RADIATION-CURABLE COMPOSITIONS COMPRISING MALEIMIDE COMPOUNDS AND METHOD FOR PRODUCING A SUBSTRATE WITH A
CURED LAYER
The invention relates generally to radiation-curable compositions comprising maleimide compounds, to a substrate with a cured coating, and to methods for producing the same. In particular, the present invention relates to radiation-curable compositions, comprising maleimide compounds, suitable for use in filled compositions as inks, coatings, hard coats, lacquers and/or adhesives for substrates such as plastic films, metal films, fiber optics, recordable media, compact discs (CD and CD-R) , digital versatile discs (DVD) , as well as thin layer stereolithographic or rapid prototyping applications.
BACKGROUND OF THE INVENTION Numerous photoinitiators with varying structures are commercially available for use in different systems. However, nearly all commercially available radiation curing processes require a large percentage of these expensive initiators to be incorporated into the formulation. Many times the cost of the overall system is significantly impacted by the presence of these expensive initiators.
Although large percentages are required to achieve the desired cure rates, a relatively large
portion of the expensive photoinitiators added is not consumed or does not bind into the cured system. Indeed, the use of these conventional photoinitiators typically results m the production of small molecule photo-byproducts. The presence of the residual photoactive compounds or extractables result m degradation of the physical properties of the cured system, such as decreased color fastness, discoloration, and lower resistance to oxidative degradation. In addition, the residual photomitiator and/or photo-byproducts lead to slow release of contaminants to the environment and contribute to long-term degradation in performance of the cured system.
Moreover, it is generally believed that thin coatings of conventional radiation-curable compositions do not cure well at low radiation dose levels because of an oxidation or oxygen inhibition effect. The oxygen inhibition effect most strongly effects coating surfaces that are exposed or were exposed to air or other oxygen rich environments for extended periods. It is believed that oxygen is absorbed into the coating which interferes with or prevents the curing of radiation-curable compositions using conventional photoinitiators, particularly at low radiation levels. The thinner the coating layer the more profound the oxygen inhibition effect, due to the high surface area to volume ratio which supports fast oxygen diffusion into the layer.
WO 98/07759 discusses a method for photopolymerizmg and photopolymerizable compositions comprising maleimide compounds. In particular, this reference discusses the use of several mono- and multifunctional aliphatic maleimide compounds for the
photopolymerization of acrylates, in other words, as photoinitiating compounds. According to WO 98/07759, the photopolymerizable compositions comprise aliphatic amines as co- initiators to improve cure speed. The disadvantage of such compositions is that they cure at lower rates and require higher dosages of energy to cure than compositions using conventional photoinitiators. For example, in WO 97/31981 150 micrometer thick layers of radiation- curable compositions comprising e.g. maleimide compounds are cured with a UV dose of 2 J/cm2, whereas in practice often less than 0.5 J/cm2 is used.
Summary of the Invention An object of the present invention is to provide a method for producing a coated substrate, and a radiation-curable composition that allows a high cure rate, in particular a cure rate comparable with conventional photoinitiated compositions. More in particular a curing rate such that at 0.5 J/cm2 irradiation more than 85% of the ethylenically- unsaturated functional groups of the radiation-curable composition have reacted, preferably more than 90%, preferably, at the bottom as well as at the surface of the layer of the radiation-curable composition applied on the substrate.
A further object of the present invention is to provide radiation-curable filled compositions, ink, coating, hard coat, lacquer and/or adhesive compositions comprising maleimide compounds, that are suitable for substrates such as plastic films, metal films, fiber optics (including coated fiber optics), recordable media (e.g., as a hardcoat) , CD and CD-R
lacquers, DVD adhesives and/or thin layer stereolithographic or rapid prototyping applications.
Another object of the present invention is to provide a radiation-curable composition that minimizes and/or overcomes the effect of oxygen inhibition and achieves suitable surface and/or through cure particularly when applied m thin layers (i.e., 20 μm or less, preferably 15 μm or less) .
The present invention relates to radiation- curable compositions comprising a) at least one compound having ethylenically unsaturated bonds other than those m maleimide groups as defined under (b) , further called maleimide-free compound; b) at least one aliphatic maleimide compound; and c) an aliphatic amme group comprising compound wherein component (c) is an amme functional acrylic polymer. Surprisingly, the amme functional acrylic polymer is very effective as amme synergist and the resulting composition shows a remarkably good cure speed. Moreover, said amines are non-extractable .
The invention also relates to a radiation curable ink composition for coloring coated optical glass fibers wherein the ink composition comprises a (meth) acrylate functional oligomer, a reactive diluent, a maleimide compound (b) , and at least one pigment m an amount of about 1 to about 15 wt . % . Further, the invention relates to a radiation-curable DVD adhesive composition, to a radiation-curable CD or CD-R lacquer, to a substrate with a cured layer and to two substrates adhered to each other with a cured layer.
The invention relates to a coated optical fiber and to a ribbon or bundle of a plurality of coated optical fibers.
The present invention is thus directed to radiation-curable compositions comprising maleimide compounds, which can act as polymerization initiators. In contrast to conventional photoinitiators, substantially all of the maleimides are consumed during initiation and/or photopolymeπzation . Thus, the present invention can minimize or eliminate problems associated with the residue (s) resulting from the use of large percentages of conventional photoinitiators.
