EP1990206B1 - Method and device for embossing a component with two mutually inclined surface areas by means of a digital printing process - Google Patents

Method and device for embossing a component with two mutually inclined surface areas by means of a digital printing process Download PDF

Info

Publication number
EP1990206B1
EP1990206B1 EP08008534A EP08008534A EP1990206B1 EP 1990206 B1 EP1990206 B1 EP 1990206B1 EP 08008534 A EP08008534 A EP 08008534A EP 08008534 A EP08008534 A EP 08008534A EP 1990206 B1 EP1990206 B1 EP 1990206B1
Authority
EP
European Patent Office
Prior art keywords
printing
surface region
transition region
relative movement
print head
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
Application number
EP08008534A
Other languages
German (de)
French (fr)
Other versions
EP1990206A3 (en
EP1990206A2 (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Interglarion Ltd
Original Assignee
Interglarion Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Interglarion Ltd filed Critical Interglarion Ltd
Priority to PL08008534T priority Critical patent/PL1990206T3/en
Priority to SI200830414T priority patent/SI1990206T1/en
Publication of EP1990206A2 publication Critical patent/EP1990206A2/en
Publication of EP1990206A3 publication Critical patent/EP1990206A3/en
Application granted granted Critical
Publication of EP1990206B1 publication Critical patent/EP1990206B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B41PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
    • B41JTYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
    • B41J3/00Typewriters or selective printing or marking mechanisms characterised by the purpose for which they are constructed
    • B41J3/407Typewriters or selective printing or marking mechanisms characterised by the purpose for which they are constructed for marking on special material
    • B41J3/4073Printing on three-dimensional objects not being in sheet or web form, e.g. spherical or cubic objects

Definitions

  • the invention relates to a method and a device for printing a component by means of a digital printing method, which component has a first and a second surface area.
  • the task of printing components with two surface areas, which are inclined at an angle to each other and connected to each other via a transition region may be, for example, plates or strips with at an angle of, for example, 90 ° to each other arranged side surfaces which are connected to each other via an edge formed with a radius or a transition region.
  • Such components are printed after mechanical finishing, for example, with an ink jet process, so that their entire visible surface to the outside receives a pleasing appearance, for example, provided with a homogeneous ink layer or with a pattern that runs steadily over the entire surface.
  • a printing method for printing a component having two mutually perpendicular surface areas is described, which merge into one another via an inclined surface 116.
  • each surface area is a printhead 60.
  • the inclined surface is printed so that the printheads are each moved beyond the associated surface area, so that at least one part of the inclined surface is printed.
  • a middle region of the inclined surface is printed by both printheads.
  • the US 2001019340 A1 describes a printing method and a device for its implementation, in which or when printing three-dimensional surfaces on a printhead trained printing nozzles are each controlled such that only those printing nozzles are activated, the distance from the surface to be printed is within a predetermined value ,
  • the EP 1 479 524 A1 also generally describes a method of manufacturing a component having a surface of predetermined appearance, wherein adjacent surface areas disposed at an angle to each other are patterned such that the pattern smoothly transitions from one surface area to the other surface area. There are no indications regarding the printing of a transition area between the surfaces.
  • the invention has for its object to provide a method and an apparatus with which it is possible to easily print a transition region formed between two surface regions forming an angle with one another in such a way that a homogeneous printing of the transition region takes place.
  • the claim 8 is directed to an apparatus for solving the relevant part of the invention task.
  • a digital printing method is understood to mean printing methods in which a liquid in the form of individual liquid droplets is sprayed onto individual surface elements of a surface to be printed by means of at least one digital data set from at least one spray nozzle in order to produce a predetermined pattern on the surface. which can also have the appearance of a homogeneous coloring. Different colors can be produced by different color liquids, which are sprayed in the form of droplets on a surface element or immediately adjacent surface elements. Different color intensities can be produced by the number of droplets reaching a surface element or immediately adjacent surface elements and / or, more recently, by different volumes of the liquid droplets.
  • a typical example of a digital printing process is the so-called inkjet printing process in which ink or dye liquid droplets are ejected from a printhead having a plurality of spray nozzles.
  • the droplets are generated by thermal evaporation (bubblejet) or by means of piezoelectric elements and sprayed.
  • Fig. 1 has a component to be printed 10, in the example shown a edge strip, a non-printing base 12, a likewise not to be printed lateral side 14, a first flat surface area to be printed 16, a to be printed curved transition area 18 in a flat to be printed second Surface area 20 on.
  • the surface regions 16 and 20 are perpendicular to one another and in each case continuously transition into the transition region 18, which extends over an angular range of 90 degrees and has a radius of curvature r.
  • a print head of a per se known ink jet printing device is described, which is formed for example as a pressure bar and over the entire in Fig. 1 extends perpendicular to the plane of the drawing length of the component 10.
  • a pressure bar contains, for example, a plurality of printheads arranged in mutual overlap along its length, so that each surface element can be covered with liquid droplets.
  • the printing of the component 10 takes place in the illustrated example such that initially under relative movement between the component 10 and the print head 20 in a direction perpendicular to the plane perpendicular to the paper plane extension direction of the component 10 and parallel to the surface region 16 (x-direction) of the first Surface region 16 and a part of the transition region 18 is printed.
  • the control data stored in an EDP system are distorted with respect to the curved transition region 18 in the x-direction compared to a template, which shows the pattern to be generated on the curved surface of the transition region, so that depending on the angle ⁇ , the x-direction with the respective tangent to the surface of the transition region forms, the pattern is stretched.
  • the amount of liquid sprayed off is changed as a function of x.
  • x 0 is in Fig. 1 denotes the beginning of the transition region.
  • the quantity of liquid to be sprayed off per relative movement unit in the x-direction is constant relative to the color intensity to be achieved.
  • the intensity of the printing ie the amount of liquid to be emitted per unit of relative movement in the x direction for the generation of a predetermined color intensity, remains over a distance x 1 , starting from x 0 Fig.
  • Fig. 1 is initially constant to the right and then decreases between x 1 and x 2 , for example, linearly, and is set to zero when reaching the point x 2 , so that the according to Fig. 1 lowest part of the transition region 18, which is very strongly inclined to the x-direction, is not printed in this printing step.
  • step II in which the second surface area 20 is printed and the in Fig. 1 is shown as y-direction.
  • the intensity in the range between y 1 and y 2 decreases to zero, so that the region of the transition region 18 which is inclined more than 60 degrees to the y direction is not printed in this method step.
  • the described printing method achieved in a simple manner that the transition region in well-defined way (exact formation of the pattern due to sufficiently large angle of incidence of the droplet direction on the surface (between 90 degrees and 30 degrees)) is printed with good pattern quality, the intensity remains constant in that in the transition region, is printed on in both printing steps (x and y), the pressure intensity of the one printing step decreases and that of the other printing step increases, so that the sum intensity is approximately constant.
  • the two printing steps I, II can be carried out, for example, by first performing the printing step x such that the component 12 is moved from right to left under the print head 22, then the component 12 corresponding to the angle of inclination of the first surface area 16 and the first surface area 16 second surface area 20 to each other in the illustrated example by 90 degrees) and is then moved from left to right under the print head 22, wherein the printing operation begins when the point B is located under the print head and the printing ends when the location y 2 is located under the printhead.
  • the described method according to which a curved surface can be printed without a print head or the component to be printed being pivoted during the printing process, can be used for a wide variety of components.
  • Fig. 2 shows a cross section through a component in which two relief-like surface regions 16 and 20 are interconnected via a transition region 18, wherein the angle ⁇ , the surface regions 16 and 20 together form, about 60 degrees.
  • a first printing step I the surface region 20 is printed with a first part of the transition region 18.
  • the surface region 16 is printed with a part of the transition region 18 in a second printing step II, wherein the parts of the transition region which are printed in the printing step I and in the printing step II overlap ,
  • the pressure intensity ie the amount of pressure fluid delivered per unit of relative movement, can already be modulated during the printing of the relief-like surface areas 16 and 20 depending on the respective angle of inclination between the surface area and the direction of movement.
  • Fig. 3 shows a component 10 with three mutually perpendicular to each other forming planar surface areas which are interconnected via curved transition areas, wherein the radii of curvature of the transition regions may be the same or different.
  • the surface to be printed on the component 10 is printed in three printing steps I, II and III, in which the component 10 is pivoted to the print head 22 in each case by 90 degrees.
  • the transition areas are, as based on the Fig. 1 portrayed, printed.
  • Fig. 4 shows a component 10 whose surface is to be completely printed;
  • the steps I, II and III correspond to the embodiment according to FIG Fig. 3
  • step IV in which the underside of the component 10 is to be printed, the print head 22 and the component 10 are pivoted to each other such that the relative movement between the print head 22 and component 10 is parallel to the bottom.
  • Fig. 5 shows a circular bar, which is advantageously printed in four printing steps I to IV, wherein in each of the printing operations to both end regions toward control operations are performed, as shown in the Fig. 1 for the transitional area between Fig. 5 the printing steps II and III have been explained.
  • Fig. 6 provides a plan view of a developed surface, for example, of the component 10 according to Fig. 3 with the same length formation of the side regions 20 and 20 '.
  • the meanings of x 1 , x 2 and y 1 , y 2 respectively correspond to those of FIG Fig. 1 .
  • those surface parts are designated, which are printed in the respective printing process x and y (there are two mutually rotated by 180 degrees printing operations y) with an intensity of 100%, that is, all the colors of which, for example a decor is composed, based on the relative movement in the direction of x or y is 100% delivered.
  • the respective ink application is reduced from 100% to 0%, whereby this reduction can be directly proportional decreasing with respect to the inclination angle or the linear relative movement distance.
  • Fig. 7 to 9 show examples according to which the printing steps I and II according to Fig. 1 can be controlled.
  • Fig. 7 shows an example in which the surface part which is printed with decreasing intensity in step I completely overlaps that surface part which is printed in full intensity in step II and vice versa, the surface part which is printed with decreasing intensity in step II, overlaps the part printed in step I with full intensity.
  • Fig. 8 Fig. 14 shows a case where the respective surface portions printed with decreasing intensity overlap but are not congruent.
  • Fig. 9 shows the case in which the surface parts, which are each printed with decreasing intensity, are congruent.
  • Fig. 7 to 9 are for the surface of the component according to Fig. 6 each to be presented twice, ie to the respective Fig. 7 to 9 joins the Fig. 6 to the left mirror the same figure again.
  • Fig. 10 Based on Fig. 10 is below under a similar consideration as in Fig. 1 explains how to achieve a print intensity on the transition region 18 in the printing steps I (relative movement between the print head and the first surface region 16 in the x direction) and the printing step II (relative movement between the print head and the second surface region 20 in the y direction) , which leads to a constant pressure intensity over the entire transition region 18.
  • the geometry of the pattern to be created in the transition region 18 can be transformed in a manner known per se by distorting the pattern data used for the control according to the angle ⁇ such that the pattern is printed undistorted in spite of the linear relative movement.
  • Fig. 11 shows the basic structure in an apparatus for performing the method according to the invention.
  • the printhead 22 which is designed, for example, as a bar, is attached to a drive device 30 with which the print head 22 can be moved in the direction of the vertical double arrow W. Opposite the print head is the component 10 to be printed, which is held by a drive device 32, by means of which it is movable in the direction of the horizontal double arrow Z and in the direction of the double arrow R about an axis perpendicular to the paper plane axis.
  • the position of the component 10 relative to a stationary reference point can be detected by means of a sensor device 34.
  • an electronic control device 36 with a control panel 38 and a screen 40 is provided.
  • the electronic control device 36 includes a microprocessor with program and data storage and is known per se in construction and will therefore not be explained in detail.
  • the print head 22 does not extend over the entire width of the component 10 to be printed, it can advantageously also be moved in a direction perpendicular to the plane of the paper by means of the drive device 30.
  • the drive device 32 by means of which the component 10 can be pivoted, can also be designed such that the component 10 can be pivoted about three mutually perpendicular spatial axes.
  • the drive devices 30 and 32 can be designed in many different ways, wherein it must be ensured that the relative movements necessary for carrying out the method according to the invention are possible between the print head 22 and the component 10.

