EP1353802B1 - Verfahren zur herstellung von thermisch vernetzten, lasergravierbaren flexodruckelementen undmehrschichtverbunde - Google Patents
Verfahren zur herstellung von thermisch vernetzten, lasergravierbaren flexodruckelementen undmehrschichtverbunde Download PDFInfo
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- EP1353802B1 EP1353802B1 EP02702237A EP02702237A EP1353802B1 EP 1353802 B1 EP1353802 B1 EP 1353802B1 EP 02702237 A EP02702237 A EP 02702237A EP 02702237 A EP02702237 A EP 02702237A EP 1353802 B1 EP1353802 B1 EP 1353802B1
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- GUTAMRLAIZPNHT-UHFFFAOYSA-N n-(tert-butyldiazenyl)formamide Chemical compound CC(C)(C)N=NNC=O GUTAMRLAIZPNHT-UHFFFAOYSA-N 0.000 description 1
- QYZFTMMPKCOTAN-UHFFFAOYSA-N n-[2-(2-hydroxyethylamino)ethyl]-2-[[1-[2-(2-hydroxyethylamino)ethylamino]-2-methyl-1-oxopropan-2-yl]diazenyl]-2-methylpropanamide Chemical compound OCCNCCNC(=O)C(C)(C)N=NC(C)(C)C(=O)NCCNCCO QYZFTMMPKCOTAN-UHFFFAOYSA-N 0.000 description 1
- 239000004745 nonwoven fabric Substances 0.000 description 1
- 229920003207 poly(ethylene-2,6-naphthalate) Polymers 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 229920006267 polyester film Polymers 0.000 description 1
- 229920003245 polyoctenamer Polymers 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 150000004053 quinones Chemical class 0.000 description 1
- 239000006100 radiation absorber Substances 0.000 description 1
- 238000010526 radical polymerization reaction Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000004071 soot Substances 0.000 description 1
- 230000003595 spectral effect Effects 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 239000011029 spinel Substances 0.000 description 1
- 229910052596 spinel Inorganic materials 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229920006132 styrene block copolymer Polymers 0.000 description 1
- 239000011115 styrene butadiene Substances 0.000 description 1
- 229920003048 styrene butadiene rubber Polymers 0.000 description 1
- 150000003440 styrenes Chemical class 0.000 description 1
- 230000008961 swelling Effects 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
- GJBRNHKUVLOCEB-UHFFFAOYSA-N tert-butyl benzenecarboperoxoate Chemical compound CC(C)(C)OOC(=O)C1=CC=CC=C1 GJBRNHKUVLOCEB-UHFFFAOYSA-N 0.000 description 1
- SWAXTRYEYUTSAP-UHFFFAOYSA-N tert-butyl ethaneperoxoate Chemical compound CC(=O)OOC(C)(C)C SWAXTRYEYUTSAP-UHFFFAOYSA-N 0.000 description 1
- 125000000999 tert-butyl group Chemical group [H]C([H])([H])C(*)(C([H])([H])[H])C([H])([H])[H] 0.000 description 1
- CIHOLLKRGTVIJN-UHFFFAOYSA-N tert‐butyl hydroperoxide Chemical compound CC(C)(C)OO CIHOLLKRGTVIJN-UHFFFAOYSA-N 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 229920000428 triblock copolymer Polymers 0.000 description 1
- JSPLKZUTYZBBKA-UHFFFAOYSA-N trioxidane Chemical class OOO JSPLKZUTYZBBKA-UHFFFAOYSA-N 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
- 229910006540 α-FeOOH Inorganic materials 0.000 description 1
- 229910003153 β-FeOOH Inorganic materials 0.000 description 1
- 229910006299 γ-FeOOH Inorganic materials 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
- B41C—PROCESSES FOR THE MANUFACTURE OR REPRODUCTION OF PRINTING SURFACES
- B41C1/00—Forme preparation
- B41C1/02—Engraving; Heads therefor
- B41C1/04—Engraving; Heads therefor using heads controlled by an electric information signal
- B41C1/05—Heat-generating engraving heads, e.g. laser beam, electron beam
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S430/00—Radiation imagery chemistry: process, composition, or product thereof
- Y10S430/146—Laser beam
Definitions
- the invention relates to a method for producing thermally crosslinked, laser-engravable flexographic printing elements, the production of relief printing plates from the laser-engravable flexographic printing elements, and the thermally non-crosslinked flexographic printing elements.
- EP-A 0 640 043 discloses the preparation of a soot-containing, elastomeric layer by photocrosslinking. But this layer has only a thickness of 0.076 mm, while the typical thickness of commercially available flexographic printing plates 0.5 to 7 mm.
- thermoplastic elastomers are elegantly using Extrusion and calendering at elevated temperatures using thermal stable photoinitiators produced.
- thermally decomposing initiators difficult, because of the high working temperatures and because of the high shear in the preparation of the thermally crosslinkable mixture in the extruder can lead to premature crosslinking.
- Temperature sensitivity of the crosslinkable mixture are low working temperatures of clearly below 100 ° C required, so that, for example, a processing in one Two-screw extruder precipitates.
- the object of the invention is to provide a method for producing laser engravable Flexographic printing plates with thermally crosslinked, elastomeric relief-forming layer provide.
- a multi-layer composite at least comprising one Two-layer composite from the depot layer D and the depot layer D directly adjacent uncrosslinked precursor layer V produced for the relief-forming layer E.
- the precursor layer V contains at least one elastomeric binder as a component (A).
- elastomeric binder all known, including for the production of photopolymerizable flexographic printing plates used are used.
- elastomeric binders and thermoplastic elastomers Binder suitable.
- suitable binders are the known ones Triblock copolymers of the SIS or SBS type, which are also fully or partially hydrogenated can. It is also possible to use ethylene / propylene / diene elastomeric polymers, Ethylene / acrylic acid rubbers or elastomeric polymers based on acrylates or Acrylate copolymers are used. Further examples of suitable polymers are in DE-A 22 15 090, EP-A 084 851, EP-A 819 984 or EP-A 553 662. It can It is also possible to use mixtures of two or more different binders.
- the type and amount of binder used will be determined by those skilled in the art depending on the desired properties of the printing relief selected. As a rule, the Amount of the binder 50 to 90 wt .-%, preferably 60 to 90 wt .-%, based on the Sum of all components of the precursor layer, ie the sum of components (a) to (D).
- the precursor layer contains at least one ethylenically unsaturated monomer as Component (b).
- ethylenically unsaturated monomers can be used in principle those which are also commonly used for the production of photopolymerizable Flexographic printing elements are used.
- the monomers are said to bind with the binders be compatible and at least one polymerizable, ethylenically unsaturated Have double bond.
- Suitable monomers generally have a boiling point of greater than 100 ° C at atmospheric pressure and a molecular weight of up to 3,000 g / mol, preferably up to 2,000 g / mol.
