The field of this application relates generally to the manufacture of thin-layer composites and, more particularly but not exclusively, to composite door skins made from an isocyanate-based resin and cellulosic and/or noncellulosic fibers.
U.S. Pat. No. 7,399,438 of Clark et al., which is incorporated herein by reference, describes methods of manufacturing lignocellulosic composite materials and doors made of a frame structure covered by thin-layers of such composite materials known as door skins. The composite materials and door skins may be made by mixing wood fiber, wax, and a resin binder, and then pressing the mixture under conditions of elevated temperature and pressure to form a thin-layer wood composite that is then bonded to the underlying door frame or core. As described in the '438 patent, composite door skins are conventionally formed by pressing wood fragments between heated dies in the presence of a binder at temperatures exceeding 275° F. (135° C.). The resin binder used in the door skin may be an isocyanate-based resin, a formaldehyde-based resin, a thermoplastic resin, or a thermoset resin.
A significant problem in the manufacture of wood-based composite products that are exposed to the outdoor environment and extreme interior environments is that upon exposure to variations in temperature and moisture, the wood can lose water and shrink, or gain water and swell. This tendency to shrink and/or swell can significantly limit the useful lifetime of most exterior wood products, such as wooden doors, often necessitating replacement after only a few years. The problem is particularly prevalent in extremely wet climates and extremely hot or dry climates. Door skins made of a composite mixture of wood fibers, fiberglass, and a resin binder have recently been introduced in the market, which provide improved resistance to moisture. Composite materials and door skins made of fiberglass and resin and without any cellulosic fiber content are also known.
The '438 patent describes a process utilizing isocyanate-based resins instead of formaldehyde-based resins to yield lignocellulosic fiber composite door skins having increased resistance to changes in environmental moisture. Isocyanate-based resins may also provide environmental benefits over formaldehyde-based resins. However, the present inventors have found that it is more difficult in some respects to make composites with isocyanate-based resins than with formaldehyde-based resins. For example, isocyanate-based resins have a greater tendency to adhere to the working surfaces of the steel dies used for pressing the composite mixture. This tendency can lead to a build-up of resin or composite material on the die surface, which causes undesirable defects in the surface finish of door skins.
The '438 patent describes several generally complementary approaches to inhibiting adhesion and build-up on die surfaces, including the use of an internal release agent in the composite mixture, the application of a release agent on the surface of a mat of the composite mixture prior to pressing the mat, and the application of anti-bonding agents on the die surface. Some of the various anti-bonding agents described in the '438 patent involve coating the die surface with a liquid composition that is baked into the die to form a stable anti-bonding coating that can be used for 2000 press cycles. The '438 patent also describes that the use of a release agent and/or an anti-bonding agent during the manufacture of cellulosic composite door skins may allow for increased resin content in the composite, which may improve the strength and surface finish of door skins. Notwithstanding the use of anti-bonding agents on the dies and release agents in or on the composite mixture, a build-up will eventually form on the dies over the course of many successive pressing cycles, requiring the dies to be regularly removed from the press for cleaning and recoating with the anti-bonding agent. Removal and recoating of the dies leads to equipment downtime, added expense, and waste.
Accordingly, a need exists for improved means and methods of preventing composite adhesion to and build-up on the dies used for pressing door skins and other composite materials.
A method of forming a thin-layer moisture-resistant fiber composite material such as a door skin involves forming a loose mat from a mixture of fibers and at least 1% by weight of resin such as an organic isocyanate resin, then pressing the mat between a pair of heated dies at least one of which includes a working surface coated with a hard ormosil coating. The ormosil coating preferably includes a cross-linked organically-modified silica network and has a hardness exceeding 6H pencil hardness. The dies may be heated to between 250° F. and 425° F. (121° C. to 218° C.), such that when the mat is pressed for sufficient time, e.g. greater than 15 seconds at more than 100 psi (690 kPa), the resin interacts with the fibers to form a consolidated fiber composite sheet material having a thickness in the range of about 1 mm to 13 mm.