Abstract

The method involves controlling a pressure medium left from a printhead (22) in such a manner that a part of a transition region (18) is only printed. The transition region is strongly inclined to a direction of two relative movements, where the medium has low gradient to the respective movements. Respective distances of the movements of injected fluid amount are gradually reduced to zero during printing of the part of the region, so that the part is partially printed. An independent claim is also included for a device for printing a component by an inkjet printing method.

Description

Die Erfindung betrifft ein Verfahren und eine Vorrichtung zum Bedrucken eines Bauteils mittels eines digitalen Druckverfahrens, welches Bauteil einen ersten und einen zweiten Oberflächenbereich aufweist.The invention relates to a method and a device for printing a component by means of a digital printing method, which component has a first and a second surface area.

In der Praxis stellt sich in unterschiedlichsten Anwendungsbereichen die Aufgabe, Bauteile mit zwei Oberflächenbereichen zu bedrucken, die in einem Winkel zueinander geneigt und über einen Übergangsbereich miteinander verbunden sind. Solche Bauteile können beispielsweise Platten oder Leisten mit in einem Winkel von beispielsweise 90° zueinander angeordneten Seitenflächen sein, die über eine mit einem Radius ausgebildete Kante bzw. einem Übergangsbereich miteinander verbunden sind. Solche Bauteile werden nach mechanischer Fertigbearbeitung beispielsweise mit einem Tintenstrahlverfahren bedruckt, so dass ihre gesamte nach außen hin sichtbare Oberfläche ein gefälliges Aussehen erhält, beispielsweise mit einer homogenen Farbschicht oder mit einer Musterung versehen wird, die stetig über die gesamte Oberfläche verläuft. Bekannt ist, einen Druckkopf und ein zu bedruckendes Bauteil während des Bedruckens relativ zueinander derart zu bewegen, dass der Druckkopf möglichst unter Konstanthaltung seines Abstandes ständig senkrecht auf die zu bedruckende Oberfläche gerichtet ist. Dies erfordert sowohl einen hohen mechanischen Aufwand der jeweiligen Vorrichtung als auch einen hohen Aufwand bezüglich der Datenverarbeitung zur Steuerung der Vorrichtung.In practice, in a wide variety of applications, the task of printing components with two surface areas, which are inclined at an angle to each other and connected to each other via a transition region. Such components may be, for example, plates or strips with at an angle of, for example, 90 ° to each other arranged side surfaces which are connected to each other via an edge formed with a radius or a transition region. Such components are printed after mechanical finishing, for example, with an ink jet process, so that their entire visible surface to the outside receives a pleasing appearance, for example, provided with a homogeneous ink layer or with a pattern that runs steadily over the entire surface. It is known to move a print head and a component to be printed during the printing relative to each other such that the print head is constantly directed as possible while keeping its distance constant perpendicular to the surface to be printed. This requires both a high mechanical complexity of the respective device as well as a high cost of data processing for controlling the device.

In der US 2003218663 A1 , von der im Oberbegriff des Anspruchs 1 ausgegangen wird, ist ein Druckverfahren zum Bedrucken eines Bauteils mit zwei zueinander senkrechten Oberflächenbereichen beschrieben, die über eine Schrägfläche 116 ineinander übergehen. Zur Bedruckung jedes Oberflächenbereiches dient ein Druckkopf 60. Die Schrägfläche wird derart bedruckt, dass die Druckköpfe jeweils über den zugehörigen Oberflächenbereich hinaus bewegt werden, so dass mindestens jeweils ein Teil der Schrägfläche bedruckt wird. Vorteilhafterweise wird ein mittlerer Bereich der Schrägfläche von beiden Druckköpfen bedruckt.In the US 2003218663 A1 , is based on the preamble of claim 1, a printing method for printing a component having two mutually perpendicular surface areas is described, which merge into one another via an inclined surface 116. For printing each surface area is a printhead 60. The inclined surface is printed so that the printheads are each moved beyond the associated surface area, so that at least one part of the inclined surface is printed. Advantageously, a middle region of the inclined surface is printed by both printheads.

Die US 2001019340 A1 beschreibt ein Druckverfahren bzw. eine Vorrichtung zu dessen Durchführung, bei dem bzw. der beim Bedrucken von dreidimensionalen Oberflächen an einem Druckkopf ausgebildete Druckdüsen jeweils derart angesteuert werden, dass nur diejenigen Druckdüsen aktiviert werden, deren Entfernung von der zu bedruckenden Oberfläche innerhalb eines vorbestimmten Wertes liegt.The US 2001019340 A1 describes a printing method and a device for its implementation, in which or when printing three-dimensional surfaces on a printhead trained printing nozzles are each controlled such that only those printing nozzles are activated, the distance from the surface to be printed is within a predetermined value ,

In der DE 100 31 030 A1 ist ganz allgemein ein Verfahren zum Herstellen flächiger Bauteile mit vorbestimmtem Oberflächenaussehen beschrieben, bei welchem Verfahren die Bauteile mittels eines programmierbaren Druckverfahrens bedruckt werden. Dabei können auch Bauteile mit zueinander geneigten Oberflächen bedruckt werden. Hinsichtlich der Bedruckung eines Übergangsbereiches zwischen den geneigten Oberflächen finden sich keine Hinweise.In the DE 100 31 030 A1 In general, a method for producing flat components with a predetermined surface appearance is described, in which method the components are printed by means of a programmable printing method. It is also possible to print components with mutually inclined surfaces. Regarding the printing of a transition region between the inclined surfaces, there are no indications.

