Patent Application
20230089669
There are numerous types of abrasive articles. For example, an abrasive article generally comprises abrasive particles bonded together as a bonded abrasive article, bonded to a backing as a coated abrasive article, or bonded into and/or onto a three-dimensional nonwoven substrate as a nonwoven abrasive article. Each type of abrasive article may also be provided in a variety of forms. For example, a coated abrasive article can comprise a first layer (also known as a make coat), a plurality of abrasive particles adhered thereto and therein, and a second layer (also known as a size coat). In some instances, a third layer (also known as a supersize coat) may be applied over the size coat. Alternatively, a coated abrasive article may be a lapping coated abrasive comprising an abrasive coating (which also can be referred to as an “abrasive layer”) bonded to a backing where the abrasive coating comprises a plurality of abrasive particles dispersed in a binder. In addition, a coated abrasive article may be a structured abrasive comprising a plurality of precisely shaped abrasive composites bonded to a backing. In this instance, the abrasive composites comprise a plurality of abrasive particles. Abrasives articles are used to abrade a wide variety of substrates or workpieces made from, for example, wood, plastic, fiberglass, or soft metal alloys, or having a layer of enamel or paint. Typically, there is some degree of space between these abrasive particles. During the abrading process, material abraded from the substrate or workpiece, also known as swarf, tends to fill the spaces between abrasive particles. The filling of spaces between abrasive particles with swarf and the subsequent build-up of swarf is known as loading. Loading presents a concern because the life of the abrasive article is reduced and the cut rate of the abrasive article decreases (thus, more force may be required to abrade). In addition, loading is an exponential problem; once swarf begins to fill in the spaces between abrasive particles, the initial swarf acts as a “seed” or “nucleus” for additional loading.
The abrasive industry has sought loading-resistant or anti-loading materials to use in abrasive articles. Preferred materials have been zinc stearate and calcium stearate. One theory for the success of metal stearates as an anti-loading agent is that the metal stearate coating powders off the coated abrasive surface during the abrading process, which in turn causes the swarf to also powder off of the surface, thus reducing the amount of loading.
Stearate coatings for the prevention of loading have been utilized by the abrasives industry for several decades. It has been common to utilize a binder with the stearate to assist in applying and retaining the coating on the abrasive surface. Some improvements over the years have been made by utilizing stearates with higher melting points, for example, calcium or lithium stearate and by incorporating additives to enhance anti-loading performance, for example, fluorochemicals.
Although there have been a number of improvements recently for backings, bond systems, and minerals of coated abrasives, comparable improvements in anti-loading components have not yet been achieved or combined with the desired manufacturing and performance requirements for sandpaper. While stearate based anti-loading solutions are initially viable, they tend to slough off during use and are costlier to manufacture in terms of both time and materials. That is, the industry is still seeking a component which is easy to apply, is relatively inexpensive, and can be utilized during abrading of a variety of workpieces including paint, wood, wood sealers, plastic, fiberglass, composite material, and automotive body fillers and putties.
In the present disclosure, an anti-loading composition for an abrasive article has been developed which meets the needs of the industry, i.e., the present disclosure relates to an abrasive article construction containing an anti-loading composition which significantly reduces loading, is coatable, is durable, and is relatively inexpensive to manufacture. In particular, the use of the anti-loading compositions of the present disclosure as a size coat at least reduces if not eliminates the need for a supersize coat, while offering comparable if not superior performance and durability. Further, the abrasive articles can be made sufficiently flexible such that they are well-suited for sanding intricate details in wooden architectural element such as moldings, raised panels, carvings, flutings, etc., and can be comfortably be rolled or folded for control and ability to get into tight spots.
In one aspect, the present disclosure provides an abrasive article including a backing with a first major surface and an opposing second major surface, an abrasive layer bonded to at least a portion of the first major surface, with the abrasive layer comprising abrasive particles retained in a make coat. The article further includes an anti-loading size layer at least partially disposed on the abrasive layer, wherein the anti-loading size layer comprises a urea aldehyde size coat binder at a concentration of at least 20 percent by weight of the composition, a blocked acid catalyst, and wax at a concentration of no greater than about 20 percent by weight of the composition.
In another aspect, the present disclosure provides an abrasive article including a backing with a first major surface and an opposing second major surface, and an abrasive layer bonded to at least a portion of the first major surface, the abrasive layer comprising abrasive particles retained in a make coat. The article further includes an anti-loading size layer at least partially disposed on the abrasive layer, wherein the size layer comprises a urea aldehyde size coat binder, a blocked acid catalyst, wax, and a latex.
The present disclosure also relates to a method of making an abrasive article comprising (a) providing a backing having at least one major surface; (b) applying a make precursor over the at least one major surface of the backing; (c) embedding a plurality of abrasive particles into and/or onto the make precursor; (d) at least partially curing the make precursor to form a make coat; (e) applying anti-loading composition over the make coat and the plurality of abrasive particles, said precursor comprising a urea aldehyde binder resin, blocked acid catalyst, and wax; and (f) curing the anti-loading composition to form a size coat.
As used herein, the term “m.p.” refers to melting point or melting range as indicated.
The words “preferred” and “preferably” refer to embodiments of the disclosure that may afford certain benefits, under certain circumstances. However, other embodiments may also be preferred, under the same or other circumstances. Furthermore, the recitation of one or more preferred embodiments does not imply that other embodiments are not useful, and is not intended to exclude other embodiments from the scope of the disclosure.
As recited herein, all numbers should be considered modified by the term “about”.
As used herein, “a”, “an”, “the”, “at least one”, and “one or more” are used interchangeably. Thus, for example, a core comprising “a” pattern of recesses can be interpreted as a core comprising “one or more” patterns.
As used herein as a modifier to a property or attribute, the term “generally”, unless otherwise specifically defined, means that the property or attribute would be readily recognizable by a person of ordinary skill but without requiring absolute precision or a perfect match (e.g., within +/−20% for quantifiable properties). The term “substantially”, unless otherwise specifically defined, means to a high degree of approximation (e.g., within +/−10% for quantifiable properties) but again without requiring absolute precision or a perfect match. Terms such as same, equal, uniform, constant, strictly, and the like, are understood to be within the usual tolerances or measuring error applicable to the particular circumstance rather than requiring absolute precision or a perfect match.
The above summary of the present disclosure is not intended to describe each disclosed embodiment or every implementation of the present invention. The description that follows more particularly exemplifies illustrative embodiments. In several places throughout the application, guidance is provided through lists of examples, which examples can be used in various combinations. In each instance, the recited list serves only as a representative group and should not be interpreted as an exhaustive list.
The present disclosure will be further described with reference to the accompanying drawings, in which:
Layers in certain depicted embodiments are for illustrative purposes only and are not intended to absolutely define the thickness, relative or otherwise, or the location of any component. While the above-identified figures set forth several embodiments of the disclosure, other embodiments are also contemplated, as noted in the discussion. In all cases, this disclosure presents the disclosure by way of representation and not limitation. It should be understood that numerous other modifications and embodiments can be devised by those skilled in the art, which fall within the scope and spirit of the principles of the invention.
An improved abrasive article can be evaluated based on certain performance properties. First, such an article typically a desirable balance between cut and finish—that is, an acceptable efficiency in removing material from the workpiece, along with an acceptable smoothness of the finished surface. Second, an abrasive article would typically avoid excessive “loading”, or clogging, which occurs when debris or swarf become trapped between the abrasive particles and hinder the cutting ability of the coated abrasive. Third, the abrasive article would desirably be durable to provide for longevity in use. Fourth, the abrasive article would be relatively simple and cost-effective to manufacture.
The inventors of the present disclosure discovered an anti-loading composition that can advantageously balance among or improve performance in each of the above properties. The present inventors discovered that by modifying a size coat precursor with at least wax and a blocked acid catalyst, the resulting abrasive article does not require a supersize coat to exhibit superior anti-loading properties and maintain cut durability. Moreover, by incorporating the anti-loading materials into the size resin itself, the present inventors are able to provide abrasive articles that avoid the gradual loss of anti-loading protection and durability endemic to peripheral coatings (e.g., stearate-based supersize coats). Moreover, the compositions offer an extended manufacturing time (i.e., pot life) before they coalesce or precipitate.
