DE102004052135A1 - Coated metal substrate especially a hard metal with a wear protection layer consisting of high purity Al2O3 nanocrystals and containing residual pressure stresses useful in tool production - Google Patents
Coated metal substrate especially a hard metal with a wear protection layer consisting of high purity Al2O3 nanocrystals and containing residual pressure stresses useful in tool production Download PDFInfo
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- DE102004052135A1 DE102004052135A1 DE102004052135A DE102004052135A DE102004052135A1 DE 102004052135 A1 DE102004052135 A1 DE 102004052135A1 DE 102004052135 A DE102004052135 A DE 102004052135A DE 102004052135 A DE102004052135 A DE 102004052135A DE 102004052135 A1 DE102004052135 A1 DE 102004052135A1
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- 239000000758 substrate Substances 0.000 title claims abstract description 45
- 229910052751 metal Inorganic materials 0.000 title claims abstract description 27
- 239000002184 metal Substances 0.000 title claims abstract description 27
- 239000002347 wear-protection layer Substances 0.000 title claims abstract description 16
- 238000004519 manufacturing process Methods 0.000 title claims description 11
- 229910052593 corundum Inorganic materials 0.000 title description 5
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 title description 2
- 229910001845 yogo sapphire Inorganic materials 0.000 title description 2
- 239000002159 nanocrystal Substances 0.000 title 1
- 239000010410 layer Substances 0.000 claims abstract description 69
- 238000000034 method Methods 0.000 claims abstract description 38
- 238000007704 wet chemistry method Methods 0.000 claims abstract description 6
- 238000003980 solgel method Methods 0.000 claims abstract description 3
- 238000000576 coating method Methods 0.000 claims description 19
- 239000011248 coating agent Substances 0.000 claims description 14
- 229910018072 Al 2 O 3 Inorganic materials 0.000 claims description 13
- 239000000463 material Substances 0.000 claims description 12
- 229910052574 oxide ceramic Inorganic materials 0.000 claims description 7
- 238000010304 firing Methods 0.000 claims description 6
- 239000011224 oxide ceramic Substances 0.000 claims description 6
- 230000004048 modification Effects 0.000 claims description 3
- 238000012986 modification Methods 0.000 claims description 3
- 229910000760 Hardened steel Inorganic materials 0.000 claims 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims 1
- 229910001315 Tool steel Inorganic materials 0.000 claims 1
- 238000009792 diffusion process Methods 0.000 claims 1
- 239000002923 metal particle Substances 0.000 claims 1
- 239000010936 titanium Substances 0.000 claims 1
- 229910052719 titanium Inorganic materials 0.000 claims 1
- 230000008021 deposition Effects 0.000 abstract description 2
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 230000001105 regulatory effect Effects 0.000 abstract 1
- 238000005229 chemical vapour deposition Methods 0.000 description 8
- 238000005240 physical vapour deposition Methods 0.000 description 8
- 239000000126 substance Substances 0.000 description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 238000005422 blasting Methods 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 229910052804 chromium Inorganic materials 0.000 description 3
- 239000011651 chromium Substances 0.000 description 3
- 239000010431 corundum Substances 0.000 description 3
- 239000002346 layers by function Substances 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 238000005507 spraying Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 239000000919 ceramic Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000003618 dip coating Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 239000002243 precursor Substances 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 238000007669 thermal treatment Methods 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001354 calcination Methods 0.000 description 1
- 239000012876 carrier material Substances 0.000 description 1
- 239000011195 cermet Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000007062 hydrolysis Effects 0.000 description 1
- 238000006460 hydrolysis reaction Methods 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 229910052594 sapphire Inorganic materials 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 229910003158 γ-Al2O3 Inorganic materials 0.000 description 1
Classifications
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- 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
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/02—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition
- C23C18/12—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition characterised by the deposition of inorganic material other than metallic material
- C23C18/1204—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition characterised by the deposition of inorganic material other than metallic material inorganic material, e.g. non-oxide and non-metallic such as sulfides, nitrides based compounds
- C23C18/1208—Oxides, e.g. ceramics
-
- 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
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/02—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition
- C23C18/12—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition characterised by the deposition of inorganic material other than metallic material
- C23C18/1229—Composition of the substrate
- C23C18/1241—Metallic substrates
-
- 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
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/02—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition
- C23C18/12—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition characterised by the deposition of inorganic material other than metallic material
- C23C18/125—Process of deposition of the inorganic material
- C23C18/1254—Sol or sol-gel processing
-
- 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
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/02—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition
- C23C18/12—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition characterised by the deposition of inorganic material other than metallic material
- C23C18/125—Process of deposition of the inorganic material
- C23C18/1283—Control of temperature, e.g. gradual temperature increase, modulation of temperature
-
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/322—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer only coatings of metal elements only
-
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
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- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/347—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with layers adapted for cutting tools or wear applications
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- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/36—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including layers graded in composition or physical properties
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- Chemical & Material Sciences (AREA)
- Inorganic Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
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- General Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Dispersion Chemistry (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
Description
Die Erfindung betrifft ein beschichtetes Metallsubstrat, insbesondere aus Hartmetall, mit einer Verschleißschutzschicht, welche Druckeigenspannungen aufweist und ein Verfahren zu seiner Herstellung.The The invention relates to a coated metal substrate, in particular made of carbide, with a wear protection layer, which compressive stresses and a method for its preparation.