- esters or Amides of acrylic acid or methacrylic acid with mono- or polyfunctional alcohols are particularly advantageous.
- Examples suitable monomers are butyl acrylate, 2-ethylhexyl acrylate, lauryl acrylate, 1,4-butanediol diacrylate, 1,6-hexanediol diacrylate, 1,6-hexanediol dimethacrylate, 1,9-nonanediol diacrylate, Trimethylolpropane triacrylate, dioctyl fumarate and N-dodecylmaleimide. It is also possible to use mixtures of different monomers. As a rule the total amount of the monomers is 5 to 30% by weight, preferably 5 to 20% by weight, based on the sum of components (a) to (d).
- the precursor layer may further comprise an absorber for laser radiation as a component (c) included.
- the precursor layer preferably contains such an absorber.
- Suitable absorbers for laser radiation have a high absorption in the range of Laser wavelength on.
- absorbers are suitable which have a high absorption in the near infrared, as well as in the longer-wave VIS range of the electromagnetic spectrum exhibit.
- Such absorbers are particularly suitable for absorbing the radiation from powerful Nd-YAG lasers (1064 nm) and IR diode lasers, which are typically Wavelengths between 700 and 900 nm and between 1200 and 1600 nm exhibit.
- Suitable absorbers for the laser radiation are in the infrared spectral range strongly absorbing dyes such as phthalocyanines, naphthalocyanines, Cyanines, quinones, metal complex dyes such as dithiolenes or photochromic dyes.
- suitable absorbers are inorganic pigments, in particular intensively colored inorganic pigments such as chromium oxides, iron oxides, carbon black or metallic Particle.
- Particularly suitable as an absorber for laser radiation are finely divided carbon blacks with a Particle size between 10 and 50 nm.
- suitable absorbers for laser radiation are iron-containing solids, in particular intensively colored iron oxides.
- iron oxides are commercially available and are commonly used as color pigments or as pigments for magnetic recording.
- Suitable absorbers for laser radiation are, for example, FeO, goethite (alpha-FeOOH), akaganeite (beta-FeOOH), lepidocrocite (gamma-FeOOH), hematite (alpha-Fe 2 O 3 ), maghemite (gamma-Fe 2 O 3 ), magnetite (Fe 3 O 4 ) or Berthollide.
- doped iron oxides or mixed oxides of iron with other metals can be used.
- Examples of mixed oxides are Umbra Fe 2 O 3 xn MnO 2 or Fe x Al (1-x) OOH, in particular various spinel black pigments such as Cu (Cr, Fe) 2 O 4 , Co (Cr, Fe) 2 O 4 or Cu (Cr, Fe, Mn) 2 O 4 .
- Examples of dopants are, for example, P, Si, Al, Mg, Zn or Cr. Such dopants are usually added in small amounts in the course of the synthesis of the oxides to control particle size and particle shape.
- the iron oxides can also be coated. Such coatings can be applied, for example, to improve the dispersibility of the particles. These coatings may for example consist of inorganic compounds such as SiO 2 and / or AIOOH.
- organic coatings for example organic adhesion promoters such as aminopropyl (trimethoxy) silane.
- organic adhesion promoters such as aminopropyl (trimethoxy) silane.
- absorbers for laser radiation are FeOOH, Fe 2 O 3 and Fe 3 O 4 , very particularly preferably Fe 3 O 4 .
- the size of the iron-containing, inorganic solids used, in particular the iron oxides is selected by the person skilled in the art, depending on the desired properties of the recording material. However, solids with an average particle size of more than 10 ⁇ m are generally unsuitable. Since iron oxides in particular are anisometric, this information refers to the longest axis.
- the particle size is preferably less than 1 ⁇ m. It is also possible to use so-called transparent iron oxides which have a particle size of less than 0.1 ⁇ m and a specific surface area of up to 150 m 2 / g.
- Ferrous metal pigments are particularly suitable as absorber for laser radiation ferrous compounds. Particularly suitable are acicular or rice-kernel-shaped Pigments with a length between 0.1 and 1 ⁇ m. Such pigments are as Magnetic pigments known for magnetic recording. In addition to the iron can also, other dopants such as Al, Si, Mg, P, Co, Ni, Nd or Y may be present or the ferrous metal pigments may be coated therewith. Iron metal pigments are surface oxidized to protect against corrosion and consist of an optionally doped Iron core and an optionally doped iron oxide shell.
- the amount of added absorber is determined by the skilled person depending on the respective desired properties of the laser-engravable flexographic printing selected. In this In the context, the person skilled in the art will consider that the added absorbers are not only speed and efficiency of the engraving of the elastomeric layer by laser but also other properties of the flexographic printing element, such as for example, its hardness, elasticity, thermal conductivity or ink acceptance. in the As a rule, therefore, more than 20% by weight of the absorber for laser radiation is the sum all components of the laser-engravable elastomeric layer unsuitable. Preferred is the amount of the laser radiation absorber is 0.5 to 15% by weight and more preferably 0.5 to 10 wt .-%.
- the precursor layer V may optionally contain further additives as component (d) for adjustment contain the desired properties of the relief layer.
- further additives are Plasticizers, fillers, dyes, compatibilizers or dispersing aids.
- the amount of such further constituents should, however, as a rule be 20% by weight, preferably 10 wt .-%, based on the sum of the components (a) to (d), not exceed.
- the depot layer D also contains an elastomeric binder as component (e). It the same elastomeric binders can be used, which are also used in the Precursor layer can be used, are preferred in precursor and Depot harsh the used the same elastomeric binder.
- the depot layer D contains at least one thermally decomposing polymerization initiator as component (f).
- Suitable polymerization initiators are in principle all thermal initiators suitable for the radical polymerization are used, such as peroxides, hydroperoxides or Azo compounds.
- Suitable thermal initiators decompose only in the final step of the process according to the invention, the thermal crosslinking, with high reaction rate in radicals. They are largely thermally stable in the preceding process steps of melting, mixing, extruding and calendering or casting from solution or dispersion, evaporation of the solvent and lamination.
- substantially thermally stable in this context means that the initiators decompose at most slowly in the course of carrying out these steps of the process according to the invention, that crosslinking of the layer and / or the mixture by polymerization can take place only to a minor extent.
- the thermal stability of an initiator is usually given by the temperature of the 10 h half-life 10 ht 1/2 , ie the temperature at which 50% of the original amount of initiator has decomposed into free radicals after 10 h. Further details can be found in "Encylopedia of Polymer Science and Engineering", Vol. 11, pp. 1ff., John Wiley & Sons, New York, 1988.
- Initiators which are suitable in particular for carrying out the process according to the invention usually have a 10 ht 1/2 of at least 60 ° C., preferably of at least 70 ° C. Particularly suitable initiators have a 10 ht 1/2 of 80 ° C to 150 ° C.