Referring now to the drawings,
As used herein, the expression “coating” refers generally to at least a single layer of generally flowable material, such as a liquid or a solid powder that can be applied directly to a surface. A coating, therefore, does not include a separate sheet of material laminated to a surface. As used herein, the expression “layer” refers generally to a material forming a discrete stratum, which may be continuous or discontinuous relative to a surface.
In one end use application of the disclosure, the abrasive article 10 may be used for hand sanding a work surface, such as a wooden surface or work piece. That is, the abrasive article 10 may be used to remove material from a surface by contacting the abrasive article 10 directly with one's hand (i.e., without the aid of a tool, such as a sanding block) and subsequently moving the abrasive article 10 against the work surface. It will be recognized that the present disclosure may also be used with manually-operated sanding tools and sanding blocks, or with power tools.
The backing layer 11, the make layer 12, and the abrasive particles 13, and the anti-loading size layer 16 are each described in detail below.
The backing 11 may be constructed from various materials known in the art for making abrasive articles, including coated abrasive backings and porous backings (e.g., nonwovens). Suitable materials for the backing 11 also include any of the materials commonly used to make sandpaper including, for example, paper, cloths (cotton, polyester, rayon) polymeric films such as thermoplastic films, foams, and laminates thereof. The backing 11 will typically have sufficient strength for handling during processing, sufficient strength to be used for the intended end use application. The thickness of the backing generally ranges from about 0.02 to about 5 millimeters, more preferably from about 0.05 to about 2.5 millimeters, and most preferably from about 0.1 to about 0.4 millimeters, although thicknesses outside of these ranges may also be useful. The backing 11 may be unitary; that is, it may consist of a single layer. In other certain embodiments it may be a composite backing of multiple layers, if desired.
The backing 11 may be made of any number of various materials including those conventionally used as backings in the manufacture of abrasive articles. Exemplary backings include polymeric film (including primed films) such as polyolefin film (e.g., polypropylene including biaxially oriented polypropylene, polyester film, polyamide film, cellulose ester film), metal foil, mesh, foam (e.g., natural sponge material or polyurethane foam (see U.S. Pat. No. 6,406,504 to Lise et al.)), cloth (e.g., cloth made from fibers or yarns comprising polyester, nylon, silk, cotton, and/or rayon), scrim, paper, coated paper, vulcanized paper, vulcanized fiber, nonwoven materials, combinations thereof, and treated versions thereof. The backing may also be a laminate of two materials (e.g., paper/film, cloth/paper, film/cloth). Cloth backings may be woven or stitch bonded. In some embodiments, the backing is a thin and conformable polymeric film capable of expanding and contracting in transverse (i.e., in-plane) directions during use. The stretching of the backing material can be elastic (with complete spring back), inelastic (with zero spring back), or some mixture of both. This property can help promote contact between the abrasive particles 14 and the underlying substrate, and can be useful when the substrate includes raised and/or recessed areas. Numerous suitable backing materials for abrasive articles of the present disclosure are detailed and exemplified in U.S. Pat. No. 5,954,844 (Law et al.).
Highly conformable polymers that may be used in the backing 11 include certain polyolefin copolymers, polyurethanes, and polyvinyl chloride. One particularly preferred polyolefin copolymer is an ethylene-acrylic acid resin (available under the trade designation “PRIMACOR 3440” from Dow Chemical Company, Midland, Mich.). Optionally, ethylene-acrylic acid resin is one layer of a bilayer film in which the other layer is a polyethylene terephthalate (PET) carrier film. In this embodiment, the PET film is not part of the backing 11 itself and is stripped off prior to using the abrasive article 10.
The choice of backing material may depend on the intended application of the abrasive article. The thickness and smoothness of the backing is typically chosen to be suitable to provide the desired thickness and smoothness of the coated abrasive article, wherein such characteristics of the coated abrasive article may vary depending, for example, on the intended application or use of a coated abrasive article. The backing 11 may be flexible, such as described in US Publication No. 2017/0043450 (Graham et al.) or resilient, such as described in U.S. Pat. No. 6,406,504.
The backing 11 may be cast (e.g., from solvent or water) or extruded. It may contain one or more additives such as fillers, melt processing aids, antioxidants, flame retardants, colorants, or ultraviolet light stabilizers.
The backing 11 may, optionally, have at least one of a saturant, a presize layer and/or a backsize layer. The purpose of these materials is typically to seal the backing and/or to protect yarn or fibers in the backing. If the backing is a cloth material, at least one of these materials is typically used. The addition of the presize layer or backsize layer may additionally result in a ‘smoother’ surface on either the front and/or the back side of the backing.
In some embodiments, the backing layer 11 is formed of paper. In some embodiments, paper is a desirable material for the backing layer 11 because it is readily available and is typically low in cost. Paper backings are available in various weights, which are usually designated using letters ranging from “A” to “F”. The letter “A” is used to designate the lightest weight papers, and the letter “F” is used to designate the heaviest weight papers.
In presently preferred embodiments, the backing layer is formed of a unitary or composite film. Suitable film materials for the backing 11 include polymeric films, including primed films, such as polyolefin film (e.g., polypropylene including biaxially oriented polypropylene, polyamide film, cellulose ester film), polyester films, and thermoplastic polyurethane films. Useful polyester films may be manufactured from various types of thermoplastic polyester resins, including polyethylene terephthalate (PET), polytetramethylene terephthalate, polyethylene-2, 6-naphthalate, and poly-1,4-cyclohexylene dimethyl terephthalate. Polyester copolymers (e.g., polyethylene terephthalate/isophthalate, polyethylene terephthalate/adipate, polyethylene terephthalate/sebacate, polyethylene terephthalate/sulfoisophthalate, and polyethylene terephthalate/azelate) may also be useful. In some embodiments of the articles, processes, and methods of the present disclosure, the polyester film backing comprises polyethylene terephthalate (PET). In some embodiments, the polyester film backing has a uniform composition throughout its thickness. In other embodiments, PET or any of the polyesters described above may be included in a layer of a multilayer film backing. In these cases, the polyester layer would be in contact with the primer layer.
In polyester film backings useful for practicing some aspects the present disclosure, the film backing would be considered monolithic (that is, having a generally uniform film composition) and is not fibrous. Particularly, the film backing is not a nonwoven material. The polyester film backing can be described as a dense film and not an open, lofty, fibrous web.
Polyester film backings useful for practicing some aspects of the present disclosure can have a variety of thicknesses. In some embodiments, the thickness of the polyester film backing is in a range from 1 micrometer to 500 micrometers, 10 micrometers to 350 micrometers, 25 micrometers to 250 micrometers, or 35 micrometers to 200 micrometers.
In some embodiments, the polyester film backing is surface-treated before the primer layer is applied. Useful surface treatments include electrical discharge in the presence of a suitable reactive or non-reactive atmosphere (e g., plasma, glow discharge, corona discharge, dielectric barrier discharge or atmospheric pressure discharge); ultraviolet light exposure, electron beam exposure, flame discharge, and scuffing. The surface treatment can be applied as the polyester film backing is being made or in a separate process. In some embodiments, the polyester film backing is surface-treated using corona discharge. An example of a useful corona discharge process is described in U.S. Pat. No. 5,972,176 (Kirk et ah).
The polyester film backing useful for practicing the present disclosure may be oriented, either uniaxially or biaxially. Orientation of a film at a temperature above its glass transition temperature can be useful for enhancing at least one of the stiffness, modulus, or creep resistance of the film. Orientation can conveniently be carried out by conventional methods such as mechanical stretching (drawing) or tubular expansion with heated air or gas. Examples of useful draw ratios are in the range of 2.5 to 6 times in the machine, cross-machine direction, or both the machine and cross-machine directions. Larger draw ratios (for example, up to about 8 times) may also be useful if the film is oriented in only one direction. For biaxially oriented film backings, the film may be stretched equally in the machine and cross-machine directions or unequally in the machine and cross-machine directions.
