U.S. patent application number 16/455852 was filed with the patent office on 2019-10-17 for polyurethane based rigid flooring laminate.
The applicant listed for this patent is Schneller LLC. Invention is credited to Henry C. Ashton, Gilles Le Du, Robert L. Gray, Robert G. Pierson.
Application Number | 20190315092 16/455852 |
Document ID | / |
Family ID | 42678529 |
Filed Date | 2019-10-17 |
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United States Patent
Application |
20190315092 |
Kind Code |
A1 |
Pierson; Robert G. ; et
al. |
October 17, 2019 |
POLYURETHANE BASED RIGID FLOORING LAMINATE
Abstract
The laminate according to the invention is a multiple layer
structure and contains predominantly urethane-based polymeric
materials in the cap and base layers thereof, with no significant
amount of PVC. As such, under combustion conditions, the laminate
releases substantially no harmful halogen-based bases, such as HCl
or other toxic gases, and exhibits toxicity and smoke generation
parameters well below acceptable industry standards.
Inventors: |
Pierson; Robert G.; (Akron,
OH) ; Ashton; Henry C.; (Aurora, OH) ; Gray;
Robert L.; (Hudson, OH) ; Du; Gilles Le;
(Akron, OH) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
Schneller LLC |
Kent |
OH |
US |
|
|
Family ID: |
42678529 |
Appl. No.: |
16/455852 |
Filed: |
June 28, 2019 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
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15269265 |
Sep 19, 2016 |
10336035 |
|
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16455852 |
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|
12716502 |
Mar 3, 2010 |
9446564 |
|
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15269265 |
|
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61156980 |
Mar 3, 2009 |
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Current U.S.
Class: |
1/1 |
Current CPC
Class: |
B32B 2307/50 20130101;
B32B 27/08 20130101; B32B 2260/021 20130101; B32B 2270/00 20130101;
Y10T 428/24942 20150115; B32B 2262/065 20130101; B32B 2260/046
20130101; B32B 27/308 20130101; B32B 27/285 20130101; Y10T
428/24851 20150115; Y10T 428/31511 20150401; B32B 7/12 20130101;
B32B 2471/00 20130101; B32B 27/34 20130101; B32B 5/22 20130101;
B32B 2262/101 20130101; B32B 27/12 20130101; B32B 2605/00 20130101;
B32B 2262/106 20130101; B32B 27/304 20130101; B32B 27/281 20130101;
B32B 27/40 20130101; B32B 5/024 20130101; B32B 2262/0269 20130101;
B32B 27/38 20130101; B32B 2307/72 20130101; Y10T 428/31554
20150401; B32B 2307/734 20130101; B32B 2262/02 20130101; Y10T
428/31551 20150401; B32B 27/302 20130101; B32B 27/36 20130101; B32B
27/18 20130101; B32B 2307/5825 20130101; B32B 5/26 20130101; B32B
2262/0223 20130101; B32B 27/20 20130101; B32B 27/286 20130101; B32B
5/022 20130101; B32B 2255/00 20130101; B32B 2255/26 20130101; B32B
2307/554 20130101; B32B 2307/75 20130101 |
International
Class: |
B32B 7/12 20060101
B32B007/12; B32B 27/36 20060101 B32B027/36; B32B 27/28 20060101
B32B027/28; B32B 27/12 20060101 B32B027/12; B32B 27/20 20060101
B32B027/20; B32B 27/40 20060101 B32B027/40; B32B 27/30 20060101
B32B027/30; B32B 27/08 20060101 B32B027/08; B32B 27/38 20060101
B32B027/38; B32B 5/22 20060101 B32B005/22; B32B 27/34 20060101
B32B027/34; B32B 5/26 20060101 B32B005/26; B32B 5/02 20060101
B32B005/02; B32B 27/18 20060101 B32B027/18 |
Claims
1. A laminate structure comprising: a backing layer comprising, by
weight, from about 20% to about 80% a fiber reinforcement and from
about 80% to about 20% with a thermoset or thermoplastic polymer
resin matrix; a base layer comprising an alloy layer made of
polyurethane in combination with a terpolymer comprising polyamide,
polyester and polyether or a combination thereof; and an adhesive
layer disposed on a first surface of the base layer between the
backing layer and the base layer; and a cap layer comprising
polyurethane, wherein the peel resistance between the combination
of the cap layer and base layer and the backing layer is at least
about 103 Newtons (N) per 25 millimeters after aging for at least
500 hours.
2. The laminate of claim 1, wherein the laminate meets the toxicity
flaming and non-flaming test protocols pursuant to AITM 2.0007 with
respect to HCN, CO, NO.sub.2, SO.sub.2/H.sub.2S, HF, and HCl
limits, said limits being less than 150, 1000, 100, 100, 100, and
150 respectively as measured by specific optical density, in
addition to Federal Aviation Regulation 25.853 MD with regard to
the parameters of vertical burn, drip time and char of the
laminate, said limits being less than 15 seconds, 5 seconds and 203
mm respectively, and further having a tear strength of greater than
50 Newtons according to ISO 4674, method A, and an areal density of
between 1800 and 2100 grams per square meter.
3. The laminate of claim 1, wherein the base layer includes the
polyurethane/terpolymer as a sub layer in combination with at least
one other sub layer selected from a primer sub layer, a fiber sub
layer and a sealing sub layer.