Hartstoffschichten werden zur Verminderung des Verschleißes, insbesondere bei Werkzeugen zur Erhöhung der Standzeiten aufgebracht.Hard coatings are used to reduce wear, especially in tools to increase the service life applied.
Bei beschichteten Hartmetallsubstraten stehen durch unterschiedliche thermische Ausdehnungskoeffizienten von Verschleißschutzschicht- und Substratwerkstoff die Funktionsschichten häufig unter Zugeigenspannungen. Mit Zunahme der Zugspannungen vermindert sich die beabsichtigte Erhöhung der Verschleißbeständigkeit. Häufig führen zu hohe Zugeigenspannungen sogar zum Ablösen der Schichten vom Substrat. Dies trifft auch auf die Werkstoffpaarung Hartmetallsubstrat/oxidkeramische Schicht, insbesondere Al2O3-Schicht zu.In the case of coated cemented carbide substrates, the functional layers are often subject to tensile stresses due to different coefficients of thermal expansion of the wear protection layer material and the substrate material. As the tensile stresses increase, the intended increase in wear resistance decreases. Often too high tensile stresses even lead to the detachment of the layers from the substrate. This also applies to the material combination carbide substrate / oxide ceramic layer, in particular Al 2 O 3 layer.
Die Hartstoffschichten werden mit klassischen Verfahren des PVD (physical vapour deposition) bzw. des CVD (chemical vapour deposition) auf das Substrat aufgebracht. Dabei ist nachteilig, dass insbesondere bei der Kombination Hartmetallsubstrat/Al2O3-Schicht Zugeigenspannungen auftreten.The hard material layers are applied to the substrate by classical methods of PVD (physical vapor deposition) or CVD (chemical vapor deposition). It is disadvantageous that tensile stresses occur in particular in the combination of cemented carbide substrate / Al 2 O 3 layer.
Mit verschiedenen im Stand der Technik bekannten Verfahren wurde versucht, den Auswirkungen dieser Spannungen entgegenzuwirken.With various methods known in the art have been attempted to counteract the effects of these tensions.
Nach
Ferner
ist in
Die Druckspannungen werden bei diesen beiden Verfahren allerdings in einer Zwischenschicht und nicht in der eigentlichen Funktionsschicht, nämlich der Verschleißschutzschicht erzeugt.The Compressive stresses in these two methods, however, in an intermediate layer and not in the actual functional layer, namely the wear protection layer generated.
In
Die Hartstoffschichten zur Verminderung des Verschleißes, damit zur Erhöhung der Standzeiten insbesondere von Werkzeugen, werden mit klassischen Verfahren des PVD (physical vapour deposition) bzw. des CVD (chemical vapour deposition) auf das Substrat aufgebracht.The Hard material layers to reduce wear, so that to increase the life of tools, in particular, are classic Process of PVD (physical vapor deposition) or CVD (chemical vapor deposition) applied to the substrate.