In the illustrated embodiment, the backing layer 11 is continuous. That is, the backing layer 11 does not contain holes, openings, slits, voids, or channels extending there through in the Z-direction (i.e., the thickness or height dimension) that are larger than the randomly formed spaces between the material itself when it is made. The backing may also contain openings (i.e., be perforated), or contain slits. In some embodiments, the backing layer 11 is generally non-extensible. As used herein, the term “non-extensible” refers to a material having an elongation at break of no greater than about 25%. In some embodiments, the material has an elongation at break of no greater than about 10%. In some embodiments, the material has an elongation at break of no greater than about 5%.
In certain embodiments, such as when the backing 11 is formed of paper or polymeric film, the backing 11 may be relatively thin, and typically has a thickness of no greater than about 1.5 mm, no greater than about 1 mm, or no greater than about 0.75 mm. In such embodiments, the backing 11 is generally not resilient. The backing 11 may also be porous or non-porous. In another embodiment, such as when the backing 11 is a foam material, the backing 11 may be somewhat thicker. For example, in embodiments having a foam backing, the backing may have a thickness of at least about 2 mm, at least about 5 mm, or at least about 10 mm.
In embodiments featuring a flexible backing, the backing may have an average tensile strength in the range of from 500 to 3200 pounds per square inch (psi) (3.4 to 22.1 MPa), preferably 1000 to 2500 psi (6.9 to 17.2 MPa), more preferably 1600 to 2100 psi (11.0 to 14.5 MPa), and an average ultimate elongation (i.e., elongation at break) of 230 to 530 percent, preferably 300 to 460 percent, and more preferably 350 to 410 percent.
The backing 11 may also be formed of a cloth material. Cloth materials are desirable because they are generally tear resistant and are generally more durable than paper and film materials. In addition, cloth backings tolerate repeated bending and flexing during use. Cloth backings are generally formed of woven cotton or synthetic yarns that are treated to make them suitable for use as a coated abrasive backing. As is the case with paper backings, cloth backings are available in various weights, which are usually designated using a letter ranging from “J” to “M” with the letter “J” designating the lightest weight cloth, and the letter “M” designating the heaviest weight cloths.
The backing 11, particularly but not exclusively in embodiments featuring a polyethylene film, can include a primer layer. Suitable primer layer composition include a water based polyurethane, sulfonated co-polyester, aziridine crosslinker, and surfactant.
The backing 11 may also include a nonwoven fiber web, such that abrasive article 10 is a nonwoven abrasive article. Nonwoven fiber webs suitable for use in the aforementioned abrasive articles are well known in the abrasives art. The fibers may comprise continuous fiber, staple fiber, or a combination thereof. Mixtures of fibers with differing linear densities may be useful, for example, to provide an abrasive article that upon use will result in a specifically preferred surface finish. The fiber web may be made, for example, by conventional air laid, carded, stitch bonded, spun bonded, spun-laced, wet laid, and/or melt blown procedures.
The fiber web is typically reinforced, for example, using a prebond resin (e.g., a phenolic, urethane, or acrylic resin), by including core-sheath fibers, and/or by mechanical entanglement (e.g., hydroentanglement, or needletacking) using methods well-known in the art. The fiber web may optionally incorporate or be secured to a scrim and/or backing (e.g., using glue or a hot-melt adhesive or by needletacking), if desired, for additional reinforcement. Nonwoven fiber webs are typically selected to be suitably compatible with adhering binders and abrasive particles while also being processable in combination with other components of the article, and typically can withstand processing conditions (e.g., temperatures) such as those employed during application and curing of the curable composition. The fibers may be chosen to affect properties of the abrasive article such as, for example, flexibility, elasticity, durability or longevity, abrasiveness, and finishing properties. Examples of fibers that may be suitable include natural fibers, synthetic fibers, and mixtures of natural and/or synthetic fibers. Examples of synthetic fibers include those made from polyester (e.g., polyethylene terephthalate), nylon (e.g., hexamethylene adipamide, or polycaprolactam), polypropylene, acrylonitrile (i.e., acrylic), rayon, cellulose acetate, polyvinylidene chloride-vinyl chloride copolymers, and vinyl chloride-acrylonitrile copolymers. Examples of suitable natural fibers include cotton, wool, jute, and hemp. The fiber may be of virgin material or of recycled or waste material, for example, reclaimed from garment cuttings, carpet manufacturing, fiber manufacturing, or textile processing. The fiber may be homogenous or a composite such as a bicomponent fiber (e.g., a co-spun sheath-core fiber). The fibers may be tensilized and crimped. Combinations of fibers may also be used.
Prior to coating with a curable composition (i.e., make layer 12), the nonwoven fiber web typically has a weight per unit area (i.e., basis weight) of at least about 100 grams per square meter (gsm), at least about 200 gsm, or at least about 300 gsm; and/or less than about 500 gsm, less than about 450 gsm, or less than about 400 gsm, as measured prior to any coating (e.g., with the curable composition or optional pre-bond resin), although greater and lesser basis weights may also be used. In addition, prior to impregnation with the curable composition, the fiber web typically has a thickness of at least about 1 millimeters (mm), at least about 2 mm, or at least about 3 mm; and/or less than about 100 mm, less than about 50 mm, or less than about 25 mm, although greater and lesser thicknesses may also be useful.
Frequently, as known in the abrasive art, it is useful to apply a pre-bond resin to the nonwoven fiber web prior to coating with the make coat. The pre-bond resin serves, for example, to help maintain the nonwoven fiber web integrity during handling, and may also facilitate bonding of the make resin to the nonwoven fiber web. Examples of prebond resins include phenolic resins, urethane resins, hide glue, acrylic resins, urea-formaldehyde resins, melamine-formaldehyde resins, epoxy resins, and combinations thereof. The amount of pre-bond resin used in this manner is typically adjusted toward the minimum amount consistent with bonding the fibers together at their points of crossing contact. In those cases, wherein the nonwoven fiber web includes thermally bondable fibers, thermal bonding of the nonwoven fiber web may also be helpful to maintain web integrity during processing. Various other optional conventional treatments and additives may be used in conjunction with the nonwoven fiber web such as, for example, application of antistatic agents, lubricants, or corona treatment. Further details regarding nonwoven abrasive articles and methods for their manufacture can be found, for example, in U.S. Pat. No. 2,958,593 (Hoover et al.); U.S. Pat. No. 4,227,350 (Fitzer); U.S. Pat. No. 4,991,362 (Heyer et al.); U.S. Pat. No. 5,712,210 (Windisch et al.); U.S. Pat. No. 5,591,239 (Edblom et al.); U.S. Pat. No. 5,681,361 (Sanders); U.S. Pat. No. 5,858,140 (Berger et al.); U.S. Pat. No. 5,928,070 (Lux); U.S. Pat. No. 6,017,831 (Beardsley et al.); and U.S. Pat. No. 6,207,246 (Moren et al.).
In general, any adhesive make coat 12 may be used to adhere the abrasive particles 13 to the backing 11. “Make coat” and “make layer” are used interchangeably, and refer to the layer(s) of hardened (i.e., cured) resin over the backing 11 of the article 10. The make layer 12 can be prepared by curing a make precursor to adhere a plurality of abrasive particles to the backing. Suitable materials for the adhesive make layer 12 include, for example, phenolic resins (such as phenolic formaldehyde resins), aminoplast resins having pendant α, β-unsaturated carbonyl groups, urethane resins, epoxy resins, ethylenically unsaturated resins, acrylated isocyanurate resins, vinyl acetate resins (e.g., polyvinyl acetate), melamine resins, urea-aldehyde resins, isocyanurate resins, acrylated urethane resins, acrylated epoxy resins, bismaleimide resins, fluorene-modified epoxy resins, and combinations thereof.
Organic binders suitable for a make and or size layer are formed from an organic binder precursor; it is, however, within the scope of the present disclosure to use a water-soluble binder precursor or water-dispersible binder precursor, such as hide glue.
Phenolic resins are commonly used as an abrasive article make coat precursor because of their thermal properties, availability, cost and ease of handling. Two common types of phenolic resins are resole and novolac. Resole phenolic resins have a molar ratio of formaldehyde to phenol, of greater than or equal to one to one, typically between 1.5:1.0 to 3.0:1.0. Novolac resins have a molar ratio of formaldehyde to phenol, of less than one to one. The phenolic resin is preferably a resole phenolic resin, or at least a formaldehyde containing phenolic resin. Alkaline catalysts suitable for catalyzing the reaction between aldehyde and phenolic components of resole phenolic resins include sodium hydroxide, barium hydroxide, potassium hydroxide, calcium hydroxide, organic amines, and sodium carbonate, all as solutions of the catalyst dissolved in water.
