prevented.
- FIG. 1 shows a schematic structure of a device according to the invention
- FIG. 2 shows a schematic 3D representation of a section of a coating produced according to the invention
- 3 shows a schematic representation of a multilayer layer produced according to the invention
- FIG. 4 shows a schematic illustration of a further multilayer layer produced according to the invention
- FIG. 5 shows a schematic representation of a third multilayer layer produced according to the invention.
- FIG. 1 schematically shows a section of a coating chamber 1 during a coating process.
- a layer 3 is applied to a substrate 2 at a chamber pressure of approximately 10 "3 to 10 " 2 mbar.
- a first material 5 is atomized by a sputter source 4.
- a second material 7 is sputtered with the material 5 simultaneously or with a time delay from a sputter source 6.
- the energy input locally defined according to the invention into the two materials 5, 7 takes place by means of the plasma 8 shown schematically in FIG is provided as plasma gas.
- the plasma 8 is generated, for example, with a microwave radiation of the frequency 2.45 GHz with a layer-dependent power of preferably 1 kW.
- the microwave radiation is coupled in, for example, via a rod antenna (not shown in more detail).
- the sputtering source 4 can comprise a metal, a metal oxide target or a mixed target, wherein the metal can be, for example, titanium, chromium, copper, zirconium or the like.
- a gas supply 9 and 10 two different reaction gases can be metered in as required during the coating.
- oxygen can be metered into the coating chamber 1 by the gas supply 9 in order to produce oxidic ceramic layers. If a sputter source 4 with a metal oxide target is used, oxidic ceramic layers can also be produced without an oxygen supply by means of the gas supply 9.
- the sputter source 6 can comprise, for example, a silicon and / or carbon target, so that the sputter source 6 enables the formation of the amorphous matrix, such as silicon nitride or the like, in particular with nitrogen supplied by the gas supply 10.
- the gas supply 10 can also supply other gases, so that other matrices can also be produced if required.
- the reaction of the sputtering components mostly takes place on the substrate.
- additional energy is introduced into the atomized or deposited particles by the plasma 8 by means of the ECR microwave source without the substrate being heated to any significant extent.
- the substrate temperature can be kept comparatively low. Due to the energy introduced by the ECR microwave source, particles of nanometer size, for example titanium oxide particles, are formed in the coating 3 on the substrate by diffusion of the initially amorphously deposited particles. Consequently, the high temperatures of the substrate which lead to the formation of the nanostructured coating according to the prior art are not required, so that temperature-sensitive substrates can also be coated according to the invention.
- the coating is scalable, without, for example, the substrate having to be used as an electrode for compacting the applied coating.
- a special embodiment of the invention comprises a voltage source which, for example, provides an RF bias voltage on the substrate. In this way, primarily only charging of the substrate 2 is prevented, so that in particular the deposition of the materials 5, 7 does not change disadvantageously even over a comparatively longer coating period.
- the nanocrystallites 11 can be TiO, TiN, ZrN, ZrO, TiC, SiC, carbon or corresponding nanocrystallites 11 and various mixtures thereof with grain sizes in the range from 5 to 20 nm.
- the proportion of the surface volume in the total volume is very high and the interfaces between the nanocrystallites 11 and the amorphous matrix 12 are comparatively sharp.
- FIG. 3 schematically shows a layer structure of a coating 3 produced according to the invention, the nanoscale multilayer layer 3 being applied to the substrate 2.
- layer 3 comprises an adhesion promoter 13, which can optionally be applied and, for example, consists of a metallic layer, such as an approximately 300 nm thick titanium adhesive layer.
- a layer according to FIG. 2, for example an amorphous silicon nitride layer 12 with nanoscale titanium oxide and / or carbon particles 11, can be applied as the next layer 14.
- a cover layer 15 can optionally be applied, which preferably consists of amorphous carbon ,
- three-dimensional components such as drills or the like can also be coated with a corresponding nanoscale multilayer layer 3.
- the three-layer structure ensures, in particular by means of the adhesion promoter 13, good adhesion of the superhard ceramic metal oxide layer 14 to the substrate 2.
- the cover layer 15 ensures, for example with a similar hardness, a high coefficient of friction, so that in particular the frictional properties of the nanostructured layer in a run-in phase of mechanically stressed components or machine elements, such as. B-. Shafts, bearing components, pistons, gears or the like, the two friction partners or over the entire life of the two friction partners is improved.
- a layer structure according to FIG. 4 can be provided.
- the adhesion promoter 13 and a layer 14, which for example comprises an amorphous carbon network 12 with nanoscale titanium oxide particles 11, are optionally provided.
- an alternative layer structure can in turn be provided with an optional adhesion promoter 13 and an amorphous carbon layer 16 and a layer 14 with an amorphous silicon nitride layer 12 and nanoscale titanium oxide particles 11.
- nanostructured metal oxide layers 14 can also be applied to diamond-like carbon layers 16, for example in order to improve the running-in behavior of wear protection layers with a lower coefficient of friction.
- nanostructured metal oxide layers 14 with or without inclusions or Upper cover layer 15 can be used as a wear protection layer for the highest load collectives with novel multifunctional properties. For example, due to their non-stick and advantageous rubbing properties, these can be used as dry lubricant layers for machining stainless steel, aluminum or the like.
- self-cleaning properties of titanium oxide layers can be combined with anti-scratch properties.
- Oxidic ceramic layers are generally advantageous because they have a high chemical inertness, are optically transparent and have a lower coefficient of friction than, for example, nitride layers.
- ceramic oxide layers have so far been used only to a limited extent in production, primarily due to the more sensitive, reactive process control than with nitridic layer systems.
- the stoichiometric oxygen content can be set here, for example, by regulating optical emission.
- oxidic ceramics are characterized by good rubbing properties and high chemical resistance with high layer hardness.
- nanocrystalline powder material can generally be supplied to an ion source or synthesized by means of this.