Der Erfindung liegt die Aufgabe zugrunde, ein beschichtetes Metallsubstrat und ein Verfahren zu seiner Herstellung anzugeben, wobei die Schicht nach der Herstellung Druckspannungen und eine hohe Haftfestigkeit aufweist.Of the Invention is based on the object, a coated metal substrate and to provide a method for its production, wherein the layer according to the production has compressive stresses and a high adhesive strength.
Erfindungsgemäß wird die Aufgabe mit einem Substrat, welches die in Anspruch 1 angegebenen Merkmale und mit einem Verfahren, welches die in Anspruch 13 angegebenen Merkmale aufweist, gelöst.According to the invention Task with a substrate, which specified in claim 1 Features and with a method, which specified in claim 13 Has features solved.
Vorteilhafte Ausgestaltungen sind in den Unteransprüchen angegeben.advantageous Embodiments are specified in the subclaims.
Das erfindungsgemäße Verfahren verwendet zur Herstellung von oxidkeramischen Hartstoffschichten, vorzugsweise Al2O3, nasschemische Verfahrensschritte, beispielsweise die Sol-Gel-Technologie. Hier wird eine Vorstufe des Oxides (als Sol bzw. Gel) auf das Substrat durch Tauchen, Sprühen, oder andere geeignete Methoden aufgebracht. Anschließend wird das Gel durch einen zweistufigen Brennprozess in die gewünschte Hartstoffmodifikation umgewandelt.The process according to the invention uses wet-chemical process steps, for example the sol-gel technology, for the production of oxide-ceramic hard material layers, preferably Al 2 O 3 . Here, a precursor of the oxide (as sol or gel) is applied to the substrate by dipping, spraying, or other suitable methods. Subsequently, the gel is converted by a two-stage firing process into the desired hard material modification.
Es hat sich herausgestellt, dass die Schicht dann über eine gute Haftfestigkeit verfügt, wenn entweder das Substrat oder eine zusätzlich aufgebrachte Zwischenschicht über geeignete Elemente verfügt, die in die Verschleißschicht eindiffundieren. Gleichzeitig bewirken diese Elemente die Erzeugung von Druckeigenspannungen in der Funktionsschicht.It has been found that the layer then has a good adhesive strength when ent neither the substrate nor an additionally applied intermediate layer has suitable elements which diffuse into the wear layer. At the same time, these elements cause the generation of residual compressive stresses in the functional layer.
Über die Zeitdauer des Brennprozesses ist die absolute Höhe der Spannungen bis in einen bestimmten Bereich wählbar. Eine nachträgliche Behandlung der Schicht ist nicht notwendig. Auch ist nicht das Aufbringen einer Zwischenschicht mit Druckeigenspannungen notwendig.About the Duration of the burning process is the absolute height of the voltages up to one selectable range. An afterthought Treatment of the layer is not necessary. Also is not the application an intermediate layer with residual compressive stresses necessary.
Die Erfindung zeichnet sich durch eine Reihe von Vorteilen aus. Hierzu zählen insbesondere:
- 1. Wegen der Reinheit der Ausgangssubstanzen, die für das Verfahren eingesetzt werden, ist die Schicht chemisch an allen Stellen des Substrates hochrein an Al2O3, so dass eine hochqualitative Oxidkeramik entsteht.
- 2. Die Zusammensetzung der Schicht ist in Bereichen über den thermischen Prozess steuerbar (Verhältnis von α/γ-Al2O3), während dies beim CVD-Verfahren nur über chemische Beimengungen möglich ist.
- 3. Verfahren ist einfach und bedarf außer einem Schutzgas- bzw. Vakuumofen keiner teuren Anlagen. Es kann daher auch von kleineren Unternehmen zur Beschichtung verwendet werden.
- 4. Im Gegensatz zu CVD- und PVD-Verfahren können auch große Oberflächen beschichtet werden.
- 5. Während die Beschichtung von inneren Oberflächen für die klassischen Verfahren an das Verhältnis von Durchmesser zu Tiefe gebunden ist, sind infolge des nasschemischen Verfahrens auch kleinste Bohrungen mit großer Länger beschichtbar.