Examples of commercially available phenolic resins include those known under the trade designations VARCUM and DUREZ from Occidental Chemical Corp., Tonawanda, N.Y.; AEROFENE and AEROTAP from Ashland Chemical Company, Columbus, Ohio; RESINOX from Monsanto, St. Louis, Mo.; and BAKELITE from Union Carbide, Danbury, Conn.
Resole phenolic resins are typically coated as a solution with water and/or organic solvent (e.g., alcohol). Typically, the solution includes about 70 percent to about 85 percent solids by weight, although other concentrations may be used. If the solids content is very low, then more energy is required to remove the water and/or solvent. If the solids content is very high, then the viscosity of the resulting phenolic resin is too high which typically leads to processing problems.
It is also within the scope of the present disclosure to modify the physical properties of a phenolic resin. For example, a plasticizer, latex resin, or reactive diluent may be added to a phenolic resin to modify flexibility and/or hardness of the cured phenolic binder.
A commonly preferred aminoplast resin is one having at least one pendant α, β-unsaturated carbonyl groups per molecule, which can be prepared according to the disclosure of U.S. Pat. No. 4,903,440 (Larson et al.) which is incorporated herein by reference.
Aminoplast resins have at least one pendant α, β-unsaturated carbonyl group per molecule or oligomer. These unsaturated carbonyl groups can be acrylate, methacrylate or acrylamide type groups. Examples of such materials include N-hydroxymethyl-acrylamide, N,N′-oxydimethylenebisacrylamide, ortho and para acrylamidomethylated phenol, acrylamidomethylated phenolic novolac and combinations thereof. These materials are further described in U.S. Pat. Nos. 4,903,440; 5,055,113; and 5,236,472 all incorporated herein by reference.
Polyurethanes may be prepared by reacting near stoichiometric amounts of polyisocyanates with polyfunctional polyols. The more common types of polyisocyanates are toluene diisocyanate (TDI) and 4,4′-diisocyanatodiphenylmethane (MDI) which are available under the trade designations “Isonate” from Upjohn Polymer Chemicals, Kalamazoo, Mich. and “Mondor” from Miles, Inc., Pittsburgh, Pa. Common polyols for flexible polyurethanes are polyethers such as polyethylene glycols, which are available under the trade designations CARBOWAX from Union Carbide, Danbury, Conn.; VORANOL from Dow Chemical Co., Midland, Mich.; and PLURACOL E from BASF Corp., Mount Olive, N.J.; polypropylene glycols, which are available under the trade designations PLURACOL P from BASF Corp. and VORANOL from Dow Chemical Co., Midland, Mich.; and polytetramethylene oxides, which are available under the trade designations POLYMEG from QO Chemical Inc., Lafayetts, Ind.; POLY THF from BASF Corp., Mount Olive, N.J.; and TETRATHANE from DuPont, Wilmington, Del. Hydroxyl functional polyesters are available under the trade designations MULTRANOL and DESMOPHENE from Miles, Inc., Pittsburgh, Pa. Virtually all polyurethane formulations incorporate one or more catalysts. Tertiary amines and certain organometallic compounds, especially those based on tin, are most common Combinations of catalysts may be used to balance the polymer-formation rate.
Epoxy resins have an oxirane ring and are polymerized by the ring opening. Such epoxide resins include monomeric epoxy resins and polymeric epoxy resins. These resins can vary greatly in the nature of their backbones and substituent groups. For example, the backbone may be of any type normally associated with epoxy resins and substituent groups thereon can be any group free of an active hydrogen atom that is reactive with an oxirane ring at room temperature. Representative examples of acceptable substituent groups include halogens, ester groups, ether groups, sulfonate groups, siloxane groups, nitro groups and phosphate groups. Examples of some preferred epoxy resins include 2,2-bis4-(2,3-epoxypropoxyphenol)propane (diglycidyl ether of bisphenol A) and commercially available materials under the trade designations, EPON 828″, “EPON 1004, and EPON 1001F, available from Shell Chemical Co., Houston, Tex.; “DER-331”, “DER-332”, and “DER-334” available from Dow Chemical Co., Midland, Mich. Other suitable epoxy resins include glycidyl ethers of phenol formaldehyde novolac (e.g., “DEN-431” and “DEN-438” available from Dow Chemical Co., Midland, Mich.). Other epoxy resins include those described in U.S. Pat. No. 4,751,138 (Tumey et al.), incorporated herein by reference.
Urea-aldehyde resins employed in precursor compositions of the present disclosure may be comprised of a reaction product of urea or any urea derivative and any aldehyde which are capable of being rendered coatable, have the capability of curing together at an accelerated rate in the presence of a catalyst, preferably a cocatalyst, and which afford an abrasive article with abrading performance acceptable for the intended use. Urea-formaldehyde resins are generally preferred in the abrasive industry, as noted above, because of their availability, low cost, and ease of handling Urea-aldehyde resins preferably are 30-95% solids, more preferably 60-80% solids, with a viscosity ranging from about 125 to about 1500 cps (Brookfield viscometer, number 3 spindle, 30 rpm 25° C.) before addition of water and catalyst and have molecular weight (number average) of at least about 200, preferably varying from about 200 to 700. Urea aldehyde resins useful for the present disclosure include those described in U.S. Pat. No. 5,486,219 (Ford et al.), incorporated herein by reference.
Urea resin binder precursor systems typically employ a cocatalyst system. The cocatalyst may consist essentially of a Lewis acid, typically aluminum chloride (AlCl3), and an organic or inorganic salt. A Lewis acid catalyst is defined simply as a compound which accepts an electron pair, and preferably has an aqueous solubility at 15° C. of at least about 50 grams/cc.
Lewis acids (or compounds which behave as Lewis acids) include aluminum chloride, iron (III) chloride, and copper (II) chloride. A Lewis acid which is commonly used is aluminum chloride in either its non-hydrated form (AlCl3) or hexahydrate from (AlCl3 6H2O).
Acrylate resins include both monomeric and polymeric compounds that contain atoms of carbon, hydrogen and oxygen, and optionally, nitrogen and the halogens. Oxygen or nitrogen atoms or both are generally present in ether, ester, urethane, amide, and urea groups. Ethylenically unsaturated compounds preferably have a molecular weight of less than about 4,000 and are preferably esters made from the reaction of compounds containing aliphatic monohydroxy groups or aliphatic polyhydroxy groups and unsaturated carboxylic acids, such as acrylic acid, methacrylic acid, itaconic acid, crotonic acid, isocrotonic acid, maleic acid, and the like. Representative examples of acrylate resins include methyl methacrylate, ethyl methacrylate, ethylene glycol diacrylate, ethylene glycol dimethacrylate, hexanediol diacrylate, triethylene glycol diacrylate, trimethylolpropane triacrylate, glycerol triacrylate, pentaerythritol triacrylate, pentaerythritol trimethacrylate, pentaerythritol tetraacrylate and pentaerythritol tetramethacrylate, as well as these unsaturated monomers, for example, styrene, divinylbenzene, vinyl toluene.
Acrylated isocyanurates are isocyanurate derivates having at least one pendant acrylate group, which are further described in U.S. Pat. No. 4,652,274 (Boettcher et al.), incorporated herein by reference. A preferred acrylated isocyanurate is the triacrylate of tris(hydroxyethyl) isocyanurate.
Acrylated urethanes are diacrylate esters of hydroxy terminated isocyanate extended polyesters or polyethers. Examples of commercially available acrylated urethanes include those available under the trade designations, UVITHANE 782, CMD 6600, CMD 8400, and CMD 8805, from Radcure Specialties, Inc., Atlanta, Ga.
Acrylated epoxies are monoacrylate and diacrylate esters of epoxy resins, such as the diacrylate esters of bisphenol A epoxy resin. Examples of commercially available acrylated epoxies include CMD 3500, CMD 3600, and CMD 3700, available from Radcure Specialties, Inc., Atlanta, Ga.