Abstract
Disclosed is a device for ceramic-type coating of a substrate (2), provided with means for applying a material (5, 7), especially by means of plasma (8), to the surface of the substrate (2), enabling ceramic coating (3) of relatively temperature-sensitive substrates (2) in comparison with prior art. This is achieved by providing an energy source, which is different from the source (4,6) of the material (5,7) which is provided for coating, for locally defined provision of energy to the material (3,5, 7, 8) disposed in front of/or on the surface.
Description
"Vorrichtung zur keramikartigen Beschichtung eines Substrates""Device for Ceramic-Like Coating of a Substrate"
Die Erfindung betrifft eine Vorrichtung zur keramikartigen Beschichtung eines Substrates nach dem Oberbegriff des Anspruchs 1.The invention relates to a device for ceramic-like coating of a substrate according to the preamble of claim 1.
Stand der TechnikState of the art
Vor allem mit Plasmaverfahren können keramikartige Schichten mit hervorragenden mechanischen, elektrischen, optischen und chemischen Eigenschaften hergestellt werden. Entsprechende Verfahren werden schon länger für die Beschichtung von Werkzeugen zur Standzeitverlängerung oder zur Erhöhung der Lebensdauer von mechanisch belasteten Bauteilen oder Maschinenelernenten, wie z. B. Wellen, Lagerkomponenten, Kolben, Zahnräder oder dergleichen, sowie zur dekorativen Gestaltung von Oberflächen eingesetzt. Hierbei kommen zahlreiche metallische Verbindungen, wie z. B. hochschmelzende Oxide, Nitride und Karbide von Aluminium, Titan, Zirkonium, Chrom oder Silizium zum Einsatz. Insbesondere die titanbasierten SchichtSysteme, wie TiN-, TiCN- oder TiAlN-SchichtSysteme, werden vor allem als Verschleißschutz auf Zerspanwerkzeuge eingesetzt.
Es sind auch superharte Materialien bekannt, die eine Kombination eines nanokristallinen (nc) , harten Übergangsmetallnitrids MenN mit amorphem (a) Si3N4 darstellen. In solchen nc-MeN/a-SI3N4-Kompositmaterialien nimmt beispielsweise die Härte mit abnehmender Kristallitgröße unterhalb von etwa 4 bis 5 Nanometer stark zu und nährt sich bei 2 bis 3 Nanometer an derjenigen des Dia antes an. Insbesondere die mehrphasige Struktur der Beschichtung führt beispielsweise zu Schichten mit Härten > 2500 HV bei vergleichsweise geringer Sprödheit .Especially with plasma processes, ceramic-like layers with excellent mechanical, electrical, optical and chemical properties can be produced. Appropriate methods have long been used for the coating of tools to extend the service life or to increase the life of mechanically stressed components or machine elements, such as. B. shafts, bearing components, pistons, gears or the like, and used for the decorative design of surfaces. Here come numerous metallic compounds, such as. B. high-melting oxides, nitrides and carbides of aluminum, titanium, zirconium, chromium or silicon are used. In particular, the titanium-based coating systems, such as TiN, TiCN or TiAlN coating systems, are mainly used as wear protection on cutting tools. Superhard materials are also known which represent a combination of a nanocrystalline (nc), hard transition metal nitride Me n N with amorphous (a) Si 3 N 4 . In such nc-MeN / a-SI 3 N 4 composite materials, for example, the hardness increases sharply with decreasing crystallite size below about 4 to 5 nanometers and approximates that of the diaantes at 2 to 3 nanometers. In particular, the multi-phase structure of the coating leads, for example, to layers with a hardness> 2500 HV with comparatively low brittleness.
Entsprechende Schichten werden insbesondere durch Plasma- activated Chemical Vapor Deposition (PACVD) Verfahren bei Temperaturen von ca. 500 bis 600°C hergestellt. So wird insbesondere durch die vergleichsweise hohe Temperatur des Substrats und folglich der Beschichtung eine Diffusion entsprechend amorph abgeschiedener Beschichtungsbestandteile und somit die Bildung von Nanokristalliten in einer amorphen Matrix ermöglicht.Corresponding layers are produced in particular by plasma-activated chemical vapor deposition (PACVD) processes at temperatures of approximately 500 to 600 ° C. In particular, the comparatively high temperature of the substrate and consequently the coating enable diffusion of correspondingly amorphously deposited coating components and thus the formation of nanocrystallites in an amorphous matrix.
Nachteilig hierbei ist jedoch, dass vergleichsweise temperaturempfindliche Werkstoffe, wie beispielsweise zahlreiche Kunst- oder Verbundstoffe, zu Gefügeveränderung neigende Legierungen oder dergleichen, nicht beschichtet werden können.The disadvantage here, however, is that comparatively temperature-sensitive materials, such as, for example, numerous plastics or composites, alloys or the like which tend to change the structure, cannot be coated.
Vorteile der ErfindungAdvantages of the invention
Aufgabe der Erfindung ist es demgegenüber, eine Vorrichtung zur keramikartigen Beschichtung eines Substrates, wobei Mittel zum Aufbringen eines Werkstoffes, insbesondere mittels eines Plasmas, auf einer Oberfläche des Substrates vorgesehen sind, vorzuschlagen, die gegenüber dem Stand der Technik auch eine keramikartige Beschichtung von vergleichsweise temperaturempfindlichen Substraten ermöglicht.
Diese Aufgabe wird ausgehend von einer Vorrichtung der einleitend genannten Art durch die kennzeichnenden Merkmale des Anspruchs 1 gelöst .In contrast, the object of the invention is to propose a device for ceramic-like coating of a substrate, means for applying a material, in particular by means of a plasma, to a surface of the substrate being provided which, compared to the prior art, also include a ceramic-like coating of comparatively temperature-sensitive Allows substrates. This object is achieved on the basis of a device of the type mentioned in the introduction by the characterizing features of claim 1.
Durch die in den Unteransprüchen genannten Maßnahmen sind vorteilhafte Ausführungen und Weiterbildungen der Erfindung möglich.Advantageous designs and developments of the invention are possible through the measures mentioned in the subclaims.