The invention further relates to a method for producing a substrate with a cured layer comprising the steps of:
(l) applying a radiation-curable composition to a substrate to form a layer on the substrate wherein the composition comprises a) at least one maleimide-free compound having ethylenically unsaturated bonds, and b) at least one aliphatic maleimide compound; and
(ii) radiation-curmg said layer with radiation of a wavelength between 200-800 nm, characterized that the composition is applied m such a way that the layer before cure has a thickness of less than about 20 micrometer .
Preferably, said method for producing a substrate with a cured layer is used for at least one of the previously described applications and is not used for testing purposes.
In common applications, the surface that is at least partially coated and at least partially cured
is at least about 1 cm2, preferably at least about 2 cm2, more preferably at least about 3 cm2.
Preferably, the substrate is not a gold- coated aluminium plate. In another preferred embodiment the method for producing a substrate with a cured layer does not comprise a step, such as for example a pre-bake or post-bake step at higher temperatures, such as in the range of between 80 and 200°C. Optionally, the coating composition according to the present invention contains a non- reactive solvent. If the coating composition contains a non-reactive solvent, the layer according to the present invention can even be applied in a thickness greater than 20 micrometer, if - after evaporation of the non-reactive solvent - a layer before cure is obtained of less than about 20 micrometer. Preferably, the layer before cure has a thickness of between 1 and 19 micrometer, more preferably between 2 and 15 micrometer, most preferred between 2 and 10 micrometer.
When aliphatic maleimides are used in compositions applied in said thin layers, the degree of cure is surprisingly good. Thus, surprisingly, a thickness effect has been observed when using maleimide compounds as photoinitiating compounds instead of or additionally to conventional photoinitiators. When using relatively low cure doses, maleimide containing layers having a thickness of greater than 20 μm (e.g. 100 μm) show insufficient bottom or through-cure whereas -surprisingly- when said layers are applied in a thickness of less than 20 μm, the through-cure is remarkably better.
Furthermore, the invention relates to a method for producing a substrate with a cured layer wherein a radiation-curable composition comprising a) at least one compound having ethylenically unsaturated bonds other than those in maleimide groups as defined under (b) , and (b) at least one aliphatic maleimide compound, is applied to a substrate to form a layer on the substrate that is sufficiently thin that said layer, when radiation-cured with an irradiation of 0,125 J/cm2, is characterized by more than 85% reaction of the ethylenically unsaturated groups at the bottom and at the surface of said layer.
The bottom of said layer can be defined as that side of the layer which is located close to or against the substrate .
DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS OF THE
PRESENT INVENTION
Preferably, the radiation-curable composition of the present invention is applied m such a thickness that the layer after evaporation of non- reactive solvent, which optionally is present, and before cure has a thickness of less than about 20 micrometer; preferably less than about 19 micrometer, more preferably less than about 15 micrometer, and particularly preferred less than about 10 micrometer. Typically, the thickness will be greater than about 1 micrometer, preferably greater than about 2 micrometer. Generally speaking, a coating can shrink between about 4 and about 8 % by curing. Hence, a cured coating will have a thickness of less than the original pre-coat
thickness. The term "original pre-coat thickness" relates to the thickness of the uncured coating as applied and after evaporation of non-reactive solvent, which optionally is present. The radiation-curable composition comprises a) at least one maleimide-free compound having ethylenically-unsaturated functionality and b) at least one maleimide compound.
Both components a) and b) may include mixtures of compounds. Maleimide-free herein refers to compounds that do not include a maleimide moiety.
Examples of the ethylenically-unsaturated functional group in compounds of component (a) include (meth) acrylate, propenylether, vinylether, allylether, (substituted) styrene, N-vinyl, fumarate, maleate, itaconate, (meth) acrylamide, and mixtures of these. Preferred ethylenically-unsaturated functional groups are (meth) acrylate, N-vinyl, styrene and vinylether. Most preferred compounds for component (a) include (meth) acrylate functional compounds.
The term "acrylate (d) " as further used herein can be defined as acrylate (d) or as methacrylate (d) .
Component (a) is preferably a mixture of oligomers and reactive diluents. Component (a) may be present in an amount of between 20 wt . % and 90 wt . % , preferably between 35 wt . % and 70 wt. %, more preferably between 40 wt . % and 65 wt . %. Also preferred is a mixture of monofunctional and multifunctional compounds. Examples of suitable oligomers comprise acrylated polyethers, acrylated polyesters, acrylated urethanes, acrylated epoxies, vinyl -ether functional urethanes and the like. For example, the acrylated
urethanes can have polyether, polyester, polycarbonate, hydrocarbon backbones and the like.
The reactive diluents can be mono- or multi-functional. Examples of suitable reactive diluents are laurylacrylate, ethylacrylate , ethoxyethylacrylate , phenoxyethylacrylate , hexanedioldiacrylate , triethyleneglycol divinylether, trimethylol propanetriacrylate , isobornylacrylate, N- vinyl caprolactone, N-vinyl pyrrolidone, diethyleneglycol diacrylate, cyclohexyldimethanol diacrylate and the like.