Die EP 1 479 524 A1 beschreibt ebenfalls allgemein ein Verfahren zum Herstellen eines Bauteils mit einer Oberflächen vorbestimmten Aussehens, wobei auf einander angrenzende Oberflächenbereiche, die in einem Winkel zueinander angeordnet sind, ein Muster derart aufgebracht wird, dass das Muster von dem einem Oberflächenbereich zu dem anderen Oberflächenbereich stetig übergeht. Hinsichtlich der Bedruckung eines Übergangsbereichs zwischen den Oberflächen finden sich keine Hinweise.The EP 1 479 524 A1 also generally describes a method of manufacturing a component having a surface of predetermined appearance, wherein adjacent surface areas disposed at an angle to each other are patterned such that the pattern smoothly transitions from one surface area to the other surface area. There are no indications regarding the printing of a transition area between the surfaces.

Der Erfindung liegt die Aufgabe zugrunde, ein Verfahren und eine Vorrichtung anzugeben, mit dem bzw. der es möglich ist, einen zwischen zwei einen Winkel miteinander bildenden Oberflächenbereichen ausgebildeten Übergangsbereich in einfacher Weise derart zu bedrucken, dass eine homogene Bedruckung des Übergangsbereiches erfolgt.The invention has for its object to provide a method and an apparatus with which it is possible to easily print a transition region formed between two surface regions forming an angle with one another in such a way that a homogeneous printing of the transition region takes place.

Der auf das Verfahren gerichtete Teil der Erfindungsaufgabe wird mit den Merkmalen des Anspruchs 1 gelöst.The directed to the method part of the invention task is solved with the features of claim 1.

Die auf den Anspruch 1 rückbezogenen Verfahrensansprüche sind auf vorteilhafte Ausführungsformen und Weiterbildungen des erfindungsgemäßen Verfahrens gerichtet.The dependent claims back to claim 1 are directed to advantageous embodiments and developments of the method according to the invention.

Der Anspruch 8 ist auf eine Vorrichtung zum Lösen des diesbezüglichen Teils der Erfindungsaufgabe gerichtet.The claim 8 is directed to an apparatus for solving the relevant part of the invention task.

Unter einem digitalen Druckverfahren werden in der vorliegenden Anmeldung Druckverfahren verstanden, bei denen unter elektronischer Steuerung mittels wenigstens eines digitalen Datensatzes aus wenigstens einer Spritzdüse eine Flüssigkeit in Form einzelner Flüssigkeitströpfchen auf einzelne Oberflächenelemente einer zu bedruckenden Oberfläche gespritzt wird, um auf der Oberfläche ein vorbestimmtes Muster, das auch das Aussehen einer homogenen Färbung haben kann, zu erzeugen. Unterschiedliche Farben lassen sich durch unterschiedliche Farbflüssigkeiten erzeugen, die in Form von Tröpfchen auf ein Oberflächenelement oder unmittelbar benachbarte Oberflächenelemente gespritzt werden. Unterschiedliche Farbintensitäten lassen sich durch die Anzahl der auf ein Oberflächenelement oder unmittelbar benachbarte Oberflächenelemente gelangende Tröpfchen und/oder - in neuerer Zeit - durch unterschiedliche Volumina der Flüssigkeitströpfchen erzeugen. Ein typisches Beispiel eines digitalen Druckverfahrens ist das sog. Tintenstrahldruckverfahren, bei dem Tinten- bzw. Färbeflüssigkeitströpfchen aus einem Druckkopf mit mehreren Spritzdüsen abgespritzt werden. Die Tröpfchen werden durch thermische Verdampfung (bubblejet) oder mit Hilfe von Piezoelementen erzeugt und abgespritzt.In the present application, a digital printing method is understood to mean printing methods in which a liquid in the form of individual liquid droplets is sprayed onto individual surface elements of a surface to be printed by means of at least one digital data set from at least one spray nozzle in order to produce a predetermined pattern on the surface. which can also have the appearance of a homogeneous coloring. Different colors can be produced by different color liquids, which are sprayed in the form of droplets on a surface element or immediately adjacent surface elements. Different color intensities can be produced by the number of droplets reaching a surface element or immediately adjacent surface elements and / or, more recently, by different volumes of the liquid droplets. A typical example of a digital printing process is the so-called inkjet printing process in which ink or dye liquid droplets are ejected from a printhead having a plurality of spray nozzles. The droplets are generated by thermal evaporation (bubblejet) or by means of piezoelectric elements and sprayed.

Die Erfindung wird im Folgenden anhand schematischer Zeichnungen beispielsweise und mit weiteren Einzelheiten erläutert, wobei das digitale Druckverfahren wie ein Tintenstrahldruckverfahren durchgeführt wird.The invention is explained below with reference to schematic drawings, by way of example and with further details, wherein the digital printing method is carried out like an ink-jet printing method.

In den Figuren stellen dar:

Fig. 1
eine Querschnittsansicht eines zu bedruckenden Bauteils mit Erläuterungen zur Durchführung eines erfindungsgemäßen Verfahrens,
Fig. 2 bis 5
Querschnitte durch unterschiedliche, zu bedruckende Bauteile,
Fig. 6
eine Aufsicht auf die abgewickelte Oberfläche eines Bauteils,
Fig. 7 bis 9
Darstellungen zur Erläuterung von unterschiedlichen Ausführungsformen des erfindungsgemäßen Verfahrens,
Fig. 10
eine der Fig. 1 ähnliche Ansicht zur Erläuterung einer weiteren Durchführungsform des erfindungsgemäßen Verfahrens und
Fig. 11
eine schematische Ansicht einer Vorrichtung zur Durchführung des erfindungsgemäßen Verfahrens.
In the figures represent:
Fig. 1
a cross-sectional view of a component to be printed with explanations for carrying out a method according to the invention,
Fig. 2 to 5
Cross sections through different components to be printed,
Fig. 6
a view of the unwound surface of a component,
Fig. 7 to 9
Representations for explaining different embodiments of the method according to the invention,
Fig. 10
one of the Fig. 1 Similar view for explaining a further embodiment of the method according to the invention and
Fig. 11
a schematic view of an apparatus for performing the method according to the invention.

Gemäß Fig. 1 weist ein zu bedruckendes Bauteil 10, im dargestellten Beispiel eine Kantleiste, eine nicht zu bedruckende Unterseite 12, eine ebenfalls nicht zu bedruckende seitliche Seite 14, einen ersten ebenen, zu bedruckenden Oberflächenbereich 16, einen zu bedruckenden gekrümmten Übergangsbereich 18 in einen ebenen zu bedruckenden zweiten Oberflächenbereich 20 auf. Die Oberflächenbereiche 16 und 20 stehen senkrecht aufeinander und gehen jeweils stetig in den Übergangsbereich 18 über, der sich um einen Winkelbereich von 90 Grad erstreckt und einen Krümmungsradius r hat.According to Fig. 1 has a component to be printed 10, in the example shown a edge strip, a non-printing base 12, a likewise not to be printed lateral side 14, a first flat surface area to be printed 16, a to be printed curved transition area 18 in a flat to be printed second Surface area 20 on. The surface regions 16 and 20 are perpendicular to one another and in each case continuously transition into the transition region 18, which extends over an angular range of 90 degrees and has a radius of curvature r.

Mit 22 ist ein Druckkopf einer an sich bekannten Tintenstrahldruckeinrichtung beschrieben, der beispielsweise als Druckbalken ausgebildet ist und sich über die gesamte in Fig. 1 senkrecht auf der Zeichnungsebene stehenden Länge des Bauteils 10 erstreckt. Ein solcher Druckbalken enthält beispielsweise mehrere längs seiner Länge in gegenseitiger Überlappung angeordnete Druckköpfe, so dass jedes Oberflächenelement mit Flüssigkeitströpfchen belegt werden kann. Mittels elektronischer Steuerung der Relativstellung zwischen Spritzdüse(n) und zu bedruckender Oberfläche sowie der Art und der Menge der auf ein Oberflächenelement gelangenden Flüssigkeitsmenge lassen sich vorbestimmte digital gespeicherte Muster auf der zu bedruckenden Oberfläche präzise erzeugen.At 22, a print head of a per se known ink jet printing device is described, which is formed for example as a pressure bar and over the entire in Fig. 1 extends perpendicular to the plane of the drawing length of the component 10. Such a pressure bar contains, for example, a plurality of printheads arranged in mutual overlap along its length, so that each surface element can be covered with liquid droplets. By means of electronic control of the relative position between the spray nozzle (s) and the surface to be printed and the type and amount of liquid reaching a surface element, predetermined digitally stored patterns can be precisely produced on the surface to be printed.

