EP2151324B1 - Method for producing a rotative printing plate for insertion in a roller rotation printing method - Google Patents

Method for producing a rotative printing plate for insertion in a roller rotation printing method Download PDF

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Publication number
EP2151324B1
EP2151324B1 EP09009725.4A EP09009725A EP2151324B1 EP 2151324 B1 EP2151324 B1 EP 2151324B1 EP 09009725 A EP09009725 A EP 09009725A EP 2151324 B1 EP2151324 B1 EP 2151324B1
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Prior art keywords
layer
composite
composite material
cylinder
composite layer
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EP09009725.4A
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German (de)
French (fr)
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EP2151324A3 (en
EP2151324A2 (en
Inventor
Yvonne Bohne
Christian Dr. Elsner
Bernd Prof. Dr. Rauschenbach
Claudia Dr Jahn
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Prinovis Dresden & Co KG GmbH
Leibniz Institut fuer Oberflachenmodifizierung eV
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Prinovis Dresden & Co KG GmbH
Leibniz Institut fuer Oberflachenmodifizierung eV
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Priority to PL09009725T priority Critical patent/PL2151324T3/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B41PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
    • B41CPROCESSES FOR THE MANUFACTURE OR REPRODUCTION OF PRINTING SURFACES
    • B41C1/00Forme preparation
    • B41C1/02Engraving; Heads therefor
    • B41C1/04Engraving; Heads therefor using heads controlled by an electric information signal
    • B41C1/05Heat-generating engraving heads, e.g. laser beam, electron beam
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B41PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
    • B41CPROCESSES FOR THE MANUFACTURE OR REPRODUCTION OF PRINTING SURFACES
    • B41C1/00Forme preparation
    • B41C1/18Curved printing formes or printing cylinders
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B41PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
    • B41NPRINTING PLATES OR FOILS; MATERIALS FOR SURFACES USED IN PRINTING MACHINES FOR PRINTING, INKING, DAMPING, OR THE LIKE; PREPARING SUCH SURFACES FOR USE AND CONSERVING THEM
    • B41N1/00Printing plates or foils; Materials therefor
    • B41N1/16Curved printing plates, especially cylinders
    • B41N1/22Curved printing plates, especially cylinders made of other substances