4. The laminate of claim 3, wherein the fiber sub layer comprises
at least one of glass, aramid, carbon, PVA, hemp, jute, organic
fiber, synthetic fiber disposed in a thermoset or thermoplastic
resin.
5. The laminate of claim 1, wherein the bondability between the
combination of the cap layer and base layer and the backing layer
is at least about 31 N/25 mm according to the ISO 4578 test
method.
6. The laminate of claim 1, wherein the adhesive layer comprises by
weight, from about 50% to about 70% polymer and from about 30% to
about 50% flame retardant additive.
7. The laminate of claim 1, wherein the adhesive layer comprises no
flame retardant additive.
8. The laminate of claim 1, wherein the laminate comprises from
about 30 grams per square meter to about 150 grams per square meter
adhesive layer disposed between the adhesive primer and the
substrate layer of the surface layer.
9. The laminate of claim 1, wherein the at least one of the backing
layers and the base layer comprises from about 100 grams per square
meter to about 400 grams per square meter fiber reinforcement, and
wherein the fiber reinforcement is a woven fabric.
10. The laminate structure of claim 1, wherein the laminate
releases no HCL during combustion.
11. The laminate structure of claim 1, further including a
decorative layer.
12. The laminate of claim 1, wherein the laminate is produced by a
roll-forming process and has an areal density of about 2300 grams
per square meter or less.
13. A laminate structure comprising: a backing layer comprising, by
weight, from about 40% to about 50% polyester, and from about 50%
to about 60% by weight fiber reinforcement; a base layer comprising
a polyurethane alloy comprising polyurethane in combination with a
terpolymer comprising polyamide, polyester and polyether or a
combination thereof sub layer containing polyurethane in
combination with a copolymer of at least two of polyamide,
polyether, polyester, polyether, polyimide, polyphenylene oxide and
polystyrene; a first adhesive layer disposed between the backing
layer and the base layer, the adhesive layer comprising a
thermoplastic polyurethane; a cap layer disposed on a surface of
the base layer opposite the backing layer and comprising a
polyurethane-based material; and a second adhesive layer disposed
between the base layer and the cap layer, wherein the laminate
structure having no amount of PVC in any component layer of the
laminate, and exhibits abrasion resistance of less than 400 mg
according to ISO 9352.
14. The laminate of claim 13 further comprising a primer layer
disposed between the adhesive layer and the reinforcing backing
layer.
15. The laminate of claim 14, wherein the second adhesive layer
disposed between the base layer and the cap layer contains an
organic or inorganic pigment.
16. The laminate of claim 15 further comprising one or more
decorative or print layers disposed between the cap layer and the
colored adhesive layer.
17. A laminate structure comprising: a backing layer comprising, by
weight from about 20% to about 80% fiber reinforcement and from
about 80% to about 20% thermoset or thermoplastic polymer; a base
layer comprising polyurethane-based material; and an adhesive layer
disposed on a first surface of the base layer between the backing
layer and the base layer; and a cap layer comprising polyurethane,
wherein the laminate meets the toxicity flaming and non-flaming
test protocols pursuant to AITM 2.0007 with respect to HCN, CO,
NO.sub.2, SO.sub.2/H.sub.2S, HF, and HCl limits, said limits being
less than 150, 1000, 100, 100, 100, and 150 respectively as
measured by specific optical density, in addition to Federal
Aviation Regulation 25.853 MD with regard to the parameters of
vertical burn, drip time and char of the laminate, said limits
being less than 15 seconds, 5 seconds and 203 mm respectively.
18. A laminate structure comprising: a backing layer comprising, by
weight, from about 40% to about 50% polyester, and from about 50%
to about 60% by weight fiber reinforcement; a base layer comprising
a sub layer containing polyurethane; a first adhesive layer
disposed between the backing layer and the base layer, the adhesive
layer comprising a thermoplastic polyurethane; and a cap layer
disposed on a surface of the base layer opposite the backing layer
and comprising a polyurethane-based material, wherein the laminate
does not generate harmful halogen gases upon combustion, and
produces NBS smoke levels of less than 200 according to the ASTN
E662 flaming mode test method and by specific optical density (Ds)
@ 4 min. non-flaming mode test method.
19. The laminate of claim 18 further comprising, a second adhesive
layer disposed between the base layer and the cap layer.
20. The laminate of claim 19, wherein the second adhesive layer
disposed between the base layer and the cap layer contains an
organic or inorganic pigment, and further comprising one or more
decorative or print layers disposed between the cap layer and the
colored adhesive layer.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This patent application is a continuation application of
U.S. application Ser. No. 15/269,265 filed Sep. 19, 2016, now U.S.
Pat. No. 10,336,035 issuing Jul. 2, 2019, which is a continuation
application of U.S. application Ser. No. 12/716,502 filed Mar. 3,
2010, now U.S. Pat. No. 9,446,564 issued Sep. 20, 2016, which
claims priority to and the benefit of U.S. Provisional Application
No. 61/156,980, filed on Mar. 3, 2009, which are incorporated
herein by reference in their entirety.
FIELD OF THE INVENTION
[0002] The present invention relates to multi-layered rigid
flooring laminates and to a method for making the same. More
specifically, the present invention relates to multi-layer
laminates having reduced toxicity and smoke levels during
combustion, as well as improved dimensional stability, and methods
of producing the laminates.