Die Bedruckung des Bauteils 10 erfolgt in dem dargestellten Beispiel derart, dass zunächst unter Relativbewegung zwischen dem Bauteil 10 und dem Druckkopf 20 in einer Richtung senkrecht zur auf der Papierebene senkrecht stehenden Erstreckungsrichtung des Bauteils 10 und parallel zum Oberflächenbereich 16 (x-Richtung) der erste Oberflächenbereich 16 und ein Teil des Übergangsbereiches 18 bedruckt wird. Die in einem EDV-System abgelegten Steuerungsdaten sind bezüglich des gekrümmten Übergangsbereiches 18 in x-Richtung gegenüber einer Vorlage, die das auf der gekrümmten Oberfläche des Übergangsbereiches zu erzeugende Muster zeigt, verzerrt, so dass abhängig vom Winkel α, den die x-Richtung mit der jeweiligen Tangente an die Oberfläche des Übergangsbereiches bildet, das Muster gedehnt wird. Des Weiteren wird zur Konstanthaltung der Musterintensität über den Übergangsbereich die abgespritzte Flüssigkeitsmenge abhängig von x verändert.The printing of the component 10 takes place in the illustrated example such that initially under relative movement between the component 10 and the print head 20 in a direction perpendicular to the plane perpendicular to the paper plane extension direction of the component 10 and parallel to the surface region 16 (x-direction) of the first Surface region 16 and a part of the transition region 18 is printed. The control data stored in an EDP system are distorted with respect to the curved transition region 18 in the x-direction compared to a template, which shows the pattern to be generated on the curved surface of the transition region, so that depending on the angle α, the x-direction with the respective tangent to the surface of the transition region forms, the pattern is stretched. Furthermore, in order to keep the pattern intensity constant over the transition area, the amount of liquid sprayed off is changed as a function of x.

Mit x0 ist in Fig. 1 der Beginn des Übergangsbereiches bezeichnet. Für x-Werte gemäß Fig. 1 links von x0 ist die je Relativbewegungseinheit in x-Richtung abzuspritzende Flüssigkeitsmenge bezogen auf die zu erreichende Farbintensität konstant. Sobald die Stelle x0 erreicht wird, nimmt die bezogen auf eine bestimmte Relativbewegung zwischen Druckkopf 22 und Bauteil 10 in x-Richtung zu bedruckende Fläche des Übergangsbereiches zu. Die Intensität der Bedruckung, d.h. die je Einheit der Relativbewegung in x-Richtung für die Erzeugung einer vorbestimmten Farbintensität abzustrahlende Flüssigkeitsmenge, bleibt über eine Strecke x1, ausgehend von x0 gemäß Fig. 1 nach rechts zunächst konstant und nimmt dann zwischen x1 und x2 ab, beispielsweise linear ab, und wird bei Erreichen der Stelle x2 auf Null gestellt, so dass der gemäß Fig. 1 unterste Teil des Übergangsbereiches 18, der zur x-Richtung sehr stark geneigt ist, in diesem Druckschritt gar nicht bedruckt wird.With x 0 is in Fig. 1 denotes the beginning of the transition region. For x-values according to Fig. 1 To the left of x 0 , the quantity of liquid to be sprayed off per relative movement unit in the x-direction is constant relative to the color intensity to be achieved. As soon as the point x 0 is reached, relative to a certain relative movement between the print head 22 and component 10 in the x direction to be printed area of the transition region to. The intensity of the printing, ie the amount of liquid to be emitted per unit of relative movement in the x direction for the generation of a predetermined color intensity, remains over a distance x 1 , starting from x 0 Fig. 1 is initially constant to the right and then decreases between x 1 and x 2 , for example, linearly, and is set to zero when reaching the point x 2 , so that the according to Fig. 1 lowest part of the transition region 18, which is very strongly inclined to the x-direction, is not printed in this printing step.

Zusammengefasst ist bei dem geschilderten Druckvorgang die Druckintensität von A (Beginn des ersten Oberflächenbereiches 16) bis zur Stelle x1 (α = 45°) konstant 100%, und nimmt dann zwischen α = 45° und beispielsweise α = 60° auf 0% ab. Der Bereich, in dem die Neigung zwischen dem Übergangsbereich 18 und dem ersten Oberflächenbereich 16 größer als 60 Grad ist, wird in dem geschilderten Druckschritt gar nicht bedruckt, da bei so starken Neigungswinkeln infolge des Abprallens von Tröpfchen keine definierten Verhältnisse vorliegen.In summary, the pressure intensity of A (beginning of the first surface area 16) to the point x 1 (α = 45 °) is constant 100% in the described printing process, and then decreases between α = 45 ° and for example α = 60 ° to 0% , The region in which the inclination between the transition region 18 and the first surface region 16 is greater than 60 degrees, is not printed in the described printing step, since at such strong angles of inclination due to the rebound of droplets are no defined conditions.

An den geschilderten Druckschritt I schließt sich ein weiterer Druckschritt II an, in dem der zweite Oberflächenbereich 20 bedruckt wird und der in Fig. 1 als y-Richtung dargestellt ist. Zunächst wird wiederum mit einer Intensität von 100% vom Punkt B bis zum Punkt y1 gedruckt, indem die Oberfläche des Übergangsbereiches 18 zur y-Richtung um 45 Grad geneigt ist. Anschließend nimmt die Intensität in dem Bereich zwischen y1 und y2 (Neigung um 60 Grad) auf Null ab, so dass der zur y-Richtung stärker als 60 Grad geneigte Bereich des Übergangsbereiches 18 in diesem Verfahrensschritt nicht bedruckt wird.At the described printing step I is followed by a further printing step II, in which the second surface area 20 is printed and the in Fig. 1 is shown as y-direction. First, again with an intensity of 100% from the point B to the point y 1 printed by the surface of the transition region 18 is inclined to the y-direction by 45 degrees. Subsequently, the intensity in the range between y 1 and y 2 (inclination by 60 degrees) decreases to zero, so that the region of the transition region 18 which is inclined more than 60 degrees to the y direction is not printed in this method step.

Insgesamt wird mit dem geschilderten Druckverfahren auf einfache Weise erreicht, dass der Übergangsbereich in wohl definierter Weise (genaue Ausbildung des Musters wegen ausreichend großer Auftreffwinkel der Tröpfchenrichtung auf die Oberfläche (zwischen 90 Grad und 30 Grad)) mit guter Musterqualität bedruckt wird, wobei die Intensität dadurch konstant bleibt, dass im Übergangsbereich, auf den in beiden Druckschritten (x und y) gedruckt wird, die Druckintensität des einen Druckschrittes abnimmt und die des anderen Druckschrittes zunimmt, so dass die Summenintensität annähernd konstant ist.Overall, with the described printing method achieved in a simple manner that the transition region in well-defined way (exact formation of the pattern due to sufficiently large angle of incidence of the droplet direction on the surface (between 90 degrees and 30 degrees)) is printed with good pattern quality, the intensity remains constant in that in the transition region, is printed on in both printing steps (x and y), the pressure intensity of the one printing step decreases and that of the other printing step increases, so that the sum intensity is approximately constant.

Die beiden Druckschritte I, II können beispielsweise dadurch ausgeführt werden, dass der Druckschritt x zunächst derart ausgeführt wird, dass das Bauteil 12 von rechts nach links unter den Druckkopf 22 hindurch bewegt wird, das Bauteil 12 dann entsprechend dem Neigungswinkel des ersten Oberflächenbereiches 16 und des zweiten Oberflächenbereiches 20 zueinander im dargestellten Beispiel um 90 Grad) gedreht wird und anschließend von links nach rechts unter dem Druckkopf 22 hindurch bewegt wird, wobei der Druckvorgang beginnt, wenn sich die Stelle B unter dem Druckkopf befindet und der Druckvorgang endet, wenn sich die Stelle y2 unter dem Druckkopf befindet.The two printing steps I, II can be carried out, for example, by first performing the printing step x such that the component 12 is moved from right to left under the print head 22, then the component 12 corresponding to the angle of inclination of the first surface area 16 and the first surface area 16 second surface area 20 to each other in the illustrated example by 90 degrees) and is then moved from left to right under the print head 22, wherein the printing operation begins when the point B is located under the print head and the printing ends when the location y 2 is located under the printhead.

Das beschriebene Verfahren, gemäß dem eine gekrümmte Oberfläche bedruckt werden kann, ohne dass ein Druckkopf oder das zu bedruckende Bauteil während des Druckvorgangs verschwenkt wird, kann für unterschiedlichste Bauteile angewendet werden.The described method, according to which a curved surface can be printed without a print head or the component to be printed being pivoted during the printing process, can be used for a wide variety of components.