Bismaleimide resins are further described in the assignee's U.S. Pat. No. 5,314,513, which is incorporated herein by reference.
Catalysts and/or curing agents may be added to the make coat precursor to initiate and/or accelerate the polymerization process. The make coat precursor can include a radiation-cured resin. A radiation-curing resin is a resin that is at least partially hardened or is at least partially polymerizable by radiation energy. Depending on the resin material to be used, an energy source such as heat, infrared radiation, electron beam radiation, ultraviolet radiation, or a visible light radiation is suitable for initiating cure.
In addition to thermosetting resins, a hot melt resin may also be used. For example, a make coat precursor system may comprise a hot melt pressure sensitive adhesive which can be energy cured to provide a binder. In this instance, because the make precursor is a hot melt composition, it is particularly useful with porous cloth, textile or fabric backings. Since this make precursor does not penetrate the interstices of the porous backing, the natural flexibility and pliability of the backing is preserved. Exemplary hot melt resins are described in U.S. Pat. No. 5,436,063 (Follett et al.), incorporated herein by reference.
The hot melt binder precursor system may comprise an epoxy-containing material, a polyester component, and an effective amount of an initiator for energy curing the binder. More particularly, the binder precursor can comprise from about 2 to 95 parts of the epoxy-containing material and, correspondingly, from about 98 to 5 parts of the polyester component, as well as the initiator. An optional hydroxyl-containing material having a hydroxyl functionality greater than 1 may also be included.
The make coat 12 may be coated onto the backing 11 by any conventional technique, such as knife coating, spray coating, roll coating, rotogravure coating, curtain coating, and the like.
In general, any abrasive particles 13 may be used in the abrasive articles of this disclosure. Suitable abrasive particles include, for example, fused aluminum oxide, heat treated aluminum oxide, alumina-based ceramics, silicon carbide, zirconia, alumina-zirconia, garnet, emery, diamond, ceria, cubic boron nitride, ground glass, quartz, titanium diboride, sol gel abrasives and combinations thereof. The abrasive particles 13 can be either shaped (e.g., rod, triangle, or pyramid) or unshaped (i.e., irregular). The term “abrasive particle” encompasses abrasive grains, agglomerates, or multi-grain abrasive granules. The abrasive particles 13 can be deposited onto the make coat 12 by any conventional technique such as electrostatic coating or drop coating.
Abrasive particles suitable for use in abrasive layers utilized in practice of the present disclosure include any abrasive particles known in the abrasive art. Exemplary useful abrasive particles include fused aluminum oxide based materials such as aluminum oxide, ceramic aluminum oxide (which may include one or more metal oxide modifiers and/or seeding or nucleating agents), and heat-treated aluminum oxide, silicon carbide, co-fused alumina-zirconia, diamond, ceria, titanium diboride, cubic boron nitride, boron carbide, garnet, flint, emery, sol-gel derived abrasive particles, and blends thereof. Desirably, the abrasive particles comprise fused aluminum oxide, heat-treated aluminum oxide, ceramic aluminum oxide, silicon carbide, alumina zirconia, garnet, diamond, cubic boron nitride, sol-gel derived abrasive particles, or mixtures thereof. Examples of sol-gel abrasive particles include those described U.S. Pat. No. 4,314,827 (Leitheiser et al.); U.S. Pat. No. 4,518,397 (Leitheiser et al.); U.S. Pat. No. 4,623,364 (Cottringer et al.); U.S. Pat. No. 4,744,802 (Schwabel); U.S. Pat. No. 4,770,671 (Monroe et al.); U.S. Pat. No. 4,881,951 (Wood et al.); U.S. Pat. No. 5,011,508 (Wald et al.); U.S. Pat. No. 5,090,968 (Pellow); U.S. Pat. No. 5,139,978 (Wood); U.S. Pat. No. 5,201,916 (Berg et al.); U.S. Pat. No. 5,227,104 (Bauer); U.S. Pat. No. 5,366,523 (Rowenhorst et al.); U.S. Pat. No. 5,429,647 (Laramie); U.S. Pat. No. 5,498,269 (Larmie); and U.S. Pat. No. 5,551,963 (Larmie).
The abrasive particles may be in the form of, for example, individual particles, agglomerates, abrasive composite particles, alpha alumina abrasive shards, and mixtures thereof. Exemplary agglomerates are described, for example, in U.S. Pat. No. 4,652,275 (Bloecher et al.) and U.S. Pat. No. 4,799,939 (Bloecher et al.). It is also within the scope of the present disclosure to use diluent erodible agglomerate grains as described, for example, in U.S. Pat. No. 5,078,753 (Broberg et al.). Abrasive composite particles comprise abrasive grains in a binder. Exemplary abrasive composite particles are described, for example, in U.S. Pat. No. 5,549,962 (Holmes et al.). Alpha alumina abrasive shards are described in U.S. Pat. No. 9,446,502 (Erickson et al.). Examples of suitable shaped abrasive particles include those produced by molding a sol-gel, drying, and sintering the dried sol-gel to obtain shaped ceramic abrasive particles as described in U.S. Pat. No. 5,201,916 (Berg), U.S. Pat. No. 5,984,988 (Berg), Re. 35,570 (Rowenhorst), U.S. Pat. No. 8,034,137 (Enckson), U.S. Pat. No. 8,123,828 (Culler), U.S. Pat. No. 8,142,531 (Adefris), U.S. Pat. No. 8,142,891 (Culler), U.S. Pat. No. 8,142,532 (Erickson), and U.S. Pat. No. 8,764,865 (Boden), and in U.S. Patent Publication Nos. 2010/319269 (Erickson) and 2015/0052825 (Adefris). Shaped abrasive agglomerate particles may also be useful for practicing the present disclosure, for example, agglomerates including various abrasive particles in a ceramic matrix such as those disclosed in U.S. Pat. No. 5,975,988 (Christianson), U.S. Pat. Nos. 6,319,108, 6,702,650, and 6,951,504 (each to Adefris) and in International Publication No. WO2015/088953 (Kasai) and agglomerates including shaped abrasive particles in an organic resin matrix such as those disclosed in U.S. Patent Publication No. 2014/0080393 (Ludwig).
The abrasive particles typically have an average diameter of from about 0.1 to about 2000 micrometers, more desirably from about 1 to about 1300 micrometers. Abrasive particles are generally graded to a given particle size distribution before use. Such distributions typically have a range of particle sizes, from coarse particles to fine particles. In the abrasive art, this range is sometimes referred to as a “coarse”, “control”, and “fine” fractions. The size of the abrasive particles used for a particular abrading application will be apparent to those skilled in the art.
Abrasive particles graded according to abrasive industry accepted grading standards specify the particle size distribution for each nominal grade within numerical limits. Such industry accepted grading standards (i.e., abrasive industry specified nominal grade) include those known as the American National Standards Institute, Inc. (ANSI) standards, Federation of European Producers of Abrasive Products (FEPA) standards, and Japanese Industrial Standard (JIS) standards.
ANSI grade designations (i.e., specified nominal grades) include: ANSI 4, ANSI 6, ANSI 8, ANSI 16, ANSI 24, ANSI 36, ANSI 40, ANSI 50, ANSI 60, ANSI 80, ANSI 100, ANSI 120, ANSI 150, ANSI 180, ANSI 220, ANSI 240, ANSI 280, ANSI 320, ANSI 360, ANSI 400, and ANSI 600. FEPA grade designations include P8, P12, P16, P24, P36, P40, P50, P60, P80, P100, P120, P150, P180, P220, P320, P400, P500, P600, P800, P1000, and P1200. JIS grade designations include JIS8, JIS12, JIS16, JIS24, JIS36, JIS46, JIS54, JIS60, JIS80, JIS100, JIS150, JIS180, JIS220, JIS240, JIS280, JIS320, JIS360, JIS400, JIS600, JIS800, JIS1000, JIS1500, J152500, JIS4000, JIS6000, JIS8000, and JIS10,000. For use in hand sanding applications such as wood trim and moldings (painted or unpainted) with shaped three-dimensional surfaces, the abrasive particles have a size distribution falling within the range of ANSI grades 100 to 320, inclusive.
