EP2728035B1 - Method for altering the surface properties of components - Google Patents
Method for altering the surface properties of components Download PDFInfo
- Publication number
- EP2728035B1 EP2728035B1 EP12190803.2A EP12190803A EP2728035B1 EP 2728035 B1 EP2728035 B1 EP 2728035B1 EP 12190803 A EP12190803 A EP 12190803A EP 2728035 B1 EP2728035 B1 EP 2728035B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- component
- temperature
- layer material
- layer
- nickel
- 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.)
- Active
Links
- 238000000034 method Methods 0.000 title claims description 29
- 239000000463 material Substances 0.000 claims description 45
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 42
- 230000008018 melting Effects 0.000 claims description 26
- 238000002844 melting Methods 0.000 claims description 26
- 239000011248 coating agent Substances 0.000 claims description 25
- 238000000576 coating method Methods 0.000 claims description 25
- 229910052759 nickel Inorganic materials 0.000 claims description 21
- 238000010438 heat treatment Methods 0.000 claims description 16
- 238000004519 manufacturing process Methods 0.000 claims description 15
- 229910045601 alloy Inorganic materials 0.000 claims description 10
- 239000000956 alloy Substances 0.000 claims description 10
- 238000009792 diffusion process Methods 0.000 claims description 8
- 239000000654 additive Substances 0.000 claims description 5
- 230000000996 additive effect Effects 0.000 claims description 5
- 238000005530 etching Methods 0.000 claims description 5
- 239000000126 substance Substances 0.000 claims description 5
- 239000007788 liquid Substances 0.000 claims description 4
- 238000007747 plating Methods 0.000 claims description 4
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 238000007654 immersion Methods 0.000 claims description 3
- 229910001092 metal group alloy Inorganic materials 0.000 claims description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical group [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 2
- 238000000137 annealing Methods 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- 239000000470 constituent Substances 0.000 claims description 2
- 238000009499 grossing Methods 0.000 claims description 2
- 239000000155 melt Substances 0.000 claims description 2
- 239000002184 metal Substances 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 claims description 2
- 239000000203 mixture Substances 0.000 claims description 2
- 229910052698 phosphorus Inorganic materials 0.000 claims description 2
- 239000011574 phosphorus Substances 0.000 claims description 2
- 239000010410 layer Substances 0.000 description 26
- 238000004026 adhesive bonding Methods 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 229910001026 inconel Inorganic materials 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 238000000110 selective laser sintering Methods 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/02—Pretreatment of the material to be coated
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/06—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/06—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases
- C23C10/08—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases only one element being diffused
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/06—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases
- C23C10/14—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases more than one element being diffused in one step
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/06—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases
- C23C10/16—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases more than one element being diffused in more than one step
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/18—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/18—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions
- C23C10/20—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions only one element being diffused
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/18—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions
- C23C10/20—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions only one element being diffused
- C23C10/22—Metal melt containing the element to be diffused
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/18—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions
- C23C10/26—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions more than one element being diffused
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/60—After-treatment
-
- 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
- C23C26/00—Coating not provided for in groups C23C2/00 - C23C24/00
- C23C26/02—Coating not provided for in groups C23C2/00 - C23C24/00 applying molten material to the substrate
Definitions
- the present invention relates to a method for changing the surface properties of components, which are built up incrementally in layers from a component material, for example, and a correspondingly produced component.
- Generative manufacturing processes in which a workpiece is built up from material increments in layers, are increasingly used in the prior art not only for the production of prototypes, but also for the production of components in small series.
- additive manufacturing processes are also suitable for the production of components for which other manufacturing processes cannot be carried out or can only be carried out with considerable difficulty.
- components manufactured by generative processes should also have a corresponding surface quality in the form of low roughness.
- due to the manufacturing process this is not the case immediately after the additive manufacturing, since the layer-by-layer design of the component on the surfaces results in steps and roughness according to the application of the layers.
- Examples of methods for changing the surface properties of components, in which the surface of the component is coated with a layer material and the coated component is subjected to a heat treatment, are from US 2011/117385 A1 , of the US 2007/0269676 A1 and the DE 10 2005 059299 A1 known. Methods involving deposition in an immersion bath are disclosed in US Pat EP 0 861 919 A2 and EP 1 930 477 A1 known.