- Suitable initiators include certain peroxyesters, such as t-butyl peroctoate, t-amyl peroctoate, t-butyl peroxy isobutyrate, t-butyl peroxymaleic acid, t-amyl perbenzoate, Di-t-butyl diperoxyphthalate, t-butyl perbenzoate, t-butyl peracetate or 2,5-di (benzoylperoxy) -2,5-dimethylhexane, certain diperoxyketals such as 1,1-di (t-amylperoxy) cyclohexane, 1,1-di (t-butylperoxy) cyclohexane, 2,2-di (t-butylperoxy) butane or ethyl 3,3-di (t-butylperoxy) butyrate, certain dialkyl peroxides such as di-t-butyl peroxide, t-butyl cumene
- azo compounds such as 1- (t-butylazo) formamide, 2- (t-butylazo) isobutyronitrile, 1- (t-butylazo) cyclohexanecarbonitrile, 2- (t-butylazo) -2-methylbutanenitrile, 2,2'-azobis (2-actoxypropane), 1,1'-azobis (cyclohexanecarbonitrile), 2,2'-azobis (isobutyronitrile) or 2,2'-azobis (2-methylbutanenitrile).
- the concentration of the thermally decomposing initiators in the depot layer depends according to the thickness of the depot layer relative to the thickness of the laser-engravable, relief-forming elastomeric layer.
- the concentration of the thermally decomposing polymerization initiators is after diffusion and before thermal crosslinking in the Precursor layer about 1 to 5 wt .-%, preferably about 2 to 3 wt .-%, based on the Sum of all the components then present in the precursor layer.
- the thickness of the Depot layer is usually half to 1/30 of the total thickness of Precursor layer and depot layer taken together, for example 1/10 of Total thickness of both layers.
- the concentration of thermally decomposing Polymerization initiators in the depot layer double to 30 times the desired Concentration of the polymerization after diffusion into the Precursor layer, for example, at a layer thickness of the deposit layer of 1/10 of Total layer thickness of both layers 20 to 30 wt .-%, based on the sum of Components (e) to (h).
- the total thickness of relief-forming elastomeric layer D or precursor layer V and Depot layer D is generally 0.4 to 7 mm.
- the depot layer may optionally contain an absorber for laser light as component (g) contain. Suitable absorbers are the absorbers previously mentioned as component (c) in the quantities indicated there.
- the depot layer then contains an absorber when it is according to an embodiment of the method according to the invention during the Laser engraving on the printing side of the flexographic printing element remains and together is laser-engraved with the relief-forming layer E.
- the depot layer may optionally contain further additives as component (h) for adjusting the Properties of the depot layer such as plasticizers, fillers, dyes, compatibilizers or dispersing agents in amounts of up to 20 wt.%, Preferably until to 10% by weight.
- further additives as component (h) for adjusting the Properties of the depot layer such as plasticizers, fillers, dyes, compatibilizers or dispersing agents in amounts of up to 20 wt.%, Preferably until to 10% by weight.
- the preparation of the two-layer composite from depot layer D and precursor layer V can be done in different ways.
- this is in the context of a multi-layer composite manufactured, which comprises the two-layer composite and next to other layers, carriers and / or Protective films used in laser-engravable flexographic printing elements or in general Flexographic printing elements are conventional includes.
- the multi-layer composite by a dimensionally stable carrier film on one side and by a peelable Protective film on the other side or also limited by two protective films. Between a depot layer D and coated with this carrier film can be usual adhesive layer be present.
- the printing side of the elastomeric, laser-engravable relief-forming layer or optionally also an overlying, laser-engravable deposit layer D can be used to improve the upper layer Have printing properties.
- a peelable protective film can be made with a detackifying layer Be coated (release layer).
- Suitable dimensionally stable carriers S are plates and films of metals such as steel, Aluminum, copper or nickel or of plastics such as polyethylene terephthalate (PET), Polyethylene naphthalate (PEN), polybutylene terephthalate (PBT), polyamide, polycarbonate, if appropriate, also fabrics and nonwovens, such as glass fiber fabric and composite materials made of glass fibers and plastics.
- PET polyethylene terephthalate
- PEN Polyethylene naphthalate
- PBT polybutylene terephthalate
- polyamide polycarbonate
- fabrics and nonwovens such as glass fiber fabric and composite materials made of glass fibers and plastics.
- a dimensionally stable carrier come above all dimensionally stable carrier films such as polyester films, in particular PET or PEN foils in question.
- the thickness of the carrier film is generally 75 to 225 microns.
- the carrier film may be coated with an adhesive layer A.
- the multilayer element may have a thin top layer T on the precursor layer V or the laser-engravable depot layer D include.
- a top layer can essential parameters for the printing behavior and color transfer, such as roughness, Abrasiveness, surface tension, surface tack or solvent resistance be changed on the surface, without the typical characteristics of the Printing form such as hardness or elasticity are influenced surface properties and layer properties can therefore be independent of each other be changed to achieve an optimal print result.
- the composition the upper class is limited only insofar as the laser engraving is underneath the laser-engravable layer may not be affected and the Upper layer with this together must be removable.
- the upper class should be thin be opposite to the laser-engravable layer. As a rule, the thickness exceeds the Upper layer not 100 microns, preferably the thickness is between 1 and 80 microns, especially preferably between 3 and 10 microns.
- the upper layer itself should be good be laser engravable.
- the multilayer element can also be a non-laser-engravable underlayer U which is located between the carrier and the laser-engravable layer.
- Such sublayers can be the mechanical properties of the relief printing plates be changed without affecting the relief typical properties of the printing form.
- the multi-layer element optionally against mechanical damage be protected by a, for example made of PET protective film P, based on the uppermost layer, and each before engraving with lasers must be deducted.
- the thickness of the protective films is generally 75 to 225 microns.
- the protective film can be coated with a "release layer" R.
- the thickness of the entire multilayer element is generally 0.7 to 7 mm.
- the shaping of the precursor layer of one of the components (a) to (d) containing Mixture may be before, during or after contacting the precursor layer V or the mixture with the depot layer D done.
- the method according to the invention is the Two-layer composite of D and V by extruding a melt containing the Components (a) to (d), and calendering of this melt between a first film and a second film is produced, wherein at least one film with the depot layer D is coated.
- Only one or both foils can be coated with the depot layer D. be between depository layer D and film can be present more layers.
- Preferably, only one film is coated with a depot layer.
- the other slide can also be coated with other layers. It can also coextrude several layers be, for example, the precursor layer V and an overlying Upper class T.
- the method according to the invention is a preparation of the thermally crosslinkable Flexographic printing elements also by conventional twin-screw extrusion and calendering the crosslinkable layer possible.
- This method offers the advantage of being low Thickness tolerances are maintained, the mixture of components during the Extrusion process takes place and layer thicknesses> 1 mm are available.
- the Two-layer composite of D and V by laminating one with the depot layer D. coated first film on a coated with the precursor layer V second film produced. Between depot layer D and first film or between precursor layer V and second film may be further layers.
