BACKGROUND OF THE INVENTION
[0001] Radiation curable coatings are highly desirable because they can be cured without
the need to evaporate substantial amounts of solvent. Therefore, curing can be accomplished
rapidly and with less release of volatile organic compounds into the atmosphere. Also,
radiation curing can be carried out at relatively low temperatures, thereby lending
itself to use with temperature sensitive substrates such as wood and plastic. The
use of electron beam radiation is particularly favored for curing thick coatings and
coatings that are heavily pigmented.
[0002] It is known to cure certain coating compositions to a glossy finish using electron
beam radiation to initiate the crosslinking reactions that result in a cured film.
The curing of typical radiation curable coating compositions is inhibited by the presence
of oxygen, so it is conventional to provide a substantially inert atmosphere (e.g.,
less than 200 parts per million oxygen) in the electron beam exposure apparatus. It
can be costly to maintain the required degree of inertness accurately and constantly.
Slight variations in the oxygen concentration can lead to uneven coating appearance
with conventional methods and compositions. It would be desirable to reduce the sensitivity
of an electron beam curing system to oxygen when producing glossy coatings.
[0003] It is known to add accelerator compounds (e.g., tertiary amino compounds) to coating
compositions to at least partially overcome the inhibition of curing due to oxygen,
thereby increasing the amount of oxygen that can be permitted in the radiation curing
chamber. Although the accelerators provide processing advantages, they generally have
deleterious effects on the coating, such as yellowing and/or surface roughness. The
accelerators can sometimes also have a negative effect on the ease of applying the
coating composition onto the substrate.
[0004] Multi-step radiation curing processes, which may include a combination of electron
beam and ultraviolet radiation, have been employed to produce low gloss coatings.
In these prior art processes oxygen (air) was intentionally present during the first
radiation curing step to initially inhibit polymerization at surface portions of the
coating, and curing of the coating was completed in a subsequent step in an inert
atmosphere. Shrinkage of underlying layers during the first step caused pigment particles
to be driven into the surface portions, whereby the surface contained a larger amount
of pigment than the body of the film which reduced the gloss of the film without sacrificing
film strength or rheology properties of the coating composition. U.S. Patent Nos.
3,918,393 (Hahn) and 4,048,036 (Prucnal) illustrate this approach. Multi-step radiation
curing techniques have also been proposed for producing textured finishes in U.S.
Patent Nos. 4,421,784 (Troue), 3,840,448 (Osbome et al.), and 4,411,931 (Duong) wherein
surface wrinkling of the coating is induced by the staged curing process. Those of
skill in the art would have considered two stage radiation cure processes inappropriate
for producing high gloss finishes.
SUMMARY OF THE INVENTION
[0005] By the present invention it has been found that electron beam radiation can be employed
to yield high gloss finishes from certain coating compositions without requiring the
fully inert atmosphere (i.e. less than 200 parts per million oxygen) required by prior
art processes. The process uses a two step curing process and selected coating compositions.
Achieving high gloss finishes from a two step process is surprising in view of the
fact that multi-step processes have previously been used for producing low gloss finishes.
Furthermore, the substantial lessening of the requirement for a fully inert atmosphere
during the electron beam radiation step is highly advantageous for the sake of reducing
costs associated with atmosphere control.
[0006] The first step of the process of the present invention involves irradiation with
an electron beam, followed by a subsequent step of exposure to ultraviolet radiation.
The electron beam step may take place in air or in a partially inert atmosphere including
at least 1000 ppm oxygen, preferably at least 2 percent oxygen by volume, whereby
the surface of the coating remains wet or uncured. The ultraviolet radiation step
takes place in a substantially inert atmosphere (less than 1000 parts per million
oxygen) whereby curing of the coating is substantially completed. Although an inert
atmosphere is required in the ultraviolet step, it may be noted that the conditions
need not be controlled as rigorously as in prior art electron beam processes.
[0007] The present invention is defined by the use of a radiation curable composition comprising
:
(a) 10-99 weight % of a resin binder curable by radiation exposure in the presence
of at least one photoinitiator compound, the resin being selected from those containing
acrylyloxy groups and whose curing by radiation exposure is substantially inhibited
by the presence of oxygen;
(b) 0.01-4 weight % of a non-volatile photoinitiator having molecular weight of at
least 1000 and
(c) 0.01-1 weight % of flow control agent selected from the group consisting of siloxane
compounds and fluorocarbon compounds,
in a method for producing a high gloss, radiation cured coating comprising applying
to a substrate said composition to form a coating;
in a first exposure step, exposing the coating, in an atmosphere containing greater
than 1000 part per million of oxygen, to ionizing radiation so as to at least partially
cure a subsurface layer of the coating while leaving at least a partially uncured
surface layer; and
in a subsequent exposure step, exposing the at least partially cured coating, in an
atmosphere containing less than 1000 parts per million of oxygen, to ultraviolet radiation
sufficient to cure the surface of the coating and produce a coating having a high
gloss surface.