The hard ormosil coating may be characterized by a dry film thickness of approximately 25 to 80 microns (micrometers (μm)) or more, abrasion resistance greater than 50,000 cycles (BSI Standard 7069:1988) and scratch resistance of at least 12 grams critical load using a 90° diamond indenter, and may allow the composite sheet forming process to be repeated for 20,000 cycles without substantially degrading an anti-bonding property of the ormosil coating. In some embodiments, the ormosil coating includes inorganic additives, such as metal oxide particles or nanoparticles dispersed within the silica network. In some embodiments, the ormosil coating includes alkyl or aryl groups chemically bonded to the silica network, which may result in the coating being hydrophobic so as to exhibit an advancing water contact angle of greater than 90 degrees and a total surface energy of less than approximately 25 mJ/m2, including a polar surface energy component of less than approximately 6 mJ/m2.
The ormosil coating may be formed by a sol-gel process in which an admixture of at least two distinct reactive chemical components is matured before being applied to the die and cured, preferably by heating the coated die to an increased temperature, in the range of 385° F. to 660° F. (196° C. to 349° C.) for example. To promote coating adhesion, the die working surface is preferably roughened to approximately 2.5 to 6.0 microns (μm) Ra before the ormosil coating is applied thereto.
Systems for manufacturing a thin-layer moisture-resistant fiber composite material from a mixture of cellulosic fibers and resin are also disclosed, in which a metallic working surface of equipment that is exposed to the mixture during processing is coated with the above-described ormosil coating to thereby inhibit buildup of the resin and fibers on the working surface. The equipment may include a pair of dies that are heated to between 250° F. and 425° F. (121° C. and 218° C.), at least one of which is coated with the ormosil coating, or other equipment in the system, such as a blender, blowline piping, a refiner, or a conveyor belt for example.
Use of the ormosil coatings described herein may yield composite sheet material products having improved surface quality, edge sharpness, and/or increased draw angles, or other benefits.
Further aspects of various embodiments will be apparent from the following detailed description which proceeds with reference to the accompanying drawings.
As used herein, a thin-layer composite comprises a sheet or generally flat composite structure that is significantly longer and wider than it is thick. Examples of thin-layer composites include door skins that are used to cover the frame or core of a door to provide the outer surface of the door. Such door skins may comprise composite sheets that are only about 1 to about 13 mm thick, but may have a surface area of about 10-24 square feet (about 0.9 to 22 square meters) or more. Door skins may be flat and smooth or may be contoured to simulate a frame-and-panel construction and/or textured to simulate natural wood grain. Other thin-layer cellulosic composite products include medium density fiberboard (MDF), hardboard, particleboard, oriented strand board (OSB) and other composite panel products reinforced with wood chips, wood fibers, or other cellulosic fibers. These composite products may be made in sheets ranging in thickness from about 2 mm to about 30 mm.
In still other embodiments, noncellulosic fibers may be used instead of refined cellulosic fiber material. Fiber-reinforced composite materials that do not include cellulosic fibers include fiberglass composites made from sheet molding compound (SMC) or bulk molding compound (BMC) including a polyester resin, or by a process known as long-fiber injection (LFI) using a polyurethane resin. LFI composites are useful for making building materials, including door skins, as described in U.S. patent application Ser. No. 11/112,540, filed Apr. 21, 2005, and published as US 2006-0266222 A1, which is incorporated herein by reference.
As shown at process station 108, the fibers (whether cellulosic, noncellulosic, or both) are mixed with an appropriate binder resin, and optionally one or more of a catalyst, a wax, an internal release agent, a tackifier, a filler and/or other additives, until a uniform composite mixture is formed. Alternatively, the resin may be added to the cellulosic fiber prior to addition of noncellulosic fibers. The composite mixture may then be formed by former 110 into a loose mat which is modified to the desired thickness by using a shave-off roller 112 and pre-compressed by a roller 116 or some other pressing mechanism to a density of about 3 to about 12 pounds per cubic foot. While the mat moves along a conveyor 118, a trimmer 120, such as a flying saw, trims the pre-compressed mat into segments sized to fit within the press, after which a release agent may optionally be applied to the top surface of the mat segments. The pre-compressed mat segments are then loaded into a platen press, and compressed between two dies under conditions of increased temperature and pressure. For example, pressing conditions may comprise pressing the mat for about 15 seconds between dies heated to about 300° F. (about 149° C.), which apply pressure to the mat in the range of about 600-850 psi (about 42.2-59.8 kg/cm2), followed by about 30 seconds of a lower applied pressure of about 100-300 psi (about 7.0-21.1 kg/cm2). In some embodiments, the dies are heated to a higher temperature of approximately 400° F. or more, to accelerate the curing process. In some embodiments, the mat is pressed between the heated dies at greater than 100 psi for at least 15 seconds, and in other embodiments at greater than 250 psi for at least 15 seconds, e.g., perhaps 30 seconds or more. Generally, a recessed (female) die is used to produce the inner surface of the door skin (facing the door frame or core), and a male die shaped as the mirror image of the female die is used to produce the outside surface of the skin. The dies may include surface contours to create a paneled appearance and simulated sticking in the door skin. In some embodiments, the male die may include a surface texture that forms a wood grain pattern in the surface of the door skin. After pressing, the door skin is removed from the press, cooled, and optionally sized, primed, and humidified. The resulting thin-layer composite door skin is mounted onto a door frame or core using an adhesive and employing methods well known in the art.