BACKGROUND OF THE INVENTION
[0003] Decorative and structural panels for architectural and
transport vehicle applications commonly take the form of laminates
having a surface layer and a reinforcement layer. The surface layer
often includes a decorative layer, or outer cover, affixed to a
substrate layer that provides rigidity, the laminate as a whole
exhibiting laminate weights of about 3,000 grams per square meter.
Decorative laminates typically have a visible layer that exhibits
an embossed texture, or a print pattern, or a combination of these
and other aesthetic design features.
[0004] In transport vehicle applications, laminates employed as
surface-covering materials must meet industry established standards
with regard to not only the release of toxic fumes or gases upon
combustion, including those released with smoke, but also the
amount of smoke created during the combustion process. It is
further desirable to be able to manufacture laminates meeting
industry standards that display uniformity of the texture and print
pattern design features of the decorative portion of the laminate.
This can be difficult to achieve as any decorative feature must
maintain its integrity throughout the manufacturing process.
Non-textile flooring (NTF) laminates are generally constructed
using multiple layers of various films laminated together under
high temperature and pressure, and/or embossed, again at high
temperature and pressure, at different stages in a continuous
roll-forming manufacturing process.
[0005] Conventional methods for the manufacture of such laminates
are limited by the properties of the materials used which impose
limitations on the extent to which the combined layers can be
heated, stretched and further processed in casting and roll-forming
machinery without adversely affecting the dimensional stability of
the final product or the performance characteristics of the various
laminate-layers. Laminates have three basic dimensions which can be
represented by reference to x, y, and z axis, where the z-axis
represents the thickness of the laminate. In conventional
laminates, permanent distortion occurs along the x or y axis, or
both, when the laminate is heated and stretched in one or more
directions as a result of forces applied in a mechanical lamination
process. As the laminate cools it retains such distortion.
[0006] Conventional laminates used in the industry include one or
more layers containing PVC (polyvinyl chloride). PVC laminates
provide a low cost laminate option that is durable and low
maintenance. This type of surface laminate resists abrasion and
impact damage, making its use for flooring in high traffic areas
attractive. For some time, PVC-containing laminates have been the
best available choice for use in the transportation industry.
However, those laminates containing PVC exhibit high levels of
toxicity and smoke generation upon combustion, presenting a concern
in industrial applications, and particularly air transport
applications.
[0007] In addition, currently employed laminate structures are of a
construction which results in a higher than desired weight to
ensure rigidity and stability. These structural laminates, though
they provide adequate performance characteristics for aviation
flooring and are available in the form of sheets, also have
dimensional limitations which can result in unnecessary waste in
end-use applications.
SUMMARY
[0008] The present invention provides for various laminate
constructions, suitable for use as flooring and/or industrial
laminate applications, that exhibit desired aesthetic properties,
for example texture and graphical features, and that also exhibit
low toxicity and smoke levels upon combustion, meeting and
exceeding aviation industry standards. In one embodiment, a
dimensionally stable, multi-layered laminate structure includes a
backing layer, having by weight from about 20% to about 80%
thermoset or thermoplastic polymer selected from polysulfone,
polyester, phenolic, epoxy acrylic and vinylester and mixtures
thereof, and from about 20% to about 80% reinforcement fiber. The
backing material may be primed to accept the adhesive or promote
the adhesive by use of a primer material such as (insert material
designations). The multi-layered laminate further includes an
adhesive and primer to bind, the backing layer to a first surface
of a base layer. The primer may be a polyurethane thermoplastic or
thermoset, an epoxy or any other suitable polymer. The base layer
includes an alloy comprising polyurethane in combination with a
homopolymer or copolymer. The homopolymer or copolymer may be
selected from a combination of known polymers, including but not
limited to polyamidc, polyester, polyether, polyimide,
polyphenylene oxide, polystyrene, acrylic and combinations thereof.
In one embodiment, the copolymer comprises a terpolymer that may
contain, for example, polyamide, polyester, and polyether, such
that the base layer as a whole includes from about 10% to about
100% polyurethane, and from about 10% to about 100% terpolymer, the
terpolymer including from about 10% to about 100% of each of the
polyamide, polyester, and polyether components. Finally, a cap
layer of polyurethane is provided on a second surface of the base
layer. Generally, the polyurethane cap layer is clear, but it may
also contain a colorant. The laminate structure is intended to be
lightweight and exhibits an aerial density of about 2300 grams per
square meter or less.
[0009] In additional embodiments, the laminate structure may
further include one or more decorative layers to enhance the
aesthetics of the laminate surface. This layer, or these layers,
may be disposed between the cap layer and the base layer. For
example, options for creating a more aesthetic laminate appearance
include: the addition of pigment to, for example, the cap and/or an
adhesive layer; printing the back side of the cap layer; adding an
additional layer of print material between the cap layer and an
adhesive layer of the base layer, or any combination thereof.
[0010] In one embodiment, the laminate structure includes a backing
layer of about 1 to about 100 mils in thickness, more preferably
about 10 to 60 mils in thickness and most preferably between 10 and
40 mils in thickness. It further includes a base layer of about 1
to about 50 mils thickness, or in some embodiments about 10 to
about 35 mils thick, and in still other embodiments about 28 mils
thick. There is also included a cap layer of about 1 to about 15
mils thickness, or in some embodiments about 3 to about 10 mils
thick, and in still other embodiments about 8 mils thick.