In one embodiment of the invention, the radiation-curable composition comprises compounds having electron rich and electron poor double bonds, as described in EP-A-618237 and WO 97/31981, the entire disclosure of each are hereby incorporated by reference. The composition can comprise at least one ethylenically unsaturated compound having an electron donating group and at least one ethylenically unsaturated compound having an electron withdrawing group. In another preferred embodiment, the composition comprises only electron-poor double bonds such as (meth) acrylates , fumarate compounds, maleate compounds, maleimide compounds and the like. Suprisingly, the composition comprising only electron-poor double bonds and at least an aliphatic maleimide compound according to the present invention results in a remarkably good cure speed and achieves the objectives of the present invention. The maleimide component b) includes aliphatic maleimides which includes maleimides wherein a non-aromatic group is attached to the nitrogen of the maleimide group. Suitable compounds include mono- and
multifunctional maleimide compounds. Further suitable maleimide compounds are described in WO 98/07759 and WO 97/31981, the entire disclosure of each are hereby incorporated by reference.
Preferred maleimides include those which are represented by formula (1) or (2) as follows:
X
X
wherein X independently represents an 0 or S atom, wherein R1 represents a carbon chain comprising at least one organic group like alkyl, alkanol , alkanon, alkyl - aryl wherein a non-aromatic saturated carbon chain is attached to the nitrogen of the maleimide, and wherein FG represents a reactive functional group like amine, hydroxy, acrylate, or a linking group like ester, carbonate, urea, urethane, ether and the like. R1 may include 1, 2 or more carbon atoms. Generally, R1 will comprise less than 20 carbon atoms, preferably less than 10. Preferably, R1 is an aliphatic alkylene group, more preferably, a straight chain alkylene, but
it may comprise a cyclic group. One particularly preferred compound is cyclohexyl maleimide. Preferably, R1 comprises 1 or 2 methylene carbon spacers, more preferred 1 methylene carbon spacer. Compounds comprising two or more maleimide groups, further called multi-functional maleimide compounds, are very suitable as well.
In a preferred embodiment of the present invention, the maleimide compound comprises one or more groups according to formula (3)
X
wherein R2 is represented by one of the following
if
■c- Ύ-FT (3a)
—Y-C-R3 <3M
,3
Y-C-R . or (3c
wherein each X, independently, represent an 0 or S atom,
Y represents an O or S atom or an NH radical, Z1 and Z2 independently represent an 0 or S atom or an
NR5 radical, and wherein R3, R4 and R5 can independently represent a H atom or an organic radical.
In a preferred embodiment, the maleimide compound is a multifunctional maleimide compound. Such compound preferably is a compound according to formula
(3) wherein R3 , or at least R3 or R4 is the remainder of the backbone of a multifunctional maleimide compound. The unsaturated bond of the maleimide preferably is unsubstituted. However, the maleimide may be substituted with one alkyl or aryl group with 1-6 carbon atoms. Hence, the unsaturated bond of the maleimide in the formulae of this application can be denoted as HC = CR4 wherein R4 represent a hydrogen atom or an alkyl or aryl group with 1-6 carbon atoms. If both R4 groups are alkyl groups, the cure speed severely lowers or at least, the maleimide compound does not polymerize due to steric hinderance .
The molecular weight of the maleimide compound will generally be higher than 110 and preferably higher than 150. The molecular weight of the
maleimide compound generally will be lower than about 100,000, although the upper limit is not critical, and will be mainly determined by viscosity limitations of the radiation-curable composition. Preferably, the molecular weight will be lower than about 50,000, more preferably, lower than about 10,000, and particularly preferred below about 5,000 because such molecular weights make it more easy to formulate radiation curable compositions without non-reactive diluents. Molecular weight as used herein, unless otherwise specified, is (for oligomeric compounds) the number average molecular weight, as determined by GPC with polystyrene standards .
Multifunctional maleimide groups comprising compounds according to the invention and exemplified by formula (3) appear to be very efficient for the induction of photopolymeπzation of for example acrylates, even m the absence of any other photomitiator . Preferably, the multifunctional maleimide compound has a functionality of 1.6 or higher, more preferably 1.9 or higher, m particular preferred 2.5 or higher, as a higher functionality appears to improve cure speed and to give cured products with lower photomitiator based extractables .
The upper limit of the functionality seems to be non-critical , and the functionality will m general be lower than 20, preferably lower than 10 and m particular will be about 5 or lower. The functional maleimide compound according to this invention preferably has a carbonate, urethane, ester, amme, amide, lmide or ether as the functional group .
In one particularly preferred embodiment the maleimide groups are present as depicted in formula (4)
wherein Y is as defined above. Most preferably, Y represent an O atom or a NH radical, and R3 is as defined above.
In another particularly preferred embodiment, the maleimide groups present may be represented by formula (5) as follows:
wherein Z1, Z2, R3 , R4 and R5 are as defined above. Preferably, either R3 or R4 represents a hydrogen atom and one of R3 or R4 is an organic group, being the remainder of the backbone of the maleimide compound.
Other preferred compounds include those represented by formulaes (6) -(8) as follows:
The maleimide groups are attached via the functional group to a remainder of the molecule.
The R3-group can be any suitable organic molecule such as hydrocarbons, polyesters, polyethers, polycarbonates, polyurethanes, polyimides, polyamides, polyacrylates and the like.