Dementsprechend zeichnet sich eine erfindungsgemäße Vorrichtung dadurch aus, dass eine von einer Werkstoffquelle des zur Beschichtung vorgesehenen Werkstoffes verschiedene Energiequelle zum örtlich definierten Energieeintrag in den vor und/oder auf der Oberfläche befindlichen Werkstoff vorgesehen ist .Accordingly, a device according to the invention is characterized in that an energy source that is different from a material source of the material provided for coating is provided for locally defined energy input into the material located in front of and / or on the surface.
Erfindungsgemäß ist hierdurch, insbesondere ein innerhalb einer Lage, nanostrukturiertes keramisches, qualitativ hochwertiges Schichtsystem realisierbar, das nanostrukturierte Metallkristallite mit einer Kristallgröße bis etwa 100 nm, beispielsweise bestehend aus MeO, MeN oder MeC, in einem weiteren Gefüge, das amorph, kristallin oder metallisch ist und z.B. aus amorphen Silizium-Verbindungen oder dergleichen besteht, umfasst.According to the invention, this enables, in particular, a nanostructured ceramic, high-quality layer system to be implemented within a layer, the nanostructured metal crystallites with a crystal size of up to approximately 100 nm, for example consisting of MeO, MeN or MeC, in a further structure which is amorphous, crystalline or metallic and e.g. consists of amorphous silicon compounds or the like.
Die nanostrukturierte Lage enthält mindestens eine kristalline Hartstoffphase. Hierdurch wird insbesondere die Schichthärte wesentlich erhöht, beispielsweise können Härten von über 4000 HV bei Einlagerung von TiO-Kristalliten erreicht werden. Gleichzeitig wird die Sprδdheit der keramischen Schichten, insbesondere durch die Nanostrukturierung, abgebaut. Das gesamte Schichtsystem kann ein- oder mehrlagig, chemisch und anteilig gradiert und/oder ungradiert sein. Weiterhin kann durch eine kohlenstoffhaltige Deckschicht eine EinlaufSchicht realisiert werden.
Vorteilhafterweise können darüber hinaus entsprechende Nanokomposite, beispielsweise bei Substrattemperaturen T < 400°C, vorzugsweise bei Temperaturen T < 250°C, , abgeschieden werden, so dass auch vergleichsweise temperaturempfindliche Substrate beschichtbar sind.The nanostructured layer contains at least one crystalline hard material phase. As a result, in particular the layer hardness is significantly increased, for example hardnesses of over 4000 HV can be achieved when TiO crystallites are embedded. At the same time, the brittleness of the ceramic layers is reduced, in particular by the nanostructuring. The entire layer system can be one or more layers, chemically and partially graded and / or ungraded. Furthermore, a run-in layer can be realized by a carbon-containing cover layer. In addition, corresponding nanocomposites can advantageously be deposited, for example at substrate temperatures T <400 ° C., preferably at temperatures T <250 ° C., so that comparatively temperature-sensitive substrates can also be coated.
Erfindungsgemäß erfolgt die Zufuhr kinetischer Energie zur Erhöhung der Oberflächenbeweglichkeit und somit zur Diffusion der abgeschiedenen Werkstoffbestandteile vorzugsweise über eine zusätzliche Plasmaanregung, so dass gegenüber dem Stand der Technik insbesondere wesentlich höhere Ionendichten erzielt werden können, was auch aufgrund einer entsprechenden Veränderung der Farbe sowie der Helligkeit des Plasmas verdeutlicht wird. Mittels der Plasmaanregung bzw. höheren Ionendichte und somit höheren Energiedichte erhalten die zunächst amorph abgeschiedenen Teilchen auf dem Substrat genügend Energie zur Diffusion, um auf dem Substrat beispielsweise TiO-Kristallite in Nanometergröße bilden zu können. Auch sind hierfür weitere Plasmaquellen denkbar, die insbesondere bei niedrigerem Druck, z.B. im Feinvakuum, betrieben werden.According to the invention, the supply of kinetic energy for increasing the surface mobility and thus for the diffusion of the deposited material components preferably takes place via an additional plasma excitation, so that compared to the prior art in particular much higher ion densities can be achieved, which is also due to a corresponding change in the color and the brightness of the Plasma is made clear. By means of the plasma excitation or higher ion density and thus higher energy density, the initially amorphously deposited particles on the substrate receive enough energy for diffusion to be able to form, for example, nanometer-sized TiO crystallites on the substrate. Further plasma sources are also conceivable for this purpose, which in particular at lower pressure, e.g. be operated in a fine vacuum.
Vorzugsweise wird durch die hohe Ionenenergie bzw. Ionendichte insbesondere mittels einer Zerschlagung von bereits entstandenen Mikrokristalliten deren Aufbau verhindert und gleichzeitig das vorteilhafte nanokristalline Wachstum begünstigt. Hierdurch können u.a. auch verschiedenste dreidimensionale Bauteile entsprechend beschichtet werden.The high ion energy or ion density preferably prevents the build-up of microcrystallites which have already formed, and at the same time favors the advantageous nanocrystalline growth. This can include various three-dimensional components can be coated accordingly.
In einer besonderen Ausführungsform der Erfindung erfolgt der Energieeintrag in den auf der Oberfläche befindenden Werkstoff, so dass wiederum die zunächst amorph abgeschiedenen Teilchen auf dem Substrat genügend Energie zur Diffusion zur Verfügung haben, um wiederum auf dem Substrat beispielsweise kubische, hexagonale, metallische oder
sonstige Kristallite in Nanomentergröße bilden zu können.In a special embodiment of the invention, the energy is introduced into the material located on the surface, so that the initially amorphously deposited particles on the substrate again have enough energy available for diffusion, in turn, for example, cubic, hexagonal, metallic or on the substrate to be able to form other nanometer-sized crystallites.