- the Two-layer composite of D and V by applying a moldable mixture, solution or dispersion containing the components (a) to (d) on a film associated with the Depot layer D is coated, and optionally produced subsequent drying.
- the two-layer composite can by applying a moldable melt and then pressing or by pouring the solution or dispersion and then Drying be prepared. It can also be poured several layers on top of each other be, for example, the precursor layer V and then a top layer T.
- the thermally decomposing polymerization initiators from the deposit layer D in the precursor layer V diffuse, preferably until they are homogeneously distributed in the precursor layer V.
- the diffusion of the Polymerization initiators can by simply storing the multilayer elements over a period of 1 to 100 days, preferably 3 to 14 days.
- the Diffusion can also occur at elevated temperature, for example 30 to 80 ° C, which significantly shortens the storage time required. For example, shortened the time of storage of 7 days by raising the temperature to 80 ° C to 3 to 8 Hours.
- the depot layer D is removed in a third step (iii).
- This will be the depot layer D, for example by delamination, following the indiffusion removed from the precursor layer.
- step (iv) the thermal crosslinking of the precursor layer V to the elastomeric, laser-engravable relief-forming layer E.
- the thermal crosslinking is achieved by heating the multilayer element to temperatures of generally 80 to 220 ° C, preferably 120 to 200 ° C over a period of 2 to 30 min performed.
- the laser-engravable flexographic printing elements produced according to the invention serve as Starting material for the production of relief printing plates.
- the method includes that First, the protective film - if any - is deducted.
- step (v) becomes a printing relief in the recording material by means of a laser engraved.
- picture elements are engraved in which the flanks of the picture elements first drop off vertically and only in the lower part of the picture element broaden. As a result, a good Versockelung the pixels is still lower Tonwertzuddling reached. But it can also differently shaped flanks of the pixels engraved.
- Laser engraving is particularly suitable for CO 2 lasers having a wavelength of 10,640 nm, but also Nd-YAG lasers (1064 nm) and IR diode lasers or solid-state lasers, which typically have wavelengths between 700 and 900 nm and between 1,200 and 1,600 nm , However, it is also possible to use lasers with shorter wavelengths, provided the laser has sufficient intensity. For example, it is also possible to use a frequency-doubled (532 nm) or frequency-tripled (355 nm) Nd-YAG laser or else an excimer laser (for example 248 nm).
- the image information to be engraved is transmitted directly from the lay-out computer system to the laser apparatus.
- the lasers can be operated either continuously or pulsed.
- the relief layer is very completely removed by the laser, so that an intense Post-cleaning is usually not necessary. If desired, the obtained Pressure plate but still to be cleaned. By such a cleaning step are detached, but may not yet completely from the disk surface removed removed layer components. As a rule, simple wetting with water completely adequate.
- the Deposit layer D itself laser-engravable and lies on the printing side of the flexographic printing element before, with the relief in the depot layer D, which is a laser light absorbing Contains material, and the underlying relief-forming elastomeric layer E engraved.
- the invention also relates to multi-layer composites according to claims 7-10, comprising the Two-layer composite of depot layer D and uncrosslinked precursor layer V.
- the non-adherent, removable depot layer D may be prior to thermal crosslinking be removed without a significant influence on the surface quality occurs.
- the binders in D are chosen so that the adhesion of D in uncrosslinked Condition to V is less than 1 N / 4 cm, preferably less than 0.5 N / 4 cm.
- a conventional, designated flexographic printing plate in a twin-screw extruder ZSK 53, Werner & Pfleiderer was the homogeneous melt or moldable mixture discharged through a slot die.
- the supported peroxide deposit layers D1 and D2 were attached to a dimensionally stable film, so that the deposited peroxide deposit layer could form a layer composite during calendering with the elastomeric melt or with the moldable elastomeric mixture.
- a layer composite is understood to be the direct contact between the pressure element-forming layer V and at least one peroxide deposit layer D1 or D2 , if this contact has persisted for at least the duration of the combination process, but otherwise independent of a fixed period of contact after the unification process.
- nyloflex® FAH printing plate based on SIS block copolymers as binder (Kraton® D-1161NU from Shell), hexanediol diacrylate and dimethacrylate as monomers, oligobutadiene, PE wax and stabilizer were used in a Haake laboratory kneader at an initial temperature of 150 ° C and a rotational speed of 160 min -1 for a period of 10 minutes kneaded.
- the melt temperature settled to a constant 166 ° C, and the torque reached a plateau at about 2 Nm.
- the toluene extraction ratio of the kneaded mixture is 100%.
- the constituents of the printing plate formulation described in Example 1 of EP-A 0 326 977 were kneaded in a Haake kneader at an initial temperature of 150 ° C. and a rotational speed of 160 min -1 for a period of 10 minutes.
- the melt temperature settled to a constant 180 ° C and the torque reached a plateau at about 7 Nm.
- the toluene extraction ratio of the kneaded mixture is 100%.
- a peroxide depot adhesive layer D1 was prepared as follows: 80 g of a styrene-isoprene-styrene block copolymer (Kraton® D-1161NU from Shell) was dissolved in 185 ml of toluene at 110 ° C. After cooling the solution to 60 ° C, 20 g of dicumyl peroxide was added and stirring was continued until the solution was clear and homogeneous (about 1 hour). The solution thus prepared was applied by means of a laboratory knife in different thicknesses on a PET protective film. The resulting layers were then dried at room temperature for one day and finally at 35 ° C for 3 hours.
- Kraton® D-1161NU from Shell
- An oxygen-poor melt was produced from the components of a nyloflex® FAH printing plate by the above-mentioned method.
- the two-layer composite D1 / V was then produced by calendering the depot layers described, wherein a commercially available PET film was used as the second dimensionally stable carrier.
- Example 1a (comparative example )
- the two-layer composite D1 / V from example 1a was heated to 160 ° C. after one-week storage for a period of 20 minutes in a normal air atmosphere.
- the two-layer composite D1 / V from example 1a was first heat-treated at 80 ° C. for 3 hours and then heated to 160 ° C. for a period of 20 minutes in a normal air atmosphere.
- Another peroxide depot adhesive layer D1 was prepared as follows: 80 g of a styrene-butadiene / styrene-styrene block copolymer (Styroflex® BX 6105, BASF) were dissolved in 150 ml of toluene at 110 ° C. After cooling the solution to 60 ° C, 20 g of dicumyl peroxide were added and stirring was continued until the solution was clear and homogeneous (about 1 hour). The solution thus prepared was applied by means of a laboratory knife in different thicknesses on a PET protective film. The resulting layers were then dried at room temperature for one day and finally at 35 ° C. for 3 hours.
- a styrene-butadiene / styrene-styrene block copolymer (Styroflex® BX 6105, BASF) were dissolved in 150 ml of toluene at 110 ° C. After cooling the solution to 60
- An oxygen-poor melt was made from the components of a nyloflex® FAH Pressure plate after the o.g. Process produced.