- the desired smooth surface should be able to be produced in a simple and effective manner and in particular all surfaces of a component, that is to say surfaces of cavities and the like, should be machinable.
- the method should also be usable in the generative production of a component for smoothing the surfaces.
- a coating to the component to be machined, the coating containing components that melt at a lower temperature than the component material or form components with the component material that have a lower melting temperature than the component material and that this is coated accordingly
- Component is subjected to a heat treatment, so that a diffusion between the coating and the component is made possible.
- the combination of the applied coating with a lower melting point or components lowering the melting point on the one hand and the heat treatment on the other hand leads to diffusion processes between the coating and the component and / or to a melting of the coating and / or the original component surface, which leads to a leveling of the original rough surface of the component leads.
- the layer material can be selected from the same material as the component material, with at least one element additionally being added which lowers the melting point.
- the layer material can also be formed by only one component of the component material, namely preferably the main component of the component material.
- the main alloy component in the form of a technically pure metal could therefore be selected as the layer material.
- the layer can be formed from technically pure nickel as the main component of the nickel-based alloy.
- Technically pure nickel is understood here to mean a material which consists of almost 100% nickel, but which may have impurities to the extent of the technical circumstances.
- a nickel-based alloy alloyed with a melting point-lowering element can also be selected, wherein boron and / or phosphorus, for example, can be selected as the melting point-lowering elements.
- Nickel-based alloys are to be understood as those alloys which contain nickel as the constituent with the largest proportion and which in particular comprise alloy elements which enable high-temperature use.
- Inconel IN 718 can be named for this.
- the layer material is applied in liquid form, a chemical reaction in an immersion bath being selected, for example in order to apply a nickel layer.
- a chemical reaction in an immersion bath being selected, for example in order to apply a nickel layer.
- Such a method is usually known as chemical nickel plating.
- the heat treatment can be carried out at a temperature in the range of the melting temperature of the layer material and below the melting temperature of the component material.
- the temperature can be selected in a range which ranges from a temperature 30% below the melting temperature to a temperature of 5% above the melting temperature of the layer material.
- the heat treatment takes place in the area of the solution annealing temperature of the component material.
- the heat treatment of a layer of chemical nickel can also be carried out at a temperature just above the melting temperature, so that the coating and / or the original surface of the component melts.
- this can be done by a property-sensitive removal method, such as etching, so that the original surface can be exposed again.
- etching a property-sensitive removal method, such as etching
- a correspondingly manufactured component in particular an additive manufactured component, therefore has an edge zone which either comprises a coating or has at least formed a diffusion zone when the coating has been removed again.
- the coating of this component has the component material provided with a melting point lowering element or a coating of a component of the component material.
- the Figure 1 shows as an example the surface of a generatively produced component 1, which has a rough surface 2 after the incremental, layered structure.
- the component can have been formed by selective laser sintering, by stereolithographic methods, by layer-by-layer gluing or melting.
- the layer-by-layer production results in roughness on the surfaces.
- the method of the present invention used to process the surface can be any method of the present invention used to process the surface.
- the Figure 2 shows the sectional view of component 1 Figure 1 after applying a coating 3, for example by chemical nickel plating.
- a coating 3 for example by chemical nickel plating.
- the component 1 to be nickel-plated is immersed in a suitable liquid, so that nickel is deposited on the surface 2 of the component 1 by a corresponding chemical reaction of the components contained in the liquid.
- the layer thicknesses of the deposited chemical nickel can be varied in the range from 1 ⁇ m to 100 ⁇ m.
- the component is subjected to a heat treatment which makes it possible for ingredients to diffuse exchange between the layer 3 and the component 1.
- the heat treatment temperature can preferably also be selected such that the temperature is in the range of the melting temperature of the layer material, so that the rough surface 2 can be easily melted.
- the diffusion processes and / or the melting of the surface 2 lead to a change in the surface properties, as shown schematically in FIG Figure 3 is shown.
- the interface between the layer 3 and the component 1 now represents a smooth interface 4, since the diffusion processes and / or the melting result in a flattening of the above component areas.
- such a heat-treated layer 3 can, for example, be better machinable and / or solderable and / or chemically and / or mechanically removable.
- the component can be manufactured according to the state of manufacture Figure 3 Find use.
- Etching processes are suitable as property-sensitive removal processes, the etching agent being matched to the composition of the coating.