In vorteilhafter Weise ist eine Mikrowelleneinheit für den Energieeintrag vorgesehen, so dass beispielsweise beim Sputtern die Ionendichte des Werkstoffs durch Zusatzionisation erhöht werden kann. Hierdurch können vorteilhafte Ionisationsdichten von ungefähr 1010 bis 1013 Ionen pro cm3 realisiert werden, so dass der zunächst amorph abgeschiedene Werkstoff auf dem Substrat genügend Energie zur Diffusion zur Verfügung hat. Vorzugsweise wird hierfür Mikrowellenstrahlung zur sogenannten Elektron Cyklotron Resonanzanregung (ECR) vorgesehen.A microwave unit is advantageously provided for the energy input, so that, for example, the ion density of the material can be increased by additional ionization during sputtering. In this way, advantageous ionization densities of approximately 10 10 to 10 13 ions per cm 3 can be achieved, so that the material which is initially amorphously deposited on the substrate has sufficient energy available for diffusion. For this purpose, microwave radiation for so-called electron cyclotron resonance excitation (ECR) is preferably provided.
In einer besonderen Ausführungsform der Erfindung ist eine Ionenquelleneinheit für den Energieeintrag vorgesehen, so dass wiederum eine vorteilhafte Plasmaanregung bzw. Erhöhung der Ionisationsdichte realisiert wird, wodurch die Diffusion des zunächst amorph abgeschiedenen Werkstoffes auf dem Substrat ermöglicht wird.In a special embodiment of the invention, an ion source unit is provided for the energy input, so that in turn advantageous plasma excitation or an increase in the ionization density is realized, thereby permitting the diffusion of the initially amorphously deposited material on the substrate.
Alternativ hierzu kann beispielsweise auch eine DC- oder RF- angeregte Hohlkathodeneinheit oder dergleichen für den erfindungsgemäßen Energieeintrag vorgesehen werden. Diesen Einheiten gemeinsam ist der erfindungsgemäße örtlich definierte Energieeintrag vorzugsweise in den vor der Oberfläche des Substrates befindenden Werkstoff.As an alternative to this, a DC or RF excited hollow cathode unit or the like can also be provided for the energy input according to the invention. Common to these units is the locally defined energy input according to the invention, preferably into the material located in front of the surface of the substrate.
Weiterhin ist in vorteilhafter Weise eine UV-Einheit oder dergleichen vorgesehen. Mit diesen Einheiten erfolgt vorzugsweise der Eintrag zusätzlicher kinetischer Energie zur Diffusion der zunächst auf dem Substrat amorph abgeschiedenen Teilchen in den auf der Oberfläche des Substrats befindenden Werkstoff.Furthermore, a UV unit or the like is advantageously provided. These units are preferably used to introduce additional kinetic energy for the diffusion of the particles initially deposited amorphously on the substrate into the material on the surface of the substrate.
In einer besonderen Weiterbildung der Erfindung ist eine Kühlvorrichtung zur Kühlung des Substrates vorgesehen.
Hierdurch wird in vorteilhafter Weise gewährleistet, dass eine möglichst weitestgehende Absenkung der Substrattemperatur realisiert wird. Insbesondere mittels dieser Maßnahme sind temperaturempfindlichere Substrate beschichtbar.In a special development of the invention, a cooling device for cooling the substrate is provided. This advantageously ensures that the substrate temperature is reduced as far as possible. In particular, this measure makes it possible to coat more temperature-sensitive substrates.
Vorzugsweise wird die Kühlvorrichtung mittels einem metallischen oder sonstigen gut wärmeleitenden Substrattrager realisiert . Darüber hinaus kann die Kühlvorrichtung auch von einem vorteilhaften Kühlmittel durchströmt werden, so dass eine weitere Absenkung der Substrattemperatur erreicht werden kann.The cooling device is preferably implemented by means of a metallic or other highly thermally conductive substrate carrier. In addition, an advantageous coolant can also flow through the cooling device, so that a further reduction in the substrate temperature can be achieved.
In einer besonderen Ausführungsform der Erfindung ist eine Spannungsquelle zur Erzeugung eines elektrischen Feldes zwischen der Werkstoffquelle und dem Substrat vorgesehen. Hierdurch wird gewährleistet, dass beispielsweise ein vorteilhafter Potentialverlauf zwischen der Werkstoffquelle und dem Substrat erzeugt wird und dass eine Aufladung des Substrates, insbesondere mittels einer RF-Substrat- oder Biasspannung, verhindert wird.In a special embodiment of the invention, a voltage source for generating an electrical field is provided between the material source and the substrate. This ensures that, for example, an advantageous potential profile is generated between the material source and the substrate and that charging of the substrate, in particular by means of an RF substrate or bias voltage, is prevented.
Ausführungsbeispielembodiment
Ein Ausführungsbeispiel der Erfindung ist in der Zeichnung dargestellt und wird anhand der Figuren nachfolgend näher erläutert •An embodiment of the invention is shown in the drawing and is explained in more detail below with reference to the figures.
Im Einzelnen zeigenShow in detail
Fig. 1 einen schematischen Aufbau einer erfindungsgemäßen Vorrichtung,1 shows a schematic structure of a device according to the invention,
Fig. 2 eine schematische 3D-Darstellung eines Ausschnitts einer erfindungsgemäß hergestellten Beschichtung,
Fig. 3 eine schematische Darstellung eines erfindungsgemäß hergestellten mehrlagigen Schicht,2 shows a schematic 3D representation of a section of a coating produced according to the invention, 3 shows a schematic representation of a multilayer layer produced according to the invention,
Fig. 4 eine schematische Darstellung eines weiteren erfindungsgemäß hergestellten mehrlagigen Schicht und4 shows a schematic illustration of a further multilayer layer produced according to the invention
Fig. 5 eine schematische Darstellung eines dritten erfindungsgemäß hergestellten mehrlagigen Schicht.5 shows a schematic representation of a third multilayer layer produced according to the invention.