This molecule can be of low or high molecular weight and can comprise ethylenically unsaturated groups.
Suitable molecules can be derived from
hydroxy or amine functional molecules such as, for example, from cyclohexanol, butanol, triethylene glycol hexanediol, trimethylolpropane, pentaerythritol, dipentaerythritol , amine functional dendrimers like Astramol®, polyethyleneglycol , polypropylene-glycol , amine functional polyesters, available as Jeffamine®, acid or hydroxyfunctional polyesters derived from diols, diacids and/or hydroxy acids, acid, amino or hydroxyfunctional acrylic polymers, isophorone diisocyanate, toluene diisocyanate, and trimerization products therefrom, polycarbonate-diols , and the like.
For multifunctional compounds, preferred backbone molecules are polyethers, polycarbonates, polyesters, and acrylic polymers and most preferred polyalcohols and polyethers such as ethoxylated or propoxylated trimethylol propane or trimethylolethane, (ethoxylated) pentaerithritol , pentaerithritol diacrylate (propoxylated) glycerol, polytetrahydrofuran, polyethylenoxide, polypropyleneoxide and the like. Examples of suitable maleimide compounds include cyclohexylmaleimide, 2 -ethylhexylmaleimide, n- butylmaleimide, laurylmaleimide, triethyleneglycol- jbiscarbonatebisethylmaleimide, 2 -ethylcarbonate ethylmaleimide , 2-isopropylurethaneethyl maleimide, 2- acryloylethylmaleimide, acetoxyethylmaleimide , isophoronebisurethane bisethylmaleimide , jbisethylmaleimide carbonate, 4 , 9-dioxa-l , 12 dodecane jbismaleimide the reaction product of N [ (chloroformyl) methyl] maleimide with e.g. 1,6- hexanediol, trimethylolpropane, pentaerythritol, tri- or tetraethylene glycol, polypropyleneglycol , polytetramethyleneglycol , hydroxy functional polyester,
ethanol, n-butanol, t -butanol, monohydroxy functional polyethers, 4-hydroxybutylvinylether and the like. Preferably, cyclohexylmaleimide is used.
The maleimide compound preferably is present in the radiation-curable composition in an amount between 0.01-60 wt.%, preferably between 0.1-20 wt . % , more preferably between 0.2 and 10 wt.%.
The radiation-curable composition used in the method of the present invention comprises components (a) and (b) ; for purposes of definition of w . amounts, the total amount of (a) + (b) is 100 wt.%, and additional compounds that can be present are defined relative to the amount of (a) + (b) , unless otherwise specified. The compositions comprising (a) and (b) are radiation-curable as such. Nevertheless, cure speed can be further improved by using conventional photoinitiators, preferably free-radical photoinitiators such as type I and type II photoinitiators. Examples of suitable type I
(homolytic) photoinitiators are benzoin derivatives, methylolbenzoin and 4-benzoyl-l , 3 -dioxolane derivatives, benzilketals , α, α-dialkoxyacetophenones , α-hydroxy alkylphenones , α-aminoalkylphenones , acylphosphine oxides, acylphosphine sulphides, halogenated acetophenone derivatives and the like. Commercial examples of suitable type I photoinitiators are Darocur 1173 (2 -hydroxy-2 -methyl -1 -phenylpropane-1 - one as the active component) , Irgacure 184 (hydroxy- cyclohexyl phenyl ketone as the active component), Irgacure 907 (2 -methyl-1- [4 - ( ethylthio) phenyl] -2 - morpholino propan-1-one) , Irgacure 369 (2-benzyl-2-
dιmethylammo-1- (morpholmophenyl) -butan-1-one as the active component), acylphosphmes such as Luciπn TPO (2 , 4 , 6- tπmethylbenzoyl diphenyl phosphine oxide), Irgacure 819 (bis (2 , 4 , 6-trιmethylbenzoyl) -phenyl - phosphine- oxide) . Also mixtures of type I photoinitiators can be used. For pigmented systems such as inks, Irgacure 907 is preferred.
Examples of suitable Type- I I (hydrogen abstraction) photoinitiators aromatic ketones such as benzophenone, xanthone, derivatives of benzophenone, Michler's ketone, thioxanthone and other xanthone derivatives like ITX (isopropyl thioxanthone) , anthraqumones , coumarme m an amount between 0.1-10 wt.%, preferably at least 2.0 wt.% (relative to (a) + (b) ) . Chemical derivatives and combinations of these photoinitiators can also be used.
Type-II photoinitiators generally are used with an amme synergist .
When using compound (b) according to the present invention, with or without the presence of a Type-II photomitiator, amme synergists are not necessary, m particular if curing is performed under a nitrogen atmosphere. Hence, amme synergists (c) are preferably present m an amount of less than 1 wt.%, and more preferably less than 0.1 wt . % . If curing is performed under an oxygen containing atmosphere, like in air, an amme synergist (c) can be useful m amounts up to 10 wt.%, preferably amounts between 0.1-5 wt . % . Preferably, the amme synergist or amme compound (c) is chosen from the group consisting of a monomer tertiary amme compound, an oligomer (polymer) tertiary amme compound, a poly erizable am o acrylate
compound, a polymerized amino acrylate compound and mixtures thereof .