With reference to
With reference to
Exemplary fibers, resins, release agents, waxes, catalysts, additives and other ingredients of the composite mixture, as well as parameters for and variations on methods of manufacture and composite materials made thereby, are described in further detail in U.S. Pat. No. 7,399,438 of Clark et al., issued Jul. 15, 2008; in U.S. Patent Application Publication No. US 2006/0266222 A1, published Dec. 1, 2005; and in U.S. Provisional Patent Application No. 61/355,934, filed Jun. 17, 2010, all of which are incorporated herein by reference for the disclosure of such details.
As described above, in certain embodiments, one or both of the dies 12, 14 may be coated with an anti-bonding agent.
In accordance with an embodiment, the anti-bonding agent may include a hard anti-bonding coating that is abrasion resistant and that will not degrade at temperatures achieved at the die surface or after many thousands of cycles between the peak temperature and lower operating temperatures. The peak temperatures achieved at the die surfaces may approach or exceed the 280-425° F. nominal operating temperature of the heated dies due to applied pressure and other factors. An exemplary anti-bonding coating may have a dry film thickness (DFT) of approximately 40 microns (μm) and an abrasion resistance of greater than 50,000 cycles, as measured using a standard reciprocal abrasion test for cookware—BSI Standard No. BS 7069:1988, with a 4.5 kg force and 3M 7447 Scotch-Brite abrasive pad. In one embodiment, the anti-bonding coating may have a pencil hardness exceeding 6H. Other embodiments of the anti-bonding coating may have a pencil hardness exceeding 7H or 8H. In some embodiments, the anti-bonding coating may have a pencil hardness exceeding 9H. In still another embodiment, the anti-bonding coating may have a hardness exceeding 5 on the Mohs scale. In yet another embodiment, the anti-bonding coating may have a hardness exceeding 6 or 7 on the Mohs scale. The anti-bonding coating may have a scratch resistance and/or adhesion sufficient to withstand critical scratch loads in excess of 6, 8, 10, 12, 14, 16, 18, or 20 grams using a 90° diamond indenter stylus pressed with progressively increasing loads against the coated substrate which is moved via a movable stage at a constant rate, wherein the critical load to failure is the load at which the coating is breached and the indenter reaches the substrate surface. In addition to excellent abrasion resistance and/or hardness, embodiments of the anti-bonding coating may comprise a vitreous material having chemically bonded alkyl groups and/or aryl groups with hydrophobic properties that withstand more than 4000 pressing cycles, and preferably more than 10,000 pressing cycles, at the 280-425° F. nominal operating temperature. Some embodiments of the anti-bonding coatings may retain their hydrophobic and/or anti-bonding properties after more than 20,000, 30,000, 40,000 or 50,000 press cycles of a process for making fiber-reinforced composites using pMDI resin. In other words, in some embodiments the press may be cycled more than 20,000 times to make more than 20,000 sheets of composite materials, such as >20,000 door skin master panels, without substantially degrading an anti-bonding property of the anti-bonding coating as determined by measurement of contact angles (ASTM D7334-08) to determine surface energy, which should not increase more than 10%. The use of a vitreous material such as modified silica may provide for enhanced adhesion of the anti-bonding coating to the die surface and strong chemical bonding of alkyl and/or aryl groups with the network. The die may preferably be made of a steel containing at least some silica to promote adhesion.