- the two-layer composite D1 / V was then produced by calendering the described depot layers, wherein a commercially available PET film was used as the second dimensionally stable carrier.
- Example 2a (comparative example )
- the two-layer composite D1 / V from Example 2a was heated to 160 ° C. after one-week storage for a period of 20 minutes in a normal air atmosphere.
- the two-layer composite D1 / V from example 2a was first heat-treated at 80 ° C. for 3 hours and then heated to 160 ° C. for a period of 20 minutes in a normal air atmosphere.
- a peroxide depot release layer D2 was prepared as follows: 80 g of a polyamide hot melt adhesive (Macromelt® 6208, Henkel) was dissolved in a mixture of 90 ml of toluene and 90 ml of 1-propanol at 95 ° C. After cooling the solution to 60 ° C, 20 g of dicumyl peroxide was added and stirring was continued until the solution was clear and homogeneous (about 1 hour). The solution thus prepared was applied by means of a laboratory knife in different thicknesses on a PET protective film. The resulting layers were then dried at room temperature for one day and finally at 35 ° C. for 3 hours.
- a polyamide hot melt adhesive Macromelt® 6208, Henkel
- An oxygen-poor melt was made from the components of a nyloflex® FAH Pressure plate after the o.g. Process produced.
- the two-layer composite D2 / V was then classified by calendering Depot layer produced, as a second dimensionally stable carrier is a commercial PET film was used.
- Example 3a (comparative example )
- the resulting two-layer composite of peroxide depot release layer and elastomeric Pressure element forming layer was stored for one week at room temperature.
- the two-layer composite D2 / V from Example 3a was separated after one-week storage, that is, the depot release layer D2 was removed from the precursor layer.
- the peroxide-containing precursor layer V was heated to 160 ° C for a period of 20 minutes in a normal air atmosphere.
- the two-layer composite D2 / V from Example 3a was separated after one-week storage, that is, the depot release layer D2 was removed from the precursor layer.
- the peroxide-containing precursor layer V was first annealed at 80 ° C. for 3 hours and then heated to 160 ° C. for a period of 20 minutes in a normal air atmosphere.
- Another peroxide depot adhesive layer D1 was prepared as follows: 64 g of an ethylene-propylene-diene terpolymer (Buna EP G-KA 8869, Bayer) and 6 g of an aliphatic ester plasticizer (Plastomoll® DNA, BASF) were dissolved in 260 ml of toluene at 110 ° C solved. After cooling the solution to 60 ° C, 30 g of dicumyl peroxide was added and stirring was continued until the solution was clear and homogeneous (about 1 hour). The solution thus prepared was applied by means of a laboratory knife in different thicknesses on a PET protective film. The resulting layers were then dried at room temperature for one day and finally at 35 ° C. for 3 hours.
- the two-layer composite D1 / V was then produced by calendering the described depot layers, wherein a commercially available PET film was used as the second dimensionally stable carrier.
- Example 4a (comparative example )
- the two-layer composite D1 / V from example 4a was heated to 160 ° C. after storage for one week for a period of 20 minutes in a normal air atmosphere.
- the two-layer composite D1 / V from example 4a was first heat-treated at 80 ° C. for 3 hours and then heated to 160 ° C. for a period of 20 minutes in a normal air atmosphere.
- Another peroxide depot adhesive layer D1 was prepared as follows: 64 g of a cyclic rubber (Vestenamer® 6213, Creanova) and 6 g of an aliphatic ester plasticizer (Plastomoll® DNA, BASF) were dissolved in 150 ml of toluene at 110 ° C. After cooling the solution to 60 ° C, 30 g of dicumyl peroxide was added and stirring was continued until the solution was clear and homogeneous (about 1 hour). The solution thus prepared was applied by means of a laboratory knife in different thicknesses on a PET protective film. The resulting layers were then dried at room temperature for one day and finally at 35 ° C. for 3 hours.
- the two-layer composite D1 / V was then produced by calendering the described depot layers, wherein a commercially available PET film was used as the second dimensionally stable carrier.
- Example 5a (comparative example )
- the resulting two-layer composite of peroxide Depothaft für elastomeric Printing element-forming layer was stored for one week at room temperature.
- the two-layer composite D1 / V from example 5a was heated to 160 ° C. after storage for one week for a period of 20 minutes in a normal air atmosphere.
- the two-layer composite D1 / V from Example 5a was first heat-treated at 80 ° C. for 3 hours and then heated to 160 ° C. for a period of 20 minutes in a normal air atmosphere.
- Another peroxide depot adhesive layer D1 was prepared as follows: 80 g of an ethylene-propylene-diene terpolymer (Buna EP G-KA 8869, Bayer AG) were dissolved in 260 ml of toluene at 110.degree. After cooling the solution to 60 ° C, 20 g of dicumyl peroxide was added and stirring was continued until the solution was clear and homogeneous (about 1 hour). The solution thus prepared was applied by means of a laboratory knife in different thicknesses on a PET protective film. The resulting layers were then dried at room temperature for one day and finally at 35 ° C. for 3 hours.
- an ethylene-propylene-diene terpolymer (Buna EP G-KA 8869, Bayer AG) were dissolved in 260 ml of toluene at 110.degree. After cooling the solution to 60 ° C, 20 g of dicumyl peroxide was added and stirring was continued until the solution was clear and homogeneous (about 1
- a pigmented elastomeric pressure element-forming layer V was prepared as follows: 87% by weight of an ethylene-propylene-diene terpolymer (Buna EP G-KA 8869, Bayer AG) and 13 wt .-% of a basic carbon black (Printex® A, Degussa Huels) were in a Haake lab kneader pre-compounded. The precompound was subsequently in so much Toluene solved that a 25 weight percent solution was formed in toluene. The way prepared solution was so by means of a laboratory knife on a PET protective film applied so that after evaporation of the solvent, a dry layer thickness of about 800 microns was obtained.
- the two-layer composite D1 / V was then produced by laminating the depot layer described.
- Example 6a (comparative example )
- the resulting two-layer composite of peroxide depot and pigmented elastomeric pressure element forming layer was at room temperature for one week stored.
- the two-layer composite D1 / V from example 6a was heated to 160 ° C. after storage for one week for a period of 20 minutes in a normal air atmosphere.
- the two-layer composite D1 / V from Example 6a was first heat-treated at 80 ° C. for 3 hours and then heated to 160 ° C. for a period of 20 minutes in a normal air atmosphere.
- Another peroxide depot layer D1 was prepared as follows: 80 g of Kraton® D-1161 NU were dissolved in 190 ml of toluene at 110 ° C. After cooling the solution to 60 ° C, 20 g of dicumyl peroxide was added and stirring was continued until the solution was clear and homogeneous (about 1 hour). The solution thus prepared was applied by means of a laboratory knife in different thicknesses on a PET protective film. The resulting layers were then dried at room temperature for one day and finally at 35 ° C. for 3 hours.