Fig. 2 zeigt einen Querschnitt durch ein Bauteil, bei dem zwei reliefartige Oberflächenbereiche 16 und 20 über einen Übergangsbereich 18 miteinander verbunden sind, wobei der Winkel γ, den die Oberflächenbereiche 16 und 20 miteinander bilden, etwa 60 Grad beträgt. In einem ersten Druckschritt I wird der Oberflächenbereich 20 mit einem ersten Teil des Übergangsbereiches 18 bedruckt. Nach einer Relativschwenkung zwischen dem Druckkopf 22 und dem Bauteil 10 um den Winkel γ wird in einem zweiten Druckschritt II der Oberflächenbereich 16 mit einem Teil des Übergangsbereiches 18 bedruckt, wobei die Teile des Übergangsbereiches, die im Druckschritt I und im Druckschritt II bedruckt werden, überlappen. Die Druckintensität, d.h. die je Einheit der Relativbewegung abgegebene Druckflüssigkeitsmenge kann bereits während der Bedruckung der reliefartig ausgebildeten Oberflächenbereiche 16 und 20 abhängig vom jeweiligen Neigungswinkel zwischen dem Oberflächenbereich und der Bewegungsrichtung moduliert werden. Fig. 2 shows a cross section through a component in which two relief-like surface regions 16 and 20 are interconnected via a transition region 18, wherein the angle γ, the surface regions 16 and 20 together form, about 60 degrees. In a first printing step I, the surface region 20 is printed with a first part of the transition region 18. After a relative pivoting between the print head 22 and the component 10 by the angle γ, the surface region 16 is printed with a part of the transition region 18 in a second printing step II, wherein the parts of the transition region which are printed in the printing step I and in the printing step II overlap , The pressure intensity, ie the amount of pressure fluid delivered per unit of relative movement, can already be modulated during the printing of the relief-like surface areas 16 and 20 depending on the respective angle of inclination between the surface area and the direction of movement.

Fig. 3 zeigt ein Bauteil 10 mit drei jeweils einen rechten Winkel miteinander bildenden ebenen Oberflächenbereichen, die über gekrümmte Übergangsbereiche miteinander verbunden sind, wobei die Krümmungsradien der Übergangsbereiche gleich oder unterschiedlich sein können. Die zu bedruckende Oberfläche des Bauteils 10 wird in drei Druckschritten I, II und III bedruckt, bei denen das Bauteil 10 zum Druckkopf 22 jeweils um 90 Grad verschwenkt wird. Die Übergangsbereiche werden, wie anhand der Fig. 1 geschildert, bedruckt. Fig. 3 shows a component 10 with three mutually perpendicular to each other forming planar surface areas which are interconnected via curved transition areas, wherein the radii of curvature of the transition regions may be the same or different. The surface to be printed on the component 10 is printed in three printing steps I, II and III, in which the component 10 is pivoted to the print head 22 in each case by 90 degrees. The transition areas are, as based on the Fig. 1 portrayed, printed.

Fig. 4 zeigt ein Bauteil 10, dessen Oberfläche vollständig bedruckt werden soll; dabei entsprechen die Schritte I, II und III der Ausführungsform gemäß Fig. 3. Im Schritt IV, in dem die Unterseite des Bauteils 10 bedruckt werden soll, sind der Druckkopf 22 und das Bauteil 10 derart zueinander verschwenkt, dass die Relativbewegung zwischen Druckkopf 22 und Bauteil 10 parallel zu der Unterseite erfolgt. Fig. 4 shows a component 10 whose surface is to be completely printed; In this case, the steps I, II and III correspond to the embodiment according to FIG Fig. 3 , In step IV, in which the underside of the component 10 is to be printed, the print head 22 and the component 10 are pivoted to each other such that the relative movement between the print head 22 and component 10 is parallel to the bottom.

Bei der Bedruckung der spitzwinkeligen Kante 24 müssen keine besonderen Steuerungsmaßnahmen ergriffen werden, da beispielsweise der Seitenbereich beim Bedrucken der Unterseite abgeschattet ist und umgekehrt die Unterseite beim Bedrucken des Seitenbereiches abgeschattet ist. Beim Bedrucken der stumpfwinkeligen Kante 28 dagegen muss, um Überintensitäten zu vermeiden, die jeweilige Druckintensität in einem kurzen Abstand vor dem Erreichen der Kante bzw. der Begrenzung der jeweiligen Fläche vermindert werden.When printing the acute-angled edge 24, no special control measures need to be taken because, for example, the side area is shaded when printing on the underside and, conversely, the underside is shaded when printing the side area. When printing the obtuse-angled edge 28, on the other hand, in order to avoid over-intensities, the respective pressure intensity must be reduced within a short distance before reaching the edge or the boundary of the respective surface.

Fig. 5 zeigt einen kreisrunden Stab, der vorteilhafter Weise in vier Druckschritten I bis IV bedruckt wird, wobei in jedem der Druckvorgänge zu beiden Endbereichen hin Steuervorgänge durchgeführt werden, wie sie anhand der Fig. 1 für den Übergangsbereich zwischen gemäß Fig. 5 den Druckschritten II und III erläutert wurden. Im Beispiel der Fig. 5 wird beispielsweise die Druckintensität jeweils vermindert, wenn der Neigungswinkel α größer 30° ist und beträgt bei α = 45° Null. Fig. 5 shows a circular bar, which is advantageously printed in four printing steps I to IV, wherein in each of the printing operations to both end regions toward control operations are performed, as shown in the Fig. 1 for the transitional area between Fig. 5 the printing steps II and III have been explained. In the example of Fig. 5 For example, the pressure intensity is reduced in each case when the inclination angle α is greater than 30 ° and is zero at α = 45 °.

Fig. 6 stellt eine Aufsicht auf eine abgewickelte Oberfläche beispielsweise des Bauteils 10 gemäß Fig. 3 bei gleichlanger Ausbildung der Seitenbereiche 20 und 20' dar. Die Bedeutungen von x1, x2 und y1, y2 entsprechen jeweils denen der Fig. 1. Mit den mit x1 und y1 sind diejenigen Oberflächenteile bezeichnet, die im jeweiligen Druckvorgang x und y (es gibt zwei gegeneinander um 180 Grad verdrehte Druckvorgänge y) mit einer Intensität von 100% bedruckt werden, d.h., dass sämtliche Farben, aus denen beispielsweise ein Dekor zusammengesetzt ist, bezogen auf die Relativbewegung in Richtung x oder y zu 100% abgegeben wird. Im Differenzbereich zwischen jeweils x1 und x2 sowie y1 und y2 wird der jeweilige Farbauftrag von 100% auf 0% vermindert, wobei diese Verminderung bezogen auf den Neigungswinkel oder die lineare Relativbewegungsstrecke direkt proportional abnehmend sein kann. Fig. 6 provides a plan view of a developed surface, for example, of the component 10 according to Fig. 3 with the same length formation of the side regions 20 and 20 '. The meanings of x 1 , x 2 and y 1 , y 2 respectively correspond to those of FIG Fig. 1 , With the x 1 and y 1 , those surface parts are designated, which are printed in the respective printing process x and y (there are two mutually rotated by 180 degrees printing operations y) with an intensity of 100%, that is, all the colors of which, for example a decor is composed, based on the relative movement in the direction of x or y is 100% delivered. In the difference range between x 1 and x 2 as well as y 1 and y 2 , the respective ink application is reduced from 100% to 0%, whereby this reduction can be directly proportional decreasing with respect to the inclination angle or the linear relative movement distance.

Fig. 7 bis 9 zeigen Beispiele, entsprechend denen die Druckschritte I und II gemäß Fig. 1 gesteuert werden können. Fig. 7 to 9 show examples according to which the printing steps I and II according to Fig. 1 can be controlled.

Fig. 7 zeigt ein Beispiel, bei dem der Oberflächenteil, der im Schritt I mit abnehmender Intensität bedruckt wird, denjenigen Oberflächenteil vollständig überlappt, der im Schritt II mit voller Intensität bedruckt wird und umgekehrt, der Oberflächenteil, bei dem im Schritt II mit abnehmender Intensität bedruckt wird, den Teil überlappt, der im Schritt I mit voller Intensität bedruckt wird. Fig. 7 shows an example in which the surface part which is printed with decreasing intensity in step I completely overlaps that surface part which is printed in full intensity in step II and vice versa, the surface part which is printed with decreasing intensity in step II, overlaps the part printed in step I with full intensity.

Fig. 8 zeigt einen Fall, bei dem die jeweiligen Oberflächenteile, in denen mit abnehmender Intensität bedruckt wird, sich überlappen, jedoch nicht deckungsgleich sind. Fig. 8 Fig. 14 shows a case where the respective surface portions printed with decreasing intensity overlap but are not congruent.

Fig. 9 zeigt den Fall, bei dem die Oberflächenteile, die jeweils mit abnehmender Intensität bedruckt werden, deckungsgleich sind. Fig. 9 shows the case in which the surface parts, which are each printed with decreasing intensity, are congruent.