In Fig. 1 ist schematisch ein Ausschnitt einer Beschichtungskammer 1 während einem Beschichtungsvorgang dargestellt. Hierbei wird auf ein Substrat 2 eine Schicht 3 bei einem Kammerdruck von ungefähr 10"3 bis 10"2 mbar aufgebracht . So wird von einer Sputterquelle 4 ein erster Werkstoff 5 zerstäubt . Entsprechend wird von einer Sputterquelle 6 ein zweiter Werkstoff 7 gleichzeitig oder zeitversetzt mit dem Werkstoffs 5 zerstäubt. Der erfindungsgemäß örtlich definierte Energieeintrag in die beiden Werkstoffe 5, 7 erfolgt mittels dem in Fig. 1 schematisch dargestellten Plasma 8. Die Plasmaerzeugung bzw. auch Plasmaanregung erfolgt beispielsweise mittels einer nicht näher dargestellten ECR-Mikrowellenquelle, wobei beispielsweise Argon, Helium, Sauerstoff oder dergleichen als Plasmagas vorgesehen ist. Das Plasma 8 wird beispielsweise mit einer Mikrowellenstrahlung der Frequenz 2,45 GHz mit einer schichtdicken abhängigen Leistung von vorzugsweise 1 kW erzeugt. Die Mikrowellenstrahlung wird beispielsweise über eine nicht näher dargestellte Stabantenne eingekoppelt .1 schematically shows a section of a coating chamber 1 during a coating process. In this case, a layer 3 is applied to a substrate 2 at a chamber pressure of approximately 10 "3 to 10 " 2 mbar. A first material 5 is atomized by a sputter source 4. Correspondingly, a second material 7 is sputtered with the material 5 simultaneously or with a time delay from a sputter source 6. The energy input locally defined according to the invention into the two materials 5, 7 takes place by means of the plasma 8 shown schematically in FIG is provided as plasma gas. The plasma 8 is generated, for example, with a microwave radiation of the frequency 2.45 GHz with a layer-dependent power of preferably 1 kW. The microwave radiation is coupled in, for example, via a rod antenna (not shown in more detail).
Beispielsweise kann die Sputterquelle 4 ein Metall, ein Metalloxidtarget oder ein Mischtarget umfassen, wobei das Metall beispielsweise Titan, Chrom, Kupfer, Zirkonium oder dergleichen sein kann.
Mittels einer Gaszufuhr 9 und 10 können während der Beschichtung je nach Bedarf zwei verschiedene Reaktionsgase zudosiert werden. Beispielsweise kann durch die Gaszufuhr 9 Sauerstoff in die Beschichtungskammer 1 zudosiert werden, um oxidische Keramikschichten herzustellen. Wird gegebenenfalls eine Sputterquelle 4 mit einem Metalloxidtarget verwendet, so können oxidische Keramikschichten auch ohne eine Sauerstoffzufuhr mittels der Gaszufuhr 9 hergestellt werden.For example, the sputtering source 4 can comprise a metal, a metal oxide target or a mixed target, wherein the metal can be, for example, titanium, chromium, copper, zirconium or the like. By means of a gas supply 9 and 10, two different reaction gases can be metered in as required during the coating. For example, oxygen can be metered into the coating chamber 1 by the gas supply 9 in order to produce oxidic ceramic layers. If a sputter source 4 with a metal oxide target is used, oxidic ceramic layers can also be produced without an oxygen supply by means of the gas supply 9.
Die Sputterquelle 6 kann beispielsweise ein Silizum- und/oder Kohlenstofftarget umfassen, so dass die Sputterquelle 6 insbesondere mit durch die Gaszufuhr 10 zugeführtem Stickstoff die Bildung der amorphen Matrix, wie Siliziumnitrid oder dergleichen, ermöglicht. Alternativ kann die Gaszufuhr 10 auch andere Gase zuführen, so dass bei Bedarf auch andere Matrices hergestellt werden können.The sputter source 6 can comprise, for example, a silicon and / or carbon target, so that the sputter source 6 enables the formation of the amorphous matrix, such as silicon nitride or the like, in particular with nitrogen supplied by the gas supply 10. Alternatively, the gas supply 10 can also supply other gases, so that other matrices can also be produced if required.
Erfahrungsgemäß erfolgt die Reaktion der Sputterbestandteile größtenteils erst auf dem Substrat. Mittels der ECR-Mikro- wellenquelle wird erfindungsgemäß durch das Plasma 8 zusätzliche Energie in die zerstäubten bzw. abgeschiedenen Partikel eingetragen, ohne dass das Substrat nennenswert erwärmt wird. Hierdurch kann die ' Substrattemperatur vergleichsweise klein gehalten werden. Aufgrund der durch die ECR-Mikrowellenquelle eingetragene Energie erfolgt die Bildung von Partikel in Nanometergrδße, beispielsweise von Titanoxidpartikeln, in der Beschichtung 3 auf dem Substrat durch Diffusion der zunächst amorph abgeschiedenen Teilchen. Folglich werden die hohen Temperaturen des Substrats , die zur Bildung der nanostrukturierten Beschichtung gemäß dem Stand der Technik führen, nicht benötigt, so dass erfindungsgemäß auch temperaturempfindliche Substrate beschichtet werden können.Experience has shown that the reaction of the sputtering components mostly takes place on the substrate. According to the invention, additional energy is introduced into the atomized or deposited particles by the plasma 8 by means of the ECR microwave source without the substrate being heated to any significant extent. As a result, the substrate temperature can be kept comparatively low. Due to the energy introduced by the ECR microwave source, particles of nanometer size, for example titanium oxide particles, are formed in the coating 3 on the substrate by diffusion of the initially amorphously deposited particles. Consequently, the high temperatures of the substrate which lead to the formation of the nanostructured coating according to the prior art are not required, so that temperature-sensitive substrates can also be coated according to the invention.
Erfindungsgemäß" ist die Beschichtung beliebig skalierbar,
ohne dass beispielsweise das Substrat als Elektrode zur Verdichtung der aufgebrachten Beschichtung verwendet werden muss. Eine besondere Ausführungsform der Erfindung umfasst jedoch eine Spannungsquelle, die beispielsweise eine RF- Biasspannung an dem Substrat vorsieht. Hierdurch wird vor allem lediglich eine Aufladung des Substrats 2 verhindert, so dass sich insbesondere die Abscheidung der Werkstoffe 5, 7 auch über einen vergleichsweise längeren Beschichtungszeitraum nicht nachteilig verändert .According to the invention "the coating is scalable, without, for example, the substrate having to be used as an electrode for compacting the applied coating. A special embodiment of the invention, however, comprises a voltage source which, for example, provides an RF bias voltage on the substrate. In this way, primarily only charging of the substrate 2 is prevented, so that in particular the deposition of the materials 5, 7 does not change disadvantageously even over a comparatively longer coating period.