In accordance with an embodiment, the anti-bonding agent is a hard PTFE-free non-stick coating. Some such coatings are applied via a sol-gel technique to form a ceramic or ceramic-like matrix, or a cross-linked network having excellent hardness and abrasion resistance. In some embodiments, the anti-bonding coating is organically modified silica (ormosil). In other embodiments, the anti-bonding coating comprises a silica network modified with organic and inorganic components (an organic-inorganic hybrid). Anti-bonding coatings applied by the sol-gel technique include coatings offered by Whitford Worldwide Co. of Elverson, Pa., USA under the trade name FUSION; by Thermolon Ltd. of Hong Kong under the trade names ROCKS, ENDURANCE, FLEXITY, and RESILIENCE; by Ceratech Co., Ltd. of Busan, Korea under the trade names CT-100, CT-200, CT-600, CT-700, and CT-800; and by ILAG Industrielack AG of Lachen, Switzerland under the trade names CERALON and ILASOL. The Thermolon, Ceratech and ILAG coatings are advertised to comprise a ceramic matrix including primarily silicon and oxygen (i.e., silica (SiO2)), modified with relatively small amounts of other inorganic materials and pigment.
Other anti-bonding coatings include ceramic coatings applied from a liquid solution including a volatile solvent, such as CERAKOTE Press Release coatings offered by NIC Industries, Inc. of White City, Oreg., and dry powdered coating materials applied by a plasma spray process to form a hard ceramic coating.
Some embodiments of the anti-bonding coating may comprise a ceramic matrix or network including primarily silicon and oxygen (i.e., silica (SiO2)), modified with a metal oxide, metal hydride, alkaline earth metals, and/or lanthanoid. In one embodiment, the silica network is modified with alkyl groups and an inorganic pigment, and relatively small amounts (0.1% to 5.0%) of alumina (Al2O3) and/or titania (TiO2) particles or nanoparticles dispersed within the silica network. In another embodiment, the silica network is further modified with particles or nanoparticles of copper chromite black spinel and/or manganese dioxide (MnO2) dispersed within the silica network. The modified silica may be characterized as a polysiloxane or a polysilsesquioxane. In some embodiments, the silica network is modified with an organic non-polar molecule, such as alkyl groups or aryl groups, so as to have a very low surface energy. In one embodiment, the organic modifier includes methyl groups. In another embodiment, the organic modifier forms polydimethylsiloxane (PDMS). In some embodiments, the anti-bonding agent is substantially free of fluorine.
Some embodiments of an organic-inorganic hybrid silica used in the anti-bonding coating may include functional additives. Functional additives may include pulverized, powdered, or nano-particulate natural stone materials or minerals, such as quartz, monzonite, gneiss, rhyolitic tuff, tourmaline, obsidian, or lava, and ion-exchange materials such as strontium, vanadium, zirconium, cerium, neodymium, lanthanum, barium, rubidium, cesium or gallium.
The presence of a low-friction and low-adhesion anti-bonding coating according to the present disclosure may enable the composite material of the mat to flow to some extent along the high draw angle contours of the die during pressing, to achieve improved distribution and density of composite material in the high draw angle regions 302 (
To prepare dies 202 and 204 for coating, the working surfaces 206, 208 of the dies are first degreased with a caustic agent and hot water. One suitable caustic agent is Morado Super Cleaner sold by ZEP, Inc. of Atlanta, Ga. Next, the working surfaces 202, 204 are roughened by sandblasting or, preferably, blasting with an abrasive blast medium having a particle size finer than sand, such as fused alumina having a particle size in the range of approximately 60 microns to 125 microns, or about 80 grit. To promote adhesion of the anti-bonding coating, the working surfaces 202 and 204 are roughened to a roughness on the Ra scale of approximately 2.0 to 6.0 microns and preferably about 3.0±0.5 microns. When roughening, care is taken to impart similar roughness to all contoured surfaces of the die, including the sticking. To properly roughen the sticking and other profiled surfaces, the grit is blasted perpendicularly to the surfaces, starting with the sticking and any other angled surfaces. After roughening, the dies are cleaned to remove grit. For example, the dies may be blown off with compressed air that has been filtered and passed through an oil separator to remove dirt and oil from the compressed air.