- the removal of material can be stopped after reaching the interface 4, so that the component 2 with the smoothed surface 5 is present.
- the correspondingly manufactured components are thus characterized either by the presence of a coating on the surface or, in the case of removal of the coating after the heat treatment has been carried out, by a diffusion zone in the edge zone of component 1 due to the diffusion with the previously existing coating.
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemically Coating (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Description
Die vorliegende Erfindung betrifft ein Verfahren zur Änderung der Oberflächeneigenschaften von Bauteilen, die beispielsweise inkrementell schichtweise aus einem Bauteilmaterial aufgebaut werden, sowie ein entsprechend hergestelltes Bauteil.The present invention relates to a method for changing the surface properties of components, which are built up incrementally in layers from a component material, for example, and a correspondingly produced component.
Generative Fertigungsverfahren, bei denen ein Werkstück aus Inkrementen aus Material schichtweise aufgebaut wird, werden im Stand der Technik zunehmend nicht nur für die Herstellung von Prototypen eingesetzt, sondern auch zur Herstellung von Bauteilen in Kleinserien. Darüber hinaus bieten sich derartige generative Herstellungsverfahren auch für die Herstellung von Bauteilen an, für die andere Herstellungsverfahren nicht oder nur mit erheblichen Schwierigkeiten durchgeführt werden können. Dies führt dazu, dass generativ hergestellte Bauteile auch eine entsprechende Oberflächengüte in Form einer geringen Rauheit aufweisen sollen. Dies ist jedoch aufgrund des Herstellungsverfahrens unmittelbar nach der generativen Herstellung nicht gegeben, da durch die schichtweise Ausbildung des Bauteils an den Oberflächen entsprechend der Aufbringung der Schichten Stufen und Rauigkeiten entstehen.Generative manufacturing processes, in which a workpiece is built up from material increments in layers, are increasingly used in the prior art not only for the production of prototypes, but also for the production of components in small series. In addition, such additive manufacturing processes are also suitable for the production of components for which other manufacturing processes cannot be carried out or can only be carried out with considerable difficulty. This means that components manufactured by generative processes should also have a corresponding surface quality in the form of low roughness. However, due to the manufacturing process, this is not the case immediately after the additive manufacturing, since the layer-by-layer design of the component on the surfaces results in steps and roughness according to the application of the layers.
Es ist deshalb bereits versucht worden, durch Aufbringung von Schichten, die die Unebenheiten ausfüllen sollen, die Oberflächengüte zu verbessern. Dies ist beispielsweise in der
Andere Verfahren zur Herstellung glatter Oberflächen, wie beispielsweise Schleifen, Strahlen, Polieren, Elektropolieren und dergleichen, sind aufwendig und können unter Umständen nur an bestimmten, frei zugänglichen Oberflächen durchgeführt werden.Other processes for the production of smooth surfaces, such as grinding, blasting, polishing, electropolishing and the like, are complex and, under certain circumstances, can only be carried out on certain, freely accessible surfaces.
Beispiele für Verfahren zur Änderung von Oberflächeneigenschaften von Bauteilen, bei denen jeweils die Oberfläche des Bauteils mit einem Schichtmaterial beschichtet wird und das beschichtete Bauteil einer Wärmebehandlung unterzogen wird, sind aus der
Es ist deshalb Aufgabe der vorliegenden Erfindung, ein Verfahren zur Änderung der Oberflächeneigenschaften von Bauteilen bereitzustellen, bei dem eine ausreichend gute Oberflächengüte erreicht wird, die ausreichend ist, um beispielsweise an derartig hergestellten Bauteilen optische Messverfahren oder eine zerstörungsfreie Bauteilprüfung, beispielsweise hinsichtlich Oberflächenrissprüfung, Wirbelstromprüfung usw., durchführen zu können.It is therefore an object of the present invention to provide a method for changing the surface properties of components, in which a sufficiently good surface quality is achieved which is sufficient, for example, to carry out optical measurement methods or non-destructive component testing on components manufactured in this way, for example with regard to surface crack testing, eddy current testing, etc.