[0008] The present invention is furthermore defined by the method for producing a high gloss,
radiation cured coating comprising:
applying to a substrate a coating composition comprising:
10-99 weight % of a radiation curable resin binder which contains acryloxy groups
and whose curing by radiation exposure is substantially inhibited by the presence
of oxygen,
0.01-4 weight % of a non-volatile photoinitiator having molecular weight of at least
1000 and
0.01-1 weight % of a flow control agent selected from the group consisting of siloxane
compounds and fluorocarbon compounds;
in a first exposure step, exposing the coating, in an atmosphere containing greater
than 1000 part per million of oxygen, to ionizing radiation so as to at least partially
cure a subsurface layer of the coating while leaving at least a partially uncured
surface layer; and
in a subsequent exposure step, exposing the at least partially cured coating, in an
atmosphere containing less than 1000 parts per million of oxygen, to ultraviolet radiation
sufficient to cure the surface of the coating and produce a coating having a high
gloss surface.
DETAILED DESCRIPTION
[0009] The binder or vehicle in the coating composition used in the present invention comprises
at least one resin (monomer, oligomer, or polymer) which is curable by exposure to
radiation in the presence of one or more of the photoinitiators disclosed herein.
Binder constitutes 10 to 99, preferably 50 to 99, percent by weight of the total coating
composition. Many such resins are known in the art and may be used in the present
invention. The resins suitable for use in the present invention as defined above are
characterized by inhibition of curing by the presence of oxygen (such as in air).
Oxygen inhibition permits maintaining an at least partially uncured surface layer
during the initial curing step with the electron beam. A particular category of useful
radiation curable compounds are characterized by a plurality of acrylyloxy groups
and the ability to free radically addition polymerize upon being initiated by a photoinitiator
or ionizing radiation. Unless otherwise indicated either directly or by context, acrylic
unsaturation is used in its broad sense to mean the unsaturation provided by unsubstituted
acrylyl groups or a-substituted acrylyl groups such as methacrylyl, ethacrylyl and
a-chloroacrylyl. Examples of these compounds are the diacrylates and dimethacrylates
of ethylene glycol, 1,3-propanediol, propylene glycol, 2,3-butanediol, 1,4-butanediol,
2-ethylbutane-1,4-diol, 1,5-pentanediol, 1,6-hexanediol, 1,7-heptanediol, 1,8-octanediol,
1,9-nonanediol, 1,10-decanediol, 2,10-decanediol, 1,4-cyclohexanediol, 1,4-dimethylolcyclohexane,
2,2-diethylpropane-1,3-diol, 2,2-dimethylpropane-1,3-diol, 3-methylpentane-1,4-diol,
2,2-diethylbutane-1,3-diol, 4,5-nonanediol, diethylene glycol, triethylene glycol,
propylene glycol, neopentyl glycol, 5,5-dimethyl-3,7-dioxanonane-1,9-diol, 2,2-dimethyl-3-hydroxypropyl
2,2-dimethyl-3-hydroxypropionate; the triacrylates and diacrylates of glycerol, 1,1,1-trimethylolpropane
and trimethylolethane; and the tetraacrylates, triacrylates, and diacrylates of pentaerythritol
and erythritol. The acrylyloxy groups in each of the molecules are usually the same,
but they may be different as exemplified by the compound 2,2-dimethyl-1-acrylyloxy-3-methacrylyloxypropane.
[0010] Further examples of satisfactory polyacrylyloxy compounds that may be included in
the radiation curable resin include polyacrylyloxy functional polyesters, polamides,
polyacrylates, polyethers, polycarbonates or polyurethanes as well as polyacrylyloxy
functional compounds of mixed functionality such as polyacrylyloxy functional poly(ester-urethanes),
poly(ester-amides) and poly(ether-urethanes). Mixtures of compounds having a plurality
of acrylyloxy groups may be used, if desired.
[0011] The amount of polymerizable compound having a plurality of acrylyloxy groups present
in the coating composition is subject to wide variation. The compound is present in
an amount in the range of from 10 to 99 percent by weight based on the weight of the
binder of the coating composition. An amount in the range of from about 20 to 97 percent
is typical. From about 30 to 95 percent by weight of the binder is preferred.
[0012] Monomers having monoacrylic functionality which crosslinks with the compound having
polyacrylyloxy functionality may optionally be present in the coating composition.