Sol-gel type anti-bonding coatings, such as Whitford FUSION, are generally transported and stored as a two-part coating systems that must be mixed, matured, and applied soon after the two liquid solutions are mixed and matured. The coating may be an admixture including a first component of a silane or oligomer thereof and a second component of colloidal silica including a substantial amount of silica nanoparticles. Some embodiments may involve an admixture of more than two components. In one embodiment, the first component includes methyltrimethoxysilane (MTMS), tetraethoxysilane (TEOS), or a mixture thereof. In one embodiment the first component comprises an approximately 2:1 weight ratio mixture of methyltrimethoxysilane to tetraethoxysilane. The second component may include at least 10% wt silica particles sized between 0.1 and 1.0 microns in an aqueous suspension. In one embodiment, the second component includes 20-50% wt silica nanoparticles and less than about 10% wt of functional fillers or additives, such as nanoparticles of metal oxides or hydrides and natural minerals or stone materials, such as one or more of those listed above. The size and type and amount of additives may be selected to yield a roughened surface finish, a matte finish having the texture of an egg shell, or a smooth finish, and may impart functional properties such as improved hydrophobicity, improved adhesion to the steel die substrate, improved hardness, toughness, abrasion resistance, and scratch resistance. Surface additives such as silicone surface additives or polyacrylate surface additives may be added to the second component to help with leveling and/or adhesion of the coating, and to inhibit the formation of craters in the coating. The silica sol may be activated by a dilute acid or alcohol, such as isopropyl alcohol between 1-5% wt in the second component.
In one embodiment, the first component may comprise a mixture of methyltrimethoxysilane (CH3Si(OCH3)3), 0.0% to 5% inorganic pigments, and 5-15% alcohol (including any of isopropyl alcohol, ethyl alcohol or methyl alcohol, or a mixture thereof), and the second component may comprise 30-50% wt. colloidal silica mixed with 2-20% alcohol (including any of isopropyl alcohol, ethyl alcohol or methyl alcohol, or a mixture thereof), 0.1 to 5% titania nanoparticles, optionally 0.1 to 5% alumina nanoparticles, copper chromite black spinel, and/or other additives, and the balance water.
The maturing and curing process may involve a hydrolysis reaction (1):
which is followed by a condensation reaction, as follows (2):
In an exemplary embodiment, before mixing the two components of the coating together, each is stirred or agitated well to ensure that solids and components are evenly distributed. In one example the components are each agitated using a drum roller (also known as a drum rotater) for approximately one hour. After agitation, the two liquid components are then mixed using a batch stirrer or mixer. Once mixed, the mixture is matured by agitating the mixture with a drum roller or paint shaker while exposing the drum to air temperature of approximately 100° F. to 108° F. (38-42° C.) for approximately three hours. In one embodiment, the mixture is matured by agitating with a drum roller or paint shaker while heating the mixture to about 104° F. (40° C.) for two hours, followed by an additional hour of agitation by the drum roller. The matured mixture may then be filtered through a screen having a mesh size of 300-400 micron to remove any large particles.
The die is pre-heated to approximately 86° F. to approximately 93° F. (30-34° C.), before applying the mixed and matured coating to the die surface. Several coats of the matured mixture are applied to the pre-heated die surface using a conventional spray gun, electrostatic spray, another technique used for painting, or another coating technique, to achieve a cured dry film thickness of approximately 25-80 microns (approximately 0.0010 to 0.0032 inches). In one embodiment, three coats of the matured mixture are applied to the die surface using a conventional spray gun to achieve a dry film thickness of approximately 35 to 60 microns (approximately 0.0014 to 0.0024 inches). The liquid mixture is preferably applied in an ambient environment of approximately 84° F. (29° C.) and a relative humidity of less than approximately 70%. The coated die is then baked to cure the coating and remove excess liquid.