Die gewünschte glatte Oberfläche soll jedoch in einfacher und effektiver Weise herstellbar sein und insbesondere sollen möglichst alle Flächen eines Bauteils, also auch Flächen von Hohlräumen und dergleichen bearbeitbar sein. Insbesondere soll das Verfahren auch bei der generativen Herstellung eines Bauteils für die Glättung der Oberflächen einsetzbar sein.However, the desired smooth surface should be able to be produced in a simple and effective manner and in particular all surfaces of a component, that is to say surfaces of cavities and the like, should be machinable. In particular, the method should also be usable in the generative production of a component for smoothing the surfaces.
Diese Aufgabe wird gelöst durch ein Verfahren mit den Merkmalen des Anspruchs 1.This object is achieved by a method with the features of
Vorteilhafte Ausgestaltungen sind Gegenstand der abhängigen Ansprüche.Advantageous refinements are the subject of the dependent claims.
Gemäß der Erfindung wird vorgeschlagen, auf dem zu bearbeitenden Bauteil eine Beschichtung aufzubringen, wobei die Beschichtung Bestandteile enthält, die bei einer niedrigeren Temperatur schmelzen als das Bauteilmaterial oder mit dem Bauteilmaterial Komponenten bilden, die eine niedrigere Schmelztemperatur als das Bauteilmaterial aufweisen und dass das entsprechend beschichtete Bauteil einer Wärmebehandlung unterzogen wird, sodass eine Diffusion zwischen der Beschichtung und dem Bauteil ermöglicht wird. Durch die Kombination der aufgebrachten Beschichtung mit niedrigerem Schmelzpunkt oder Schmelzpunkt erniedrigenden Bestandteilen einerseits sowie der Wärmebehandlung andererseits, kommt es zu Diffusionsvorgängen zwischen der Beschichtung und dem Bauteil und/oder zu einem Anschmelzen der Beschichtung und/oder der ursprünglichen Bauteiloberfäche, was zu einer Einebnung der ursprünglich rauen Oberfläche des Bauteils führt.According to the invention, it is proposed to apply a coating to the component to be machined, the coating containing components that melt at a lower temperature than the component material or form components with the component material that have a lower melting temperature than the component material and that this is coated accordingly Component is subjected to a heat treatment, so that a diffusion between the coating and the component is made possible. The combination of the applied coating with a lower melting point or components lowering the melting point on the one hand and the heat treatment on the other hand leads to diffusion processes between the coating and the component and / or to a melting of the coating and / or the original component surface, which leads to a leveling of the original rough surface of the component leads.
Das Schichtmaterial kann aus dem gleichen Material gewählt werden, wie das Bauteilmaterial, wobei zusätzlich mindestens ein Element beigefügt sein sollte, welches den Schmelzpunkt erniedrigt. Alternativ kann das Schichtmaterial auch durch lediglich einen Bestandteil des Bauteilmaterials gebildet werden, nämlich vorzugsweise die Hauptkomponente des Bauteilmaterials. Bei einer metallischen Legierung, die für das Bauteilmaterial verwendet wird, könnte also die Hauptlegierungskomponente in Form eines technisch reinen Metalls als Schichtmaterial gewählt werden.The layer material can be selected from the same material as the component material, with at least one element additionally being added which lowers the melting point. Alternatively, the layer material can also be formed by only one component of the component material, namely preferably the main component of the component material. In the case of a metallic alloy that is used for the component material, the main alloy component in the form of a technically pure metal could therefore be selected as the layer material.
Bei der Verwendung einer Nickelbasislegierung als Bauteilmaterial z.B. für die generative Herstellung von temperaturbelasteten Bauteilen von Strömungsmaschinen, wie beispielsweise Gasturbinen oder Flugtriebwerken, kann die Schicht aus technisch reinem Nickel als dem Hauptbestandteil der Nickelbasislegierung gebildet werden. Unter technisch reinem Nickel wird hierbei ein Material verstanden, welches zu nahezu 100 % aus Nickel besteht, jedoch im Umfang der technischen Gegebenheiten Verunreinigungen aufweisen kann.When using a nickel-based alloy as component material e.g. For the additive manufacturing of temperature-stressed components of turbomachines, such as gas turbines or aircraft engines, the layer can be formed from technically pure nickel as the main component of the nickel-based alloy. Technically pure nickel is understood here to mean a material which consists of almost 100% nickel, but which may have impurities to the extent of the technical circumstances.