The amine-synergist may include tertiary amine compounds, such as alkanol-dialkylamines (e.g., ethanol-diethylamine), and ethylenically-unsaturated amine-functional compounds including amine-functional polymer compounds. The ethylenically-unsaturated amine compounds may also include dialkylaminoalkyl (meth) acrylates (e.g. , diethylaminoethylacrylate) or N-morpholinoalkyl-
(meth) acrylates (e.g., N-morpholinoethyl-acrylate) . It appeared that in particular N-morpholino-ethylacrylate was a very efficient amine-synergist when used in combination with an aliphatic maleimide like cyclohexylmaleimide, and with a type II photoinitiator like benzophenone and optionally in the presence of an amine functional acrylic polymer as further described.
Suitable amine functional, ethylenically- unsaturated polymer compounds may include acrylated polymers. Such acrylated polymers may include the acrylated acrylic polymers such as those described in U.S. Patent 5/847,021 (Tortorello et al . ) , the entire disclosure of which is hereby incorporated by reference. It will be appreciated that these same amine functional, ethylenically-unsaturated polymer compounds, such as an acrylic polymer comprising an aliphatic amine functional group, may be suitable as at least one maleimide-free compound (a) of the compositions and be present in the amounts noted above for component (a) , preferably in amounts between 35 and 70 wt . %.
In particular, the acrylated acrylic polymer may include those formed by a vinyl addition
copolymer formed by reacting at least one ethylenically-unsaturated, hydroxy functional co- polymerizable monomer with at least one ethylenically- unsaturated, amine functional monomer. The amine functional monomer may include tertiary amines and/or aliphatic amines and preferably aliphatic tertiary amines. Suitable ethylenically-unsaturated, amine functional monomers include dialkylaminoalkyl (meth) acrylates such as diethylaminoethyl acrylate and/or morpholino- alkyl (meth) acrylates such as N-morpholino- ethylacrylate . Preferably, the ethylenically- unsaturated polymer will comprise the vinyl addition, hydroxy and amine functional copolymer as a backbone with the ethylenically-unsaturated groups linked via urethane linkages. Most preferred is the amine functional acrylated acrylic polymer. These polymeric amine synergists appear to be very effective, and have the additional advantage that these amines are non- extractable, and are part of the ultimate network.
In one preferred embodiment of the present invention the radiation-curable composition comprises (a) at least one maleimide-free compound having ethylenically unsaturated bonds (b) a monofunctional aliphatic maleimide,
(c) an amine functional acrylated acrylic polymer, and
(d) a benzophenone compound.
Preferably, component (b) is cyclohexyl maleimide.
In another preferred embodiment of the present invention the radiation-curable composition comprises components (a) - (d) as described in the
previous preferred embodiment and additionally comprises a N-morpholmo (meth) acrylate , more preferably N-morpholmoethylacrylate as an amme- synergist . The radiation-curable composition optionally comprises, in addition to components (a), (b) and the at least one amme synergist (c) , a photomitiator (d) , These components are preferably present amounts, relative to the total weight of (a) + (b) + (c) of: component (b) 0.1-10 wt.%, component (c)
0.01-10 wt.%, more preferably 0.04-9.0 wt.% and component (d) 0.01-15 wt.%, more preferably 0.15-15 wt.%. Furthermore, it is preferred to use type II photoinitiators as component (d) . And when the maleimide component includes alkylmaleimides, it is preferred to use a higher amount of type II photomitiator than maleimide. Preferably, the type II photomitiator is present m an amount of more than 2 wt . % . The above amounts are m particular applicable if the compounds used have a relatively low molecular weight. Thus, if the amme forms part of a polymer, the amme group containing monomer with which the polymer is made will be present - m polymerized form - m 0.1-10 wt.%. Equally, if maleimide groups are part of a polymer, more than 10 wt.% of the maleimide comprising polymer can be used. The amounts can also be defined terms of equivalent molar amounts, m concreto by the units meq of functional group per g of the formulation. C4H2N02 is the functional group for the maleimide compound, benzophenone is taken as the functional group for the Type II photomitiator, and for the amme functional compound dimethylammo is
taken as the functional group. The amounts in equivalent molar amounts preferably will be 0.01 - 1.0 meq of maleimide groups per g of the formulation (more preferred 0.1-0.7 meq/g, particularly preferred, 0.1 to 0.5 meq/g); 0.01-0.8 meq of type II photomitiat g groups per g of the formulation (more preferred 0.05- 0.6 meq/g, particularly preferred, 0.1 to 0.4 meq/g) and 0.01-2 meq/g of alkylammo groups per gram of the formulation (more preferred 0.1-1.5 meq/g, particularly preferred 0.1 to 1.0 meq/g) .
In systems where fast curing is desired, it may be preferred to include additional ethylenically- unsaturated components particularly those with labile hydrogens . Suitable compounds include alkoxylated compounds, particularly alkoxylated monomers. These alkoxylated compounds may include ethoxylated and propoxylated compounds preferably having from 2-9 alkoxylated groups, for example, ethoxylated hexanedioldiacrylate, ethoxylated trimethylolpropane triacrylate, ethoxylated jbisphenol A dimethacrylate, ethoxylated nonyl phenol acrylate, propoxylated hexanedioldiacrylate, propoxylated trimethylolpropane triacrylate, propoxylated bisphenol A dimethacrylate, propoxylated nonyl phenol acrylate and propoxylated glycerol triacrylate.