Examples of monoacrylic functional monomers which may be used are methyl acrylate,
ethyl acrylate, propyl acrylate, butyl acrylate, hexyl acrylate, hexyl ethyl acrylate,
hexyl butyl acrylate, 2-ethyl hydroxy acrylate, octyl acrylate, hydroxy ethyl acrylate,
hydroxy butyl acrylate, caprclactone-hydroxyl alkyl acrylate reaction products, and
2-ethyl hydroxy acrylate. The preferred monoacrylic functional monomers are liquid
compounds miscible with the polyacrylyloxy compound. A benefit from the use of one
or more monoacrylic functional monomers is that the monoacrylic functional monomer
may act as a reactive solvent for the polyacrylyloxy functional compound, thereby
providing coating compositions having a satisfactory low viscosity while using relatively
small amounts or no volatile, nonreactive solvent.
[0013] The monoacrylic functional monomer, or mixtures of monoacrylic functional monomers,
may be employed over a broad range, although none is required. The amount of such
monomer when used should be sufficient to provide a liquid, flowable, interpolymerizable
mixture. When used, the monomer will ordinarily be present in the coating composition
in the range of from about 0 to about 80 percent by weight of the binder of the coating
composition. Typically, the monoacrylic functional monomer will be present in the
range of from about 0 to about 30 percent by weight of the binder. Other monovalent
functional monomers may be employed as known in the radiation curing art, including
N-vinyl-2-pyrolidone, vinyl neodecanoate, and other ethylenic unsaturated monomers
known to be suitable for radiation curable coatings.
[0014] The present invention employs a coating composition containing a photoinitiator.
Photoinitiators absorb radiation and thereby obtain energy to form free radicals that
initiate polymerization of the binder resin. The photoinitiator in the present invention
is one which forms free radicals upon exposure to actinic radiation, viz., ultraviolet
light. In order to produce the high gloss finishes of the present invention, photoinitiators
are selected that are non-volatile, which is generally related to the molecular weight
of the photoinitiator. Therefore, for the purpose of the present invention, the non-volatile
photoinitiator is characterized by a molecular weight of at least 1000.
[0015] In selecting photoinitiators, one of skill in the art would consider it expedient
to select compounds that are soluble and stabile in the particular composition.
[0016] There are many photoinitiators which may be used in the coating compositions. One
class of compounds useful as photoinitiators in the present invention are acetophenone
derivatives meeting the definition of non-volatile set forth above, in particular
substituted acetophenone derivatives. Many acetophenone derivatives are known as photoinitiators,
a large number of which are disclosed in U.S. Patent No. 4,229,274 (Carlblom).
[0017] The amount of photoinitiator present in the coating composition is at least 0.01
weight percent based on total solids content of the coating composition. Although
larger amounts could be used, it is usually uneconomical to use more than 5 percent
of the photoinitiator. According to the present invention, the amount of photoinitiator
does not exceed 4 weight percent. Typically, the photoinitiator may be present in
an amount of at least 0.1 percent, most often in the range of from 0.5 percent to
2 percent. Mixtures of more than one photoinitiator compound may be used.
[0018] The coating compositions employed in the present invention include a surfactant of
the type that serves as a flow control agent or leveling agent selected from siloxane
compounds and fluorocarbon compounds. Suitable products are commercially available
for this purpose. The preferred class of flow control agents are siloxane compounds,
examples of which are "BYK®-310, a polyester modified dimethylpolysiloxane" from Byk
Chemie, Wallingford, Connecticut, and "Versaflow 102", a modified methyl siloxane
from Shamrock Technologies, Inc., Newark, New Jersey. Examples of fluorocarbon flow
control agents are the "Zonyl®" surfactants from DuPont and the "Fluororad®" surfactants,
particularly "FC430," from 3M. The flow control agents for use in the present invention
are characterized by the property of assisting leveling of the coatings used in the
present invention after application onto a substrate, without substantial interference
with the application process itself. The flow control agent should have relatively
low volatility. The flow control agent is present in the compcsition in amounts ranging
from 0.01 to 1.0 percent by weight based on total solids content of the composition.
[0019] Pigments may be included in the coating composition. Examples of opacifying pigments
include titanium dioxide (rutile or anatase), zinc oxide, zirconium oxide, zinc sulfide
and lithopone. Examples of coloring pigments include iron oxides, cadmium sulfide,
carbon black, phthalocyanine blue, phthalocyanine green, indanthrone blue, ultramarine
blue, chromium oxide, burnt umber, benzidine yellow, toluidine red, aluminum powder
and aluminum flakes. Examples of extender pigments include silica, barytes, calcium
carbonate, barium sulfate, talc, aluminum silicates, sodium aluminum silicates, potassium
aluminum silicates and magnesium silicate. A single pigment may be used or mixtures
of pigments may be employed. When the pigment is ultraviolet light absorbing, it should
be used in amounts which do not preclude curing of the interior of the coating. The
maximum amount is therefore related to the thickness of the coating to be cured. Thin
coatings may tolerate more ultraviolet light absorbing pigment than thick coatings.