Definitions

  • the invention relates to a method for erasing and re-imaging a rotary printing form for use in a web-fed rotary printing process with the method steps of claim 1.
  • Rotogravure in contrast to other printing processes such as flat, screen, digital or screen printing, is suitable for the production of predominantly high-stock products.
  • Characteristic of rotogravure printing is that the individual dots of the printed image lie deepened in the surface of the plate cylinder. They are referred to as cups and result from the print image transfer by means of engraving or etching. During the printing process, depending on their volume, they take up the appropriate amount of printing ink and apply it punctiform to the substrate.
  • the already engraved engraved copper layer is additionally provided with a hard chrome plating, to which galvanic application methods are used.
  • Such "classic" metal coated rotary printing plates may be reused after printing by removing the thin copper coating to the surface of the steel cylinder.
  • a disadvantage of these classic metal-coated rotary printing plates is in particular that on the one hand a large number of process steps with high time and cost and on the other environmentally polluting galvanic coating steps are required.
  • a method and apparatus for gravure printing by means of a erasable and reusable gravure printing form are known.
  • the gravure printing forms shown there are formed as a solid cylinder, as a tubular or thin-walled sleeve on which a basic grid is engraved analogously to a conventional gravure mold in copper.
  • a layer of chromium and then a hard coating such as diamond-like carbon, titanium nitride or tungsten carbide applied.
  • anilox rollers which carry thermally sprayed ceramic coatings, in which a gravure gravure grid is engraved by means of laser.
  • the imaging is carried out by thermal ablation by means of a pixel transfer device by imagewise removing filler material from the depressions.
  • the known gravure form passes through an erasing process in which the filler material and residual ink from the printing process are completely or partially removed by means of laser. Subsequently, the basic grid of the gravure mold can be refilled again, whereby it is prepared for the imaging with a new print job.
  • EP 1 410 924 A1 a manufacturing method for a gravure printing is known in which only a wear-resistant layer is applied according to the desired application to the cylindrical printing plate.
  • This wear-resistant layer forms the engraving surface of the printing form and may consist of a hard material, composite material or metal. Different coating methods are mentioned. Cups for receiving the ink are formed by mechanical engraving, laser engraving or etching. For reuse, it is intended to remove the imaged wear-resistant layer chemically, electrochemically or mechanically after the printing process.
  • DE 31 09 096 A1 teaches a gravure mold with a closed plastic surface, wherein as plastic, for example, epoxy resins and as filler material of the plastic is used carbon black.
  • DE-A1-101 15 434 describes prepolymer and anilox filler for depth-variable laser ablation.
  • the present invention seeks to provide a method for erasing and re-imaging a rotary printing form or a gravure cylinder or a gravure printing form, in which a cell structure can be deleted very quickly.
  • a composite material curing by polymerization after the coating process comprising at least one organic binder with nano- and / or microparticles contained therein is applied as the coating material.
  • the image information-bearing cell structure can be generated by laser engraving and after the printing process, the cell structure is leveled by a re-coating process with said composite and thus available for re-imaging.
  • the wells formed with laser beams are significantly contour sharper than in the prior art and thus suitable to ensure a much better, print result.
  • the material is sufficiently hard, tensile and compressive strength, elongation at break, modulus of elasticity and wear resistance are suitable to withstand the high mechanical stresses associated with a high speed web-fed rotary printing process. Also the heat resistance is sufficient for such loads.
  • the claimed composite layer advantageously has a low coefficient of expansion, which has an advantageous effect on its bonding to the substrate.
  • the radiation-curable micro- or nanoparticles have an advantageous effect in terms of abrasion resistance of the composite material.
  • optical and thermal absorption, dissipation and / or emission properties of such a layer can be advantageously influenced by the embedding of micro- or nanoparticles, i. H.
  • the above-mentioned flow processes and smearing effects, which usually occur during laser engraving of other plastic layers, are so greatly reduced that the lasered cell structure is made much sharper than is possible with other known plastic coatings.
  • the composite layers mentioned are not only advantageous with regard to cup formation by means of a laser, they also have other advantages with respect to deletion of the cup structure.
  • the layers are easy to recoat, d. H. a deletion process can be performed without having to completely detach a composite layer from its backing.
  • Existing structures can be erased by "over-lasers" and the surface re-coated in the required layer thickness with composite material.
  • the composite filling the cells of the structuring can be exposed by laser radiation and then completely refilled. This will “delete” the structure and provide it for refining after refilling. Both the "over-lasing" of existing structures, as well as the exposure and subsequent refilling can only on sections of the molding Thus, it is possible to delete a printing cylinder only partially or to provide new image information.
  • the composite material in principle, it is also possible to coat the composite material with a non-metallic barrier layer after imaging, which has a greater hardness and / or a greater solvent resistance than the coating material itself.
  • a non-metallic barrier layer after imaging, which has a greater hardness and / or a greater solvent resistance than the coating material itself.
  • the durability of the barrier layer on the surface of the composite layer is improved by the microparticles and nanoparticles.
  • the barrier layer comprises silazane or SiOx compounds.
  • the provision of carbon and / or nitrogen atoms in the barrier layer has also proved to be advantageous.
  • Claim 4 deals with the curing of the composite layer.
  • the cylinder jacket surface can be provided in a conventional manner with a basic structure.
  • Such a ballard skin together with the composite layer applied to it, can be detached from the base cylinder without negatively affecting the structure of the base cylinder.
  • a ballard skin is produced by electroplating on so-called ground copper an approximately 0.1 mm thick copper skin, which can be provided with a surface structure. After the print run, the ballard skin can be removed from the printing cylinder.
  • Ballardhaut can also be a non-metallic intermediate layer, for.
  • a primer fulfill the detachment function.
  • the layer thickness of the composite layer can be between 15 and 150 ⁇ m.
  • the laser engraving ie the embossing of wells by means of laser radiation, can be carried out particularly well with pulsed lasers.
  • the depth and shape of the wells in the composite layer can be adjusted by the number of pulses per spot and the energy deposited by the laser beam.
  • the Composite layer compared to other plastic coatings has far more favorable, optical and thermal absorption properties, can be engraved by laser entry arbitrary cup shapes, such as square, triangular, round.
  • different depth profiles on a basic shaped body can be generated, for. B. in step shape, in the form of a Gaussian curve or wedge-shaped.
  • the Be firmungsablauf the layer can be done either locally individually or by a raster method.
  • the laser beams can be directed via scanners or multiple axis systems onto the composite layer to be imaged.
  • the cup shape can advantageously take place via beam shaping of the laser beam.
  • beam shaping can be realized by diaphragms, masks and / or other optical elements.
  • Such a laser-registered structuring can be erased by laser ablation and the composite layer, which is then thinned in the ablated areas, re-coated, whereby coating material can be saved.
  • the refilling of the partially removed wells leads to a closed composite surface layer.
  • the time saving achievable in this case represents a significant advantage of the method according to the invention.
  • an applied composite layer Before being imaged by laser engraving, an applied composite layer can be smoothed mechanically or also by laser action, which leads to a further improvement of the printing result.
  • the imageable surface formed by a composite layer has, as a first component, the following compounds: acrylates of radically UV-curing systems, cycloaliphatic epoxides, aliphatic epoxides and compounds of cationically UV-curing systems.
  • Such compounds for the composite layer lead to particularly advantageous laser engraving results with highly definable cup shape.
  • the composite layer comprises several multifunctional radiation curing crosslinkable monomers, oligomers or polymers which may comprise orthogonal functional groups.
  • the particles of the nanocomposite layer are micro- or nanoscale metal or semimetal oxides or oxides of transition metals or mixed oxides in powder form or organometallic particles. Compounds of Al 2 O 3 , SiO 2 , ZrO 2 , TiO 2 have proved to be particularly advantageous for the nanocomposite layer.
  • the compounds of the composite layer may be provided with an organophilic envelope.
  • the layer thickness of the composite layer can be between one nanometer as the theoretical lower limit and one millimeter.
  • the hardness of the composite layer should be greater than 200 N / mm 2 (Marten hardness).
  • the cup structure of the composite layer should be chosen so that the depth of the wells is less than the thickness of the composite layer.
  • the composite layer may carry a quenching layer that completely overlaps the wells.
  • rotary printing plate 1 consists essentially of a cylindrical mold base body with structuring 2 and a non-metallic coating material, which can be applied to the surface, that is, the cylinder surface 4 of the mold body 2.
  • the coating material is according to Fig. 2 from a composite material 3 and thus forms a composite layer 33.
  • the composite material 3 comprises an acrylate-based matrix 5 and substantially uniformly distributed nanoparticles 6, which - as in Fig. 2 shown schematically - can have different shapes and sizes.
  • a non-metallic barrier layer 8 is applied, which has a greater hardness than the composite material 3.
  • a laser engraving method is used.
  • the cell structure 9 can be seen in drawing figure 2.
  • the surface 4 of the molded basic body 2 can be provided with a basic structure 20 on which a ballard skin 21 is applied, which ultimately carries the composite layer 33.
  • a ballard skin 21 prior to application of the composite layer 33 is merely an option intended to facilitate the complete detachment of a coating from the mold base body 2.
  • ballast skin 21 applied to the mold base body 2 may be provided with a structuring.
  • the composite layer 33 is arranged without ballard skin directly on the mold base body 2.
  • the cylinder jacket surface 4 is provided with a z. B. web-like basic structure 20, which increases the contact area.
  • the cell structure 9 can have different shapes, depths and / or dimensions.
  • the composite layer 33 can be formed from a coating material 3 which can comprise a very wide variety of chemical compositions.
  • the compositions can be selected by the person skilled in the art within the stated ranges in such a way that a scratch-resistant, abrasion-resistant and solvent-resistant coating is formed, which, as far as the core idea of the invention is concerned, ensures virtually residue-free laser engravability.

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  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Plasma & Fusion (AREA)
  • Printing Plates And Materials Therefor (AREA)
  • Manufacture Or Reproduction Of Printing Formes (AREA)

Description

Die Erfindung betrifft ein Verfahren zum Löschen und Neubebildern einer rotativen Druckform zum Einsatz in einem Rollenrotationsdruckverfahren mit den Verfahrensschritten des Patentanspruches 1.The invention relates to a method for erasing and re-imaging a rotary printing form for use in a web-fed rotary printing process with the method steps of claim 1.

Der Rotationstiefdruck ist im Gegensatz zu anderen Druckverfahren wie Flach-, Hoch-, Digital- oder Siebdruck zur Herstellung vorwiegend auflagenstarker Produkte geeignet. Kennzeichnend für den Rotationstiefdruck ist, dass die einzelnen Punkte des Druckbildes vertieft in der Oberfläche des Druckformzylinders liegen. Sie werden als Näpfchen bezeichnet und resultieren aus der Druckbildübertragung mittels Gravur oder Ätzung. Beim Druckvorgang nehmen sie, abhängig von ihrem Volumen, die entsprechende Menge an Druckfarbe auf und geben sie punktförmig an den Bedruckstoff ab.Rotogravure, in contrast to other printing processes such as flat, screen, digital or screen printing, is suitable for the production of predominantly high-stock products. Characteristic of rotogravure printing is that the individual dots of the printed image lie deepened in the surface of the plate cylinder. They are referred to as cups and result from the print image transfer by means of engraving or etching. During the printing process, depending on their volume, they take up the appropriate amount of printing ink and apply it punctiform to the substrate.