- 6. Die Schicht ist nicht texturiert und besitzt keine säulenartige Kristallstruktur
- 7. Mit dem Beschichtungszyklus können gleichzeitig Werkzeugstähle gehärtet werden. Ist das Sol auf bereits gehärteten und/oder angelassenen Stählen aufgebracht, wird eine partielle Wärmebehandlung der Schicht beispielsweise mit einem Laserstrahl notwendig.
- 1. Due to the purity of the starting materials used for the process, the layer is chemically highly pure Al 2 O 3 at all points of the substrate, so that a high-quality oxide ceramic is formed.
- 2. The composition of the layer is controllable in areas by the thermal process (ratio of α / γ-Al 2 O 3 ), while in the CVD process this is only possible via chemical admixtures.
- 3. The process is simple and requires no protective gas or vacuum furnace no expensive equipment. It can therefore also be used by smaller companies for coating.
- 4. In contrast to CVD and PVD processes, even large surfaces can be coated.
- 5. While the coating of inner surfaces for the classical methods is bound to the ratio of diameter to depth, even the smallest bores can be coated for a long time due to the wet-chemical process.
- 6. The layer is not textured and does not have a columnar crystal structure
- 7. The coating cycle can simultaneously harden tool steels. If the sol is applied to already hardened and / or tempered steels, a partial heat treatment of the layer, for example with a laser beam, becomes necessary.
Die Erfindung wird im Folgenden anhand eines Ausführungsbeispieles näher erläutert.The Invention will be explained in more detail below with reference to an embodiment.
In der zugehörigen Zeichnung zeigen:In the associated Show drawing:
Als Schichtwerkstoff wurde hier Al2O3 gewählt. Diese Substanz zeichnet sich durch hohe Härte und durch eine gegenüber Schichtwerkstoffen mit hohem metallischen Bindungsanteil relativ geringe Wärmeleitfähigkeit aus. Diese Eigenschaften sind sehr vorteilhaft für Beschichtungen, welche für die Hochgeschwindigkeitsbearbeitung bestimmt sind.As a coating material here Al 2 O 3 was chosen. This substance is characterized by high hardness and by a relatively low thermal conductivity compared to coating materials with a high metallic bond content. These properties are very beneficial for coatings designed for high speed machining.
Die Abscheidung der Substanz mit konventionellen Beschichtungsverfahren, CVD bzw. PVD, gestalten sich nicht einfach.The Deposition of the substance with conventional coating methods, CVD or PVD, are not easy.
Als Substrat wurde Hartmetall verwendet. Die Schichtdicke sollte im Bereich von 0,5 bis 6 μm liegen. Über den direkten Sol-Gel-Prozess sind diese Dicken nur über eine Mehrfachbeschichtung erreichbar.When Substrate was used carbide. The layer thickness should be in Range of 0.5 to 6 microns are. On the direct sol-gel process, these thicknesses are only a multiple coating reachable.
Bei der Sol-Gel-Technik wird aus Precursorlösungen das flüssige Sol, die Ausgangssubstanz, hergestellt. Über den Prozess der Hydrolyse entsteht ein Gel, das durch eine anschließende mehrstufige Wärmebehandlung in eine Oxidkeramik umgewandelt wird.at the sol-gel technique turns precursor solutions into the liquid sol, the starting substance, prepared. About the process of hydrolysis A gel is created by a subsequent multi-stage heat treatment is converted into an oxide ceramic.
Als Ausgangsstoff zur Schichtherstellung kann auch durch ein über den Sol-Gel-Prozess hergestelltes Produkt redispergiert werden.When Starting material for the layer production can also by a over the Sol-gel be prepared product redispersed.
Zur Herstellung einer oxidkeramischen Schicht ist es notwendig, das Substrat mit dem flüssigen Sol zu benetzen. Dieser Vorgang kann mit allen bekannten Verfahren zum Beschichten aus dem flüssigen Zustand erfolgen.to Production of an oxide ceramic layer, it is necessary that Substrate with the liquid Sol to moisten. This process can be done with all known methods for coating from the liquid Condition done.