When the pigment does not significantly absorb ultraviolet light, there is usually
greater latitude in the amounts which may be employed. When pigment is used, it is
generally present in an amount in the range of from about 0.1 to about 70 percent
by weight of the coating composition. Often it is present in an amount in the range
of from about 0.5 to about 50 percent. Usually it is present in an amount in the range
of from about 1 to about 35 percent by weight of the coating composition. Dyes and
tints may optionally be included in the coating composition as replacements for all
or some of the pigment content.
[0020] Other optional ingredients are resinous pigment dispersants, viscosity control agents
(e.g., cellulose acetate butyrate or resinous acrylics), plasticizers, or grinding
vehicles such as non-reactive acrylics. There are many resinous additives which are
commercially available which may be used for these purposes. These additives are used
in the manner and in amounts known to the art, such as 0 to 20 weight percent of the
total composition.
[0021] Another ingredient which is often included in coating compositions of this type is
a non-reactive, volatile organic solvent. However, in preferred embodiments of the
present invention, no such non-reactive solvent need be included. In other embodiments
of the invention, solvent may be present, but in lesser amounts than conventional.
It is generally advantageous to minimize the amount of organic solvent, but if reduction
of viscosity is desired for a particular application, the present invention does not
preclude adding larger amounts of a non-reactive solvent or mixtures of several solvents.
Examples of suitable non-reactive organic solvents are acetone, methyl ethyl ketone,
methyl isobutyl ketone, methyl alcohol, ethyl alcohol, propyl alcohol, isopropyl alcohol,
butyl alcohol, secutyl alcohol, isobutyl alcohol, tert-butyl alcohol, amyl alcohol,
hexyl alcohol, 2-ethylhexyl alcohol, cellosolve, ethyl cellosolve, cellosolve acetate,
2-ethylhexyl acetate, tetrahydrofuran, and aliphatic naphtha. When solvent of this
type is used it is ordinarily present in the coating composition in the range of from
about 0.1 to about 40 percent by weight of the vehicle of the coating composition.
From about 0 to about 15 percent is typical. The preferred compositions are solvent-free.
[0022] The listing of optional ingredients discussed above is by no means exhaustive. Other
ingredients may be employed in their customary amounts for their customary purposes
so long as they do not seriously interfere with good coatings practice or the obtaining
of cured coatings of high gloss.
[0023] The coating compositions used in the invention are usually prepared by simply admixing
the various ingredients. The compounds comprising the photocatalyst system may be
premixed and then admixed with the other ingredients of the coating composition or
they may be added separately. Although mixing is usually accomplished at room temperature,
elevated temperatures are sometimes used. The maximum temperature which is usable
depends upon the heat stability of the ingredients. Temperatures above about 200°F
(93°C) are only rarely employed.
[0024] The radiation curable coating compositions employed in the invention are generally
used to form cured adherent coatings on substrates. The substrate is coated with the
coating composition using substantially any technique known to the art. These include
spraying, curtain coating, dipping, roller application, printing, brushing, drawing
and extrusion. Wet, uncured coatings, as applied to a substrate have thicknesses of
at least 1.0 mil (0.025 millimeter), preferably at least 2.5 mils (0.06 millimeters),
in order to achieve the high gloss effect of the present invention. Theoretically
there is no upper limit for wet coating thickness, but in order to effect first stage
curing of lower strata at practical radiation power levels, it is expedient to limit
coating thickness to 5 to 8 mils (0.13 to 0.2 millimeters). Cured coatings of the
ultraviolet light curable coating composition employed in the invention usually have
thicknesses in the range of from 1 to 5 mils (0.025 to 0.13 millimeter). More often
they have thicknesses in the range of from 2 to 4 mils (0.05 to 0.1 millimeter).
[0025] Substrates which may be coated with the compositions may vary widely in their properties.
Organic substrates such as wood, fiberboard, particle board, composition board, paper,
cardboard and various polymers such as polyesters, polyamides, cured phenolic resins,
cured aminoplasts, acrylics, polyurethanes and rubber may be used. Inorganic substrates
are exemplified by glass, quartz and ceramic materials. Many metallic substrates may
be coated. Exemplary metallic substrates are iron, steel, stainless steel, copper,
brass, bronze, aluminum, magnesium, titanium, nickel, chromium, zinc and alloys.
[0026] The method of curing the coating composition involves a two step radiation exposure
wherein the applied coating layer is cured in a subsurface portion in a first step
by exposure to ionizing radiation (e.g., electron beam radiation or laser) in the
presence of oxygen (i.e., greater than 1000 ppm) whereby curing at the surface is
inhibited. In a subsequent step the curing is completed throughout the remainder of
the coating thickness by means of ultraviolet radiation in an at least partially inert
atmosphere (i.e., less than 1000 ppm oxygen).