Beim Druck von Zeitschriften und Katalogen (Illustrationstiefdruck) kommt erschwerend hinzu, dass die Zeit zwischen Dateieingang und Fertigstellung der Druckform und letztendlich der Auslieferung des Druckproduktes eine entscheidende Rolle spielt. Die Papierbahngeschwindigkeit ist mit > 15 m/s sehr hoch und die bei Bahnbreiten bis 4.32 m übertragenen Farbmengen sehr groß. Um diese schnell genug trocknen zu können, wird lösemittelhaltige Farbe eingesetzt.When printing magazines and catalogs (illustration gravure printing) is made more aggravating that the time between file entry and completion of the printing form and ultimately the delivery of the printed product plays a crucial role. The paper web speed is very high at> 15 m / s and the quantities of ink transferred at web widths of up to 4.32 m are very large. To dry them fast enough, solvent-based paint is used.

In der Praxis kommen dafür unterschiedliche Verfahren zur Herstellung dieser Näpfchen und unterschiedliche Materialien, in welches die Näpfchen eingebracht werden, zur Anwendung.In practice, different methods for producing these wells and different materials, in which the wells are introduced, are used.

Als grundlegender Stand der Technik sind seit vielen Jahren Tiefdruckformen bekannt, die aus einem Stahlzylinder mit einer Kupfergrundbeschichtung bestehen. Auf diese Kupfergrundbeschichtung wird eine weitere Kupferschicht als Gravurkupferschicht aufgalvanisiert, die eine Schichtstärke von ca. 0,5 mm aufweist. Diese Gravurkupferschicht wird oberflächenbearbeitet und anschließend graviert, um in sie ein Druck- oder Schriftbild in Form von Näpfchen einzuprägen.As a basic state of the art gravure printing is known for many years, which consist of a steel cylinder with a copper base coat. On top of this copper base coat, another copper layer is electroplated as an engraving copper layer, which has a layer thickness of approximately 0.5 mm. This engraved copper layer is surface-treated and then engraved to impress in it a print or typeface in the form of wells.

Zur Verbesserung der Verschleißfestigkeit wird die bereits gravierte Gravurkupferschicht zusätzlich mit einer Hartverchromung versehen, wozu galvanische Auftragsmethoden verwendet werden.To improve the wear resistance, the already engraved engraved copper layer is additionally provided with a hard chrome plating, to which galvanic application methods are used.

Derartige "klassische" rotative Druckformen mit Metallbeschichtung können nach dem Druck durch Entfernen der dünnen Kupferbeschichtung bis auf die Oberfläche des Stahlzylinders erneut verwendet werden.Such "classic" metal coated rotary printing plates may be reused after printing by removing the thin copper coating to the surface of the steel cylinder.

Nachteilig an diesen klassischen metallbeschichteten rotativen Druckformen ist insbesondere, dass zum einen eine Vielzahl von Verfahrensschritten mit hohem Zeit- und Kostenaufwand und zum anderen umweltbelastende galvanische Beschichtungsschritte erforderlich sind.A disadvantage of these classic metal-coated rotary printing plates is in particular that on the one hand a large number of process steps with high time and cost and on the other environmentally polluting galvanic coating steps are required.

Als weiterer Stand der Technik sind bereits Verfahren zur Herstellung lösch- und wieder verwendbarer Tiefdruckformen bekannt, die sich in der Patentliteratur wie folgt darstellen:
Beispielsweise beschreibt WO 02/40272 A1 ein Verfahren zur Herstellung von Rasternäpfchen in vorzugsweise rotationssymmetrische Grundkörper mittels zeitlich modulierter, insbesondere gepulster Laserstrahlung. Über den für die Informationseinprägung vorgesehenen Oberschichtbereich wird eine Abtragsunterstützungsschicht aufgebracht, durch die hindurch Rasternäpfchen mittels Laserstrahlung in die Oberschichtbereiche durch Materialablation eingebracht werden. Anschließend wird diese Abtragsunterstützungsschicht mit dem Ziel entfernt, gratfreie Rasternäpfchen zu erhalten.
As a further prior art, processes for the production of erasable and reusable intaglio printing plates are already known, which are represented in the patent literature as follows:
For example, describes WO 02/40272 A1 a method for the production of screening cups in preferably rotationally symmetrical basic body by means of time-modulated, in particular pulsed laser radiation. An ablation support layer is applied over the upper layer area provided for the information embossing, through which sieve cups are introduced by means of laser radiation into the upper layer areas by material ablation. Subsequently, this erosion assist layer is removed with the aim of obtaining burr-free screen wells.

Ein in EP 1568490 A1 beschriebenes, hochauflösendes Direktlaserverfahren von Chrom- bzw. Kupferzylindern erzielt im Vergleich zur herkömmlichen elektromechanischen oder Laser-Gravur deutlich höhere Näpfchenauflösungen und damit feinere Konturen im Druckbild. Nachteilig ist allerdings die erheblich verlängerte Gravurzeit bei nicht verringerten Herstellungskosten der Zylinder.An in EP 1568490 A1 described, high-resolution direct laser process of chrome or copper cylinders achieved in comparison to conventional electromechanical or laser engraving significantly higher cell resolutions and thus finer contours in the printed image. However, a disadvantage is the significantly extended engraving time at not reduced manufacturing costs of the cylinder.

Aus DE 10 2005 052 156 A1 sind ein Verfahren und eine Vorrichtung für den Tiefdruck mittels einer lösch- und wieder verwendbaren Tiefdruckform bekannt. Die dort dargestellten Tiefdruckformen sind als Vollzylinder, als rohr- oder dünnwandiges Sleeve ausgebildet, auf die ein Grundraster analog zu einer konventionellen Tiefdruckform in Kupfer graviert wird. Zur Erhöhung der Haltbarkeit wird auf die mit dem Grundraster gravierte Schicht zunächst eine Chromschicht und anschließend eine Hartbeschichtung wie z. B. diamantähnlicher Kohlenstoff, Titannitrid oder Wolframcarbid aufgebracht.Out DE 10 2005 052 156 A1 For example, a method and apparatus for gravure printing by means of a erasable and reusable gravure printing form are known. The gravure printing forms shown there are formed as a solid cylinder, as a tubular or thin-walled sleeve on which a basic grid is engraved analogously to a conventional gravure mold in copper. To increase the durability is on the engraved with the basic layer first a layer of chromium and then a hard coating such. As diamond-like carbon, titanium nitride or tungsten carbide applied.

Außerdem sind Rasterwalzen beschrieben, die thermisch gespritzte Keramikbeschichtungen tragen, in die mittels Laser ein Tiefdruckgrundraster eingraviert wird.In addition, anilox rollers are described which carry thermally sprayed ceramic coatings, in which a gravure gravure grid is engraved by means of laser.

Aus dieser Druckschrift ist bekannt, dass zur Erhöhung der Abriebfestigkeit dem Füllmaterial Hartstoffpulver mit, einer Korngröße von kleiner als 1 µm, beizumengen ist.From this document it is known that to increase the abrasion resistance of the filler hard powder with, a particle size of less than 1 micron, is to be added.

Die Bebilderung erfolgt durch thermische Ablation mittels einer Bildpunkt-Übertragungseinrichtung, indem aus den Vertiefungen bildmäßig Füllmaterial abgetragen wird.The imaging is carried out by thermal ablation by means of a pixel transfer device by imagewise removing filler material from the depressions.