Die Figuren gemäß Fig. 7 bis 9 sind für die Oberfläche des Bauteils gemäß Fig. 6 jeweils doppelt vorzustellen, d.h. an die jeweilige der Fig. 7 bis 9 schließt sich die Fig. 6 nach links gespiegelt die gleiche Figur nochmals an.The figures according to Fig. 7 to 9 are for the surface of the component according to Fig. 6 each to be presented twice, ie to the respective Fig. 7 to 9 joins the Fig. 6 to the left mirror the same figure again.

Vorteilhaft ist, wenn mit zunehmendem Umfangswinkel, über den sich der Übergangsbereich 18 erstreckt, die Überlappung im Sinne von Fig. 9 nach Fig. 7 zunimmt.It is advantageous if with increasing circumferential angle over which the transition region 18 extends, the overlap in the sense of Fig. 9 to Fig. 7 increases.

Anhand der Fig. 10 wird im Folgenden unter einer ähnlichen Betrachtung wie in Fig. 1 erläutert, wie sich auf dem Übergangsbereich 18 in den Druckschritten I (Relativbewegung zwischen dem Druckkopf und dem ersten Oberflächenbereich 16 in x-Richtung) und dem Druckschritt II (Relativbewegung zwischen dem Druckkopf und dem zweiten Oberflächenbereich 20 in y-Richtung) eine Druckintensität erzielen lässt, die zu einer konstanten Druckintensität über den gesamten Übergangsbereich 18 führt.Based on Fig. 10 is below under a similar consideration as in Fig. 1 explains how to achieve a print intensity on the transition region 18 in the printing steps I (relative movement between the print head and the first surface region 16 in the x direction) and the printing step II (relative movement between the print head and the second surface region 20 in the y direction) , which leads to a constant pressure intensity over the entire transition region 18.

Die Geometrie des dem Übergangsbereich 18 zu erzeugenden Musters kann in an sich bekannter Weise durch Verzerrung der zur Steuerung verwendeten Musterdaten entsprechend dem Winkel α derart transformiert werden, dass das Muster trotz der linearen Relativbewegung unverzerrt gedruckt wird.The geometry of the pattern to be created in the transition region 18 can be transformed in a manner known per se by distorting the pattern data used for the control according to the angle α such that the pattern is printed undistorted in spite of the linear relative movement.

Für den Druckvorgang I gilt, dass, wenn der Winkel α der Winkel zwischen der Senkrechten durch die Mittelpunktslinie P der Oberfläche des Übergangsbereiches 18 und der Verbindungslinie zwischen der Mittelpunktslinie und der Fußpunktslinie ist, in die eine Senkrechte durch den an der Stelle x befindlichen Druckkopf 22 den Übergangsbereich 18 schneidet, dass ein Flächenbereich f des Übergangsbereiches relativ zu einem Flächenbereich f0 in der Relativbewegungsebene des Druckkopfes 22 um den Betrag 1 cos α

Figure imgb0001
vergrößert ist. Damit die Druckintensität, die nur durch den Druckvorgang I auf dem Übergangsbereich 18 erzeugt wird, konstant bleibt, gilt also: I α = I 0 cos α ,
Figure imgb0002

wobei I0 die auf dem ersten Oberflächenbereich 16 zu erzielende Druckintensität ist, und α der der jeweiligen Stelle des Übergangsbereiches zugehörende Winkel α ist. α kann in einfacher Weise in x umgerechnet werden, da gilt: x = r sin α .
Figure imgb0003
For the printing operation I, when the angle α is the angle between the perpendicular through the center line P of the surface of the transition portion 18 and the connecting line between the center line and the foot-point line into which a vertical intersects the transition region 18 by the print head 22 located at the position x, that a surface area f of the transition region relative to a surface area f 0 in the relative movement plane of the print head 22 by the amount 1 cos α
Figure imgb0001
is enlarged. Thus, the pressure intensity, which is only generated by the printing process I on the transition region 18, remains constant, then applies: I α = I 0 cos α .
Figure imgb0002

where I 0 is the pressure intensity to be achieved on the first surface area 16, and α is the angle α associated with the respective location of the transition area. α can be converted into x in a simple way, since the following applies: x = r sin α ,
Figure imgb0003

Um in dem Winkelbereich von α = 0 bis α1 eine konstante Druckintensität auf dem Übergangsbereich 18 zu erzeugen, muss die Intensität I(α) also entsprechend der oben genannten Beziehung zunehmen.In order to produce a constant pressure intensity on the transition region 18 in the angular range from α = 0 to α 1 , the intensity I (α) must therefore increase in accordance with the above-mentioned relationship.

Wenn derjenige Teil des Übergangsbereiches 18 der im Druckvorgang I und im Druckvorgang II bedruckt wird, zwischen den Winkeln α1 und α2 liegt, muss die Druckintensität zwischen α1 und α2 auf Null abnehmen, also es muss gelten: I α = f α I 0 cos α ,

Figure imgb0004

wobei die vorgenannte Beziehung für α1 < α2 gilt und f(α) eine Funktion ist, die bei α1 den Wert 1 und bei α2 den Wert Null hat.If the part of the transition region 18 which is printed in the printing process I and in the printing process II lies between the angles α 1 and α 2 , the pressure intensity between α 1 and α 2 must decrease to zero, that is to say: I α = f α I 0 cos α .
Figure imgb0004

wherein the aforementioned relationship for α 12 and applies f (α) is a function having the value 1 and α 2 is set to zero at α. 1

Im Druckschritt II gelten die vorgenannten Beziehungen in gleicher Weise, wobei für den Wert α jeweils 90° - α zu setzen ist, d.h., der Kosinus durch den Sinus zu ersetzen ist. Damit in dem Bereich α1 und α2 die Druckintensität bei Überlagerung der Druckschritte I und II konstant bleibt, muss also die folgende Beziehung gelten: f 1 α I 0 cos α + f 2 α I 0 sin α = I 0 ,

Figure imgb0005

wobei f 1 α 1 = f 2 α 2 = 1 ,
Figure imgb0006
f 1 α 1 = f 2 α 2 = 0.
Figure imgb0007

Mit der vorstehenden Beziehung wird erreicht, dass die Druckintensität von α = 0 nach α = 1 (von x0 zu x1) im Druckschritt 1 zunächst proportional zu 1 cos α
Figure imgb0008
zunimmt und dann von x1 zu x21 zu α2) auf Null abnimmt und umgekehrt die Druckintensität im Schritt II zunächst von 90 Grad zu α2 umgekehrt proportional zu sin α zunimmt, um dann von α2 nach α1 auf Null abzunehmen, wobei die Summenintensität, mit der jedes Flächenelement des Übergangsbereiches 18 resultierend aus beiden Druckvorgängen bedruckt wird, konstant gleich I0 ist.In the pressure step II, the aforementioned relationships apply in the same way, wherein 90 ° -α is to be set for the value α, ie, the cosine must be replaced by the sine. In order to In the range α 1 and α 2, the pressure intensity remains constant when superimposing the pressure steps I and II, then the following relationship must apply: f 1 α I 0 cos α + f 2 α I 0 sin α = I 0 .
Figure imgb0005

in which f 1 α 1 = f 2 α 2 = 1 .
Figure imgb0006
f 1 α 1 = f 2 α 2 = 0th
Figure imgb0007

With the above relationship, it is achieved that the pressure intensity from α = 0 to α = 1 (from x 0 to x 1 ) in the pressure step 1 is initially proportional to 1 cos α
Figure imgb0008
increases and then decreases from x 1 to x 21 to α 2 ) to zero and vice versa, the pressure intensity in step II first of 90 degrees to α 2 inversely proportional to sin α increases, then from α 2 to α 1 to zero The sum intensity with which each surface element of the transition region 18 is printed as a result of both printing operations is constantly equal to I 0 .

Mit einer Steuerung gemäß den vorstehenden Beziehungen lässt sich eine konstante Druckintensität über den gekrümmten Übergangsbereich erzielen. Mit einer Steuerung gemäß insbesonders den Fig. 7 bis 9 ist die Intensität annähernd konstant.With a control according to the above relationships, a constant pressure intensity over the curved transition region can be achieved. With a control according to the particular Fig. 7 to 9 the intensity is almost constant.

Fig. 11 zeigt den grundsätzlichen Aufbau bei einer Vorrichtung zum Durchführen des erfindungsgemäßen Verfahrens. Fig. 11 shows the basic structure in an apparatus for performing the method according to the invention.

Der beispielsweise als Balken ausgebildete Druckkopf 22 ist an einer Antriebseinrichtung 30 angebracht, mit der der Druckkopf 22 in Richtung des senkrechten Doppelpfeils W bewegbar ist. Gegenüber dem Druckkopf befindet sich das zu bedruckende Bauteil 10, das von einer Antriebseinrichtung 32 gehalten ist, mittels der es in Richtung des waagerechten Doppelpfeils Z bewegbar und in Richtung des Doppelpfeils R um eine senkrecht auf der Papierebene stehende Achse schwenkbar ist.The printhead 22, which is designed, for example, as a bar, is attached to a drive device 30 with which the print head 22 can be moved in the direction of the vertical double arrow W. Opposite the print head is the component 10 to be printed, which is held by a drive device 32, by means of which it is movable in the direction of the horizontal double arrow Z and in the direction of the double arrow R about an axis perpendicular to the paper plane axis.