Additional layers which are optionally present may include adhesive
and decorative layers, and each may be from about 0.3 to about 3
mils thick or in some embodiments about 1 to about 2 mils thick,
and in still other embodiments about. 1 mil thick. The thickness of
any particular layer or combination of layers is determined based
on such factors as the desired thickness of the overall laminate
product, as well as the thickness necessary for the layer to
provide the desired function.
[0011] In any of the embodiments described above, in accordance
with the present invention, the method for making a laminate
structure includes known laminate processing techniques. For
example, known roll-forming processing techniques may be used. In
one embodiment, the method includes applying roll-forming
processing used to first prepare the base layer 24, which includes
a urethane/copolymer mix sub layer 24a, a PVC urethane primer sub
layer 24b, a glass fiber mat sub layer 24c, and a PVC seal sub
layer 24d, and then laminate the base layer 24 to a backing layer
22 which comprises glass or other fiber material in a thermoset or
thermoplastic polymer matrix. The base layer and the backing layer
are laminated at a temperature ranging from about 170.degree. F. to
about 340.degree. F. In the base layer, sub-layer 24c comprises a
woven or nonwoven glass fiber material, pretreated by being
disposed in a thermoset or thermoplastic polymer selected from the
group of: polyester, phenolic, epoxy, polysulfone, acrylic and
mixtures thereof. The base layer further includes sub-layer 24a
comprising at least one polymer selected from polyurethane,
polyamide, polyester, polyether, polyimide, polyphenylene oxide,
polystyrene or any of these polymers in combination with any other
of these polymers. For example, polyurethane may be used alone, or
in combination with a homopolymer or copolymer, for example a
terpolymer. In example embodiments, the continuous roll-formed
laminate has an aereal density of about 2300 grams per square meter
or less, or even 2100 grams per square meter or less. In example
embodiments, the laminate provided exhibits toxicity and smoke
parameters which are well below the accepted ABS 0031 Standards
used throughout the air transport industry.
BRIEF DESCRIPTION OF THE DRAWINGS
[0012] The various embodiments of the present invention can be
understood with reference to the following drawings. The components
in the drawings are not necessarily to scale. Also, in the
drawings, like reference numerals designate corresponding parts
throughout the views.
[0013] FIG. 1 is a perspective illustration of a laminate
structure, according to an embodiment of the present invention.
[0014] FIG. 2 is a perspective illustration of another optional
laminate structure, according to an embodiment of the present
invention.
[0015] FIG. 3 is a perspective illustration of another optional
laminate structure, according to an embodiment of the present
invention.
DETAILED DESCRIPTION OF THE INVENTION
[0016] The laminate according to the invention is a multiple layer
structure and contains predominantly urethane-based polymeric
materials in the cap and base layers thereof, with no significant
amount of PVC. As such, under combustion conditions, the laminate
releases substantially no harmful halogen-based bases, such as HCl
or other toxic gases, and exhibits toxicity and smoke generation
parameters well below acceptable industry standards.
[0017] FIG. 1 is an exploded perspective illustration of a laminate
structure 10 according to an embodiment of the present invention.
According to FIG. 1, laminate structure 10 includes a backing layer
22 and a base layer 24 and a cap layer 26.
[0018] The backing layer 22 includes a fiber-reinforced thermoset
polymer made from woven or non-woven fibers impregnated in a
thermoset or thermoplastic polymer resin matrix. Suitable resins
include, but are not limited to, saturated- or unsaturated-
polysulfone, -polyphenolsulfone, -polyester, -phenolic resin,
-epoxy resin, and mixtures thereof. The term "unsaturated" is used
in reference to a thermoset polymer including a molecule having one
or more carbon-carbon double bonds, and capable of further
polymerization in a curing process, for example, by exposure to
elevated temperatures. Once the "unsaturated" polymer has been
cured and is present in the laminate structure, it is no longer
referred to herein as an "unsaturated" polymer even though it may
not be fully saturated in the cured state. For example, in various
embodiments of the manufactured laminate structure in which
polyester is present in the reinforcement layer, or the adhesive
layer, or both, the polymer is referred to herein as "polyester"
even though it may not be fully saturated in the cured state of the
laminate structure.
[0019] The amount, by weight, of resin present in the backing layer
22, can range from about 20% to about 80%, in another embodiment
from about 30% to about 70%, and in another embodiment from about
40% to about 50%. In one embodiment, the backing layer 22 contains,
by weight, from about 20% to about 80% reinforcement fiber, and in
another embodiment, from about 30% to about 70% by weight fiber,
and in yet another embodiment from about 50% to about 60% by weight
fiber. The fiber may be glass, aramids, carbon, polyvinyl alcohol
(PVA), hemp, jute, organic materials, rayon, or other suitable
fiber reinforcing material.
[0020] In one embodiment, the backing layer 22 is sufficiently
stiff to provide good telegraph resistance, but sufficiently
flexible to provide low weight and enable laminate structure 10 to
be rolled on cores, for example 3-inch to 6-inch diameter cores,
for ease of storage, transport and handling during application or
installation. Telegraph resistance is an attribute of some
structural laminates, for example, decorative NTF laminates, that
keeps any unevenness in the underlying layer from being readily
observed because of the stiffness of the NTF laminate. In addition,
laminates available as continuous roll material offer economic
advantages because less material is wasted when custom geometric
pieces are cut from the roll.