[0027] Suitable electron beam radiation for use in the first curing step may constitute
a dose of 2 to 10 megarads, preferably 3 to 7 megarads, at 150 to 300 kiloelectron
volts, preferably about 250 kiloelectron volts. Line speeds of 50 to 120 feet per
minute (15 to 36 meters per minute) are suitable. The exposure in the first ste is
chosen so as to substantially cure the portion of the coating closest to the substrate.
A portion of the coating thickness nearest to the surface will remain at least partially
uncured due to oxygen inhibition. The atmosphere in the vicinity of the coating during
the electron beam exposure should include at least 1000 ppm oxygen, preferably at
least 2 percent oxygen by volume.
[0028] Any suitable source which emits ultraviolet light, viz., electromagnetic radiation
having a wavelength in the range of from about 180 to about 400 nanometers, may be
used in the practice of the second curing step. Suitable sources are mercury arcs,
carbon arcs, medium pressure mercury lamps, high pressure mercury lamps, swirl-flow
plasma arc, ultraviolet light-emitting diodes and ultraviolet light emitting lasers.
Particularly preferred are ultraviolet light emitting lamps of the medium or high
pressure mercury vapor type. Such lamps usually have fused quartz envelopes to withstand
the heat and transmit the ultraviolet radiation and are ordinarily in the form of
long tubes having an electrode at either end.
[0029] The time of exposure to ultraviolet light and the intensity of the ultraviolet light
to which the coating composition is exposed may vary greatly. For practical commercial
line speeds, lamps rated at 200 watts per inch (7900 watts per meter) or greater are
preferred. Generally the exposure to ultraviolet light should continue until either
the film is thermoset throughout or at least cured to the point where subsequent reactions
cause the film to become thermoset throughout. Exposure of the coating to ultraviolet
light may be accomplished in the presence of an inert atmosphere, viz., an atmosphere
either containing no oxygen or only a concentration of oxygen which insignificantly
inhibits polymerization of the coating surface (less than 1000 parts per million oxygen).
Gases such as nitrogen, argon, carbon dioxide or mixtures thereof are typically the
major components of inert atmospheres, although other unreactive gases may be used.
Nitrogen is generally employed for this purpose.
[0030] Coatings produced in accordance with the present invention exhibit gloss and distinctness
of image comparable to that of coatings produced with full inerting (less than 200
parts oxygen per million). Gloss may conveniently be determined by the Standard Method
of Test for Specular Gloss, ASTM Designation D-523-67 (Reapproval 1971). Using a Gardner
60° glossmeter, the gloss of cured coatings may exceed 70 percent reflected light,
preferably greater than 80 percent, and with specific examples being in the range
of 83 to 86 percent.
[0031] Another measure of the gloss of coatings is "distinctness of image" (D.O.I.). The
particular distinctness of image test used to evaluate the present invention employs
a technique specified by General Motors Standard Engineering Test: Distinctness of
Image GM91013 Page Reference W-65.201. In this test, a light source (a Model GB11-8
Glowbox made by I2R Corporation) is used to project a series of successively smaller
images of the letter "C" onto the coated surface from a fixed distance. The smaller
the image that is reflected, the higher the D.O.I. rating on a scale of 0 to 100.
High gloss coatings generally exhibit D.O.I. ratings of at least 80, preferably at
least 85. Coatings cured with full inerting during the electron beam exposure step
may have D.O.I. ratings in the range of 90 to 100.
EXAMPLE 1
[0032] This example demonstrates a specific embodiment of the method of the present invention.
| Constituent |
Percent by weight |
| Diacrylate resin1 |
92.5 |
| Cellulose acetate butyrate resin |
4.0 |
| Lampblack pigment2 |
1.2 |
| Dispersant3 |
1.2 |
| Photoinitiator4 |
1.0 |
| Flow control agent5 |
0.1 |
| 1 Low viscosity polyester diacrylate "SR606A" from Sartomer Corporation, Exton, Pennsylvania,
U.S.A. |
| 2Grade #6 amorphous, acidic carbon from General Carbon Company, Los Angeles, California,
U.S.A. |
| 3"Sartomer 802" acrylic monomer with pigment dispersing characteristics from Sartomer
Corporation, Exton, Pennsylvania, U.S.A. |
| 4"Esacure KIP100F" photoinitiator comprising 70% oligo {2-hydroxy-2-methyl-1-[4-(methylvinyl)
phenyl] propanone} and 30%2-hydroxy-2-methyl-1-phenyl propan-1-one, from Sartomer
Corporation, Exton, Pennsylvania, U.S.A. Molecular weight is reported to be 2000. |
| 5"Versaflow 102" modified methyl siloxane from Shamrock Technologies, Inc., Newark,
New Jersey. |
[0033] A portion of the diacrylate together with the dispersant and the lampblack pigment
were ground in a pigment mill with ceramic media. The grind was then flushed out of
the mill with an additional portion of the diacrylate. The composition was then let
down with the remainder of the diacrylate premixed with the cellulose acetate butyrate,
the photoinitiator, and the siloxane flow control agent.