Die Position des Bauteils 10 relativ zu einem ortsfesten Bezugspunkt ist mittels einer Sensoreinrichtung 34 erfassbar.The position of the component 10 relative to a stationary reference point can be detected by means of a sensor device 34.

Zur Steuerung der Antriebseinrichtungen 30, 32 und der Farbdüsen des Druckkopfes 22 ist eine elektronische Steuereinrichtung 36 mit einem Bedienfeld 38 und einem Bildschirm 40 vorgesehen. Die elektronische Steuereinrichtung 36 enthält einen Mikroprozessor mit Programm- und Datenspeichern und ist in ihrem Aufbau an sich bekannt und wird daher nicht im Einzelnen erläutert.To control the drive means 30, 32 and the ink nozzles of the print head 22, an electronic control device 36 with a control panel 38 and a screen 40 is provided. The electronic control device 36 includes a microprocessor with program and data storage and is known per se in construction and will therefore not be explained in detail.

Wenn sich der Druckkopf 22 nicht über die gesamte Breite des zu bedruckenden Bauteils 10 erstreckt, kann er mittels der Antriebseinrichtung 30 vorteilhafterweise auch in eine Richtung senkrecht zur Papierebene bewegt werden. Die Antriebseinrichtung 32, mittels der das Bauteil 10 verschwenkbar ist, kann auch derart ausgebildet sein, dass das Bauteil 10 um drei aufeinander senkrecht stehende Raumachsen schwenkbar ist. Die Antriebseinrichtungen 30 und 32 können in unterschiedlichster Weise ausgebildet sein, wobei sichergestellt sein muss, dass zwischen dem Druckkopf 22 und dem Bauteil 10 die zur Durchführung des erfindungsgemäßen Verfahrens notwendigen Relativbewegungen möglich sind.If the print head 22 does not extend over the entire width of the component 10 to be printed, it can advantageously also be moved in a direction perpendicular to the plane of the paper by means of the drive device 30. The drive device 32, by means of which the component 10 can be pivoted, can also be designed such that the component 10 can be pivoted about three mutually perpendicular spatial axes. The drive devices 30 and 32 can be designed in many different ways, wherein it must be ensured that the relative movements necessary for carrying out the method according to the invention are possible between the print head 22 and the component 10.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

1010
Bauteilcomponent
1212
Unterseitebottom
1414
Seitepage
1616
erster Oberflächenbereichfirst surface area
1818
ÜbergangsbereichTransition area
2020
zweiter Oberflächenbereichsecond surface area
2222
Druckkopfprinthead
2424
Kanteedge
2626
Kanteedge
2828
Kanteedge
3030
Antriebseinrichtungdriving means
3232
Antriebseinrichtungdriving means
3434
Sensoreinrichtungsensor device
3636
elektronische Steuereinrichtungelectronic control device
3838
BedienfeldControl panel
4040
Bildschirmscreen

Claims (8)

  1. A method of printing a component (10) using an ink-jet printing process, which component has a first and a second surface region (16,20), which are inclined at an angle to one another and are joined together via a transition region (18), comprising the following steps:
    I) Printing the first surface region (16) and at least one part of the transition region (18) adjoining the first surface region, but not the second surface region (20), during a first linear relative movement between the first surface region and a print head (22) approximately parallel to the first surface region, wherein the print head sprays colouring fluid in a direction approximately perpendicular to an extension direction of the first surface region and perpendicular to the direction of the relative movement,
    II) Printing the second surface region (20) and also at least one part of the transition region (18) adjoining the second surface region, but not the first surface region (16), during a second linear relative movement between the second surface region and a print head (22) approximately parallel to the second surface region, wherein the print head sprays colouring fluid in a direction approximately perpendicular to an extension direction of the second surface region and perpendicular to the direction of the relative movement,
    characterised in that
    the printing fluid emerging from the print head (22) is controlled so that at least the part of the transition region (18), which is inclined to the greatest extent in relation to the direction of the first or second relative movement, is printed only during the step in which it has the smaller inclination in relation to the respective relative movement, and
    the quantity of fluid sprayed per section of the respective relative movement gradually decreases to nil in each one of the steps I) and II) during the printing of one part of the transition region (18), which part is also printed at least partly in the respective other one of the steps I) and II).
  2. A method according to Claim 1, wherein the part of the transition region (18), in which the printing during step I) gradually decreases to nil, is situated outside the part of the transition region in which the printing in step II) gradually decreases to nil.
  3. A method according to Claim 1, wherein the part of the transition region (18), in which the printing during step I) gradually decreases to nil, overlaps the part of the transition region in which the printing in step II) gradually decreases to nil.
  4. A method according to Claim 3, wherein the part of the transition region (18), in which the printing during step I) gradually decreases to nil, coincides with the part of the transition region in which the printing in step II) gradually decreases to nil.
  5. A method according to any one of Claims 1 to 4, wherein the printing is controlled in such a way that the first and the second surface regions (16,20) and also the transition region (18) are printed at equal intensity.
  6. A method according to any one of Claims 1 to 5, wherein the surface regions (16,20) are planar and are directed approximately perpendicularly to one another, and the transition region (18) is a cylinder segment with an angle at circumference of approximately 90 degrees and continuously adjoins the surface regions (16,20).
  7. A method according to any one of Claims 1 to 6, wherein the printing is controlled in such a way that a geometry of patterns printed on the transition region (18) during the steps I) and II) is the same.
  8. An apparatus for printing a component with an ink-jet printing process, which component has a first and a second surface region (16,20), which are inclined at an angle □ to one another and are joined together via a transition region (18), which apparatus comprises:
    at least one print head (22),
    a retaining device (32) for retaining the component (10),
    a conveying device (30,32) for generating a linear relative movement between the component and the print head,
    a device (34 for detecting the angle between the direction of the relative movement and the surface of the transition region (18) and
    a control device (36) which controls the conveying device (30,32), the pivoting device (32) and the print head (22),
    characterised in that the apparatus additionally comprises a pivoting device (32) for pivoting the component relative to the print head about an axis perpendicular to the direction of the relative movement, and in that the control device (36) controls the conveying device (30,32), the pivoting device (36) [sic] and the print head (22) in such a way that the following steps are executed:
    I) Printing the first surface region (16) and at least one part of the transition region (18) adjoining the first surface region, but not the second surface region (20), during a first linear relative movement between the first surface region and a print head (22) approximately parallel to the first surface region, wherein the print head sprays colouring fluid in a direction approximately perpendicular to an extension direction of the first surface region and perpendicular to the direction of the relative movement,
    II) Printing the second surface region (20) and also at least one part of the transition region (18) adjoining the second surface region, but not the first surface region (16), during a second linear relative movement between the second surface region and a print head (22) approximately parallel to the second surface region, wherein the print head sprays colouring fluid in a direction approximately perpendicular to an extension direction of the second surface region and perpendicular to the direction of the relative movement, wherein
    the printing fluid emerging from the print head (22) is controlled so that at least the part of the transition region (18), which is inclined to the greatest extent in relation to the direction of the first or
    second relative movement, is printed only during the step in which it has the smaller inclination in relation to the respective relative movement, and
    the quantity of fluid sprayed per section of the respective relative movement gradually decreases to nil in each one of the steps I) and II) during the printing of one part of the transition region (18), which part is also printed at least partly in the respective other one of the steps I) and II).
EP08008534A 2007-05-09 2008-05-06 Method and device for embossing a component with two mutually inclined surface areas by means of a digital printing process Active EP1990206B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PL08008534T PL1990206T3 (en) 2007-05-09 2008-05-06 Method and device for embossing a component with two mutually inclined surface areas by means of a digital printing process
SI200830414T SI1990206T1 (en) 2007-05-09 2008-05-06 Method and device for embossing a component with two mutually inclined surface areas by means of a digital printing process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102007021767A DE102007021767A1 (en) 2007-05-09 2007-05-09 Method and device for printing a component with two mutually inclined surface areas by means of a digital printing method

Publications (3)

Publication Number Publication Date
EP1990206A2 EP1990206A2 (en) 2008-11-12
EP1990206A3 EP1990206A3 (en) 2010-07-21
EP1990206B1 true EP1990206B1 (en) 2011-07-27

Family

ID=39679381

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08008534A Active EP1990206B1 (en) 2007-05-09 2008-05-06 Method and device for embossing a component with two mutually inclined surface areas by means of a digital printing process

Country Status (8)