Fig. 2 zeigt anschaulich einen schematischen dreidimensionalen Ausschnitt einer Schicht 3 mit mindestens zwei mehrkomponentigen Phasen 11, 12, wobei Nanokristallite 11 in ein amorphes, refraktäres Netzwerk 12 eingebunden sind. Beispielsweise kann es sich bei den Nanokristallite 11 um TiO- , TiN-, ZrN-, ZrO- , TiC- , SiC-, Kohlenstoff- oder entsprechende Nanokristallite 11 sowie verschiedenster Mischungen hiervon mit Korngrößen im Bereich von 5 bis 20 nm handeln. Erfindungsgemäß ist hierbei der Anteil des Oberflächenvolumens am Gesamtvolumen sehr hoch und die Grenzflächen zwischen den Nanokristalliten 11 und der amorphen Matrix 12 vergleichsweise scharf.2 clearly shows a schematic three-dimensional section of a layer 3 with at least two multi-component phases 11, 12, nanocrystallites 11 being integrated in an amorphous, refractory network 12. For example, the nanocrystallites 11 can be TiO, TiN, ZrN, ZrO, TiC, SiC, carbon or corresponding nanocrystallites 11 and various mixtures thereof with grain sizes in the range from 5 to 20 nm. According to the invention, the proportion of the surface volume in the total volume is very high and the interfaces between the nanocrystallites 11 and the amorphous matrix 12 are comparatively sharp.
In Fig. 3 ist schematisch ein Schichtaufbau einer erfindungsgemäß hergestellten Beschichtung 3 dargestellt, wobei auf dem Substrat 2 die nanoskalige Multilagenschicht 3 aufgebracht ist . Hierbei umfasst die Schicht 3 einen Haftvermittler 13, der optional aufgebracht werden kann und beispielsweise aus einer metallischen Schicht besteht, wie zum Beispiel aus einer ca. 300 nm dicken Titan-Haftschicht. Als nächste Schicht 14 kann beispielsweise eine Schicht gemäß der Fig. 2 aufgebracht werden, d. h. beispielsweise eine amorphe Siliziumnitridschicht 12 mit nanoskaligen Titanoxid- und/oder Kohlenstoff-Partikeln 11. Anschließend kann optional beispielsweise eine Deckschicht 15 aufgebracht werden, die vorzugsweise aus amorphem Kohlenstoff besteht.
Erfindungsgemäß können neben nahezu planaren Substraten auch dreidimensionale Bauteile wie Bohrer oder dergleichen mit einer entsprechenden nanoskaligen Multilagenschicht 3 beschichtet werden.FIG. 3 schematically shows a layer structure of a coating 3 produced according to the invention, the nanoscale multilayer layer 3 being applied to the substrate 2. In this case, layer 3 comprises an adhesion promoter 13, which can optionally be applied and, for example, consists of a metallic layer, such as an approximately 300 nm thick titanium adhesive layer. A layer according to FIG. 2, for example an amorphous silicon nitride layer 12 with nanoscale titanium oxide and / or carbon particles 11, can be applied as the next layer 14. Subsequently, for example, a cover layer 15 can optionally be applied, which preferably consists of amorphous carbon , In addition to almost planar substrates, three-dimensional components such as drills or the like can also be coated with a corresponding nanoscale multilayer layer 3.
Der dreilagige Schichtaufbau gewährleistet insbesondere mittels dem Haftvermittler 13 eine gute Haftung der superharten keramischen Metalloxidschicht 14 auf dem Substrat 2. Die Deckschicht 15 stellt beispielsweise bei ähnlicher Härte einen hohen Reibbeiwert sicher, so dass insbesondere die Reibeigenschaften der nanostrukturierten Schicht in einer Einlaufphase von mechanisch belasteten Bauteilen oder Maschinenelementen, wie z. B-. Wellen, Lagerkomponenten, Kolben, Zahnräder oder dergleichen, der beiden Reibpartner oder über die gesamte Lebensdauer der beiden Reibpartner verbessert wird.The three-layer structure ensures, in particular by means of the adhesion promoter 13, good adhesion of the superhard ceramic metal oxide layer 14 to the substrate 2. The cover layer 15 ensures, for example with a similar hardness, a high coefficient of friction, so that in particular the frictional properties of the nanostructured layer in a run-in phase of mechanically stressed components or machine elements, such as. B-. Shafts, bearing components, pistons, gears or the like, the two friction partners or over the entire life of the two friction partners is improved.
Alternativ zum Schichtaufbau gemäß der Fig. 3 kann ein Schichtaufbau gemäß der Fig. 4 vorgesehen werden. Hierbei ist entsprechend der Fig. 3 optional der Haftvermittler 13 und eine Schicht 14, die beispielsweise ein amorphes Kohlenstoffnetzwerk 12 mit nanoskaligen Titanoxidpartikeln 11 umfasst, vorgesehen.As an alternative to the layer structure according to FIG. 3, a layer structure according to FIG. 4 can be provided. 3, the adhesion promoter 13 and a layer 14, which for example comprises an amorphous carbon network 12 with nanoscale titanium oxide particles 11, are optionally provided.
Gemäß der Fig . 5 kann ein alternativer Schichtaufbau wiederum mit einem optional aufzubringenden Haftvermittler 13 und einer amorphen KohlenstoffSchicht 16 sowie einer Schicht 14 mit einer amorphen Siliziumnitridschicht 12 und nanoskaligen Titanoxidpartikeln 11 vorgesehen werden. So kann auch auf diamantartige Kohlenstoffschichten 16 nanostrukturierte Metalloxidschichten 14 aufgebracht werden, um beispielsweise das Einlaufverhalten von Verschleißschutzschichten mit einem niedrigeren Reibbeiwert zu verbessern.According to the Fig. 5, an alternative layer structure can in turn be provided with an optional adhesion promoter 13 and an amorphous carbon layer 16 and a layer 14 with an amorphous silicon nitride layer 12 and nanoscale titanium oxide particles 11. Thus, nanostructured metal oxide layers 14 can also be applied to diamond-like carbon layers 16, for example in order to improve the running-in behavior of wear protection layers with a lower coefficient of friction.