In many applications of these radiation- curable compositions it is desirable for the cured composition to be transparent, m other words, to be derived from a curable layer which is substantially free of coloring agent. However, there are applications wherein it is desirable for the radiation-curable composition to include color, other words, wherein the radiation-curable composition further comprises at
least one coloring agent. For these applications, which include ink coatings for identification of coated optical fibers, pigments and/or colorants are added to the radiation-curable composition. Suitable pigments or dyes are for example copper phthalocyanme blue, crystal violet lactone (blue) , crystal malachite green, sheet fed rubme (red) . The amount of pigment, if used, will general be about 0.1 w . % to about 10 wt.%, preferably between about 0.2 wt.% and about 5 wt.% relative to the coating composition.
The radiation-curable compositions can further comprise other additives, fillers and the like, such as for example flow agents, stabilizers, antioxidants , slip agents, waxes, dyes, wetting agents and the like.
The radiation-curable coating composition can be cured by different kinds of radiation, such as UV and EB radiation. The most preferred irradiation source is ultraviolet light. With respect to UV-curing equipment we refer to, for example, pages 161-234 of Chemistry and Technology of UV and EB-formulations , Volume 1, Oldring 1991. Suitable lamps employed to provide the desired high intensity and suitable wavelength and spectral distribution include for example those available from Fusion Systems, Corp. Preferably, H, D or excimer lamps are used.
It is preferred to formulate radiation- curable compositions that require less than about 0.5 J/cm2 to achieve at least about 85 percent reacted acrylic unsaturation (% RAU) , more preferably more than about 90% RAU. It is particularly preferred that the radiation-curable composition achieve such % RAU with about 0.3 J/cm2 or less. Generally, an energy input of
at least about 0.05 J/cm2 particularly of about 0.1 J/cm2 or more is required to achieve the desired cure. The radiation-curable coating composition according to the invention can be used on different substrates, for example glass, paper, wood, plastic, brick, metals such as aluminum and iron. In particular, the radiation-curable composition of the present invention can be used as coatings for substrates such as plastic films, metal films, for fiber optics (including primary and secondary coatings, and/or inks) , hard coat coatings for recordable media such as programmable cards (often referred to as "smart cards"), coatings for optical discs comprising a polymer substrate and a metallic reflective layer, and potentially further comprising at least one organic dye as a data recording medium. Examples are lacquers for CD's and CD-R's and adhesives for DVD's. A DVD can be described as comprising an adhesive composition and two optical discs adhered to one another by the adhesive composition wherein at least a portion of each disc which contacts the adhesive composition includes a radiation-cured adhesive provided by curing the radiation-curable adhesive composition. In other words, a DVD comprises two (optical discs) substrates adhered to each other with a radiation-cured adhesive or layer. These coating and/or adhesive layers are typically less than about 20 micrometer thick, preferably less than about 19 micrometer thick, more preferably less than about 15 micrometer and particularly preferred, less than about 10 micrometer thick.
The term 'optical fiber' as used herein can be defined as Optical fiber' or as 'coated optical fiber' .
Examples Examples I -IV
Compositions suitable as ink layers for coloring coated optical glass fibers, or as thin protective layers, were prepared from constituents as described in Table 1. Amounts are given in parts by weight .
Compositions were tested as clear coatings of 5-7 μm thickness and the % Reacted Acrylic
Unsaturation (%RAU) was measured using real-time infrared spectroscopy. Further, pigmented compositions were prepared by adding pigments (3 parts by weight white Ti02 and 9 parts by weight blue β-copper (II) phthalocyanine to the clear base) , and milling the resultant mixture till a homogeneous mixture was obtained. The composition was cured and the % RAU and MEK double rubs were measured, as well as adhesion to an outer primary optical fiber coating (Desolite 950- 111®, available from DSM Desotech Inc.) and the release properties from a matrix optical fiber coating (Cablelite 950-706, available from DSM Desotech Inc.).
Table 1
from Sartomer 2> hexanedioldiacrylate from Sartomer
3) Ammo group containing oligomer from synthesis A
4) ethoxylated hexanedioldiacrylate 5> silicon acrylate from UCB s) butylated hydroxy toluene
* the low number of MEK rubs is an inherent result for very thin films, even if the film is properly cured.
Synthesis A, preparation of an ammo-oligomer A
An amme functional acrylic is formed by reacting 11 wt.% methyl methacrylate , 54 wt.% 2- ethylhexyl acrylate, 5 wt . % hydroxyethyl acrylate and 30 wt.% dimethylammoethyl methacrylate m a polypropylene glycol diluent. The resulting acrylic copolymer had a Tg of -43.5°C and was present m the
diluent at a 1:1 weight ratio.