[0021] The base layer 24 includes a layer of pretreated woven glass
fabric or mat 24c. The glass component of glass layer 24c is
pretreated by disposing glass fibers, sometimes in the form of a
glass fabric or mat, in a polymer such as, for example, polyester,
phenolic, epoxy, polysulfone, and mixtures thereof, or other
similar polymers, to increase the smoothness of the surface, which
enhances the capability of the surface to adhere to another
surface, and to prevent the coatings applied thereto from
impregnating the spaces between the fibers of the fabric.
[0022] Also included is an alloy layer 24a comprising polyurethane
in combination with a homopolymer or a copolymer. The homopolymer
or copolymer may be selected from a combination of known polymers,
including but not limited to polyamide, polyester, polyether,
polyimide, polyphenylene oxide, polystyrene and combinations
thereof. In one embodiment, the copolymer comprises a terpolymer
that may contain, for example, polyamide, polyester, and polyether,
such that the base layer 24a as a whole includes from about 10% to
about 100% polyurethane, and from about 10% to about 100%
terpolymer, the terpolymer including from about 10% to about 100%
of each of the polyamide, polyester, and polyether components.
[0023] Also included in base layer 24 is a primer layer 24b,
disposed between the urethane/copolymer sub layer 24a and the glass
sub layer 24c. Primer layer 24b generally comprises a PVC urethane
composition, to enhance the adhesion of layers 24a and 24c, both of
which include a urethane component. The primer layer could also be
acrylic, urethane, epoxy, polyester or combinations thereof.
[0024] In one embodiment, the primer sub layer 24b is a thermoset
adhesive containing a resin which can include, but is not limited
to, polyester, polyurethane, epoxy, acrylic, and mixtures thereof.
The amount of primer in sub layer 24b disposed between the base
layer 24a and 24c is greater than about 0.25 oz. per square meter,
in another example, the primer can range from about a 5 to about 40
oz. per square meter, in another example, from about 0.3 to about
25 oz. per square meter and in still another example, from about
0.5 to about 20 oz. per square meter. These amounts are based on a
dry weight present in the laminate.
[0025] Finally, base layer 24 includes a very thin sealing sub
layer 24d, comprising. PVC, which serves to prevent the glass
fibers in sub layer 24c from etching the roller surface during the
roll-forming process.
[0026] Known laminates include much higher percentages of PVC,
which is not a significant component of the current laminate. In
known laminates, the base layer comparable to sub layer 24a of this
invention, generally is primarily comprised of PVC. PVC inherently
releases high levels of halogen, particularly HCl, under conditions
causing combustion. In addition, other components of known
laminates may release NOx, HF, HBR, HCN, CO, CO.sub.2 and SO.sub.2
under these same conditions. Because the release of such halogens
is harmful to those it comes in contact with and to the
environment, efforts have been made to produce materials that have
lower toxicity levels and yet exhibit the desirable wear
characteristics of PVC. The laminate according to the invention
eliminates PVC as a component of sub layer 24a, and instead
comprises a polyurethane or a polyurethane alloy that renders a
laminate product, when combined with a backing layer and a cap
layer, that does not generate harmful halogen gases, particularly I
ICI, upon combustion. An additional benefit of the laminate of the
invention is the generation of lower levels of smoke having these
harmful components entrained therein.
[0027] The laminate of the invention may include one or more
fiber-containing layers. Fiber materials which can be used in the
backing layer 22, and as part of the base sub layer 24c, for
example, can include, for example, glass, aramids, carbon,
polyvinyl alcohol (PVA), hemp, jute, organic materials, and rayon.
Depending upon the material of the fiber/woven fabric and its
specific gravity, the aereal density of the laminate can vary from
about 100 grams per square meter to about 400 grams per square
meter and all ranges there between. For example, in various
embodiments in which glass is used as the reinforced fiber, the
aereal density of glass in at least one of the backing layer 22 and
the base sub layer 24c ranges from about 200 to about 400 grams per
square meter, in another embodiment from about 250 to about 350
grams per square meter, and in another embodiment from about 275 to
about 325 grams per square meter. In another embodiment in which
aramid fiber is used, the areal density of the fiber/woven fabric
of at least one of the backing layer 22 and the base sub layer 24c
ranges from about 100 to about 300 grams per square meter, for
example.
[0028] The laminate may further include adhesive layer 23, which is
shown disposed between the backing layer 22 and the base layer 24.
Adhesive layer 23 contains a thermoplastic resin which can include,
but is not limited to, polyurethane, for example a polyester-based
polyurethane, acrylic polyamide, epoxy polyvinyl alcohol,
polyester, and mixtures thereof, as well as additional
thermoplastic polymers having similar melting temperatures and
adhesive properties. In another embodiment, adhesive layer 23
includes two or more thermoplastic polymers. For example, a
suitable adhesive layer 23 may include, by weight, from about 70%
to about 90% of a polymer as listed above, for example a
polyester-based polyurethane, and also includes from about 10% to
about 30% by weight of a second thermoplastic polymer selected from
the group of polyamide, polyvinyl alcohol, polyester, phenoxy and
mixtures thereof.
[0029] The amount of adhesive layer 23 present in laminate
structure 10, and disposed between backing layer 22 and base layer
24, can range from about 30 to about 150 grams per square meter, in
another example from about 70 to about 100 grams per square meter,
and in still another example from about 70 to about 90 grams per
square meter. The adhesive 23 may be, but does not have to be, a
heat-activated adhesive which melts during lamination at elevated
temperature as will be further described.