Nach dem Druckprozess durchläuft die bekannte Tiefdruckform einen Löschvorgang, in dem das Füllmaterial sowie Restfarbe aus dem Druckvorgang ganz oder teilweise mittels Laser entfernt werden. Anschließend kann das Grundraster der Tiefdruckform wieder neu befüllt werden, wodurch es für die Bebilderung mit einem neuen Druckauftrag vorbereitet ist.After the printing process, the known gravure form passes through an erasing process in which the filler material and residual ink from the printing process are completely or partially removed by means of laser. Subsequently, the basic grid of the gravure mold can be refilled again, whereby it is prepared for the imaging with a new print job.

Aus DE 10 2005 052 157 A1 ist eine Vorrichtung und ein Verfahren zur Bebilderung einer lösch- und wieder verwendbaren Tiefdruckform bekannt, wozu mehrere Laserstrahlen eingesetzt werden, die aus einem oder mehreren Laser stammen können.Out DE 10 2005 052 157 A1 For example, an apparatus and method for imaging a erasable and reusable gravure printing form is known, using a plurality of laser beams that may be derived from one or more lasers.

Aus EP 1 410 924 A1 ist ein Herstellungsverfahren für eine Tiefdruckform bekannt, bei dem nur eine verschleißfeste Schicht entsprechend der gewünschten Anwendung auf die zylindrische Druckform aufgebracht wird. Diese verschleißfeste Schicht bildet die Gravieroberfläche der Druckform und kann aus einem Hartstoff, Verbundwerkstoff oder Metall bestehen. Unterschiedliche Beschichtungsverfahren sind genannt. Näpfchen zur Aufnahme der Druckfarbe werden durch mechanische Gravur, Lasergravur oder Ätzverfahren ausgebildet. Zur Wiederverwendung ist vorgesehen, nach dem Druckvorgang die bebilderte verschleißfeste Schicht chemisch, elektrochemisch oder mechanisch zu entfernen.Out EP 1 410 924 A1 a manufacturing method for a gravure printing is known in which only a wear-resistant layer is applied according to the desired application to the cylindrical printing plate. This wear-resistant layer forms the engraving surface of the printing form and may consist of a hard material, composite material or metal. Different coating methods are mentioned. Cups for receiving the ink are formed by mechanical engraving, laser engraving or etching. For reuse, it is intended to remove the imaged wear-resistant layer chemically, electrochemically or mechanically after the printing process.

Aus DE 101 26 264 A1 sind ein Tiefdruckzylinder, ein Verfahren zum Herstellen eines Tiefdruckzylinders und Verfahren zum Recyceln eines Tiefdruckzylinders bekannt, wobei im Detail ein Tiefdruckzylinder beschrieben ist, bei dem auf einem mit einer Hilfsschicht versehenen Stahlzylinder eine Keramikbeschichtung mittels einem Plasmasprühverfahren aufgetragen wird. Zum "Löschen" des Tiefdruckzylinders nach dem Druckprozess ist eine Recyclingbehandlung vorgesehen, in welcher der bebilderte Zylinder abgeschliffen wird. Dadurch entsteht ein gebrauchter wieder verwendbarer Zylinderrohling.Out DE 101 26 264 A1 are known a gravure cylinder, a method for producing a gravure cylinder and method for recycling a gravure cylinder, wherein a gravure cylinder is described in detail, wherein on a provided with an auxiliary layer steel cylinder, a ceramic coating is applied by means of a plasma spraying. To "erase" the gravure cylinder after the printing process, a recycling treatment is provided in which the imaged cylinder is abraded. This creates a used reusable cylinder blank.

Aus der gattungsbildenden EP 584 857 A2 ist ein Tiefdruckzylinder bestehend aus einem Stahlzylinder mit einem das einzugravierende Druckbild tragenden Überzug bekannt. Zur Erhöhung der Standzeit des Überzugs besteht dieser aus Polyamid, wobei die Standzeit durch Zugabe von Pigmenten im Sub-µm-Bereich erhöht werden kann.From the generic EP 584 857 A2 is a gravure cylinder consisting of a steel cylinder with a the engraving image bearing coating known. To increase the service life of the coating consists of polyamide, the service life can be increased by the addition of pigments in the sub-micron range.

Generell ist zu den vorbezeichneten Quellen im Stand der Technik festzustellen, dass die dort vorgeschlagenen Polymerwerkstoffe, thermoplastische Kunststoffe, Harze, Wachse usw. den wesentlichen Anforderungen eines rotativen Tiefdruckverfahrens nicht genügen. Insbesondere sind sie nicht ausreichend toluolbeständig sowie nicht ausreichend verschleißresitent. Hinsichtlich der Qualität der Lasergravur ist festzustellen, dass es im Fokus des gravierenden Laserstrahls zu Fließerscheinungen des Materials im Näpfchen und damit zu Konturenschärfen kommt.In general, it must be stated with regard to the aforementioned sources in the prior art that the polymer materials, thermoplastics, resins, waxes, etc. proposed there do not meet the essential requirements of a rotary gravure printing process. In particular, they are not sufficiently resistant to toluene and not sufficiently resistant to wear. With regard to the quality of the laser engraving, it should be noted that the focus of the gravitational laser beam leads to flow phenomena of the material in the well and thus to contour sharpening.

JP 2000-015770 A lehrt das Löschen und Neubebildern von Tiefdruckzylindern durch Abtragen, Neuauftragen und Lasergravur einer Kunststoffschicht, wobei der zylindrische Formkörper kein vorgeformtes Näpfchenraster besitzt. JP 2000-015770 A teaches the erasing and re-imaging of gravure cylinders by ablation, reapplication and laser engraving of a plastic layer, wherein the cylindrical body does not have a preformed cell pattern.

DE 31 09 096 A1 lehrt eine Tiefdruckform mit einer geschlossenen Kunststoffoberfläche, wobei als Kunststoff beispielsweise Epoxy-Harze und als Füllmaterial des Kunststoffs Ruß verwendet wird. DE 31 09 096 A1 teaches a gravure mold with a closed plastic surface, wherein as plastic, for example, epoxy resins and as filler material of the plastic is used carbon black.

DE 196 31 469 C1 lehrt das teilweise Löschen löschbarer Druckformen für Tiefdruckverfahren, wobei die löschbare Tiefdruckform eine geschlossene Oberfläche aufweist. Die Löschung erfolgt derart teilweise, dass sie flächenabschnittsweise erfolgt. DE 196 31 469 C1 teaches the partial erasure of erasable printing forms for gravure printing processes, the erasable gravure printing form having a closed surface. The deletion is done partially so that it is area by area.

DE-A1-101 15 434 beschreibt Präpolymer und Rasterwalzen-Füllmaterial für tiefenvariable Laserablation. DE-A1-101 15 434 describes prepolymer and anilox filler for depth-variable laser ablation.

Ausgehend von diesem Stand der Technik liegt der Erfindung die Aufgabe zugrunde, ein Verfahren zum Löschen und Neubebildern einer rotativen Druckform bzw. eines Tiefdruckzylinders oder einer Tiefdruckform anzugeben, bei dem eine Näpfchenstruktur besonders schnell gelöscht werden kann.Based on this prior art, the present invention seeks to provide a method for erasing and re-imaging a rotary printing form or a gravure cylinder or a gravure printing form, in which a cell structure can be deleted very quickly.