Grundsätzlich können insbesondere nanostrukturierte Metalloxidschichten 14 mit oder ohne Einlagerungen bzw.
oberer Deckschicht 15 als Verschleißschutzschicht für höchste Belastungskollektive mit neuartigen multifunktionalen Eigenschaften eingesetzt werden. So können diese zum Beispiel aufgrund ihrer Antihaft- und vorteilhaften Reibeigenschaften als Trockenschmierstoffschichten zur Bearbeitung von Edelstahl, Aluminium oder dergleichen verwendet werden. Darüber hinaus können auch die Selbstreinigungseigenschaften von Titanoxidschichten mit Antikratzeigenschaften kombiniert werde .In principle, nanostructured metal oxide layers 14 with or without inclusions or Upper cover layer 15 can be used as a wear protection layer for the highest load collectives with novel multifunctional properties. For example, due to their non-stick and advantageous rubbing properties, these can be used as dry lubricant layers for machining stainless steel, aluminum or the like. In addition, the self-cleaning properties of titanium oxide layers can be combined with anti-scratch properties.
Generell sind oxidische Keramikschichten vorteilhaft, da diese eine hohe chemische Inertheit aufweisen, optisch transparent sind und einen niedrigeren Reibkoeffizienten als zum Beispiel Nitridschichten besitzen. Jedoch werden bislang keramische Oxidschichten vor allem aufgrund der sensibleren, reaktiveren Prozessführung als bei nitridischen SchichtSystemen nur bedingt in der Fertigung eingesetzt. Die Einstellung des stöchio etrischen Sauerstoffgehaltes kann hierbei beispielsweise durch Regelung optischer Emission erfolgen. Gleichzeitig zeichnen sich oxidische Keramiken im Einsatz durch gute Reibeigenschaften und hohe chemische Beständigkeit mit hohen Schichthärten aus .Oxidic ceramic layers are generally advantageous because they have a high chemical inertness, are optically transparent and have a lower coefficient of friction than, for example, nitride layers. However, ceramic oxide layers have so far been used only to a limited extent in production, primarily due to the more sensitive, reactive process control than with nitridic layer systems. The stoichiometric oxygen content can be set here, for example, by regulating optical emission. At the same time, oxidic ceramics are characterized by good rubbing properties and high chemical resistance with high layer hardness.
Grundsätzlich können, entsprechend der Figur 1, auch beispielsweise Chromoxidnanopartikel in einer nicht näher dargestellten Hohlkatode hergestellt werden und unter Zugabe von Siliziumnitrid durch Siliziumsputtern sowie Zugabe von Stickstoffgas bei gleichzeitiger Zusatzionisierung durch eine erfindungsgemäße Mikrowellenwellenquelle oder Hochstromionenquelle, beispielsweise nc-CrOx/a-SiNx, hergestellt werden. Optional kann wiederum anschließend eine Kohlenstoffschicht 15 zur Verbesserung der Einlaufeigenschaften entsprechender Bauteile aufgebracht werden. Erfindungsgemäß kann generell nanokristallines Pulvermaterial einer Ionenquelle zugeführt oder mittels dieser synthetisiert werden.
Bezugszeichenliste :In principle, according to FIG. 1, it is also possible, for example, to produce chromium oxide nanoparticles in a hollow cathode (not shown in more detail) and to produce them with addition of silicon nitride by silicon sputtering and addition of nitrogen gas with simultaneous additional ionization by a microwave wave source or high-current ion source according to the invention, for example nc-CrOx / a-SiNx become. Optionally, a carbon layer 15 can subsequently be applied to improve the running-in properties of corresponding components. According to the invention, nanocrystalline powder material can generally be supplied to an ion source or synthesized by means of this. Reference symbol list:
1 Beschichtungskammer1 coating chamber
2 Substrat2 substrate
3 Schicht3 layer
4 Sputterquelle4 sputter source
5 Werkstoff5 material
6 Sputterquelle6 sputter source
7 Werkstoff7 material
8 Plasma8 plasma
9 Gaszufuhr9 gas supply
10 Gaszufuhr10 gas supply
11 Nanokristallite11 nanocrystallites
12 Netzwerk12 network
13 Haftvermittler13 adhesion promoter
14 Schicht14 layer
15 Deckschicht15 top layer
16 C-Schicht
16 C layer
Claims
1. Vorrichtung zur keramikartigen Beschichtung eines Substrates (2) , wobei Mittel zum Aufbringen eines Werkstoffes (5, 7) , insbesondere mittels eines Plasmas (8) , auf einer Oberfläche des Substrates (2) vorgesehen sind, dadurch gekennzeichnet, dass eine von einer Werkstoffquelle (4, 6) des zur Beschichtung vorgesehenen Werkstoffes (5, 7) verschiedenen Energiequelle zum örtlich definierten Energieeintrag in den vor und/oder auf der Oberfläche befindlichen Werkstoff (5, 7) vorgesehen ist.1. Device for ceramic-like coating of a substrate (2), wherein means for applying a material (5, 7), in particular by means of a plasma (8), are provided on a surface of the substrate (2), characterized in that one of a Material source (4, 6) of the material (5, 7) provided for coating different energy source for locally defined energy input into the material (5, 7) located in front of and / or on the surface is provided.
2. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass eine Mikrowelleneinheit für den Energieeintrag vorgesehen ist .2. Device according to claim 1, characterized in that a microwave unit is provided for the energy input.
3. Vorrichtung nach einem der vorgenannten Ansprüche, dadurch gekennzeichnet, dass eine Ionenquelleneinheit für den Energieeintrag vorgesehen ist.3. Device according to one of the preceding claims, characterized in that an ion source unit is provided for the energy input.