To cure the coating, the die may be heated to a temperature in the range of approximately 375 to 660° F. (190-350° C.) as measured by a thermocouple placed along the side surface of the die. In one embodiment, the coating is cured by heating the die to a temperature of approximately 590 to 600° F. (310-315 C) as quickly as possible. In other embodiments, the die may be heated to a temperature in the range of approximately 385 to 660° F. or in the range of 450 to 650° F. or in the range of 550 to 620° F. The die may be heated in an air atmosphere or in an inert gas environment, in an oven or by conductive heating using a resistive electrical heater (hot plate) in contact with the outside surface of the die opposite the working surface. Alternatively, the die may be heated by an induction heating device. In some embodiments, an infrared-heating device positioned above the coated surface may be used in addition to or instead of a conductive heater, induction heater, or convection oven to reduce the curing time. Preferably the die is heated to the curing temperature as quickly as possible. However, the mass of the metal in the die will limit the rate of heating which is possible. With a resistive heater, it may take 60-120 minutes to heat the die to the necessary curing temperature. After heating it to the curing temperature, the coated die is cooled to room temperature (approximately 70° F. (21° C.)) in an air atmosphere or in an inert gas environment. In some embodiments, the die may be cooled by circulating liquid coolant through coolant pathways within the die. In other embodiments, the die may be cooled by blowing ambient air or inert gas over the surface of the die. In other embodiments, the die may be cooled by placing it on a cooling platen that has recirculating liquid coolant inside pathways within the platen. In other embodiments, the coating may cure at room temperature—a process which may take several days to complete.
After curing, the anti-bonding agent may exhibit a hardness of approximately 90 to 98 Shore D and an abrasion resistance of greater than 50,000 cycles, and in some embodiments greater than 100,000 cycles, as measured using BSI Standard No. BS 7069:1988, with a 4.5 kg force and 3M 7447 Scotch-Brite abrasive pad. In some embodiments, the anti-bonding coating may exhibit a hardness of greater than 80 Shore D, an abrasion resistance of greater than 50,000 cycles, and a scratch resistance of greater than 15 grams critical scratch loading (using a 90° diamond indenter, as described above). The anti-bonding coating is preferably hydrophobic, and in one embodiment, may exhibit an advancing water contact angle of approximately 100 to 105 degrees (ASTM D7334-08). In other embodiments, the coating may exhibit an advancing water contact angle of greater than 90 degrees, for example, 90 to 120 degrees, 100 to 150 degrees, or greater than 150 degrees (ASTM D7334-08). The coating may have a surface energy of less than approximately 30 mJ/m2 total, including dispersive and polar components (Owens/Wendt theory), wherein the polar component is less than approximately 6 mJ/m2. In other embodiments, the coating may have a total surface energy of less than approximately 25 mJ/m2 or less than approximately 22 mJ/m2, including a polar component of less than approximately 6 mJ/m2 or less than approximately 2 mJ/m2. Surface energy is calculated from contact angle measurements (sessile drop technique) for five liquids of known energy: Diidomethane, water (H2O), dimethyl sulfoxide (DMSO), formamide, and ethylene glycol.
Anti-bonding coatings having an increased hardness and/or scratch resistance may retain their anti-masking properties significantly longer than prior art coatings. For example, dies coated in accordance with the coatings described herein may withstand 20,000 or more pressing cycles without exhibiting masking or coating failure.
The anti-bonding properties of the ormosil coatings described herein may over time degrade due to exposure to heat, abrasion, chemicals, or other environmental conditions, likely due to loss of alkyl or aryl groups from the ormosil network. Some embodiments of the ormosil coatings may be rejuvenated utilizing a rejuvenating treatment, such as a wipe-on surface treatment that can be applied on top of the ormosil coating while the die is still in the press, or after the die is removed from the press. Rejuvenating treatments may include treatment solutions including a silane or silanol such as trimethylsilanol, or a fluoroalkylsilane (FAS) system such as SIVO Clear™ K1/K2, a two-part ambient curing FAS system sold by Evonik Industries AG of Essen, Germany.