- a pigmented elastomeric pressure-element-forming layer V was prepared as follows: 88.6% by weight of components of a nyloflex® FAH printing plate and 11.4% by weight of a basic carbon black (Printex® A, Degussa-Huels) were dissolved in a Haake Laborkneter pre-compounded. The precompound was then dissolved in enough toluene to form a 40% by weight solution in toluene. The solution prepared in this way was applied to a PET protective film by means of a laboratory knife in such a way that, after evaporation of the solvent, a dry layer thickness of about 800 ⁇ m was obtained. The two-layer composite D1 / V was then produced by laminating the depot layer described.
- Example 7a (comparative example )
- the resulting two-layer composite of peroxide depot and pigmented elastomeric pressure element forming layer was at room temperature for one week stored.
- the two-layer composite D1 / V from Example 7a was heated at 160 ° C. for one week after storage for a period of 20 minutes in a normal air atmosphere.
- the two-layer composite D1 / V from Example 7a was first heat-treated at 80 ° C. for 3 hours and then heated to 160 ° C. for a period of 20 minutes in a normal air atmosphere.
- Example no Base layer thickness [ ⁇ m] Depot layer thickness [ ⁇ m] Extract content of toluene [%] Breaking stress [MPa] Elongation at break [%] evaluation A1 / / 100 0.1 105 crosslinked A2 / / 36 nb nb networked, degradation 1a 800 100 100 0.2 125 crosslinked 2a 780 120 100 0.2 125 crosslinked 3a 805 95 100 0.2 130 crosslinked 6a 800 120 0.2 378 crosslinked 1b 800 100 8th 2.0 100 crosslinked 2 B 780 120 8th 1.5 60 networked 3b 805 95 9 2.4 110 networked 6b 800 120 18 0.8 125 networked 1c 800 100 8th 2.2 110 networked 2c 780 120 8th 1.7 80 networked 3c 805 95 8th 4.3 170 networked 6c 800 120 6 2.4 310 networked
- Example no Base layer thickness [ ⁇ m] Depot layer thickness [ ⁇ m] Extract content of toluene [%] Breaking stress [MPa] Elongation at break [%] evaluation B1 / / 100 0.1 140 crosslinked B2 / / 32 nb nb networked, degradation 4a 820 80 100 ⁇ 0.1 75 crosslinked 4a 770 130 100 ⁇ 0.1 70 crosslinked 5a 790 110 100 0.1 330 crosslinked 7a 800 70 100 0.1 150 crosslinked 4b 820 80 20 1.7 630 networked 4b 770 130 20 1.7 735 networked 5b 190 110 20 0.7 250 networked 7b 800 70 13 2.1 90 networked 4c 820 80 28 1.5 685 networked 4c 770 130 13 1.7 900 networked 5c 790 110 18 0.7 145 networked 7c 800 70 3 4.3 130 networked
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Plasma & Fusion (AREA)
- Manufacturing & Machinery (AREA)
- Printing Plates And Materials Therefor (AREA)
- Manufacture Or Reproduction Of Printing Formes (AREA)
- Laminated Bodies (AREA)
- Addition Polymer Or Copolymer, Post-Treatments, Or Chemical Modifications (AREA)
- Thermal Transfer Or Thermal Recording In General (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Manufacture Of Macromolecular Shaped Articles (AREA)
Description
wobei die Vorläuferschicht V
und die Depotschicht D
Der Zweischichtenverbund D1/V wurde dann durch Einkalandrieren der beschriebenen Depotschichten hergestellt, wobei als zweiter dimensionsstabiler Träger eine handelsübliche PET-Folie verwendet wurde.
Der Zweischichtverbund D1/V wurde dann durch Aufkaschieren der beschriebenen Depotschicht hergestellt.
| Beispiel Nr. | Basisschichtdicke [µm] | Depotschichtdicke [µm] | Extraktanteil Toluol [%] | Bruchspannung [MPa] | Reissdehnung [%] | Beurteilung |
| A1 | / | / | 100 | 0,1 | 105 | unvernetzt |
| A2 | / | / | 36 | n.b. | n.b. | vernetzt, Abbau |
| 1a | 800 | 100 | 100 | 0,2 | 125 | unvernetzt |
| 2a | 780 | 120 | 100 | 0,2 | 125 | unvernetzt |
| 3a | 805 | 95 | 100 | 0,2 | 130 | unvernetzt |
| 6a | 800 | 120 | 0,2 | 378 | unvernetzt | |
| 1b | 800 | 100 | 8 | 2,0 | 100 | vemetzt |
| 2b | 780 | 120 | 8 | 1,5 | 60 | vernetzt |
| 3b | 805 | 95 | 9 | 2,4 | 110 | vernetzt |
| 6b | 800 | 120 | 18 | 0,8 | 125 | vernetzt |
| 1c | 800 | 100 | 8 | 2,2 | 110 | vernetzt |
| 2c | 780 | 120 | 8 | 1,7 | 80 | vernetzt |
| 3c | 805 | 95 | 8 | 4,3 | 170 | vernetzt |
| 6c | 800 | 120 | 6 | 2,4 | 310 | vernetzt |
| Beispiel Nr. | Basisschichtdicke [µm] | Depotschichtdicke [µm] | Extraktanteil Toluol [%] | Bruchspannung [MPa] | Reissdehnung [%] | Beurteilung |
| B1 | / | / | 100 | 0,1 | 140 | unvernetzt |
| B2 | / | / | 32 | n.b. | n.b. | vernetzt, Abbau |
| 4a | 820 | 80 | 100 | < 0,1 | 75 | unvernetzt |
| 4a | 770 | 130 | 100 | < 0,1 | 70 | unvernetzt |
| 5a | 790 | 110 | 100 | 0,1 | 330 | unvernetzt |
| 7a | 800 | 70 | 100 | 0,1 | 150 | unvernetzt |
| 4b | 820 | 80 | 20 | 1,7 | 630 | vernetzt |
| 4b | 770 | 130 | 20 | 1,7 | 735 | vernetzt |
| 5b | 190 | 110 | 20 | 0,7 | 250 | vernetzt |
| 7b | 800 | 70 | 13 | 2,1 | 90 | vernetzt |
| 4c | 820 | 80 | 28 | 1,5 | 685 | vernetzt |
| 4c | 770 | 130 | 13 | 1,7 | 900 | vernetzt |
| 5c | 790 | 110 | 18 | 0,7 | 145 | vernetzt |
| 7c | 800 | 70 | 3 | 4,3 | 130 | vernetzt |
Claims (10)
- Verfahren zur Herstellung eines lasergravierbaren Flexodruckelements, umfassend eine thermisch vernetzte, elastomere, lasergravierbare reliefbildende Schicht E mit den Schritten:(i) Herstellen eines Mehrschichtverbundes, mindestens umfassend einen Zweischichtverbund aus einer Depotschicht D und einer der Depotschicht D direkt benachbarten unvernetzten Vorläuferschicht V für die reliefbildende Schicht E, und gegebenenfalls weitere Schichten, Trägerfolien und/oder Schutzfolien,
wobei die Vorläuferschicht Venthalten,(a) mindestens ein elastomeres Bindemittel,(b) mindestens ein ethylenisch ungesättigtes Monomer,(c) gegebenenfalls einen Absorber für Laserstrahlung, sowie(d) gegebenenfalls weiteren Additive,
wobei die Depotschicht D(e) mindestens ein elastomeres Bindemittel,(f) mindestens einen thermisch zerfallenden Polymerisationsinitiator,(g) gegebenenfalls einen Absorber für Laserstrahlung, sowie(h) gegebenenfalls weitere Additiven,(ii) Eindiffundieren lassen der thermisch zerfallenden Polymerisationsinitiatoren aus der Depotschicht D in die Vorläuferschicht V,(iii) gegebenenfalls Entfernen der Depotschicht D, und(iv) thermische Vernetzung der Vorläuferschicht V zu der vernetzten elastomeren, lasergravierbaren reliefbildenden Schicht E. - Verfahren nach Anspruch 1, dadurch gekennzeichnet, dass der Zweischichtverbund aus D und V durch Extrudieren einer Schmelze, enthaltend die Komponenten (a) bis (d), und Kalandrieren dieser Schmelze zwischen eine erste Folie und eine zweite Folie, wobei mindestens eine Folie mit der Depotschicht D beschichtetet ist, hergestellt wird.