Diese Aufgabe wird durch die Merkmale des Verfahrensanspruches 1 gelöst. Vorteilhafte Weiterbildungen der Erfindung ergeben sich aus den Unteransprüchen.This object is achieved by the features of method claim 1. Advantageous developments of the invention will become apparent from the dependent claims.

Als Kern der Erfindung wird es angesehen, dass als Beschichtungsmaterial ein nach dem Beschichtungsvorgang durch Polymerisation aushärtendes Kompositmaterial umfassend wenigstens ein organisches Bindemittel mit darin enthaltenen Nano- und/oder Mikroteilchen aufgebracht wird.It is regarded as the core of the invention that a composite material curing by polymerization after the coating process comprising at least one organic binder with nano- and / or microparticles contained therein is applied as the coating material.

Dadurch ist es möglich, in einer einzigen Technologiesequenz ein strahlenhärtbares Kompositmaterial auf die Zylinderoberfläche des Formgrundkörpers aufzubringen, das dort ausgehärtet werden kann, die bildinformationstragende Näpfchenstruktur über Lasergravur generiert werden kann und nach dem Druckprozess die Näpfchenstruktur über einen erneuten Beschichtungsprozess mit dem genannten Komposit eingeebnet wird und somit für eine erneute Bebilderung zur Verfügung steht.This makes it possible to apply a radiation-curable composite material in a single technology sequence on the cylinder surface of the mold body, which can be cured there, the image information-bearing cell structure can be generated by laser engraving and after the printing process, the cell structure is leveled by a re-coating process with said composite and thus available for re-imaging.

Es hat sich gezeigt, dass durch die Kombination einer Matrix auf Acrylatbasis und darin enthaltenen Nanoteilchen die Lasergravierbarkeit der gebildeten Oberfläche deutlich verbessert ist. Bei bekannten nichtmetallischen Beschichtungsmaterialien treten bei der Lasergravur regelmäßig erhebliche Schwierigkeiten auf, der auftreffende Laserstrahl führt zu thermisch bedingten Fließvorgängen im Umfeld des Strahls, so dass durch den Laserstrahl keine ausreichend scharfen Näpfchenstrukturen ausgebildet werden können. Die beim Stand der Technik entstehenden Näpfchen sind in der Regel von einem Kraterrand umgeben, der zu einer deutlichen Verschlechterung der Bildqualität des Druckproduktes führt. Die in Anspruch 1 als Kennzeichen formulierte Kombination von Mikro- bzw. Nanoteilchen, eingebettet in einem Kompositmaterial, wie einer Polymermatrix, z. B. einem Polyacrylat, vermeidet derartige negative Fließerscheinungen. Die mit Laserstrahlen ausgebildeten Näpfchen sind deutlich konturschärfer als beim Stand der Technik und mithin geeignet, ein weit besseres, Druckergebnis zu gewährleisten. Darüber hinaus ist das Material ausreichend hart, Zug- und Druckfestigkeit, Bruchdehnung, Elastizitätsmodul und Verschleißfestigkeit sind geeignet, um den hohen mechanischen Belastungen bei einem mit hoher Geschwindigkeit ablaufenden Rollenrotationsdruckprozess zu widerstehen. Auch die Wärmeformbeständigkeit ist ausreichend für derartige Belastungen. In thermischer Hinsicht hat die beanspruchte Kompositschicht in vorteilhafter Weise einen geringen Ausdehnungskoeffizienten, was sich vorteilhaft auf ihren Verbund mit der Unterlage auswirkt. Zudem wirken die strahlenhärtbaren Mikro- oder Nanoteilchen vorteilhaft im Sinne einer Abriebfestigkeit des Kompositmaterials.It has been found that the combination of an acrylate-based matrix and nanoparticles contained therein significantly improves the laser engravability of the surface formed. In the case of known non-metallic coating materials, laser engraving regularly presents considerable difficulties; the incident laser beam leads to thermally induced flow processes in the vicinity of the beam, so that the laser beam can not form sufficiently sharp cell structures. The resulting in the prior art cups are usually surrounded by a crater rim, which leads to a significant deterioration of the image quality of the printed product. The formulated in claim 1 combination of micro- or nanoparticles embedded in a composite material, such as a polymer matrix, for. As a polyacrylate avoids such negative flow phenomena. The wells formed with laser beams are significantly contour sharper than in the prior art and thus suitable to ensure a much better, print result. In addition, the material is sufficiently hard, tensile and compressive strength, elongation at break, modulus of elasticity and wear resistance are suitable to withstand the high mechanical stresses associated with a high speed web-fed rotary printing process. Also the heat resistance is sufficient for such loads. In thermal terms, the claimed composite layer advantageously has a low coefficient of expansion, which has an advantageous effect on its bonding to the substrate. In addition, the radiation-curable micro- or nanoparticles have an advantageous effect in terms of abrasion resistance of the composite material.

Die optischen und thermischen Absorptions-, Dissipations- und/oder Emissionseigenschaften einer solchen Schicht können durch die Einbettung von Mikro- oder Nanoteilchen vorteilhaft beeinflusst werden, d. h. die vorstehend genannten Fließvorgänge und Verschmierungseffekte, die beim Lasergravieren von anderen Kunststoffschichten in der Regel entstehen, werden so stark reduziert, dass die gelaserte Näpfchenstruktur weit schärfer ausgebildet wird als dies bei anderen bekannten Beschichtungen aus Kunststoff möglich ist. Zusätzlich ist es grundsätzlich möglich, die UVAbsorption der gehärteten Schicht auf die Wellenlänge des Gravurlasers abzustimmen, um bei einer optimierten Energieaufnahme das Gravurergebnis weiter zu verfeinern.The optical and thermal absorption, dissipation and / or emission properties of such a layer can be advantageously influenced by the embedding of micro- or nanoparticles, i. H. The above-mentioned flow processes and smearing effects, which usually occur during laser engraving of other plastic layers, are so greatly reduced that the lasered cell structure is made much sharper than is possible with other known plastic coatings. In addition, it is basically possible to tune the UV absorption of the hardened layer to the wavelength of the engraving laser in order to further refine the engraving result with an optimized energy absorption.

Die genannten Kompositschichten sind aber nicht nur vorteilhaft im Hinblick auf die Näpfchenbildung mittels Laser, weitere Vorteile haben sie hinsichtlich einer Löschung der Näpfchenstruktur zu bieten. Die Schichten lassen sich leicht nachbeschichten, d. h. ein Löschvorgang kann vorgenommen werden ohne eine Kompositschicht vollständig von ihrer Unterlage ablösen zu müssen. Durch "Überlasern" können vorhandene Strukturen gelöscht werden und die Oberfläche neu in der erforderlichen Schichtdicke mit Kompositmaterial beschichtet werden.However, the composite layers mentioned are not only advantageous with regard to cup formation by means of a laser, they also have other advantages with respect to deletion of the cup structure. The layers are easy to recoat, d. H. a deletion process can be performed without having to completely detach a composite layer from its backing. Existing structures can be erased by "over-lasers" and the surface re-coated in the required layer thickness with composite material.