A urethane acrylated acrylic was formed by reacting 43.0 wt.% of the above formed copolymer mixture, 24.19 wt.% isophorone diisocyanate, 12.63 wt.% hydroxyethyl acrylate, 20 wt.% isobornyl acrylate, 0.1 wt . % butylated hydroxy toluene (BHT) and 0.05 wt.% dibutyltindilaurate. The resulting urethane acrylated acrylic, herein referred to as Amino-oligomer A, had a viscosity (Z4 @ 10.3 s' 1 shear rate) of 343 Pa.s, a Gardner color value of 5-6 and an amine value of (meq/g) of 0.405.
Test Procedures :
%RAU - This is an FTIR method for determining the degree of cure on the surface of a coating to a depth of 1 to 3 μm, following exposure to a predetermined dose of UV radiation. A drawdown of the sample material is first formed on a glass plate. The drawdown is then exposed to the predetermined dose of UV radiation to cure the drawdown and form a coating. The coating is cut into strips, approximately 10 mm by 50 mm. An infrared spectrum of the uncured, liquid sample and an infrared spectrum of the cured sample are obtained. Infrared spectrometry is now well known and any infrared spectrometer can be utilized to obtain the infrared spectrum. The net peak area of the acrylate unsaturation absorbance for the uncured liquid sample is measured. For most acrylate-based coatings, the absorbance at about 810 cm"1 should be used. However,
if the coating contains a siloxane or other component which absorbs strongly at or near 810 cm"1 , an alternative acrylate absorbance peak can be used. The absorbances at about 1410 cm"1 and about 1635 cm"1 have been found to be satisfactory. The net peak area can be measured using the well known baseline technique m which a baseline is drawn tangent to absorbance minima on either side of the peak. The area above the baseline and under the peak is the net peak area. A reference area is then determined. The reference absorbance should not change intensity as the liquid sample is cured. Many formulations have an absorbance m the range of about 780 to about 750 cm"1 that can be used as a reference absorbance. The net peak area of the reference absorbance is measured.
The ratio of the acrylate absorbance to the reference absorbance for the uncured, liquid sample is determined using the following formula:
RL = AAL / ARL
where
AAL is the net peak area of the acrylate absorbance, ARL is the net peak area of the reference absorbance, and
RL is the area ratio for the liquid sample.
The ratio of the acrylate absorbance to the reference absorbance for the cured sample is determined using the following formula:
Rc = AAC / ARc
where
AAC is the net peak area of the acrylate absorbance, ARC is the net peak area of the reference absorbance, and Rc is the area ratio for the cured sample.
The degree of cure as a percent reacted acrylate unsaturation (%RAU) is determined using the following formula:
%RAU = [(R - Rc) x 100%] / RT.
MEK Rubs - A film of the pigmented composition was drawn on a black & white Brush Leneta Form 5DX using a #2.5 Meyer rod. The film was cured at 0.125 J/cm2 under nitrogen using a Fusion "H" lamp. The cured film was tested using a cotton swab soaked in methylethylketone . The film was rubbed in a continuous back and forth motion, with one back and forth motion equal to 2 single rubs. The number of rubs completed before the substrate is exposed is defined by the MEK rubs value.
Adhesion/Release of Inks - a sandwich structure consisting of an outer primary/an exemplary coating (which can be an ink) and a matrix, respectively, was prepared. A 3 mil thick film of a commercial outer primary coating was formed on Mylar and cured at 1.0 J/cm2 under nitrogen using a Fusion "D" lamp. A film of one of the above examples was formed on the cured outer primary coating using a 6.35 μm (0.25 mil) bird bar. This film layer was then cured at 0.35 J/cm2 under nitrogen using a "H" lamp. A 76.2 μm (3 mil) thick film
layer of a commercial matrix composition was then drawn on top using a 7.52 cm (3 inch) square bar and cured at 1.0 J/cm2 under nitrogen using a "D" lamp. This sandwich composite was cut into 1.27 cm (0.5 inch) wide strips and the adhesion to the outer primary coating and release of the matrix were observed by separating the matrix layer and peeling it from the ink layer at a 45° angle. Adhesion to the outer primary coating is measured as either "good" or "bad" and the release from the matrix material is evaluated by the sound made during release with a "zipper" sound indicating poor release and no sound or "no zip" indicating good release .
Examples V-VII
Compositions were prepared from constituents as shown in Table 2A. The described compositions are useful as outer primary coatings or as matrix materials. Curing was achieved by irradiation with an H-lamp in nitrogen atmosphere. All compositions were measured, after cure, for percentage reacted acrylic unsaturation (% RAU) both at the top surface and bottom surface of the coating layer and the results are shown in Table 2B.
Table 2A
Table 2B
At dosage of 0.5 J/cm2 and above, all coatings were cured regardless of thickness, which ranged from between 6 μm and 75 μm. However, at a dose of 0.125 J/cm2 only the thin coatings were fully cured while the bottom surface of the thick coatings were not sufficiently cured. When using conventional
photoinitiators like Darocure 1173 or Lucinn TPO, this behavior was not observed (i.e., all coatings were fully cured with 0.125 J/cm2 irradiation irrespective of a thickness) . Therefore, it has surprisingly been found that there exists an effect of layer thickness on the degree of cure (through-cure and surface cure) when using maleimide compounds as photomitiat g compounds, the effect being such that the thinner the layer the better the degree of cure (especially visible under conditions of lower cure doses) . The critical layer thickness at which at least 85% RAU is obtained at a cure dose of 0.5 J/cm2 is dependent on the specific composition (Ex. V-VII) .