- Verfahren nach Anspruch 1, dadurch gekennzeichnet, dass der Zweischichtverbund aus D und V durch Kaschieren einer mit der Depotschicht D beschichteten ersten Folie auf eine mit der Vorläuferschicht V beschichteten zweiten Folie hergestellt wird.
- Verfahren nach Anspruch 1, dadurch gekennzeichnet, dass der Zweischichtverbund aus D und V durch Auftragen einer formbaren Mischung, Lösung oder Dispersion, enthaltend die Komponenten (a) bis (d), auf eine Folie, die mit der Depotschicht D beschichtet ist, und gegebenenfalls anschließendem Trocknen hergestellt wird.
- Verfahren zur Herstellung einer Reliefdruckplatte mit den Schritten (i) bis (iv), wie in einem der Ansprüche 1 bis 4 definiert, und dem zusätzlichen Schritt(v) Eingravieren eines druckenden Reliefs in die thermisch vernetzte, elastomere reliefbildende Schicht E mittels eines Lasers.
- Verfahren nach Anspruch 5, dadurch gekennzeichnet, dass die Depotschicht D auf der druckenden Seite des Flexodruckelements vorliegt und das Relief in die Depotschicht D, die ein Laserlicht absorbierendes Material enthält, und die darunter liegende elastomere reliefbildende Schicht E eingraviert wird.
- Mehrschichtverbund, umfassend in der Reihenfolge (I) - (VII)(I) eine Trägerfolie S,(II) gegebenenfalls eine Haftschicht A,(III) eine haftende Depotschicht D,(IV) eine Vorläuferschicht V,(V) eine Oberschicht T,(VI) gegebenenfalls eine Entklebungsschicht (Release-Schicht) R,(VII) eine abziehbare Schutzfolie P, worin D und V nach Anspruch 1 definiert sind.
- Mehrschichtverbund, umfassend in der Reihenfolge (I) - (V)(I) eine Trägerfolie S,(II) eine Haftschicht A,(III) eine Vorläuferschicht V,(IV) eine lasergravierbare Depotschicht D,(V) eine abziehbare Schutzfolie P, worin D und V nach Anspruch 1 definiert sind.
- Mehrschichtverbund, umfassend in der Reihenfolge (I) - (V)(I) eine Trägerfolie S,(II) eine Haftschicht A,(III) eine Vorläuferschicht V,(IV) eine nicht haftende, entfernbare Depotschicht D,(V) eine abziehbare Schutzfolie P, worin D und V nach Anspruch 1 definiert sind.
- Mehrschichtverbund, umfassend in der Reihenfolge (I) - (VI)(I) eine abziehbare Schutzfolie P,(II) gegebenenfalls eine Entklebungsschicht (Release-Schicht) R,(III) eine Oberschicht T,(IV) eine Vorläuferschicht V,(V) eine nicht haftende, entfernbare Depotschicht D,(VI) eine abziehbare Schutzfolie P, worin D und V nach Anspruch 1 definiert sind.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10100514A DE10100514A1 (de) | 2001-01-08 | 2001-01-08 | Verfahren zur Herstellung von thermisch vernetzten, lasergravierbaren Flexodruckelementen |
| DE10100514 | 2001-01-08 | ||
| PCT/EP2002/000066 WO2002054154A2 (de) | 2001-01-08 | 2002-01-07 | Verfahren zur herstellung von thermisch vernetzten, lasergravierbaren flexodruckelementen |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1353802A2 EP1353802A2 (de) | 2003-10-22 |
| EP1353802B1 true EP1353802B1 (de) | 2004-08-18 |
Family
ID=7669948
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP02702237A Expired - Lifetime EP1353802B1 (de) | 2001-01-08 | 2002-01-07 | Verfahren zur herstellung von thermisch vernetzten, lasergravierbaren flexodruckelementen undmehrschichtverbunde |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US6794115B2 (de) |
| EP (1) | EP1353802B1 (de) |
| JP (1) | JP2004522618A (de) |
| AT (1) | ATE273796T1 (de) |
| AU (1) | AU2002235819A1 (de) |
| DE (2) | DE10100514A1 (de) |
| WO (1) | WO2002054154A2 (de) |
Families Citing this family (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2295145C9 (ru) * | 2001-08-03 | 2008-04-10 | XSYS Принт Солюшенс Дойчланд ГмбХ | Фоточувствительный флексографский элемент и способ изготовления формных пластин флексографской печати для печатания газет |
| AU2002364255A1 (en) | 2001-12-24 | 2003-07-15 | Digimarc Id Systems, Llc | Covert variable information on id documents and methods of making same |
| US7694887B2 (en) | 2001-12-24 | 2010-04-13 | L-1 Secure Credentialing, Inc. | Optically variable personalized indicia for identification documents |
| AU2002353174A1 (en) | 2001-12-24 | 2003-07-15 | Digimarc Id Systems, Llc | Laser engraving methods and compositions |
| AU2002364746A1 (en) | 2001-12-24 | 2003-07-15 | Digimarc Id Systems, Llc | Systems, compositions, and methods for full color laser engraving of id documents |
| US7728048B2 (en) | 2002-12-20 | 2010-06-01 | L-1 Secure Credentialing, Inc. | Increasing thermal conductivity of host polymer used with laser engraving methods and compositions |
| US7207494B2 (en) | 2001-12-24 | 2007-04-24 | Digimarc Corporation | Laser etched security features for identification documents and methods of making same |
| WO2003088144A2 (en) | 2002-04-09 | 2003-10-23 | Digimarc Id Systems, Llc | Image processing techniques for printing identification cards and documents |
| US7824029B2 (en) | 2002-05-10 | 2010-11-02 | L-1 Secure Credentialing, Inc. | Identification card printer-assembler for over the counter card issuing |