Auch kann in nicht erfindungsgemäßer Weise das die Näpfchen der Strukturierung ausfüllende Kompositmaterial durch Laserstrahlung freigelegt und anschließend komplett neu befüllt werden. Damit wird die Struktur "gelöscht" und stellt nach der Neubefüllung für eine neue Strukturierung bereit. Sowohl das "Überlasern" der vorhandenen Strukturen, als auch das Freilegen und anschließende Neubefüllen kann auch nur auf Teilabschnitte des Formkörpers erfolgen, damit wird es möglich, einen Druckzylinder auch nur abschnittsweise zu löschen bzw. mit neuen Bildinformationen zu versehen.Also, in a manner not according to the invention, the composite filling the cells of the structuring can be exposed by laser radiation and then completely refilled. This will "delete" the structure and provide it for refining after refilling. Both the "over-lasing" of existing structures, as well as the exposure and subsequent refilling can only on sections of the molding Thus, it is possible to delete a printing cylinder only partially or to provide new image information.

Grundsätzlich ist es auch möglich, das Kompositmaterial mit einer nichtmetallischen Barriereschicht nach der Bebilderung zu überziehen, die eine größere Härte und/oder eine größere Lösemittelbeständigkeit als das Beschichtungsmaterial selbst aufweist. In vorteilhafter Weise hat es sich gezeigt, dass die Haltbarkeit der Barriereschicht auf der Oberfläche der Kompositschicht durch die Mikro- und Nanopartikel verbessert wird. Die Barriereschicht umfasst Silazan oder SiOx-Verbindungen. Auch das Vorsehen von Kohlenstoff und/oder Stickstoffatomen in der Barriereschicht hat sich als vorteilhaft erwiesen.In principle, it is also possible to coat the composite material with a non-metallic barrier layer after imaging, which has a greater hardness and / or a greater solvent resistance than the coating material itself. Advantageously, it has been found that the durability of the barrier layer on the surface of the composite layer is improved by the microparticles and nanoparticles. The barrier layer comprises silazane or SiOx compounds. The provision of carbon and / or nitrogen atoms in the barrier layer has also proved to be advantageous.

Anspruch 4 befasst sich mit der Aushärtung der Kompositschicht. Um die Haftfähigkeit der Kompositschicht auf der Zylindermantelfläche des Formgrundkörpers zu erhöhen, kann die Zylindermantelfläche in an sich bekannter Weise mit einer Grundstrukturierung versehen sein. Es ist aber auch möglich, das Kompositmaterial auf eine Ballardhaut aufzubringen. Eine derartige Ballardhaut kann zusammen mit der auf ihr aufgebrachten Kompositschicht von dem Grundzylinder abgelöst werden, ohne die Struktur des Grundzylinders negativ zu beeinträchtigen. Eine Ballardhaut wird dadurch erzeugt, dass auf sogenanntes Grundkupfer eine etwa 0,1 mm dicke Kupferhaut aufgalvanisiert wird, die mit einer Oberflächenstruktur versehen werden kann. Nach dem Auflagendruck kann die Ballardhaut vom Druckzylinder abgezogen werden. Alternativ zur Ballardhaut kann auch eine nichtmetallische Zwischenschicht, z. B. ein Primer die Ablösefunktion erfüllen.Claim 4 deals with the curing of the composite layer. In order to increase the adhesion of the composite layer on the cylinder jacket surface of the mold base body, the cylinder jacket surface can be provided in a conventional manner with a basic structure. But it is also possible to apply the composite material on a ballard skin. Such a ballard skin, together with the composite layer applied to it, can be detached from the base cylinder without negatively affecting the structure of the base cylinder. A ballard skin is produced by electroplating on so-called ground copper an approximately 0.1 mm thick copper skin, which can be provided with a surface structure. After the print run, the ballard skin can be removed from the printing cylinder. Alternatively to Ballardhaut can also be a non-metallic intermediate layer, for. B. a primer fulfill the detachment function.

Vorteilhafterweise kann die Schichtdicke der Kompositschicht zwischen 15 und 150 µm betragen.Advantageously, the layer thickness of the composite layer can be between 15 and 150 μm.

Die Lasergravierung, d. h. das Einprägen von Näpfchen mittels Laserstrahlung, lässt sich mit gepulsten Lasern besonders gut durchführen. Die Tiefe und Form der Näpfchen in der Kompositschicht, lässt sich über die Zahl der Pulse pro Stelle und die, durch den Laserstrahl deponierte Energie einstellen. Da die Kompositschicht gegenüber anderen Kunststoffbeschichtungen weit günstigere, optische und thermische Absorptionseigenschaften aufweist, lassen sich durch Lasereintrag beliebige Näpfchenformen eingravieren, beispielsweise quadratische, dreieckige, runde. Auch unterschiedliche Tiefenprofile an einem Grundformkörper können erzeugt werden, z. B. in Stufenform, in Form einer Gaußkurve oder keilförmig. Der Bebilderungsablauf der Schicht kann entweder lokal einzeln erfolgen oder durch ein Rasterverfahren. In üblicher Weise können die Laserstrahlen über Scanner oder Mehrfachachssysteme auf die zu bebildernde Kompositschicht geleitet werden.The laser engraving, ie the embossing of wells by means of laser radiation, can be carried out particularly well with pulsed lasers. The depth and shape of the wells in the composite layer can be adjusted by the number of pulses per spot and the energy deposited by the laser beam. Because the Composite layer compared to other plastic coatings has far more favorable, optical and thermal absorption properties, can be engraved by laser entry arbitrary cup shapes, such as square, triangular, round. Also different depth profiles on a basic shaped body can be generated, for. B. in step shape, in the form of a Gaussian curve or wedge-shaped. The Bebilderungsablauf the layer can be done either locally individually or by a raster method. In the usual way, the laser beams can be directed via scanners or multiple axis systems onto the composite layer to be imaged.

Die Näpfchenform kann vorteilhafterweise über eine Strahlformung des Laserstrahls erfolgen. Eine derartige Strahlformung lässt sich durch Blenden, Masken und/oder andere optische Elemente realisieren.The cup shape can advantageously take place via beam shaping of the laser beam. Such beam shaping can be realized by diaphragms, masks and / or other optical elements.

Eine so mittels Laser eingetragene Strukturierung kann durch Laserabtrag gelöscht werden und die Kompositschicht, die dann in dem abgetragenen Bereichen ausgedünnt ist, neu beschichtet werden, wodurch Beschichtungsmaterial eingespart werden kann. Dabei führt die Neubefüllung der teilweise abgetragenen Näpfchen zu einer geschlossenen Kompositoberflächenschicht. Die hierbei erreichbare Zeiteinsparung stellt einen wesentlichen Vorteil des erfindungsgemäßen Verfahrens dar.Such a laser-registered structuring can be erased by laser ablation and the composite layer, which is then thinned in the ablated areas, re-coated, whereby coating material can be saved. The refilling of the partially removed wells leads to a closed composite surface layer. The time saving achievable in this case represents a significant advantage of the method according to the invention.