[0030] Adhesive layer 23 optionally contains a flame retardant
additive in quantities based on parts per hundred resin. As is
shown in FIG. 2, additional adhesive layers 23a and or 23b may be
included in the laminate structure. Generally, a flame retardant
additive is included in at least adhesive layers 23 and 23a, though
it may also be included in layer 23b. Suitable flame retardants
include, but are not limited to, aluminum trihydrate, magnesium
hydroxide, organophosphates, red phosphorous, phosphorus compounds,
zinc borate, boric acid, oxides of boron, melamine(s), melamine
derivatives such as salts thereof with organic or inorganic acids,
ammonium polyphosphate, ammonium pentaborate, mixtures of zinc
salts of alkali metals containing nano-clay and/or functionalized
nano-metals, and mixtures thereof. The amount of flame retardant,
alone or as a mixture of two or more flame retardant additives, can
be present in up to about 40 parts per hundred resin, in another
embodiment up to about 20 parts per hundred resin, in another
embodiment up to about 15 parts per hundred resin, and in yet
another embodiment up to about 10 parts per hundred resin, and all
ranges there between. Also, it should be understood that a flame
retardant additive is optional and therefore, in another
embodiment, the adhesive 23 contains no flame retardant additive.
That is, when the adhesive contains no flame retardant additive,
any flame retardant performance if present in the adhesive layer
would be characteristic of the inherent properties of the at least
one thermoplastic polymer used in the adhesive layer 23.
[0031] FIG. 2 is an exploded view illustration of laminate
structure 20 which includes all of the layers of laminate structure
10, and further includes optional print or decorative layer 25 and
additional adhesive layers 23a and 23b and additional primer layer
27. A primer can be used to promote the adhesion of the adhesive
layer. In both laminate structures 10 and 20 the composition of the
adhesive and primer layers is generally different. For example,
while both may be urethane-based material layers, each may contain
additives particularly suited for certain purposes.
[0032] With further reference to FIG. 2, in another embodiment,
laminate structure 20 includes a decorative layer 25. In one
embodiment the decorative layer 25 is a layer disposed beneath cap
layer 26 such that it is visible through the cap layer. Decorative
layer 25 includes, but is not limited to, a polymer selected from
acrylic, polyurethane, PVC and mixtures thereof. Decorative layer
25 may include a colorant or pigment or a so-called effect pigment
such as aluminum or Nacre. Optionally, decorative layer 25 may be
(i) opaque, or decorative layer 25 may be (ii) clear translucent,
or decorative layer 25 may be (iii) colored translucent, or
decorative layer 25 may be any combination of the foregoing. The
laminate may, in some embodiments, include additional decorative
layers including, but not limited to, at least one or more of, a
print layer, a metal layer, a varnish, and/or a polymer. For
example, a further decorative layer (not shown) can be at least one
of a printed pattern, an embossed pattern which provides texture,
and a color or pigment layer. The decorative layer 25 may further
include at least one flame retardant additive, selected from but
not limited to aluminum trihydrate, magnesium hydroxide,
organophosphates, red phosphorous, phosphorus compounds, zinc
borate, boric acid, oxides of boron, melamine(s), melamine
derivatives such as salts thereof with organic or inorganic acids,
ammonium polyphosphate, ammonium pentaborate, mixtures of zinc
salts of alkali metals containing nano-clay and/or functionalized
nano-metals, and mixtures thereof. The amount of flame retardant,
alone or as a mixture of two or more flame retardant additives, can
be present in up to about 40 parts per hundred resin, in another
embodiment up to about 20 parts per hundred resin, in another
embodiment up to 15 parts per hundred resin, and in yet another
embodiment up to about 10 parts per hundred resin, and all ranges
there between.
[0033] In other embodiments, the laminate structure 10 shown in
FIG. 1 or 2 may obtain a textured, colored, or patterned appearance
without the addition of decorative layer 25. In these embodiments,
cap layer 26 may include a pigment. Alternatively, an adhesive
layer 23b, having pigment disposed therein, may be disposed between
base layer 24 and cap layer 26. In yet another alternative
embodiment, pigment is disposed in both cap layer 26 and adhesive
layer 23b. Additionally, pigment may be disposed in base layer 24
rather than or in addition to layers 23b and/or 26. In yet another
embodiment, a texture or patterned appearance is imparted to the
laminate 10 or 20 by embossing one or more surfaces of any of the
foregoing layers 23b, 24, or 26, or any optional layer provided
there between.
[0034] With reference to FIGS. 2 and 3, FIG. 3 is an exploded view
structure of the laminate structure 30 which includes all the
layers and constituents of structure 20 with the exception of the
print or decorative layer 25 and is another embodiment of the
invention.
[0035] The cap layer 26 and base layer 24 are sometimes considered
together as the "surface layer" of the laminate. This surface layer
adheres well to the backing layer 22 such that the peel resistance
between the surface layer and the backing layer 22, when tested
according to the ISO 8510 standard test method used in the
industry, performs extremely well. After aging for 500 hours at
70.degree. C., the samples tested exhibited: peel resistance values
of at least about 103 Newtons (N) per 25 millimeters (mm), and in
another example, at least about 105 N/25 mm; and bondability,
according to test method ISO 4578, ranging from about 31 to about
33.9 N/25 mm.
[0036] As set forth in Table 1, the laminate as described herein
was tested in accord with ABD-0031 Standards. Three samples in
accord with the invention were tested to generate the data
presented in the Table. Each sample included the same or comparable
backing and adhesive layers, i.e. samples 1 and 2 used phenolic
backing material available commercially from McGill, and sample 3
included a phenolic backing material prepared by the applicant.