Da das Hartmetallsubstrat nicht über die entsprechenden Elemente verfügt, mit denen sich die Druckspannungen einstellen lassen, müssen die Hartmetalloberflächen vor dem eigentlichen Beschichten mit einer zusätzlichen Schicht überzogen werden. Diese kann über den PVD-Prozess oder durch die Sol-Gel-Technik selbst aufgebracht werden.There the carbide substrate not over has the appropriate elements, with which the compressive stresses can be set, the carbide surfaces must be present the actual coating to be coated with an additional layer. This can over applied to the PVD process or by the sol-gel technique itself become.
Diese Elemente verteilen sich gradientenartig von der Grenzfläche Substrat/Schicht oder Zwischenschicht/Schicht in die Verschleißschutzschicht hinein (Elementegradient).These Elements are distributed in gradient form from the substrate / layer interface or intermediate layer / layer into the wear protection layer (elemental gradient).
Bevorzugt werden das Tauch (dip-coating) und das Sprüh-(spray-coating) Verfahren angewendet.Prefers are the dip-coating and the spray-coating process applied.
Mittels dip-coating können sehr homogene und reproduzierbare Dicken auch über große Flächen hinweg erzeugt werden. Beim spray-coating liegen die Vorteile im Beschichten von komplexen Teilegeometrien.through dip-coating can very homogeneous and reproducible thicknesses can be generated even over large areas. In spray-coating, the advantages are in the coating of complex Part geometries.
Nach dem Aufbringen der Ausgangssubstanz ist eine thermische Behandlung (Trockgnen, Kalzinieren, Brennen) notwendig. Diese dient zur Umwandlung der Ausgangssubstanz in die nanokristalline keramische Schicht sowie zur Anbindung an das Substrat.After applying the Ausgangsubs dance is a thermal treatment (dry, calcination, burning) necessary. This serves to convert the starting substance into the nanocrystalline ceramic layer and to connect to the substrate.
Über die
Randbedingungen des Gesamtprozesses kann maßgeblich Einfluss auf die Eigenschaften
der Schicht und des Schicht/Substrat-Verbundes genommen werden:
Bei
der Beschichtung von Hartmetallen wird über die Wahl der Elemente der
Zwischenschicht und über
die thermische Behandlung bereits während der Schichtherstellung
der Druckspannungszustand in der Schicht eingestellt. Eine nachträgliche Behandlung, beispielsweise
das Strahlen der Oberfläche,
ist nicht erforderlich.The boundary conditions of the overall process can significantly influence the properties of the layer and of the layer / substrate composite:
In the coating of hard metals, the choice of the elements of the intermediate layer and the thermal treatment already during the production of the layer set the compressive stress state in the layer. Subsequent treatment, such as blasting the surface, is not required.
Die Korundschicht (α-Al2O3) ist die Modifikation des Al2O3 mit der höchsten Härte. Jedoch besitzt Korund auch eine enorme Sprödigkeit. Durch Absenkung der eigentlichen Brenntemperatur kann vorteilhaft ein Gradient von α-/γ-Al2O3-in der Schicht eingestellt werden. Die Standzeit dieser Schichten erhöht sich wesentlich gegenüber Schichten mit einer reinen Korundphase. Dieser Phasengradient ist auch beeinflussbar durch die Schichtdicke bzw. über die Anzahl von Einzelbeschichtungen bei Mehrfachschichten.The corundum layer (α-Al 2 O 3 ) is the modification of the highest hardness Al 2 O 3 . However, corundum also has a tremendous brittleness. By lowering the actual firing temperature, it is advantageously possible to set a gradient of α- / γ-Al 2 O 3 in the layer. The service life of these layers increases significantly over layers with a pure corundum phase. This phase gradient can also be influenced by the layer thickness or by the number of individual coatings in the case of multiple layers.
Die keramischen Schichten sind meist nanokristallin und weisen keine Fasertexturen auf.The Ceramic layers are mostly nanocrystalline and have none Fiber textures.
Die Haftfestigkeit dieser Schichten ist hoch. Die Schichten sind reproduzierbar sicher herstellbar mit gleichen Eigenschaften an allen Schichtbereichen und im Vergleich an allen Teilen, die mit diesem Verfahren beschichtet werden.The Adhesive strength of these layers is high. The layers are reproducible safe to produce with the same properties on all layer areas and compared to all parts coated with this method become.