Alternatively, the abrasive particles can be graded to a nominal screened grade using U.S.A. Standard Test Sieves conforming to ASTM E-11 “Standard Specification for Wire Cloth and Sieves for Testing Purposes”. ASTM E-11 proscribes the requirements for the design and construction of testing sieves using a medium of woven wire cloth mounted in a frame for the classification of materials according to a designated particle size. A typical designation may be represented as −18+20 meaning that abrasive particles pass through a test sieve meeting ASTM E-11 specifications for the number 18 sieve and are retained on a test sieve meeting ASTM E-11 specifications for the number 20 sieve. In certain embodiments, the abrasive particles have a particle size such that most of the abrasive particle pass through an 18 mesh test sieve and can be retained on a 20, 25, 30, 35, 40, 45, or 50 mesh test sieve. In various embodiments of the present disclosure, the abrasive particles can have a nominal screened grade comprising: −18+20, −20+25, −25+30, −30+35, −35+40, −40+45, −45+50, −50+60, −60+70, −70+80, −80+100, −100+120, −120+140, −140+170, −170+200, −200+230, −230+270, −270+325, −325+400, −400+450, −450+500, or −500+635.
Coating weights for the abrasive particles may depend, for example, on the make coat precursor used, the process for applying the abrasive particles, and the size of the abrasive particles, but typically range from about 5 to about 250 grams per square meter (gsm), from 20 to 100 gsm, 30 to 80 gsm, and from 45 to 65 gsm; although other amounts may also be used.
The anti-loading size layer 16 is disposed on the abrasive layer (i.e., make layer 12 and abrasive particles 13) and optionally backing 11. It may cover all, or more typically some, of either or both of the abrasive layer and the backing 11. The anti-loading size layer 16 can be prepared by curing an anti-loading composition, typically a size coat precursor. The anti-loading composition can be cured by radiation, catalyzed polymerization, or by exposure to ambient conditions (i.e., 20-25° C. and atmospheric pressure).
The anti-loading composition comprises a size binder resin (e.g., a cured and/or crosslinked size precursor). Suitable binders and precursors include those discussed hereinabove with regard to the make precursors and those commonly used in the art to prepare size precursors. The make and size precursors may have the same or different compositions, and may be applied at the same or different coat weights. In presently preferred implementations, the size binder resin is selected from the group consisting of phenolic formaldehyde resins, melamine formaldehyde resins, and urea formaldehyde resins. The amount of size binder is preferably at least 40 percent by weight (based on the total weight of the anti-loading composition), more preferably less than 50 percent by weight, more preferably at least than 60 percent by weight, more preferably at least 70 percent by weight of size binder. Accordingly, the anti-loading composition of the present disclosure forms a size layer once cured.
As mentioned above, urea resin binder precursors typically employ a cocatalyst system including a Lewis acid. The present inventors have found, however, that using a blocked acid catalyst (such as diammonium phosphate (DAP)) with a urea aldehyde resin in lieu of a Lewis acid catalyst tends to improve the stability of the binder precursor system and result in an enhanced pot life of the solution. The blocked catalyst is a salt, ester, amide, adduct, complex or any labile derivative of strong acid, wherein the blocking arrests the activity of the strong acid until such a point when the blocked acid is converted into the free acid form, thus allowing the acid to catalyze the reaction. The catalyst may be released after evaporation of the blocking groups or using reactions or rearrangements that release the acids groups through heat, oxidation, or radiation. The active catalytic species of the blocked acid catalyst does not become available until some elevated temperature or other stimulus condition is reached, such that the catalyst will not undergo a condensation reaction with a urea aldehyde resin at ambient temperatures. Particularly useful are acids, such as phosphonic or sulfonic acids that are at least partially neutralized using ammonia or amines Other suitable blocked acid catalysts in addition to diammonium phosphates include methane sulfonic acid salts, p-toluenesulfonic acid salts, dodecylbenzenesulfonic acid salts, ammonium methanesulfonate, ammonium tosylate, dinonylnaphthalenesulfonic acid, and triethylammonium dihydrogenphosphate. Other exemplary, suitable catalyst can be found in the 1997 Roy Tess Award address for the AMERICAN CHEMISTRY SOCIETY, DIVISION OF POLYMERIC MATERIALS: SCIENCE AND ENGINEERING by Werner J Blank.
The blocked acid catalyst is typically used in the urea binder precursor system at an amount ranging from about 0.1 to about 10.0 weight percent of the total weight of binder precursor (using dry %), in other embodiments at an amount ranging from about 0.1 to about 5.0 weight percent of the total weight of binder precursor
Use of a blocked acid catalyst along with the other components of the present disclosure can substantially improve the pot life of an anti-loading size composition. As used herein, the pot life of a composition is the time necessary for a recently mixed composition to reach 3000 cps, at which point it is no longer sprayable onto a surface of a backing and/or make layer. A longer pot life can lead to considerable improvements in manufacturing, as the composition does not need to be continuously mixed or replaced during operating times. This extended life can lead to a more flexible coating schedule and considerable waste reduction. In certain embodiments of the present disclosure, the pot life of an anti-loading composition including a blocked acid catalyst is at least double the pot life of anti-loading composition including a Lewis acid cocatalyst system. In other embodiment, the pot life of an anti-loading size layer including a blocked acid catalyst is at least quadruple the pot life of anti-loading size layer including a Lewis acid cocatalyst system. In presently preferred embodiments of the present disclosure, the anti-loading composition has a pot life of a least 24 hours, in some embodiments at least 36 hours, and in yet other embodiments at least 48 hours.
The anti-loading composition also includes at least 1 percent by weight (based on the total weight of the composition) of wax having a melting point onset (i.e., that temperature at which melting begins at one atmosphere of pressure (101 kPa)) in the range of from about 50° C. (122° F.) to about 143° C. (290° F.). As used throughout the specification and claims the term wax refers to all the combined total of waxes in the peripheral anti-loading composition. Individual wax components may melt outside the prescribed melting range as long as the total combination of all waxy components demonstrates the specified melting behavior.
Under presently preferred conditions and embodiments, the anti-loading composition comprises at least 1 percent by weight, at least 2 percent by weight, at least 5 percent by weight of wax, at least 10 percent by weight of wax, at least 15 percent by weight of wax, and up to 20 percent by weight of wax. As used herein, “wax” refers to hydrophobic materials having a solid state at room temperature (i.e., a melting point and a softening point above 30° C., preferably above 40° C., more preferably above 50° C. such as certain hydrocarbon materials having long chain aliphatic (fatty) oxygen-containing moieties, and, optionally, fatty ester, alcohol, acid, amide or amine, or alkyl acid phosphate groups. In presently preferred implementations, the anti-loading composition comprises no greater than 40 percent by weight, more preferably no greater than 25 percent by weight, more preferably no greater than 20 percent by weight of wax. A concentration of wax below this range may not deliver the desired anti-loading benefits, while a concentration above this range may result in excess lubricity and compromised cut durability in the anti-loading size layer.
In presently preferred implementations, the wax has a melting point onset in the range of from 60° C. to 150° C., more preferably 100° C. to 143° C., and more preferably from 110° C. to 135° C. For anti-loading compositions including a thermosetting size binder resin, it may be advantageous that the wax having a melting point onset above 100° C. (212° F.), so that wax does not melt as a result of typical abrasive manufacturing processes.
Suitable waxes for use in the anti-loading composition may include natural and synthetic waxes, both modified (e.g., oxidized) and un-modified. Suitable waxes include paraffin wax, polyethylene wax, carnuba wax, polypropylene wax, Ethylene bis stearamide (EBS) wax, and combinations thereof. The wax may be provided as an emulsion or dispersion (i.e., dispersed in water or other solvent) or micronized (i.e., powder form). Examples of suitable waxes include a synthetic hydrocarbon wax available as MP-22VF (m.p.=102-106° C.) from Micro Powders Inc., Tarrytown, N.Y.; a polyethylene wax for waterborne systems available as AQUAPOLY 215 (m.p.=105-111° C.) from Micro Powders Inc.; combinations of waxes such as, for example, a combination of polyethylene and carnauba wax available as MICROKLEAR 295 (m.p.=104-110° C.) from Micro Powders Inc.; a polyethylene wax for waterborne systems available as AQUAPOLY 250 (m.p.=117-123° C.) from Micro Powders Inc., Tarrytown, N.Y.; a high melting polyethylene wax (m.p.=(123-125° C.) available as MPP-635VF from Micro Powders Inc.; a modified polypropylene wax (m.p.=140-143° C.) available as MICROPRO 200 from Micro Powders Inc.; a modified polyethylene waxes available as AQUACER 530 and AQUACER 513 from BYK, Inc., and polyethylene wax GLIDD 6148 from Lanco and an EBS wax available as MICROMIDE 520 (m.p.=141-145° C.) from Micro Powders Inc. Particularly suitable waxes include polyethylene waxes (both modified and unmodified) and paraffin wax.