Anti-bonding coatings according to the present disclosure may also be applied to equipment other than dies that is used in the manufacture of fiber-reinforced composites. For example, the anti-bonding coating may be applied, using one of the above-described formulations, coating methods, and curing methods, to the working surfaces of machinery for mixing or conveying, such as blenders, blender casings, blowline piping, refiner discs, formers, hoppers, shavers, shave-off rollers, conveyor belts, pre-compress rollers, saws, and any other working surfaces exposed to resin or the composite mixture of fibers and resin, and especially metallic working surfaces. The anti-bonding coatings described herein may also be useful for preventing build-up of latex paint, or other paints, varnishes, or surface treatments, on the walls and other surfaces of painting booths and on the automated painting equipment used in such booths. For large objects and immovable surfaces such as painting booth walls, an ambient curing coating such as NIC Industries' MICROSLICK coating is desirable.
Visual observations of composite products made using anti-bonding coatings according to some of foregoing embodiments indicate that the use of anti-bonding coatings on the dies may yield composite materials with improved surface finish, increased gloss, decreased surface roughness, increased water resistance (as measured by increased water contact angles), reduced incidence of loose fibers at the composite surface, and improved edge sharpness and detail. For example, it is expected that a hard ceramic non-PTFE anti-bonding agent, such as Whitford FUSION, when applied to an edge feature on the die defined by an inside radius of 0.030 inch, may yield a pressed fiber composite panel having a corresponding outside edge feature having an outside radius of less than approximately 0.035 inch. Anti-bonding coatings according to the present disclosure may allow minimum die radiuses to be decreased, to yield composite parts having edges sharper than 0.030 inch radius, and in some cases sharper than 0.025 inch or sharper than 0.020 inch.
The following Examples demonstrate exemplary procedures that may be used to form a fiber composite door skin product using the anti-bonding coatings and methods described herein. While certain Examples are hypothetical in nature, they are based upon actual experimental designs that have been tested and/or contemplated.
Die: Kleen-Kut 45
Coating: ILAG ILASOL, DFT=35-40 microns
Composite mixture:
Die temperature=300° F. (149° C.)
Applied pressure=10 seconds at 800 psi, followed by 20 sec. at 250 psi
Expected functional life of coating: greater than 20,000 cycles
Die: Industeel SP300
Coating: Thermolon ROCKS, DFT=40±5 microns
Composite mixture:
Die temperature=300° F. (149° C.)
Applied pressure=10 seconds at 800 psi, followed by 20 sec. at 250 psi
Expected functional life of coating: greater than 30,000 cycles
Die: Kleen-Kut 45
Coating: Whitford FUSION, DFT=25 microns
Composite mixture:
Die temperature=300° F. (149° C.)
Applied pressure=10 seconds at 800 psi, followed by 20 sec. at 250 psi
Expected functional life of coating: greater than 10,000 cycles
Die: Industeel SP300
Coating: NIC CERAKOTE Press Release, DFT=25-30 microns
Composite mixture:
Die temperature=300° F. (149° C.)
Applied pressure=10 seconds at 800 psi, followed by 20 sec. at 250 psi
Expected functional life of coating: greater than 10,000 cycles
Throughout this specification, reference to “one embodiment,” “an embodiment,” or “some embodiments” means that a particular described feature, structure, or characteristic is included in at least one embodiment. Thus appearances of the phrases “in one embodiment,” “in an embodiment,” or “in some embodiments” in various places throughout this specification are not necessarily all referring to the same embodiment.
Furthermore, the described features, structures, characteristics, and methods may be combined in any suitable manner in one or more embodiments. Those skilled in the art will recognize that the various embodiments can be practiced without one or more of the specific details or with other methods, components, materials, etc. In other instances, well-known structures, materials, or operations are not shown or not described in detail to avoid obscuring aspects of the embodiments.
Thus, it will be obvious to those having skill in the art that many changes may be made to the details of the above-described embodiments without departing from the underlying principles of the invention. The scope of the present invention should, therefore, be determined only by the following claims.
This application is a divisional of and claims the benefit under 35 U.S.C. § 120 from U.S. patent application Ser. No. 13/233,394, filed Sep. 15, 2011, which claims the benefit under 35 U.S.C. § 119(e) of U.S. Provisional Application No. 61/383,297, filed Sep. 15, 2010, the disclosures of which are incorporated herein by reference.
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20150184395 A1 | Jul 2015 | US |
Number | Date | Country | |
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61383297 | Sep 2010 | US |
Number | Date | Country | |
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Parent | 13233394 | Sep 2011 | US |
Child | 14658495 | US |