| DE10227189A1 (de) * | 2002-06-18 | 2004-01-08 | Basf Drucksysteme Gmbh | Verfahren zur Herstellung von Flexdruckformen mittels Laser-Direktgravur |
| US7804982B2 (en) | 2002-11-26 | 2010-09-28 | L-1 Secure Credentialing, Inc. | Systems and methods for managing and detecting fraud in image databases used with identification documents |
| US7763179B2 (en) | 2003-03-21 | 2010-07-27 | Digimarc Corporation | Color laser engraving and digital watermarking |
| ATE491190T1 (de) | 2003-04-16 | 2010-12-15 | L 1 Secure Credentialing Inc | Dreidimensionale datenspeicherung |
| WO2005084959A1 (en) * | 2004-03-03 | 2005-09-15 | Kodak Il Ltd. | Novel material for infrared laser ablated engraved flexographic printing plates |
| US7284484B2 (en) | 2005-06-02 | 2007-10-23 | Van Denend Mark E | Laser ablating of printing plates and/or printing rollers to decrease taper and TIR |
| US7750267B2 (en) * | 2006-04-25 | 2010-07-06 | Van Denend Mark E | Apparatus and method for laser engraveable printing plates |
| WO2009084682A1 (ja) * | 2007-12-27 | 2009-07-09 | Asahi Kasei E-Materials Corporation | レーザー彫刻印刷原版用熱硬化性樹脂組成物 |
| JP5261014B2 (ja) * | 2008-04-23 | 2013-08-14 | 旭化成イーマテリアルズ株式会社 | レーザー彫刻用印刷原版およびその製造に用いる樹脂組成物 |
| US20100075117A1 (en) * | 2008-09-24 | 2010-03-25 | Fujifilm Corporation | Relief printing plate precursor for laser engraving, method of producing the same, relief printing plate obtainable therefrom, and method of producing relief printing plate |
| US8221577B2 (en) * | 2008-12-04 | 2012-07-17 | Eastman Kodak Company | Fabricating thermoset plates exhibiting uniform thickness |
| JP5658435B2 (ja) | 2009-03-31 | 2015-01-28 | リンテック株式会社 | マスクフィルム用部材、それを用いたマスクフィルムの製造方法及び感光性樹脂印刷版の製造方法 |
| JP5409340B2 (ja) * | 2009-12-25 | 2014-02-05 | 富士フイルム株式会社 | 熱架橋性レーザー彫刻用樹脂組成物、レーザー彫刻用レリーフ印刷版原版及びその製造方法、並びに、レリーフ印刷版及びその製版方法 |
| JP5609499B2 (ja) * | 2010-09-30 | 2014-10-22 | 東レ株式会社 | 凸版印刷版原版の製造方法 |
| JP5274599B2 (ja) * | 2011-02-22 | 2013-08-28 | 富士フイルム株式会社 | レーザー彫刻用レリーフ印刷版原版及びその製造方法、並びに、レリーフ印刷版及びその製版方法 |
| CN102789130A (zh) * | 2012-08-06 | 2012-11-21 | 深圳市宏瑞新材料科技有限公司 | 底片保护膜及其制作方法 |
| EP3159740B1 (de) * | 2015-10-22 | 2018-08-01 | Flint Group Germany GmbH | Verfahren zu generativen herstellung von reliefdruckformen |
| CN114573037B (zh) * | 2022-01-25 | 2023-09-22 | 中国人民解放军国防科技大学 | 一种激光辐照快速制备吸波材料的方法 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4323636A (en) | 1971-04-01 | 1982-04-06 | E. I. Du Pont De Nemours And Company | Photosensitive block copolymer composition and elements |
| CA1099435A (en) | 1971-04-01 | 1981-04-14 | Gwendyline Y. Y. T. Chen | Photosensitive block copolymer composition and elements |
| US4427759A (en) | 1982-01-21 | 1984-01-24 | E. I. Du Pont De Nemours And Company | Process for preparing an overcoated photopolymer printing plate |
| DE4202332A1 (de) | 1992-01-29 | 1993-08-05 | Basf Lacke & Farben | Lichtempfindliches gemisch zur herstellung von relief- und druckformen |
| US5798202A (en) | 1992-05-11 | 1998-08-25 | E. I. Dupont De Nemours And Company | Laser engravable single-layer flexographic printing element |
| US5804353A (en) * | 1992-05-11 | 1998-09-08 | E. I. Dupont De Nemours And Company | Lasers engravable multilayer flexographic printing element |
| US5259311A (en) | 1992-07-15 | 1993-11-09 | Mark/Trece Inc. | Laser engraving of photopolymer printing plates |
| DE19536805A1 (de) * | 1995-10-02 | 1997-04-03 | Basf Lacke & Farben | Zur Herstellung von Flexodruckplatten durch digitale Informationsübertragung geeignetes mehrschichtiges Aufzeichnungselement |
| DE19628541A1 (de) | 1996-07-16 | 1998-01-22 | Du Pont Deutschland | Strahlungsempfindliche Zusammensetzung und ein diese enthaltendes strahlungsempfindliches Aufzeichnungsmaterial |
| DE19711696C1 (de) * | 1997-03-20 | 1998-11-12 | Basf Drucksysteme Gmbh | Verfahren zum Herstellen eines photopolymerisierbaren Aufzeichungsmaterials |
-
2001
- 2001-01-08 DE DE10100514A patent/DE10100514A1/de not_active Withdrawn
-
2002
- 2002-01-07 EP EP02702237A patent/EP1353802B1/de not_active Expired - Lifetime
- 2002-01-07 AT AT02702237T patent/ATE273796T1/de not_active IP Right Cessation
- 2002-01-07 DE DE50200856T patent/DE50200856D1/de not_active Expired - Lifetime
- 2002-01-07 US US10/250,867 patent/US6794115B2/en not_active Expired - Lifetime
- 2002-01-07 AU AU2002235819A patent/AU2002235819A1/en not_active Abandoned
- 2002-01-07 WO PCT/EP2002/000066 patent/WO2002054154A2/de not_active Ceased
- 2002-01-07 JP JP2002554788A patent/JP2004522618A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| JP2004522618A (ja) | 2004-07-29 |
| WO2002054154A3 (de) | 2002-09-19 |
| EP1353802A2 (de) | 2003-10-22 |
| US6794115B2 (en) | 2004-09-21 |
| AU2002235819A1 (en) | 2002-07-16 |
| US20040048198A1 (en) | 2004-03-11 |
| DE10100514A1 (de) | 2002-07-11 |
| ATE273796T1 (de) | 2004-09-15 |
| DE50200856D1 (de) | 2004-09-23 |
| WO2002054154A2 (de) | 2002-07-11 |
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