In presently preferred implementations, the wax is substantially compatible with the size binder resin. As used herein, as substantially compatible wax does not form precipitate when mixed or otherwise dispersed in the size resin. Without wishing to be bound by theory, the selection of compatible wax may hinge on the relative acidity of the size binder and the surfactants included with the wax, such that waxes having a pH of at least 8 can be particularly suitable for the formaldehyde-containing size resins presently preferred.
The anti-loading composition may further include a wax compatible latex. By wax compatible latex, it is meant that the presence of the latex will not cause the formulation to become too thick to effectively coat (for example, if an anti-loading composition includes 63% solids by weight, the viscosity should generally not exceed 1000 cps to be coatable), or to segregate into different layers. Wax compatible latexes can be crosslinkable or crosslinked. Wax compatible latexes include latexes such as cellulose, natural rubber, butadiene rubber, styrene-butadiene rubber, styrene-butadiene-acrylonitrile rubber, chloroprene rubber and methyl-butadiene rubber, and acrylic, vinyl acetate and ethylene vinyl acetate emulsions. These latexes are commercially available from a variety of different sources and include those available under the trade designations RHOPLEX (e.g., RHOPLEX TR407 & RHOPLEX HA16) and ACRYLSOL commercially available from Rohm and Haas Company, FLEXCRYL and VALTAC commercially available from Air Products & Chemicals Inc., SYNTHEMUL, TYCRYL, and TYLAC commercially available from Reichold Chemical Co., HYCAR (e.g., HYCAR 2679) and GOODRITE commercially available from B. F. Goodrich, CHEMIGUM commercially available from Goodyear Tire and Rubber Co., NEOCRYL commercially available from ICI, BUTOFAN commercially available from BASF, RES commercially available from Union Carbide, DUR-O-SET, X-LINK (e.g., X-2712) and TUFCOR (e.g., TUFCOR 1214, TUFCOR 1063, and TUFCOR 5750), each commercially available from Celanese, Florence Ky. In presently preferred implementations, the latex is an acrylic, a cellulose, a vinyl acetate emulsion, an ethylene vinyl acetate emulsion, or combinations thereof. In particularly preferred implementations, the latex is a crosslinkable acrylic, cellulose, vinyl acetate, ethylene vinyl acetate, or combinations thereof
Examples of suitable cellulose latexes include, but are not limited to, alkyl cellulose (e.g., methyl cellulose, ethyl cellulose, ethyl methyl cellulose), hydroxylalkyl cellulose (e.g., hydroxymethyl cellulose, hydroxyethyl cellulose, hydroxypropyl cellulose, hydroxypropyl methyl cellulose, hdyroxyethyl methyl cellulose, and hydroxyethyl ethyl cellulose), and carboxylalkyl cellulose (e.g., carboxymethyl cellulose). In present preferred implementations of the present disclosure, the cellulose is a hydoxylalkyl cellulose latex.
In some embodiments, suitable latexes for use with the anti-loading composition have a T(g) of between about −50° C. and about 115° C., and it yet other embodiments the latex has a T(g) of between about 5° C. and about 50° C.
If present, the wax compatible latex comprises at least 1 percent by weight, more preferably at least 2 percent by weight, more preferably at least 5 percent by weight of the total weight of the anti-loading composition.
In some embodiments, the latex is included in an amount from about 1% to about 15%, by weight of the anti-loading composition, such as from about 2% to about 12%, from about 3% to about 10%, from about 4% to about 8%, by weight of the total anti-loading composition as formulated.
The make coat 16 and/or the anti-loading layer 18 may contain optional additives, such as fillers, fibers, lubricants, grinding aids, wetting agents, thickening agents, anti-loading agents, coupling agents, surfactants, pigments, dyes, coupling agents, photo-initiators, plasticizers, suspending agents, antistatic agents, and the like. Fillers are typically organic or inorganic particulates dispersed within the resin and may, for example, modify either the binder precursor or the properties of the cured layer, or both, and/or may simply, for example, be used to reduce cost. The fillers may be present, for example, to block pores and passages within the backing, to reduce its porosity and provide a surface to which the maker coat will bond effectively. The addition of a filler, at least up to a certain extent, typically increases the hardness and toughness of the cured binder. Moreover, the addition of certain fillers can also act as anti-loading materials. Inorganic particulate filler commonly has an average particle size ranging from about 0.5 micrometer to about 100 micrometers, more typically from about 1 to about 50 micrometers, and sometimes even from about 5 to about 30 micrometers. Though not wishing to be bound by theory, small particles of filler can combine with swarf from a sanded surface, such as a painted metal surface, to prevent sufficient agglomerating loading of swarf in a surface of the coated abrasive. That is, the filler particles are of such a size that, upon sanding a painted surface using the abrasive article to produce abraded swarf, particles of the anti-loading agent are released that combine with and inhibit the agglomeration of such swarf particles.
Examples of useful fillers include: metal carbonates such as calcium carbonate (in the form of chalk, calcite, marl, travertine, marble or limestone), calcium magnesium carbonate, sodium carbonate, and magnesium carbonate; silicas such as quartz, glass beads, glass bubbles and glass fibers; silicates such as talc, clays, feldspar, mica, calcium silicate (e.g., wollastonite), calcium metasilicate, sodium aluminosilicate, sodium-potassium alumina silicate, and sodium silicate; metal sulfates such as calcium sulfate, barium sulfate, sodium sulfate, aluminum sodium sulfate, and aluminum sulfate; gypsum; vermiculite; wood flour; alumina trihydrate; carbon black; metal oxides such as calcium oxide (lime), aluminum oxide, titanium dioxide, alumina hydrate, alumina monohydrate; and metal sulfites such as calcium sulfite. Fillers that can function as grinding aids include cryolite, potassium fluoroborate, feldspar, and sulfur. Cryolite may provide additional anti-loading benefits, as detailed in U.S. Pat. No. 6,451,076. The amounts of these materials are selected to provide the properties desired, as is known to those skilled in the art. If used, filler is typically present in the anti-loading composition at about 20 percent by weight of the total composition, though other concentrations may be appropriate based on the intended abrasive application.
The anti-loading composition can contain a coupling agent. Suitable examples of the coupling agent commonly used in the abrasive art include organic silane, zircoaluminate, and titanate. Suitable silane coupling agents include epoxy functional silanes, such as those described in International Publication No. WO2017062482 (Schillo-Armstrong et al.). The amount of the coupling agent is typically less than 5 wt %, preferably less than 1 wt %, of the anti-loading composition.
Any of the make and size precursors described above optionally include one or more curatives. Curatives include those that are photosensitive or thermally sensitive, and preferably comprise at least one free-radical polymerization initiator and at least one cationic polymerization catalyst, which may be the same or different.
In one exemplary method of making the article 10, the make precursor is applied to the backing 11. Next, abrasive particles 13 are applied to the make precursor, and then make precursor can be optionally partially cured (e.g., to an a-stage or b-stage). The size precursor is then applied over the make layer precursor and abrasive particles and the make and size layer precursors sufficiently cured to form a useable abrasive article. Curing may be accomplished using thermal, atmospheric (e.g., drying), and/or photochemical methods.