[0034] The composition above was applied at a wet film thickness of 2.5 mils (0.06 millimeters)
with a curtain coater onto medium density fiberboard that has been filled, sealed,
and sanded smooth. The coated substrate was cured by at a line speed of 100 feet per
minute (30.5 meters per minute), first with an electron beam manufactured by Energy
Sciences, Inc., of Woburn, Massachusetts, USA, set at 250 kilovolts terminal voltage
and 23 milliamperes beam current, yielding 5 megarads of energy, in an atmosphere
containing 10% oxygen by volume. In a second curing step the coated substrate was
subjected to ultraviolet exposure from four medium pressure mercury vapor lamps of
200 watts per inch (80 watts per centimeter) manufactured by Aetek International,
Plainfield, Illinois, USA, at a line speed of 80 feet per minute (24 meters per minute)
in a fully inerted atmosphere (nitrogen with less than 200 parts per million oxygen).
A highly glossy finish was produced as reported in Table 1.
EXAMPLE 2
[0035] This example employs the same two stage curing process with electron beam and ultraviolet
stages as used in Example 1, but uses a conventional radiation curable coating composition.
Therefore, a polymeric surfactant was not included in the composition of this example.
Also, a lower molecular weight photoinitiator was used ("Irgacure 651" from Ciba-Geigy
Corp., Hawthorne, New York, having a molecular weight of 256). Substantially lower
gloss was produced in this example as can be seen in Table 1.
EXAMPLE 3
[0036] This example employs the same prior art coating composition as in Example 2, but
curing was carried out in a single stage process using only the electron beam described
in Example 1. The electron beam stage was fully inerted. Even though curing was carried
out in a fully inerted atmosphere, the results as reported in Table 1 were not as
good as Example 1.
EXAMPLE 4
[0037] This example is the same as Example 4, with the exception that no photoinitiator
was included in the coating composition in view of the use of a single stage electron
beam curing process. The results as reported in Table 1 are the same as Example 3,
indicating that the presence of photoinitiator was not the cause of the inferior gloss
of Example 3 relative to the present invention as represented by Example 1.
TABLE 1
| |
Gloss |
D.O.I. |
| Example 1 (The invention) |
85 |
90 |
| Example 2 (Prior art composition) |
70 |
50 |
| Example 3 (Single stage) |
85 |
80 |
| Example 4 (Single stage) |
85 |
80 |
[0038] The examples set forth above demonstrate that the particular method of the present
invention (Example 1), when cured by a two stage process that does not employ full
inerting in the electron beam stage, can yield finishes having gloss subtantially
superior to that attained by a typical prior art compositions cured by the same process
(Example 2). That this result can be attained without the need to fully inert the
electron beam stage is highly advantageous and surprising. Also surprising is finding
that the gloss attained by Example 1 (the invention) is better even than that produced
by a fully inerted electron beam (Examples 3 and 4).
[0039] The invention has been disclosed in connection with specific embodiments in order
to provide the best mode of the invention, but it should be understood that other
variations and modifications as would be known to those of skill in the art can be
resorted to within the scope of the invention as defined by the claims which follow.
1. Use of a radiation curable composition comprising:
(a) 10-99 weight % of a resin binder curable by radiation exposure in the presence
of at least one photoinitiator compound, the resin being selected from those containing
acrylyloxy groups and whose curing by radiation exposure is substantially inhibited
by the presence of oxygen;
(b) 0.01-4 weight % of a non-volatile photoinitiator having molecular weight of at
least 1000 and
(c) 0.01-1 weight % of flow control agent selected from the group consisting of siloxane
compounds and fluorocarbon compounds,
in a method for producing a high gloss, radiation cured coating comprising applying
to a substrate said composition to form a coating;
in a first exposure step, exposing the coating, in an atmosphere containing greater
than 1000 part per million of oxygen, to ionizing radiation so as to at least partially
cure a subsurface layer of the coating while leaving at least a partially uncured
surface layer; and
in a subsequent exposure step, exposing the at least partially cured coating, in an
atmosphere containing less than 1000 parts per million of oxygen, to ultraviolet radiation
sufficient to cure the surface of the coating and produce a coating having a high
gloss surface.
2. The use of claim 1 wherein the photoinitiator comprises a substituted acetophenone
derivative.
3. The use of claim 1 wherein the flow control agent is a polysiloxane.
4. The use of claim 1 wherein at least 10% by weight of the binder is a polyacryloxy
compound.