With regard to the base layers of the tested laminates, all three
samples used the same seal, glass, and primer sub layers, and
included a urethane-terpolymer sub layer as the main base layer,
(24a in FIGS. 1 and 2). The use of the urethane-terpolymer
composition, as opposed to the PVC composition of known laminates,
renders significantly less HCl under combustion conditions. In
addition, PVC-based laminates degrade quickly at high temperatures.
Other known laminates contain silicone compositions, which have
significantly inferior slip resistance, and are a thermoset and
therefore cannot be recycled. Finally, all three samples tested
included a polyurethane cap layer. The results in Table 1 verify
that with regard to the production of smoke, under both flaming and
non-flaming test conditions, the laminate of the invention recorded
data well below acceptable industry standard levels. Further, when
tested according to AITM 2007, the laminate according to the
invention released no HCl, and levels of other potentially toxic
components well below acceptable levels. Table 1 provides full test
data for all areas of performance critical to qualification of the
laminate for use in the airbus transportation industry.
[0037] The laminate structures of the present invention are
relatively light weight, having a maximum aereal density up to
about 2300 grams per square meter, in another embodiment about 1800
to about 2100 grams per square meter or less, in another example,
less than about 1800 grams per square meter, and in yet another
example, an aereal density of about 1500 grams per square
meter.
TABLE-US-00001 TABLE 1 ABD-0031 Specification Property Poly.2415
Poly.2415 Texture 92R 92R Color Poly.2415 Lubrizol Blue Blue CM
Construction Cap Cap Cap + Adh Cap + Adh Backing Test McGill McGill
6100 6100 Sample Methods Spec RKH001 RKH002 RKG 621 RKG 622
Thickness ISO 2286-3 69.8 mil 64.7 mil 57.7 62.4 Weight ISO 2286-2
<2300 2087 1915 1933 1973 grams UV (DE) ASTM G- Test No change
No 0.527/1.1 .951/1.078 53 (UVA 50.100 change 340.sub.-- Static Dry
MD ISO 8295 >.25 0.973 1.022 0.816 0.687 Coefficient of Wet MD
0.83 0.878 0.706 0.59 Friction Dry XD 1.066 0.999 0.919 0.631 Wet
XD 0.845 0.755 0.704 0.637 Dynamic Dry MD >.25 0.678 0.875 0.73
0.594 Coefficient of Wet MD 0.76 0.779 0.617 0.545 Friction Dry XD
0.709 0.781 0.845 0.58 Wet XD 0.716 0.605 0.642 0.523 Dimensional
md/cmd <.2% 0.13% 0.10% 0.00% 0/0 Stability Curling EN434
(70.degree. C. <10 mm fail fail fail 9.75 1 week) Abrasion (Loss
ISO 9352 <1000 mg. 0.5558 0.6525 0.2042 0.2289 of mass) 50%
Impact Spec. Para >9 J 100% pass 40% 15.4 14.4 failure energy
2.2 Tear MD ISO 4674-1 >60 N 166.7 78.3 186 131 XD Method A
190.3 122.3 181 182 Peel MD ISO 8510-2 >50 N >50 >50 CSF
CSF Resistance or CSF (Top layer & XD xxx xxx CSF CSF
reinforcement) Peel MD 84.9 57.0 17.4 89.7 Resistance XD xxx xxx
34.6 56.4 (Top material and phenolic) Bondability ISO 4578 >20 N
31.47 33.9 29.8 32 Sealability ISO 11339 No Air Coh. Coh. 66.4 flow
(pass) (pass) Formation of Spec Para No pass pass no change pass
bubbles 2.2 bubbles Stain resistance- (Citric acid ISO 4586-2 5
rating 5 5 5 5 10%) (Red wine) Clause 15 5 5 5 5 (20% urea)
Procedure A 5 5 5 5 Vertical Burn Far 25.853 <15 sec. 0.8 5.11 0
5.3 12 sec. (After MD flame) sec. (Drip time) <5 sec. 0 0 0 0
sec. (Burn length) 203 mm. 1.53 1.87 2 1.6 in. XD <15 sec. 5.2
4.7 1.76 6.48 <5 sec. 0 0 0 0 203 mm. 1.0 1.53 1.46 1.46 Heavy
metals None None None XXX and antimony oxide Seaming EN 684 250
N/50 mm. 338 N 409 N 361 481 NBS Smoke ASTN E662 <200 171.1
106.22 121.2 101.2 (Flaming mode) (Non flaming DS @ 4 min. <200
120.7 131.2 146 113 mode) Toxicity HCN 150 2.0 2 10, 10 10 Flaming
CO 1000 150.0 100 130 250 (AITM 2.007) NO/NO.sub.2 100 80, 50 70,
90 60, 80 40 NOx retest 100 83.3 86.7 xxx Property
SO.sub.2/H.sub.2S 100 1.0 0 0 0 HF 100 0.0 0 0 0 HCI 150 0.0 0 0 0
Toxicity Non- HCN 150 0.0 0 1 2 Flaming CO 1000 0.0 0 0 50
NO/NO.sub.2 100 0.0 0 0 20 SO.sub.2/H.sub.2S 100 0.0 1 0 0 HF 100
0.0 0 0 0 HCI 150 0.0 0 0 0 Blooming No pass pass pass XXX pass
blooming @ 3 weeks Peel ISO 8510-2 >40 N 103.1 105.4 CSF
Resistance or CSF after 500 hrs. (@70.degree. C. Tear strength ISO
4674-1 >50 N 146.72 64.38 131 after 500 hrs. @70.degree. C. (MD)
(XD) Method A 158.78 86.92 113
[0038] Laminate structures herein have an abrasion resistance shown
by Taber abrasion testing, ISO 9352, with mass loss of less than
about 653 milligrams, and in another embodiment, less than about
556 milligrams.