Es ist nicht erfindungsgemäß aber auch möglich, eine mit einer Bebilderung versehene Kompositoberflächenschicht vollständig von der Zylindermantelfläche des Formgrundkörpers durch Strahlungseinwirkung oder auch mechanisch abzutragen oder abzulösen und eine im Wesentlichen völlige Neubeschichtung der Zylindermantelfläche des Formgrundkörpers durch ein Kompositmaterial vorzunehmen.It is not according to the invention but also possible to completely remove or detach a composite surface layer provided with an imaging from the cylinder jacket surface of the molded body by exposure to radiation or mechanically and to perform a substantially complete recoating of the cylinder jacket surface of the molded base body by a composite material.

Vor einer Bebilderung durch Lasergravur kann eine aufgetragene Kompositschicht mechanisch oder auch durch Lasereinwirkung geglättet werden, was zu einer weiteren Verbesserung des Druckergebnisses führt.Before being imaged by laser engraving, an applied composite layer can be smoothed mechanically or also by laser action, which leads to a further improvement of the printing result.

Beschrieben wird nun eine Tiefdruckform, die nach dem Verfahren der Ansprüche hergestellt werden kann. Die durch eine Kompositschicht gebildete bebilderbare Oberfläche weist als eine erste Komponente folgende Verbindungen auf: Acrylate von radikalisch UV-härtenden Systemen, cycloaliphatische Eposide, aliphatische Epoxide sowie Verbindungen von kationisch UV-härtenden Systemen. Derartige Verbindungen für die Kompositschicht führen zu besonders vorteilhaften Lasergravurergebnissen mit hochdefinierbarer Näpfchenform. Die Kompositschicht umfasst dabei mehrere multifunktionelle durch Strahlenhärtung vernetzbare Monomere, Oligomere oder Polymere, die orthogonale funktionelle Gruppen umfassen können. Die Partikel der Nanokompositschicht sind mikro- oder nanoskalige Metall- oder Halbmetalloxide oder Oxide von Übergangsmetallen oder Mischoxide in Pulverform oder metallorganische Partikel. Besonders vorteilhaft haben sich für die Nanokompositschicht Verbindungen aus Al2O3, SiO2, ZrO2, TiO2, erwiesen.Described is now a gravure form, which can be produced by the method of the claims. The imageable surface formed by a composite layer has, as a first component, the following compounds: acrylates of radically UV-curing systems, cycloaliphatic epoxides, aliphatic epoxides and compounds of cationically UV-curing systems. Such compounds for the composite layer lead to particularly advantageous laser engraving results with highly definable cup shape. The composite layer comprises several multifunctional radiation curing crosslinkable monomers, oligomers or polymers which may comprise orthogonal functional groups. The particles of the nanocomposite layer are micro- or nanoscale metal or semimetal oxides or oxides of transition metals or mixed oxides in powder form or organometallic particles. Compounds of Al 2 O 3 , SiO 2 , ZrO 2 , TiO 2 have proved to be particularly advantageous for the nanocomposite layer.

Die Verbindungen der Kompositschicht können mit einer organophilen Umhüllung versehen sein.The compounds of the composite layer may be provided with an organophilic envelope.

Die Schichtdicke der Kompositschicht kann zwischen einem Nanometer als theoretische Untergrenze und einem Millimeter betragen. Die Härte der Kompositschicht soll größer als 200 N/mm2 (Martenshärte) sein. Die Näpfchenstruktur der Kompositschicht soll so gewählt sein, dass die Tiefe der Näpfchen geringer ist als die Dicke der Kompositschicht. Zum Löschen einer bebilderten Kompositschicht kann die Kompositschicht eine die Näpfchen vollständig übergreifende Löschschicht tragen.The layer thickness of the composite layer can be between one nanometer as the theoretical lower limit and one millimeter. The hardness of the composite layer should be greater than 200 N / mm 2 (Marten hardness). The cup structure of the composite layer should be chosen so that the depth of the wells is less than the thickness of the composite layer. In order to erase an imaged composite layer, the composite layer may carry a quenching layer that completely overlaps the wells.

Die Verbindung ist anhand eines vorteilhaften Ausführungsbeispiels in den Zeichnungsfiguren näher erläutert. Diese zeigen:

Fig. 1:
einen schematischen Schnitt durch eine mit einer Ballardhaut versehene rotative Druckform zum Einsatz in einem Rollenrotationsdruckverfahren;
Fig. 2:
einen schematischen Detailschnitt gemäß I in Fig. 1;
Fig. 3:
eine schematische Schnittdarstellung einer alternativen rotativen Druckform;
Fig. 4:
einen schematischen Detailschnitt gemäß III. in Fig.3.
The connection is explained in more detail with reference to an advantageous embodiment in the drawing figures. These show:
Fig. 1:
a schematic section through a provided with a ballard skin rotary printing form for use in a web-fed rotary printing process;
Fig. 2:
a schematic detail section according to I in Fig. 1 ;
3:
a schematic sectional view of an alternative rotary printing plate;
4:
a schematic detail section according to III. in Figure 3 ,

Die in Fig. 1 dargestellte rotative Druckform 1 besteht im Wesentlichen aus einem zylindrischen Formgrundkörper mit Strukturierung 2 und einem nichtmetallischen Beschichtungsmaterial, das auf die Oberfläche, d. h. die Zylindermantelfläche 4 des Formgrundkörpers 2 aufgebracht werden kann. Das Beschichtungsmaterial besteht gemäß Fig. 2 aus einem Kompositmaterial 3 und bildet damit eine Kompositschicht 33 aus. Das Kompositmaterial 3 umfaßt eine Matrix auf Acrylatbasis 5 und darin im Wesentlichen gleich verteilten Nanoteilchen 6, die - wie in Fig. 2 schematisch dargestellt - unterschiedlichste Formen und Größen haben können.In the Fig. 1 illustrated rotary printing plate 1 consists essentially of a cylindrical mold base body with structuring 2 and a non-metallic coating material, which can be applied to the surface, that is, the cylinder surface 4 of the mold body 2. The coating material is according to Fig. 2 from a composite material 3 and thus forms a composite layer 33. The composite material 3 comprises an acrylate-based matrix 5 and substantially uniformly distributed nanoparticles 6, which - as in Fig. 2 shown schematically - can have different shapes and sizes.