5. The use of claim 1 wherein at least 30% by weight of the binder is a polyacryloxy
compound.
6. The method for producing a high gloss, radiation cured coating comprising: applying
to a substrate a coating composition comprising:
10-99 weight % of a radiation curable resin binder which contains acryloxy groups
and whose curing by radiation exposure is substantially inhibited by the presence
of oxygen,
0.01-4 weight % of a non-volatile photoinitiator having molecular weight of at least
1000 and
0.01-1 weight % of a flow control agent selected from the group consisting of siloxane
compounds and fluorocarbon compounds;
in a first exposure step, exposing the coating, in an atmosphere containing greater
than 1000 part per million of oxygen, to ionizing radiation so as to at least partially
cure a subsurface layer of the coating while leaving at least a partially uncured
surface layer; and
in a subsequent exposure step, exposing the at least partially cured coating, in an
atmosphere containing less than 1000 parts per million of oxygen, to ultraviolet radiation
sufficient to cure the surface of the coating and produce a coating having a high
gloss surface.
7. The method of claim 6 wherein the photoinitiator comprises a substituted acetophenone
derivative.
8. The method of claim 6 wherein the flow control agent is polysiloxane.
9. The method of claim 6 wherein at least 10% by weight of the binder is polyacryloxy
compound.
10. The method of claim 6 wherein at least 30% by weight of the binder is polyacryloxy
compound.
1. Verwendung einer strahlungshärtbaren Zusammensetzung, die folgendes umfaßt:
(a) 10-99 Gew-% eines Harzbinders, der in Anwesenheit von zumindest einer Photoinitiatorverbindung
durch Strahlungsexposition härtbar ist, wobei das Harz aus solchen Harzen gewählt
ist, die Acryloxygruppen enthalten und deren Härtung durch Strahlungsexposition durch
die Anwesenheit von Sauerstoff im wesentlichen gehemmt wird;
(b) 0,01-4 Gew-% eines nicht-flüchtigen Photoinitiators mit einem Molekulargewicht
von wenigstens 1000 und
(c) 0,01-1 Gew-% eines Verlaufmittels, gewählt aus der Gruppe bestehend aus Siloxanverbindungen
und Fluorkohlenwasserstoffverbindungen,
in einem Verfahren zur Herstellung einer hochglänzenden, strahlungsgehärteten
Beschichtung, das das Aufbringen der Zusammensetzung auf ein Substrat umfaßt, um eine
Beschichtung zu bilden;
in einem ersten Aussetzungsschritt Aussetzen der Beschichtung an ionisierende Strahlung
in einer Atmosphäre, die mehr als 1000 parts per million Sauerstoff enthält, so daß
eine unterhalb der Oberfläche liegende Schicht der Beschichtung zumindest teilweise
gehärtet wird, während eine zumindest teilweise ungehärtete Oberflächenschicht zurückbleibt;
und
in einem nachfolgenden Aussetzungsschritt Aussetzen der zumindest teilweise gehärteten
Beschichtung in einer Atmosphäre, die weniger als 1000 parts per million Sauerstoff
enthält, an ultraviolette Strahlung, die zur Härtung der Oberfläche der Beschichtung
und zur Erzeugung einer Beschichtung mit einer hochglänzenden Oberfläche ausreichend
ist.
2. Verwendung nach Anspruch 1, worin der Photoinitiator ein substituiertes Acetophenonderivat
umfaßt.
3. Verwendung nach Anspruch 1, worin das Verlaufmittel ein Polysiloxan ist.
4. Verwendung nach Anspruch 1, worin wenigstens 10 Gewichtsprozent des Binders aus einer
Polyacryloxyverbindung bestehen.
5. Verwendung nach Anspruch 1, worin wenigstens 30 Gewichtsprozent des Binders aus einer
Polyacryloxyverbindung bestehen.
6. Verfahren zur Herstellung einer hochglänzenden, strahlungsgehärteten Beschichtung,
das folgendes umfaßt:
Aufbringen einer Beschichtungszusammensetzung auf ein Substrat, die folgendes umfaßt:
10-99 Gew-% eines strahlungshärtbaren Harzbinders, der Acryloxygruppen enthält und
dessen Härtung durch Strahlungsexposition im wesentlichen durch die Anwesenheit von
Sauerstoff gehemmt wird;
0,01-4 Gew-% eines nicht-flüchtigen Photoinitiators mit einem Molekulargewicht von
wenigstens 1000 und
0,01-1 Gew-% eines Verlaufmittels, gewählt aus der Gruppe bestehend aus Siloxanverbindungen
und Fluorkohlenwasserstoffverbindungen;
in einem ersten Aussetzungsschritt Aussetzen der Beschichtung an ionisierende Strahlung
in einer Atmosphäre, die mehr als 1000 parts per million Sauerstoff enthält, so daß
eine unterhalb der Oberfläche befindliche Schicht der Beschichtung zumindest teilweise
gehärtet wird, während eine zumindest teilweise ungehärtete Oberflächenschicht zurückbleibt;
und
in einem nachfolgenden Aussetzungsschritt Aussetzen der zumindest teilweise gehärteten
Beschichtung in einer Atmosphäre, die weniger als 1000 parts per million Sauerstoff
enthält, an ultraviolette Strahlung, die zur Härtung der Oberfläche der Beschichtung
und zur Erzeugung einer Beschichtung mit einer hochglänzenden Oberfläche ausreichend
ist.