Alternativ kann bei einer Nickelbasislegierung als Bauteilmaterial auch eine mit einem Schmelzpunkt erniedrigenden Element legierte Nickelbasislegierung gewählt werden, wobei beispielsweise als Schmelzpunkt erniedrigende Elemente Bor und/oder Phosphor gewählt werden können.Alternatively, in the case of a nickel-based alloy as the component material, a nickel-based alloy alloyed with a melting point-lowering element can also be selected, wherein boron and / or phosphorus, for example, can be selected as the melting point-lowering elements.
Unter Nickelbasislegierung sind diejenigen Legierungen zu verstehen, die als Bestandteil mit dem größten Anteil Nickel aufweisen und die insbesondere Legierungselemente umfassen, die eine Hochtemperaturanwendung ermöglichen. Beispielsweise kann hierfür Inconel IN 718 genannt werden.Nickel-based alloys are to be understood as those alloys which contain nickel as the constituent with the largest proportion and which in particular comprise alloy elements which enable high-temperature use. For example, Inconel IN 718 can be named for this.
Das Schichtmaterial wird in flüssiger Form aufgebracht, wobei eine chemische Reaktion in einem Tauchbad gewählt wird, um beispielsweise eine Nickelschicht aufzubringen. Ein derartiges Verfahren ist üblicherweise als chemisch Vernickeln bekannt.The layer material is applied in liquid form, a chemical reaction in an immersion bath being selected, for example in order to apply a nickel layer. Such a method is usually known as chemical nickel plating.
Die Wärmebehandlung kann bei einer Temperatur im Bereich der Schmelztemperatur des Schichtmaterials und unterhalb der Schmelztemperatur des Bauteilmaterials durchgeführt werden. Insbesondere kann die Temperatur in einem Bereich gewählt werden, der von einer Temperatur 30 % unterhalb der Schmelztemperatur bis zu einer Temperatur von 5 % über der Schmelztemperatur des Schichtmaterials reicht.The heat treatment can be carried out at a temperature in the range of the melting temperature of the layer material and below the melting temperature of the component material. In particular, the temperature can be selected in a range which ranges from a temperature 30% below the melting temperature to a temperature of 5% above the melting temperature of the layer material.
Erfindungsgemäß erfolgt die Wärmebehandlung im Bereich der Lösungsglühtemperatur des Bauteilmaterials. Bei einer nicht erfindungsgemäßen Ausführungsform kann bei einer Schicht aus chemischem Nickel die Wärmebehandlung auch bei einer Temperatur knapp oberhalb der Schmelztemperatur durchgeführt werden, sodass ein Anschmelzen der Beschichtung und/oder der ursprünglichen Oberfläche des Bauteils erfolgt.According to the invention, the heat treatment takes place in the area of the solution annealing temperature of the component material. In an embodiment not according to the invention, the heat treatment of a layer of chemical nickel can also be carried out at a temperature just above the melting temperature, so that the coating and / or the original surface of the component melts.
Obwohl nach der Durchführung der Wärmebehandlung bereits eine geglättete Grenzschicht zwischen der Beschichtung und dem Bauteil, also eine geglättete ursprüngliche Oberflächenschicht vorliegt und somit das Bauteil bereits in diesem Zustand mit der Beschichtung Verwendung finden kann, kann ein weiterer Verfahrensschritt vorgesehen sein, der eine Entfernung der Beschichtung vorsieht.Although after the heat treatment has been carried out there is already a smoothed boundary layer between the coating and the component, that is to say a smoothed original surface layer and the component can therefore already be used with the coating in this state, a further process step can be provided which involves removing the coating provides.
Dies kann bei dem vorliegenden Verfahren durch ein eigenschaftssensitives Abtragsverfahren, wie beispielsweise Ätzen, erfolgen, sodass die ursprüngliche Oberfläche wieder freigelegt werden kann. Damit kann die für bestimmte Anwendungen störende Beschichtung wieder entfernt werden, wobei gleichzeitig eine geglättete Oberfläche des Bauteils erreicht wird.In the present method, this can be done by a property-sensitive removal method, such as etching, so that the original surface can be exposed again. The coating which is disruptive for certain applications can thus be removed again, at the same time achieving a smoothed surface of the component.