4. Vorrichtung nach einem der vorgenannten Ansprüche , dadurch gekennzeichnet, dass eine Hohlkathodeneinheit für den Energieeintrag vorgesehen ist.4. Device according to one of the preceding claims, characterized in that a hollow cathode unit is provided for the energy input.
5. Vorrichtung nach einem der vorgenannten Ansprüche, dadurch gekennzeichnet, dass eine UV-Einheit für den Energieeintrag vorgesehen ist .5. Device according to one of the preceding claims, characterized in that a UV unit is provided for the energy input.
6. Vorrichtung nach einem der vorgenannten Ansprüche , dadurch gekennzeichnet, dass eine Kühlvorrichtung zur Kühlung des Substrates (2) vorgesehen ist.6. Device according to one of the preceding claims, characterized in that a cooling device for cooling the substrate (2) is provided.
7. Vorrichtung nach einem der vorgenannten Ansprüche , dadurch gekennzeichnet, dass eine Spannungsquelle zur Erzeugung eines elektrischen Feldes zwischen der Werkstoffquelle und dem Substrat (2) vorgesehen ist. 7. Device according to one of the preceding claims, characterized in that a voltage source for generating an electric field between the material source and the substrate (2) is provided.
8. Verfahren zur Herstellung einer keramikartigen Beschichtung (3) eines Substrates (2), wobei ein Werkstoff8. A method for producing a ceramic-like coating (3) of a substrate (2), wherein a material
(5, 7) , insbesondere mittels eines Plasmas (8) , auf einer Oberfläche des Substrates (2) aufgebracht wird, dadurch gekennzeichnet, dass eine Vorrichtung nach einem der vorgenannten Ansprüche verwendet wird.(5, 7), in particular by means of a plasma (8), is applied to a surface of the substrate (2), characterized in that a device according to one of the preceding claims is used.
9. Verfahren nach Anspruch 8, dadurch gekennzeichnet, dass ein vom Werkstoffeintrag verschiedener, örtlich definierter Energieeintrag in den vor und/oder auf der Oberfläche befindlichen Werkstoff (5, 7) vorgesehen wird.9. The method according to claim 8, characterized in that a locally defined energy input different from the material input into the material located in front of and / or on the surface (5, 7) is provided.
10. Verfahren nach einem der vorgenannten Ansprüche, dadurch gekennzeichnet, dass eine Diffusion des auf der Oberfläche befindlichen Werkstoffs (5, 7) zur Bildung von Partikeln in Nanometergroße vorgesehen wird. 10. The method according to any one of the preceding claims, characterized in that a diffusion of the material located on the surface (5, 7) is provided for the formation of particles in nanometer size.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10104611A DE10104611A1 (en) | 2001-02-02 | 2001-02-02 | Device for the ceramic-like coating of a substrate |
DE10104611 | 2001-02-02 | ||
PCT/DE2002/000138 WO2002061165A1 (en) | 2001-02-02 | 2002-01-18 | Device for ceramic-type coating of a substrate |
Publications (1)
Publication Number | Publication Date |
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EP1360343A1 true EP1360343A1 (en) | 2003-11-12 |
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Application Number | Title | Priority Date | Filing Date |
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EP02701200A Ceased EP1360343A1 (en) | 2001-02-02 | 2002-01-18 | Device for ceramic-type coating of a substrate |
Country Status (5)
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US (1) | US20040144318A1 (en) |
EP (1) | EP1360343A1 (en) |
JP (1) | JP2004518026A (en) |
DE (1) | DE10104611A1 (en) |
WO (1) | WO2002061165A1 (en) |
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DE10141696A1 (en) | 2001-08-25 | 2003-03-13 | Bosch Gmbh Robert | Process for producing a nanostructured functional coating and coating that can be produced with it |
DE10256063A1 (en) | 2002-11-30 | 2004-06-17 | Mahle Gmbh | Process for coating piston rings for internal combustion engines |
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DE10305109B8 (en) * | 2003-02-07 | 2010-11-11 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Component with an electrically highly insulating layer and method for its production |
EP2348555B9 (en) | 2004-07-22 | 2013-05-08 | Nippon Telegraph And Telephone Corporation | Method for manufacturing a metal oxide thin film |
EP1643005A3 (en) * | 2004-09-01 | 2008-03-19 | EMPA Eidgenössische Materialprüfungs- und Forschungsanstalt | Depositing organic and/or inorganic nanolayers by plasma discharge |
DE102004052515B4 (en) * | 2004-10-22 | 2019-01-03 | Aesculap Ag | Surgical scissors and method for making a surgical scissors |
FR2886636B1 (en) * | 2005-06-02 | 2007-08-03 | Inst Francais Du Petrole | INORGANIC MATERIAL HAVING METALLIC NANOPARTICLES TRAPPED IN A MESOSTRUCTURED MATRIX |
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US20100021716A1 (en) * | 2007-06-19 | 2010-01-28 | Strock Christopher W | Thermal barrier system and bonding method |
FR2929264B1 (en) | 2008-03-31 | 2010-03-19 | Inst Francais Du Petrole | INORGANIC MATERIAL FORM OF SPHERICAL PARTICLES OF SPECIFIC SIZE AND HAVING METALLIC NANOPARTICLES TRAPPED IN A MESOSTRUCTURED MATRIX |
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- 2002-01-18 JP JP2002561097A patent/JP2004518026A/en active Pending
- 2002-01-18 US US10/470,400 patent/US20040144318A1/en not_active Abandoned
- 2002-01-18 EP EP02701200A patent/EP1360343A1/en not_active Ceased
- 2002-01-18 WO PCT/DE2002/000138 patent/WO2002061165A1/en active Application Filing
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Publication number | Publication date |
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WO2002061165A1 (en) | 2002-08-08 |
DE10104611A1 (en) | 2002-08-14 |
JP2004518026A (en) | 2004-06-17 |
US20040144318A1 (en) | 2004-07-29 |
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