7. Verfahren nach Anspruch 6, worin der Photoinitiator ein substituiertes Acetophenonderivat
umfaßt.
8. Verfahren nach Anspruch 6, worin das Verlaufmittel Polysiloxan ist.
9. Verfahren nach Anspruch 6, worin wenigstens 10 Gewichtsprozent des Binders aus einer
Polyacryloxyverbindung bestehen.
10. Verfahren nach Anspruch 6, worin wenigstens 30 Gewichtsprozent des Binders aus einer
Polyacryloxyverbindung bestehen.
1. Utilisation d'une composition durcissable par rayonnement comprenant :
(a) 10-99% en poids d'un liant de résine durcissable par exposition à un rayonnement
en présence d'au moins un composé photo-initiateur, la résine étant choisie parmi
celles contenant des groupes acrylyloxy et dont le durcissement par exposition au
rayonnement est sensiblement inhibé par la présence d'oxygène;
(b) 0,01-4% en poids d'un photo-initiateur non volatil ayant un poids moléculaire
d'au moins 1.000; et
(c) 0,01-1% en poids d'un régulateur de fluidité choisi dans le groupe comprenant
les composés de siloxane et les composés fluorocarbonés,
dans un procédé de production d'un revêtement durci par rayonnement, d'un brillant
élevé comprenant l'application à un substrat de ladite composition pour former un
revêtement;
dans une première étape d'exposition, l'exposition du revêtement, dans une atmosphère
contenant plus de 1.000 parties par million d'oxygène, à un rayonnement ionisant de
manière à au moins durcir partiellement une couche sous-superficlelle du revêtement
tout en laissant au moins une couche en surface partiellement non durcie; et,
dans une étape d'exposition ultérieure, l'exposition du revêtement au moins partiellement
durci, dans une atmosphère contenant moins de 1.000 parties par million d'oxygène,
à un rayonnement ultraviolet suffisant pour durcir la surface du revêtement et produire
un revêtement ayant une surface d'un brillant élevé.
2. Utilisation suivant la revendication 1, dans laquelle le photo-initiateur comprend
un dérivé d'acétophénone substitué.
3. Utilisation suivant la revendication 1, dans laquelle le régulateur de viscosité est
un polysiloxane.
4. Utilisation suivant la revendication 1, dans laquelle au moins 10% en poids du liant
sont un composé polyacryloxy.
5. Utilisation suivant la revendication 1, dans laquelle au moins 30% en poids du liant
sont un composé polyacryloxy.
6. Procédé de production d'un revêtement durci par rayonnement, d'un brillant élevé comprenant
:
l'application à un substrat d'une composition de revêtement comprenant :
10-99% en poids d'un liant de résine durcissable par rayonnement qui contient des
groupes acryloxy et dont le durcissement par exposition au rayonnement est sensiblement
inhibé par la présence d'oxygène,
0,01-4% en poids d'un photo-initiateur non volatil ayant un poids moléculaire d'au
moins 1.000, et
0,01-1% en poids d'un régulateur de fluidité choisi dans le groupe comprenant les
composés de siloxane et les composés fluorocarbonés;
dans une première étape d'exposition, l'exposition du revêtement, dans une atmosphère
contenant plus de 1.000 parties par million d'oxygène, à un rayonnement ionisant de
manière à au moins durcir partiellement une couche sous-superficielle du revêtement
tout en laissant au moins une couche en surface partiellement non durcie; et,
dans une étape d'exposition ultérieure, l'exposition du revêtement au moins partiellement
durci, dans une atmosphère contenant moins de 1.000 parties par million d'oxygène,
à un rayonnement ultraviolet suffisant pour durcir la surface du revêtement et produire
un revêtement ayant une surface d'un brillant élevé.
7. Procédé suivant la revendication 6, dans lequel le photo-initiateur comprend un dérivé
d'acétophénone substitué.
8. Procédé suivant la revendication 6, dans lequel le régulateur de fluidité est du polysiloxane.
9. Procédé suivant la revendication 6, dans lequel au moins 10% en poids du liant sont
un composé polyacryloxy.
10. Procédé suivant la revandication 6, dans lequel au moins 30% en poids du liant sont
un composé polyacryloxy.