- 11
- Metallsubstratmetal substrate
- 22
- VerschleißschutzschichtWear protection layer
- 33
- ElementegradientElementegradient
- 44
- Zwischenschichtinterlayer
Claims (17)
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DE102004052135A DE102004052135A1 (en) | 2004-06-07 | 2004-10-27 | Coated metal substrate especially a hard metal with a wear protection layer consisting of high purity Al2O3 nanocrystals and containing residual pressure stresses useful in tool production |
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Cited By (2)
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EP1849554A1 (en) | 2006-04-29 | 2007-10-31 | DLR Deutsches Zentrum für Luft- und Raumfahrt e.V. | Hard metal wear protection layers for soft and non-annealable metals |
WO2008119600A1 (en) * | 2007-03-31 | 2008-10-09 | Schaeffler Kg | Coating of a component made of tempered steel and method for the application of said coating |
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US4614673A (en) * | 1985-06-21 | 1986-09-30 | The Boeing Company | Method for forming a ceramic coating |
DE2857147C2 (en) * | 1977-11-01 | 1987-03-26 | Atomic Energy Authority Uk | Process for coating a substrate with a refractory material |
JPH02166284A (en) * | 1988-12-21 | 1990-06-26 | Mitsui Toatsu Chem Inc | Manufacture of thin film containing alumina by sol-gel processing |
DE4116522C2 (en) * | 1990-05-23 | 1994-08-18 | Fraunhofer Ges Forschung | Process for the production of substrates provided with a porous alpha-Al¶2¶O¶3¶ layer, substrates obtained by the process and coating compositions for carrying out the process |
DE19835283A1 (en) * | 1998-08-05 | 2000-02-10 | Jack Schwarz | Wear resistant layer for tools and parts of machinery is a structure formed by small scale-like layer plates located side by side and on top of one another |
EP0815285B1 (en) * | 1995-03-22 | 2001-08-22 | Queen's University At Kingston | Method for producing thick ceramic films by a sol gel coating process |
DE10036262A1 (en) * | 2000-07-26 | 2002-02-21 | Daimler Chrysler Ag | Surface layer and method for producing a surface layer |
DE19634616C2 (en) * | 1995-08-30 | 2002-06-20 | Aisin Seiki | TiAl alloy part and process for its production |
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DE2857147C2 (en) * | 1977-11-01 | 1987-03-26 | Atomic Energy Authority Uk | Process for coating a substrate with a refractory material |
US4614673A (en) * | 1985-06-21 | 1986-09-30 | The Boeing Company | Method for forming a ceramic coating |
JPH02166284A (en) * | 1988-12-21 | 1990-06-26 | Mitsui Toatsu Chem Inc | Manufacture of thin film containing alumina by sol-gel processing |
DE4116522C2 (en) * | 1990-05-23 | 1994-08-18 | Fraunhofer Ges Forschung | Process for the production of substrates provided with a porous alpha-Al¶2¶O¶3¶ layer, substrates obtained by the process and coating compositions for carrying out the process |
EP0815285B1 (en) * | 1995-03-22 | 2001-08-22 | Queen's University At Kingston | Method for producing thick ceramic films by a sol gel coating process |
DE19634616C2 (en) * | 1995-08-30 | 2002-06-20 | Aisin Seiki | TiAl alloy part and process for its production |
DE19835283A1 (en) * | 1998-08-05 | 2000-02-10 | Jack Schwarz | Wear resistant layer for tools and parts of machinery is a structure formed by small scale-like layer plates located side by side and on top of one another |
DE10036262A1 (en) * | 2000-07-26 | 2002-02-21 | Daimler Chrysler Ag | Surface layer and method for producing a surface layer |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
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EP1849554A1 (en) | 2006-04-29 | 2007-10-31 | DLR Deutsches Zentrum für Luft- und Raumfahrt e.V. | Hard metal wear protection layers for soft and non-annealable metals |
WO2008119600A1 (en) * | 2007-03-31 | 2008-10-09 | Schaeffler Kg | Coating of a component made of tempered steel and method for the application of said coating |
EP2134885B1 (en) | 2007-03-31 | 2018-01-17 | Schaeffler Technologies AG & Co. KG | Coating of a component made of tempered steel and method for the application of said coating |
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