Country Link
EP (1) EP1990206B1 (en)
AT (1) ATE517755T1 (en)
DE (1) DE102007021767A1 (en)
DK (1) DK1990206T3 (en)
ES (1) ES2370495T3 (en)
PL (1) PL1990206T3 (en)
PT (1) PT1990206E (en)
SI (1) SI1990206T1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2200478B1 (en) 2007-10-27 2015-09-30 Rehau AG + Co Edge strip for pieces of furniture
EP4052612A1 (en) * 2018-11-06 2022-09-07 Fritz Egger GmbH & Co. OG Edge strip and method for the production thereof
EP3885146B1 (en) * 2020-03-26 2023-12-27 Global Inkjet Systems Limited Stitching methods and systems

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1398100B1 (en) * 2010-02-02 2013-02-07 Palumbo INK JET PRINTING DEVICE AND METHOD, FOR SURFACES WITH SURVEYS OR RECEIVERS
DE102010054578A1 (en) * 2010-12-15 2012-06-21 Erfurt & Sohn Kg Sheets, particularly strips of wall papers, are made of paper, metal or plastic, whose front surface is printed and adjacent and adjoining front sides of longitudinal edges form image or art design
DE102017114280B4 (en) 2017-06-26 2024-04-11 Jörg R. Bauer Method for printing a curved surface and device for printing three-dimensional surfaces
AT520096B1 (en) * 2017-08-14 2019-01-15 Ifn Holding Ag Method for producing a window or door profile
DE102018121570A1 (en) * 2018-09-04 2020-03-05 ISP GmbH & Co. KG Distortion-free coating of vehicle interior surfaces
GB2579050B (en) * 2018-11-16 2021-12-01 Global Inkjet Systems Ltd Control methods and systems
AT521998B1 (en) * 2018-11-23 2021-12-15 Karl Pedross Ag Process for printing elongated profile strips and profile strips

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6460958B2 (en) * 2000-02-29 2002-10-08 Minolta Co., Ltd. Three-dimensional object printing apparatus and method
DE10031030B4 (en) * 2000-06-26 2005-08-04 Bauer, Jörg R. Method and device for producing flat components with a predetermined surface appearance and planar component, in particular front panel of a kitchen element
US7001016B2 (en) * 2002-04-03 2006-02-21 Masonite Corporation Method and apparatus for creating an image on an article and printed article
SE524371C2 (en) * 2002-07-10 2004-08-03 Nolato Ab Method and apparatus for applying a two-dimensional image to a three-dimensional surface
DE10323412B4 (en) * 2003-05-23 2007-07-05 Bauer, Jörg R. Method and device for producing a component having a surface of predetermined appearance

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2200478B1 (en) 2007-10-27 2015-09-30 Rehau AG + Co Edge strip for pieces of furniture
EP4052612A1 (en) * 2018-11-06 2022-09-07 Fritz Egger GmbH & Co. OG Edge strip and method for the production thereof
EP3885146B1 (en) * 2020-03-26 2023-12-27 Global Inkjet Systems Limited Stitching methods and systems

Also Published As

Publication number Publication date
EP1990206A3 (en) 2010-07-21
EP1990206A2 (en) 2008-11-12
SI1990206T1 (en) 2011-12-30
PL1990206T3 (en) 2011-12-30
ATE517755T1 (en) 2011-08-15
DK1990206T3 (en) 2011-10-31
DE102007021767A1 (en) 2008-11-13
ES2370495T3 (en) 2011-12-16
PT1990206E (en) 2011-09-01

Similar Documents

Publication Publication Date Title
EP1990206B1 (en) Method and device for embossing a component with two mutually inclined surface areas by means of a digital printing process
EP3208746B1 (en) Method for inkjet printing of at least one curved area of the surface of an object
EP3002128B1 (en) Method for printing on a curved surface of an object with an ink jet head
DE102007021765B4 (en) Apparatus for simultaneously printing a plurality of identical components by means of a digital printing method
EP2644392B1 (en) System for printing of an object
DE102009021608B4 (en) Device and method for painting curved outer surfaces of an aircraft
EP0429852B1 (en) Printing tower comprising at least two superposed printing units of the &#34;satellite&#34; type
EP3847029B1 (en) Distortion-free coating of vehicle interior surfaces
DE102017114280A1 (en) Method for printing a surface
DE102014221103A1 (en) A method of producing an imprint on an object having a curved surface
DE102005006092A1 (en) Inkjet printer has two print head arrangements to permit printing on non-white media with the ratio of the separation of the nozzles in the two print- heads being a rational number that is greater than one
AT510881A2 (en) THREE-DIMENSIONAL MODELING DEVICE, THREE-DIMENSIONAL MODELING METHOD AND MODEL FORMED BY THE METHOD
DE102010038332B4 (en) Coating process of at least one side surface of a tabular material
WO2020048853A1 (en) Method for distortion-free and homogeneous coating of workpieces having bidirectionally curved surfaces
DE3104077A1 (en) &#34;WRITING HEAD FOR INK JET PRINTER&#34;
EP3875280A1 (en) Method for digitally coating three-dimensional workpiece surfaces
EP3547221B1 (en) Method for printing the surface of an object
EP3656566B1 (en) Method for printing longitudinal profile strips and profile strips
DE102010047924B4 (en) Method for producing a surface formed by a hardening liquid
DE19820149B4 (en) Device for marking large flat surfaces
EP3996926B1 (en) Method for digitally printing a profiled strip
AT520096B1 (en) Method for producing a window or door profile
EP1987923B1 (en) Layer with limited air permeability for a device for positioning workpieces
EP4272969A1 (en) Device for finishing a workpiece surface with pivoting print head

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

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: INTERGLARION LIMITED

RIN1 Information on inventor provided before grant (corrected)

Inventor name: INTERGLARION LIMITED

RIN1 Information on inventor provided before grant (corrected)

Inventor name: DER ERFINDER HAT AUF SEINE NENNUNG VERZICHTET.

RIN1 Information on inventor provided before grant (corrected)

Inventor name: DER ERFINDER HAT AUF SEINE NENNUNG VERZICHTET.

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

17P Request for examination filed

Effective date: 20101116

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

RIC1 Information provided on ipc code assigned before grant

Ipc: B41J 3/407 20060101AFI20110131BHEP

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK 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

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: BOHEST AG

REG Reference to a national code

Ref country code: PT

Ref legal event code: SC4A

Free format text: AVAILABILITY OF NATIONAL TRANSLATION

Effective date: 20110825

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502008004309

Country of ref document: DE

Effective date: 20110915

REG Reference to a national code

Ref country code: NL

Ref legal event code: T3

REG Reference to a national code

Ref country code: RO

Ref legal event code: EPE

REG Reference to a national code

Ref country code: DK

Ref legal event code: T3

REG Reference to a national code

Ref country code: SK

Ref legal event code: T3

Ref document number: E 10207

Country of ref document: SK

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2370495

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20111216

REG Reference to a national code

Ref country code: PL

Ref legal event code: T3

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

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: 20111027

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: 20111127

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: 20110727

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: 20110727

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: 20110727

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: 20110727

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

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: 20110727

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: 20110727

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110727

REG Reference to a national code

Ref country code: HU

Ref legal event code: AG4A

Ref document number: E012476

Country of ref document: HU

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: 20110727

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

26N No opposition filed

Effective date: 20120502

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502008004309

Country of ref document: DE

Effective date: 20120502

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120531

REG Reference to a national code

Ref country code: DK

Ref legal event code: EBP

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120507

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120531

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: 20111027

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

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: 20110727

REG Reference to a national code

Ref country code: CH

Ref legal event code: PCAR

Free format text: NEW ADDRESS: HOLBEINSTRASSE 36-38, 4051 BASEL (CH)

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

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: 20110727

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 8

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 9

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: LU

Payment date: 20230519

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: RO

Payment date: 20230411

Year of fee payment: 16

Ref country code: PT

Payment date: 20230427

Year of fee payment: 16

Ref country code: NL

Payment date: 20230519

Year of fee payment: 16

Ref country code: IT

Payment date: 20230526

Year of fee payment: 16

Ref country code: FR

Payment date: 20230525

Year of fee payment: 16

Ref country code: DE

Payment date: 20230428

Year of fee payment: 16

Ref country code: CZ

Payment date: 20230502

Year of fee payment: 16

Ref country code: CH

Payment date: 20230602

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: TR

Payment date: 20230504

Year of fee payment: 16

Ref country code: SK

Payment date: 20230504

Year of fee payment: 16

Ref country code: SI

Payment date: 20230427

Year of fee payment: 16

Ref country code: PL

Payment date: 20230428

Year of fee payment: 16

Ref country code: AT

Payment date: 20230522

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 20230519

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20230523

Year of fee payment: 16

Ref country code: ES

Payment date: 20230724

Year of fee payment: 16