Synthesis B, preparation of an ammo-oligomer B
An amme functional acrylic is formed by reacting 25 wt.% methyl methacrylate, 60 wt.% 2- ethylhexyi acrylate, 5 wt.% hydroxyethyl acrylate and 10 wt.% dimethylammoethyl methacrylate m a polypropylene glycol diluent. The resulting acrylic copolymer had a Tg of -41 °C and was present m the diluent at a 50.7:49.3 weight ratio.
A urethane acrylated acrylic was formed by reacting 43.24 wt.% of the above formed copolymer mixture, 24.07 wt.% isophorone diisocyanate, 12.57 wt.% hydroxyethyl acrylate, 20 wt.% isobornyl acrylate, 0.1 wt . % butylated hydroxy toluene (BHT) and 0.02 wt.% dibutyltindilaurate. The resulting urethane acrylated acrylic, herein referred to as Ammo-oligomer B, had a viscosity (Z4 @ 10.3s"1) of 540 Pa . s , a Gardner color value of 4-5 and an amme value of (meq/g) of 0.136.
Examples VI I I -XVII
Radiation-curable compositions were prepared from constituents as shown m Tables 3 (A-C) . The described compositions are useful as CD lacquers including recordable-CD (r-CD) lacquers . The CD-lacquer generally has a thickness between about 4 and about 12 micrometer. The composition m Table 3B & C were inspected to determine extent of curing.
Preparation of Base Composition
Table 3A
Table notes:
1) ethoxylated (4) jbisphenol A dimethacrylate 2) propoxylated glycerol triacrylate
31 40% Epoxy Novolak acrylate/60% Trimethylolpropane triacrylate
Radiation-curable Composition
Table 3B
Table notes :
1 ] 2-hydroxy-2 -methyl-1-phenylpropane-l-one as the active component (type I photoinitiator)
In Table 3B, the coating compositions were tested by applying the coating composition
(approximately 0.5 g) to the central metallized area of the CD and spun to 4,000 rpm for 3 seconds (acceleration of 3500 rpm2) . The coated CD's were then cured under air at a dose as indicated using a Fusion unit equipped with either a "D" or "H" bulb, as indicated. After exposing the coating, the coating was evaluated on the surface: i) at the central metallized region near the spindle (at a radius of about 25 mm) , referred to as the "inner cure" (thickness of the coating is between about 4 and about 10 μm, and ii) at a medial position along the surface (at a radius between about 39 and about 54 mm) , referred to as the "surface cure" (thickness of coating is between about 7 and about 15 μm) ; and along the "outer edge" of the CD.
Typically, the inner cure represents a region where the coating is the thinnest (due to centrifugal force) and is generally the more difficult area to achieve satisfactory curing. The "outer edge" stands for the degree of cure at the side of the CD. The coating is usually very thin here, can be partially spinned over the edge of the CD, and is usually difficult to cure. The requirement of having a good cure at the outer edge of the CD is only a practical one, for the purpose of not having several CD's sticked together during handling .
The extent of cure was determined by rubbing the coated area, after exposure, with a Kimwipes and visually inspecting the surface for smears. A scale of smearing was assigned, where "5" is indicative of complete surface cure (no smearing) and "0" was indicative of no cure (extensive smearing) , w th "4" and above considered an acceptable cure.
Table 3C
1> type II (Hydrogen abstraction) photomitiator
A drawdown of each material to be tested was prepared by drawing down a coating on a glass plate at the specified thickness, using a Bird bar, commercially available from Pacific Scientific, Silver Spring, MD . The drawdown coating was dosed with 0.5 J/cm2 of radiation m air using a "H" lamp from Fusion Curing Systems, Rockville, MD .
The thickness effect is clearly visible m the % Rau Top and particularly m the % Rau Bottom when going from a 50 micrometer to a 12.5 micrometer thick film.
Example XI
Radiation-curable compositions were prepared from constituents as shown m Table 4. The described compositions are useful as CD lacquers (and recordable media hardcoats) . Curing was achieved by irradiation with a H lamp m air at different UV-doses.
The coating thickness as defined under Table 3B are applicable.
- 3!
Table 4
Table notes:
1) ethoxylated (4) jbisphenol A dimethacrylate
2) propoxylated glycerol triacrylate
3) 40% Epoxy Novolak acrylate/60% Trimethylolpropane triacrylate
Examples XII-XIII
Radiation-curable compositions were prepared from constituents as shown in Table 5. The described compositions are useful as DVD adhesives. Curing was achieved by irradiation with a D-lamp at 1
J/cm2 in air. The DVD-adhesive generally has a thickness between about 10 and about 75 μm.
The DVD-adhesives of Ex. XII and XIII have a thickness of about 25 μm.
Table 5
Table notes :
1> poly THF urethane diacrylate
2) trimethoxypropyl mercapto silane
Examples XIV-XV
Radiation-curable compositions were prepared from constituents as shown in Table 6. The described compositions are useful as DVD adhesives. Curing was achieved by irradiation with a D-lamp at 1 J/cm2 in air.
Table 6
Table notes :
1> poly THF urethane diacrylate
21 trimethoxypropyl mercapto silane