Ein entsprechend hergestelltes Bauteil, insbesondere ein generativ hergestelltes Bauteil weist somit eine Randzone auf, die entweder eine Beschichtung umfasst oder zumindest eine Diffusionszone ausgebildet hat, wenn die Beschichtung wieder entfernt worden ist. Die Beschichtung dieses Bauteils weist das mit einem Schmelzpunkt erniedrigenden Element versehene Bauteilmaterial oder eine Beschichtung aus einem Bestandteil des Bauteilmaterials auf.A correspondingly manufactured component, in particular an additive manufactured component, therefore has an edge zone which either comprises a coating or has at least formed a diffusion zone when the coating has been removed again. The coating of this component has the component material provided with a melting point lowering element or a coating of a component of the component material.
Die beigefügten Zeichnungen zeigen in rein schematischer Weise in
- Fig.1
- einen Querschnitt durch ein generativ hergestelltes Bauteil mit einer rauen Oberfläche;
- Fig.2
- einen Querschnitt durch das Bauteil aus
, das mit einer Schicht versehen ist;Figur 1 - Fig.3
- einen Querschnitt durch das Bauteil aus den
nach Durchführung einer Wärmebehandlung; und inFiguren 1 und 2 - Fig.4
- einen Querschnitt durch das Bauteil aus den
nach Abziehen der Beschichtung.Figuren 1 bis 3
- Fig. 1
- a cross section through a generatively manufactured component with a rough surface;
- Fig. 2
- a cross section through the component
Figure 1 which is provided with a layer; - Fig. 3
- a cross section through the component from the
Figures 1 and 2 after performing heat treatment; and in - Fig. 4
- a cross section through the component from the
Figures 1 to 3 after peeling off the coating.
Weitere Vorteile, Kennzeichen und Merkmale der vorliegenden Erfindung werden bei der nachfolgenden detaillierten Beschreibung eines Ausführungsbeispiels deutlich.Further advantages, characteristics and features of the present invention will become clear in the following detailed description of an exemplary embodiment.
Die
Die
Nachdem die Schicht 3 auf dem Bauteil 1 erzeugt worden ist, wird das Bauteil einer Wärmebehandlung unterzogen, die es ermöglicht, dass ein Diffusionsaustausch von Inhaltsstoffen zwischen der Schicht 3 und dem Bauteil 1 erfolgen kann. Vorzugsweise kann die Wärmebehandlungstemperatur auch so gewählt werden, dass die Temperatur im Bereich der Schmelztemperatur des Schichtmaterials liegt, sodass ein leichtes Anschmelzen der rauen Oberfläche 2 erfolgen kann. Durch die Diffusionsvorgänge und/oder das Anschmelzen der Oberfläche 2 kommt es zu einer Änderung der Oberflächeneigenschaften, wie dies schematisch in
Je nach Anwendungsfall und Einsatzgebiet kann das Bauteil im Herstellungszustand gemäß
Allerdings ist es auch möglich, die Schicht 3 wieder zu entfernen, sodass die eingeebnete Grenzfläche 4 als geglättete Oberfläche 5 am Bauteil 1 vorliegt.However, it is also possible to remove the
Als eigenschaftssensitive Abtragsverfahren kommen hierfür beispielsweise Ätzverfahren in Frage, wobei das Ätzmittel auf die Zusammensetzung der Beschichtung abgestimmt ist. Durch eine Veränderung im Ätzverhalten an der Grenzfläche 4 kann das Abtragen von Material nach Erreichen der Grenzfläche 4 gestoppt werden, sodass das Bauteil 2 mit der geglätteten Oberfläche 5 vorliegt.Etching processes, for example, are suitable as property-sensitive removal processes, the etching agent being matched to the composition of the coating. By changing the etching behavior at the
Die entsprechend hergestellten Bauteile zeichnen sich somit entweder durch das Vorliegen einer Beschichtung an der Oberfläche aus, oder, im Falle des Abtragens der Beschichtung nach Durchführung der Wärmebehandlung, durch eine durch die Diffusion mit der ehemals vorhandenen Beschichtung vorhandene Diffusionszone in der Randzone des Bauteils 1.The correspondingly manufactured components are thus characterized either by the presence of a coating on the surface or, in the case of removal of the coating after the heat treatment has been carried out, by a diffusion zone in the edge zone of
Claims (9)
- Method for changing the surface properties, in particular for smoothing the surface of a component,
characterized in that- the surface of the component is coated with a layer material which is applied in liquid form and deposited by chemical reaction in an immersion bath and which has a composition containing at least one constituent which- melts at a lower temperature than the component material or- forms, together with the component material, at least one component part that has a lower melting temperature than the component material,and in that- the coated component is subjected to a heat treatment which is carried out in the range of the solution annealing temperature of the component material such that diffusion processes can take place between the coating and the component,- the component material being a metal alloy and the layer material being a metal alloy or a technically pure metal; and- the coating being optionally removed again after the heat treatment by means of a property-sensitive removal process. - Method according to claim 1, characterized in that the layer material is a component material provided with at least one element which lowers the melting point.