Auf die Oberfläche 7 des Kompositmaterials 3 wird eine nichtmetallische Barriereschicht 8 aufgebracht, die eine größere Härte als das Kompositmaterial 3 aufweist. Um im Beschichtungsmaterial 3 eine Näpfchenstruktur 9 zum Zwecke der Bebilderung einzubringen, wird ein Lasergravurverfahren eingesetzt. Die Näpfchenstruktur 9 ist in Zeichnungsfigur 2 zu sehen. Insgesamt ist zu den Zeichnungsfiguren festzustellen, dass selbstverständlich die Größen der Teilchen 6, die Dicke der dargestellten Schichten 33, 8, 21, insgesamt die Größenverhältnisse des zylindrischen Formkörpers 2 mit den Schichtdicken und Teilchengrößen nicht der Wirklichkeit entsprechen. Aus Gründen der darstellerischen Klarheit sind die Schichtdicken und Teilchengrößen weit überzogen und relativ zueinander nicht maßstäblich dargestellt.On the surface 7 of the composite material 3, a non-metallic barrier layer 8 is applied, which has a greater hardness than the composite material 3. In order to introduce a cup structure 9 in the coating material 3 for the purpose of imaging, a laser engraving method is used. The cell structure 9 can be seen in drawing figure 2. Overall, it should be noted with respect to the drawing figures that, of course, the sizes of the particles 6, the thickness of the illustrated layers 33, 8, 21, overall the size ratios of the cylindrical shaped body 2 with the layer thicknesses and particle sizes do not correspond to reality. For reasons of illustrative clarity, the layer thicknesses and particle sizes are widely coated and not shown to scale relative to each other.

Wie ferner in Zeichnungsfigur 2 zu sehen ist, kann die Oberfläche 4 des Formgrundkörpers 2 mit einer Grundstrukturierung 20 auf der eine Ballardhaut 21 aufgebracht ist, versehen sein, die letztlich die Kompositschicht 33 trägt. Diesbezüglich sei angemerkt, dass das Aufbringen einer Ballardhaut 21 vor dem Aufbringen der Kompositschicht 33 lediglich eine Option darstellt, die das vollständige Ablösen einer Beschichtung vom Formgrundkörper 2 erleichtern soll.As can furthermore be seen in FIG. 2, the surface 4 of the molded basic body 2 can be provided with a basic structure 20 on which a ballard skin 21 is applied, which ultimately carries the composite layer 33. In this regard, it should be noted that the application of a ballard skin 21 prior to application of the composite layer 33 is merely an option intended to facilitate the complete detachment of a coating from the mold base body 2.

Zusätzlich kann die auf den Formgrundkörper 2 aufgebrachte Ballardhaut 21 mit einer Strukturierung versehen sein.In addition, the ballast skin 21 applied to the mold base body 2 may be provided with a structuring.

In den Zeichnungsfiguren 3 und 4 ist eine alternative Ausführungsform dargestellt. Hierbei ist die Kompositschicht 33 ohne Ballardhaut direkt auf den Formgrundkörper 2 angeordnet. Um die Haftwirkung zwischen der Zylindermantelfläche 4 und der Kompositschicht 33 zu erhöhen, ist die Zylindermantelfläche 4 mit einer z. B. stegähnlichen Grundstrukturierung 20 versehen, welche die Berührungsfläche erhöht.In the drawing figures 3 and 4, an alternative embodiment is shown. Here, the composite layer 33 is arranged without ballard skin directly on the mold base body 2. In order to increase the adhesion between the cylinder jacket surface 4 and the composite layer 33, the cylinder jacket surface 4 is provided with a z. B. web-like basic structure 20, which increases the contact area.

Die Näpfchenstruktur 9 kann unterschiedliche Formen, Tiefen und/oder Dimensionierungen aufweisen.The cell structure 9 can have different shapes, depths and / or dimensions.

Aus der Beschreibungseinleitung geht ferner hervor, dass die Kompositschicht 33 aus einem Beschichtungsmaterial 3 gebildet werden kann, das unterschiedlichste chemische Zusammensetzungen umfassen kann. Die Zusammensetzungen können vom Fachmann innerhalb der angegebenen Bereiche so gewählt werden, dass sich eine kratz-/abrieb- und haftfeste sowie lösungsmittelbeständige Beschichtung ausbildet, die - was den Kerngedanken der Erfindung anbelangt - eine nahezu rückstandslose Lasergravierbarkeit gewährleistet.It is also clear from the introduction to the introduction that the composite layer 33 can be formed from a coating material 3 which can comprise a very wide variety of chemical compositions. The compositions can be selected by the person skilled in the art within the stated ranges in such a way that a scratch-resistant, abrasion-resistant and solvent-resistant coating is formed, which, as far as the core idea of the invention is concerned, ensures virtually residue-free laser engravability.

Claims (10)

  1. Method for erasing and image re-setting an impression cylinder for the production of intaglio-printed illustrations between two printing operations which lead to different printed products, having the following method steps:
    - applying a non-metallic coating material onto the cylinder-sleeve face of a cylindrical basic moulding (2) of the impression cylinder, wherein a composite material (3) which can be cured by polymerization after the coating operation and comprises at least one organic binder with nanoparticles and/or microparticles (6) having a binder-compatible organophilic wrapping, which surrounds the particles (6), contained therein is applied as the coating material, in order to produce a compact surface of the composite material (3) ;
    - curing the applied coating material in order to form a composite layer (33) and
    - image re-setting by introducing a cup structure (9) into the coating material;
    - wherein, for erasing the impression cylinder which has already been used, a composite layer (3) which has already been image-set is partially removed from its subsurface without being completely detached;
    - the application to the required layer thickness takes place as an after-coating by dip coating, doctor application or roller application, using the prepolymer composite material (3), and
    - the image re-setting of the composite layer (33) is carried out by means of laser radiation prior to the subsequent printing operation.
  2. Method according to Claim 1, characterized in that a non-metallic barrier layer (8) is applied onto the surface (7) of the composite material (3) after introduction of the cup structure (9).
  3. Method according to Claim 2, characterized in that the hardened composite material (3) forms a composite layer (33), and the barrier layer (8) has a greater hardness and/or a greater resistance to solvents than the composite layer (33).
  4. Method according to one of the preceding claims, characterized in that the applied composite material (3) is cured by VUV, UV, electron or gamma radiation and/or a plasma.
  5. Method according to Claim 4, characterized in that the curing of the composite material (3) is thermally facilitated.
  6. Method according to one of the preceding claims, characterized in that the composite material (3) is structured and/or removed by the laser radiation.
  7. Method according to one of the preceding claims, characterized in that the cylinder-sleeve face (4) of the basic moulding (2) is provided with a basic structure (20).
  8. Method according to one of the preceding claims, characterized in that the erasing and/or image re-setting takes place only on part-portions of the composite layer (33).
  9. Method according to one of the preceding claims, characterized in that the composite layer (33), which has been applied to the cylinder-sleeve face (4), is mechanically smoothed prior to image re-setting.
  10. Method according to one of the preceding claims, characterized in that beam shaping of the laser radiation takes place for setting defined cup shapes.
EP09009725.4A 2008-07-28 2009-07-28 Method for producing a rotative printing plate for insertion in a roller rotation printing method Active EP2151324B1 (en)

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DK2151324T3 (en) 2014-06-23
EP2151324A3 (en) 2011-02-23
ES2459346T3 (en) 2014-05-09
DE102008035203B4 (en) 2011-01-27
DE102008035203A1 (en) 2010-02-11
EP2151324A2 (en) 2010-02-10
PL2151324T3 (en) 2014-08-29

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