[0039] When tested according to FAA specifications, as set forth in
Table 1, the laminate of the invention demonstrated a dynamic
coefficient of friction between about 0.52 and 0.78 for wet and
between about 0.58 and 0.87 for dry sled with either rubber or
leather as described in FAR 25.793 Amendment 25-51 procedure A, all
well above the required 0.25.
[0040] The laminates were also tested according to FAR 25.853 MD
with regard to vertical burn. As shown in the table, the laminate
is subjected to an open flame. The test records the time it takes
for the sample to extinguish (must be less than 15 seconds), the
drip time (must be less than 5 seconds), and the length of the char
(must be less than 203 mm or 8.02 inches). As is seen in Table 1,
the samples according to the invention recorded burn times of 0.8
sec., 5.11 sec., 5.3, 0 sec, all well below the 15 sec. limit. Drip
time for all three samples was 0, and char lengths were 1.53 in.,
1.6 in. 1.87 in and 2.0 in., again all well below the 8.02 in.
threshold.
[0041] The tear strength of laminate structures herein is well
above the required 50 Newtons, in one embodiment being greater than
about 146 Newtons, and in another embodiment, greater than about
158 Newtons according to ISO 4674, method A.
[0042] In another embodiment, laminate structures herein arc stain
resistant as per ISO 4586-2, clause 15, method A, Procedure A,
rating 5. An additional layer of adhesive, shown in FIG. 2 as
adhesive layer 23b, may be added to the laminate as discussed
hereinabove. The addition of this adhesive layer, disposed between
the base layer 24 and the cap layer 26, provides unexpected
abrasion resistance to the laminate structure. Table 1 shows, for
example with respect to Sample 1, abrasion of 555.8 mg., according
to standard test ISO 9352, which is well below the acceptable 1000
mg threshold. This test records milligrams of laminate abraided per
1000 revolutions of a wheel against the surface. With the addition
of adhesive layer 23b, the laminate loses only 200 mg if
un-pigmented and 400 mg if pigmented. Both results represent
significant abrasion resistance improvement.
[0043] The laminate structure according to the invention may be
made by a conventional roll-forming process, or other known
laminating techniques. The resulting laminate may exhibit various
dimensions, for example a fixed width along its length, such as
about 1.5 meters wide, and variable length, for example, greater
than about 6.5 meters long, in another example, from about 10
meters to about 25 meters long, and in another example, at least
about 30 meters long.
[0044] Roll-forming processing parameters may vary depending on the
chemistry of adhesive and primer and the thickness of the laminate.
For example, processing temperatures may vary. The lamination step
may be carried out at a relatively low surface temperature that
ranges from about 170.degree. F. to about 300.degree. F., in
another embodiment from about 170.degree. to about 250.degree. F.,
and in another embodiment from about 170.degree. to about
220.degree. F. Additionally, the pressure may vary from about 20
psi to about 40 psi. The roller speed can also vary and can range
from about 2 meters/minute to about 5 meters/minute, and in other
exemplary embodiments, from about 2.5 meters/minute to about 4
meters/minute.
[0045] It is to be understood that for purposes of the present
specification and claims the range and ratio limits recited herein
can be combined. For example, if ranges of 10 to 100 and 20 to 90
arc recited for a particular parameter, it is understood that the
ranges of 10 to 90 and 20 to 100 are also contemplated.
Independently, if minimum values for a particular parameter are
recited, for example, to be 1, 2, and 3, and if maximum values for
that parameter arc recited to be, for example, 8 and 9, then the
following ranges are all contemplated: 1 to 8, 1 to 9, 2 to 8, 2 to
9, 3 to 8, and 3 to 9.
[0046] The following examples of dimensionally stable laminates
made. according to embodiments of the present invention are further
disclosed, and do not otherwise limit the scope of the
invention.
[0047] Laminates in keeping with the invention were prepare and
performance tested, the data from those tests being presented in
Table 1. An exemplary laminate composition, in accord with tested
sample 1, is shown in Table 2.
TABLE-US-00002 TABLE 2 LAMINATE - SAMPLE 1 LAYER* Weight
(g/m.sup.2) % Composition Urethane cap (26) 243 12.47
Urethane/terpolymer 981 50.30 Base Layer (24a) Primer Layer (24b)
16.6 0.85 Glass Layer (24c) 218 11.19 Adhesive (23a) 33.20 1.7
Adhesive (23) 33.20 1.7 Phenolic Backing (22) 425 21.79 Total 1950
100 *numbers refer to FIGS. 1 & 2
[0048] The present invention is intended to include such
modifications and alterations in so far as they fall within the
scope of the appended claims or the equivalents thereof
* * * * *