- Method according to claim 1, characterized in that the layer material is formed from the main component part of the component material.
- Method according to any of the preceding claims, characterized in that the component material is a nickel-based alloy and the layer material is nickel, or the layer material is a nickel-based alloy alloyed with at least one element which lowers the melting point.
- Method according to claim 4, characterized in that the element which lowers the melting point is boron and/or phosphorus.
- Method according to any of the preceding claims, characterized in that the heat treatment is carried out in a range of the melting temperature of the layer material and below the melting temperature of the component material, in particular in a temperature range from a temperature 30% below the melting temperature of the layer material up to a temperature 5% above the melting temperature of the layer material.
- Method according to any of the preceding claims, characterized in that for a layer deposited by chemical nickel plating, the heat treatment is at a temperature above the melting temperature of the chemically deposited nickel.
- Method according to any of the preceding claims, characterized in that the coating is removed again after the heat treatment by means of etching.
- Method according to any of the preceding claims, characterized in that the method is used for the additive manufacturing of a component in which the component is built up incrementally in layers from a component material, in order to at least partially smooth the component surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP12190803.2A EP2728035B1 (en) | 2012-10-31 | 2012-10-31 | Method for altering the surface properties of components |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP12190803.2A EP2728035B1 (en) | 2012-10-31 | 2012-10-31 | Method for altering the surface properties of components |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2728035A1 EP2728035A1 (en) | 2014-05-07 |
| EP2728035B1 true EP2728035B1 (en) | 2020-07-01 |
Family
ID=47191534
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP12190803.2A Active EP2728035B1 (en) | 2012-10-31 | 2012-10-31 | Method for altering the surface properties of components |
Country Status (1)
| Country | Link |
|---|---|
| EP (1) | EP2728035B1 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104630697B (en) * | 2014-12-17 | 2017-08-25 | 国家电网公司 | A kind of ternary co-osmosized layer of zinc-aluminum-magnesium and preparation method |
| CN104630695B (en) * | 2015-01-27 | 2017-08-25 | 国家电网公司 | It is a kind of to be used for the allumen diffusion medium of co-penetration layer at high proportion |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0861919A2 (en) * | 1997-01-31 | 1998-09-02 | Sermatech International Inc. | Method for removal of surface layers of metallic coatings (stripping) |
| EP1930477A1 (en) * | 2006-12-07 | 2008-06-11 | General Electric Company | Method for selectively removing coatings from metal substrates |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7335427B2 (en) * | 2004-12-17 | 2008-02-26 | General Electric Company | Preform and method of repairing nickel-base superalloys and components repaired thereby |
| US20070269676A1 (en) * | 2006-05-19 | 2007-11-22 | Singer Kevin M | Diffusion barrier layer and method of making the same, and wear resistant article with the diffusion barrier layer and method of making the same |
| US8453325B2 (en) * | 2009-11-18 | 2013-06-04 | United Technologies Corporation | Method of repair on nickel based HPT shrouds |
-
2012
- 2012-10-31 EP EP12190803.2A patent/EP2728035B1/en active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0861919A2 (en) * | 1997-01-31 | 1998-09-02 | Sermatech International Inc. | Method for removal of surface layers of metallic coatings (stripping) |
| EP1930477A1 (en) * | 2006-12-07 | 2008-06-11 | General Electric Company | Method for selectively removing coatings from metal substrates |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2728035A1 (en) | 2014-05-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE112007003090B4 (en) | Method for producing a three-dimensionally shaped object | |
| DE102012212954B4 (en) | Cold sprayed and heat treated magnesium coating | |
| DE102014217858A1 (en) | Surface smoothing of generatively manufactured components and correspondingly manufactured components of a turbomachine | |
| DE102016115674A1 (en) | Additive manufacturing | |
| DE102009031313B4 (en) | Coating and method for coating a component | |
| DE102009051551A1 (en) | Method and device for producing a component of a turbomachine | |
| DE102009051479A1 (en) | Method and device for producing a component of a turbomachine | |
| EP2851455B1 (en) | Method of electroplating wear-resistant coating | |
| WO2011015187A1 (en) | Blade tip coating that can be rubbed off | |
| EP2834387B1 (en) | Slurry and method for producing an aluminum diffusion layer | |
| EP2245274A1 (en) | Device and method for the partial coating of components | |
| EP3468740A1 (en) | Methods for joining materials, and material composite | |
| DE102015201927A1 (en) | Method for cold gas spraying with mask | |