In addition, it will be recognized that the backing 11, make layer 12, and abrasive particles 13 may be provided in the form of a pre-formed (i.e., otherwise complete) abrasive sheet. That is, rather than providing a backing layer 11, which is then coated with make coat precursor and provided with abrasive particles 13 and at least partially cured to form an abrasive sheet, a pre-formed abrasive sheet including a backing, make coat and abrasive particles may be provided. The anti-loading size precursor can then be applied directly to the pre-formed abrasive sheet. If a pre-formed abrasive sheet is used, the size layer 16 may be applied using, for example, solvent coating, roll coating, hot melt coating, drop die, or powder coating techniques. For ease of manufacturing, it could be useful to provide the finished sandpaper in bulk form, and then coat the bulk sandpaper with the anti-loading size precursor prior to producing the individual sheets of sandpaper that are ultimately used by the end user. Advantageously, the elimination of a supersize coat serves to reduce the equipment necessary to create an abrasive article, leading to a meaningful reduction in manufacturing time.
A wide variety of commercially available conventional sandpaper constructions having a wide variety of backing materials (e.g., papers, films, cloths), weights (e.g., A, B, or C weight paper), and abrasive particles may be coated with an anti-loading composition according to the present disclosure.
Abrading may be carried out dry or wet. For wet abrading, the liquid may be introduced supplied in the form of a light mist to complete flood. Examples of commonly used liquids include: water, water-soluble oil, organic lubricant, and emulsions. The liquid may serve to reduce the heat associated with abrading and/or act as a lubricant. The liquid may contain minor amounts of additives such as bactericide, antifoaming agents, and the like.
Examples of workpieces include aluminum metal, carbon steels, mild steels (e.g., 1018 mild steel and 1045 mild steel), tool steels, stainless steel, hardened steel, titanium, glass, ceramics, wood, wood-like materials (e.g., plywood and particle board), paint, painted surfaces, and organic coated surfaces. The applied force during abrading typically ranges from about 1 to about 100 kilograms (kg), although other pressures can also be used.
In order that the disclosure described herein can be more fully understood, the following examples are set forth. It should be understood that these examples are for illustrative purposes only, and are not to be construed as limiting this disclosure in any manner.
P-toluenesulfonic acid monohydrate (1.90 g, 0.01 mol) was dissolved in 6.48 g water in a jar equipped with a stirbar. Next 28% by weight of ammonium hydroxide solution (0.64 g, 0.0105 mol, 0.179 g ammonium hydroxide, 0.46 g water) was added dropwise over about 30 sec.
Methanesulfonic acid (1.92 g, 0.02 mol) was dissolved in 6.68 g water in a jar equipped with a stirbar. Next 28% by weight of ammonium hydroxide solution (1.28 g, 0.021 mol, 0.357 g ammonium hydroxide, 0.92 g water) was added dropwise over about 30 sec.
Samples of coated abrasive sheets were prepared using 80 grit abrasive particles, designated as a P80 blend.
P80 is a mineral blend of 90% by weight 80 grit size premium white, heat-treated, aluminum oxide (available from Imerys Inc., Cockeysville, Md.) and 10% by weight 3M Precision Shaped Grain (PSG). The PSG shaped abrasive particles were prepared according to the disclosure of U.S. Pat. No. 8,142,531 (Adefris et al.). The PSG particles were in the general shape of equilateral triangles, with an average edge length of approximately 500 μm and a particles thickness of approximately 100 μm.
The formulation of the make coating for Examples 1-6 and Control Examples 1-3 (coated at approximately 63% solids in water) is provided in Table 1. Unless otherwise noted, values in these Examples are reported in wt. %.
The make coating was rolled coated onto a 125 gsm, “C” weight paper backing having a SBR (styrene butadiene rubber) latex barrier coating. The target coating weight of the make coating was 11.0+/−2.0 grains/24 inch2 (46+/−8 gsm) (wet weight). The P80 abrasive particles were then electrostatically coated onto the make coating, and the make coating was cured at about 150° F. (66° C.) for 20 minutes. The target coating weight of the abrasive particles was 37.0+/−2.0 grains/24 inch2 (155+/−8 gsm) (wet weight).
Samples of the make-coated abrasive sheets measuring 12 inches×35 inches (30.5 cm×88.9 cm) were then further coated with an anti-loading size composition using one of the two methods described below. The anti-loading size coating formulations are provided in the Tables and were coated at approximately 65% solids in water.
The make-coated sheet was then vertically clipped on to a spray board. The anti-loading size coating was coated on to the make-coated sheet carried out using an automated 3M ACCUSPRAY spray gun with a 3M ACCUSPRAY atomizing head (available from 3M Company, St. Paul, Minn.). The size-coated sheet was cured at about 150° F. (66° C.) for 30 minutes, and then cured at about 180° F. (82° C.) for 3 hours. The cured sheet was orthogonally flexed, laminated on a hook-and-loop fastener and die-cut into 5 inch (12.7 cm) diameter abrasive discs for further testing according to the Abrasion and Pot Life Test Methods as described below.
The target wet coating weight of the anti-loading size coating was 37.0+/−2.0 grains/24 inch (154.8+/−8.4 gsm) for all coated abrasive sheets. (coated at approximately 63% solids in water)
A 5 inch (12.7 cm) diameter abrasive disc to be tested was mounted on an electric rotary tool that was disposed over an X-Y table having a plastic panel measuring 15 inches×21 inches×0.375 inch (38.1 m×53.3 cm×0.95 cm) secured to the X-Y table. The tool was then set to traverse at a rate of 5.5 inches/second (14.0 cm/sec) in the X direction along the length of the panel, and traverse along the width of the panel (Y direction) at a rate of 3 inches/second (7.6 cm/sec). The rotary tool was then activated to rotate at 8000 rpm under no load. The abrasive article was then urged at an angle of 2.5 degrees against the panel at a load of 10 lbs (4.54 kg). The tool was then activated to move along the length and width of the board. The tool was then raised, and returned to the starting point. Ten such grinding-and-return passes along the length of the panel were completed in each cycle for a total of 10 cycles. The mass of the panel was measured before and after each cycle to determine the total mass loss in grams after each cycle. A cumulative mass loss (total cut) was determined at the end of 10 cycles. The abrasive disc was weighed before and after the completion of the test (10 cycles) to determine the wear. The total cut and cut durability data for each Example provided in the Tables is an average of three samples that were tested. Cut durability was calculated: Cut Durability (%)=Final cut (Cycle 10)/Initial cut (Cycle 1)×100.
A 500 gram solution of anti-loading composition was mixed and shaken thoroughly for at least 1 minute at room temperature and atmospheric pressure. The solution was visually observed for demonstrable changes in viscosity or precipitate. The pot life was defined as the time required for the sample solution to reach a viscosity of about 3000 cps. Viscosity was confirmed using a Brookfield viscometer, number 3 spindle, 30 rpm, 25° C. for viscosities of 125 to about 1500 cps or using a Brookfield viscometer, number 3 spindle, 15 rpm, 25° C. for viscosities of greater than 1500 cps.
Abrasive discs were prepared with P80 abrasive particles and urea-formaldehyde/wax based anti-loading size composition formulations according to the methods described above. Abrasive discs with size coats including typical Lewis Acid catalysts were also prepared as Comparative Examples. Cut and cut durability data were obtained using the Abrasion Test described above. The anti-loading size composition formulations and test results are provided in Table 2. All the formulations in Table 2 are calculated at 100% solids of raw materials regardless of the solids at which they are supplied; the weight % solids of the solution is 63% (same as the make coat).
Examples E1-E6 demonstrate a dramatic improvement in Pot Life over the Comparative Examples, while provide at least acceptable Total Cut and Cut Durability. Examples E1-E3 demonstrate a balance of enhanced Pot Life and Cut Durability.
The recitation of all numerical ranges by endpoint is meant to include all numbers subsumed within the range (i.e., the range 1 to 10 includes, for example, 1, 1.5, 3.33, and 10).
The patents, patent documents, and patent applications cited herein are incorporated by reference in their entirety as if each were individually incorporated by reference. It will be apparent to those of ordinary skill in the art that various changes and modifications may be made without deviating from the inventing concepts set from above. Thus, the scope of the present disclosure should not be limited to the structures described herein. Those having skill in the art will appreciate that many changes may be made to the details of the above-described embodiments and implementations without departing from the underlying principles thereof. Further, various modifications and alterations of the present disclosure will become apparent to those skilled in the art without departing from the spirit and scope of the invention. The scope of the present application should, therefore, be determined only by the following claims and equivalents thereof.
| Number | Date | Country | |
|---|---|---|---|
| 63244371 | Sep 2021 | US |