| EP2695964B1 (en) | Protective coating tailored to a component | |
| EP2728035B1 (en) | Method for altering the surface properties of components | |
| DE102017210909A1 (en) | Method for the additive production of a component by means of auxiliary structure | |
| DE102018212908A1 (en) | Coated valve seat area of an internal combustion engine | |
| EP3791218A1 (en) | Mirror holder for an optical mirror made from a composite material, and method for the production thereof | |
| EP2756912A1 (en) | Remelting for build-up welding | |
| DE102005044991A1 (en) | Process for producing a protective layer, protective layer and component with a protective layer | |
| EP2980263A1 (en) | Component made from a molybdenum alloy and manufacturing method for the same | |
| DE102016207893A1 (en) | Construction platform for additive manufacturing and processes | |
| DE102006054347A1 (en) | Electrode and method for producing an electrode | |
| EP2840166B1 (en) | Intermetallic anti-wear protective coating for titanium materials | |
| DE102007011728A1 (en) | Method for determining hardness difference of layer applied by coating process before and after process change, involves determining hardness difference, which is determined by determination of density before and after process change |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| 17P | Request for examination filed |
Effective date: 20121031 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| AX | Request for extension of the european patent |
Extension state: BA ME |
|
| RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: MTU AERO ENGINES GMBH |
|
| 17P | Request for examination filed |
Effective date: 20141010 |
|
| RBV | Designated contracting states (corrected) |
Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: MTU AERO ENGINES AG |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
| 17Q | First examination report despatched |
Effective date: 20170704 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R079 Ref document number: 502012016185 Country of ref document: DE Free format text: PREVIOUS MAIN CLASS: C23C0010020000 Ipc: C23C0026020000 |
|
| RIC1 | Information provided on ipc code assigned before grant |
Ipc: C23C 10/08 20060101ALI20191218BHEP Ipc: C23C 10/22 20060101ALI20191218BHEP Ipc: C23C 10/16 20060101ALI20191218BHEP Ipc: C23C 10/14 20060101ALI20191218BHEP Ipc: C23C 10/60 20060101ALI20191218BHEP Ipc: C23C 26/02 20060101AFI20191218BHEP Ipc: C23C 10/26 20060101ALI20191218BHEP Ipc: C23C 10/06 20060101ALI20191218BHEP Ipc: C23C 10/20 20060101ALI20191218BHEP Ipc: C23C 10/02 20060101ALI20191218BHEP Ipc: C23C 10/18 20060101ALI20191218BHEP |
|
| GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
| INTG | Intention to grant announced |
Effective date: 20200131 |
|
| GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
| GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
| AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP Ref country code: AT Ref legal event code: REF Ref document number: 1286262 Country of ref document: AT Kind code of ref document: T Effective date: 20200715 |
|
| REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502012016185 Country of ref document: DE |
|
| REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201001 |
|
| REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20200701 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201102 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201001 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201002 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20201022 Year of fee payment: 9 Ref country code: FR Payment date: 20201020 Year of fee payment: 9 Ref country code: GB Payment date: 20201020 Year of fee payment: 9 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201101 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502012016185 Country of ref document: DE |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 |
|
| PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
| 26N | No opposition filed |
Effective date: 20210406 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201031 Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 |
|
| REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20201031 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201031 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201031 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201031 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201031 |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 1286262 Country of ref document: AT Kind code of ref document: T Effective date: 20201031 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201031 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 502012016185 Country of ref document: DE |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 |
|
| GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20211031 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200701 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20211031 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220503 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20211031 |