Patent Application
20190345644
The present disclosure relates to the field of polymeric fibers and to the field of fibrillated reinforcement materials.
Polymer fibers spun from pure resins often possess poor mechanical properties for a given application area: such as low modulus, fatigue and wear properties. For this reason, articles—e.g., carpets—that are formed from polymeric fibers may exhibit suboptimal properties. Accordingly, there is a long-felt need in the art for improved fiber materials.
The present disclosure addresses the use of reinforcement materials (e.g., fibrillated fluoropolymer such as PTFE, ultra-high molecular weight polyethylene (UHMW-PE)) to reinforce a thermoplastic matrix for fiber spinning applications. Reinforcement is only achieved by fibrillating the additive within the matrix. The fibrillation is achieved by flow-induced orientation. These composite fibers show enhanced properties such as high modulus, improved fatigue, wear and frictional performance. As one example, fibrillated fluoropolymer reinforced resins may be spun for fiber application, as a formulation of fluoropolymer in a resin matrix yielding a fiber with enhanced properties such as high modulus, excellent fatigue and wear/friction performance, and dimensional accuracies.
In one aspect, the present disclosure provides composite fibers, comprising: a thermoplastic matrix polymer, the composite fiber having a diameter in the range of from about 2 micrometers to about 4 millimeters, and the composite fiber comprising a plurality of fibrillated reinforcement material regions disposed within the thermoplastic matrix polymer, and the melting temperature or Tg of the thermoplastic matrix material, whichever is higher, being below the melting temperature or Tg, whichever is lower, of the fibrillated reinforcement material. The thermoplastic matrix polymer is also interchangeably referred to in the context of this invention as the thermoplastic matrix material.
Also provided are articles, the articles comprising a plurality of composite fibers according to the present disclosure, the article being characterized as a woven article, a non-woven article, or any combination thereof.
Further provided are methods, comprising: using a composite fiber according to the present disclosure in additively manufacturing at least a portion of an article.
Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art. In case of conflict, the present document, including definitions, will control. Preferred methods and materials are described below, although methods and materials similar or equivalent to those described herein can be used in practice or testing. All publications, patent applications, patents and other references mentioned herein are incorporated by reference in their entirety. The materials, methods, and examples disclosed herein are illustrative only and not intended to be limiting.
The singular forms “a,” “an,” and “the” include plural referents unless the context clearly dictates otherwise. As used in the specification and in the claims, the term “comprising” may include the embodiments “consisting of” and “consisting essentially of.” The terms “comprise(s),” “include(s),” “having,” “has,” “can,” “contain(s),” and variants thereof, as used herein, are intended to be open-ended transitional phrases, terms, or words that require the presence of the named ingredients/steps and permit the presence of other ingredients/steps. However, such description should be construed as also describing compositions or processes as “consisting of” and “consisting essentially of” the enumerated ingredients/steps, which allows the presence of only the named ingredients/steps, along with any impurities that might result therefrom, and excludes other ingredients/steps. It is to be understood that the terminology used herein is for the purpose of describing particular aspects only and is not intended to be limiting. As used in the specification and in the claims, the term “comprising” can include the embodiments “consisting of” and “consisting essentially of.” Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this disclosure belongs. In this specification and in the claims which follow, reference will be made to a number of terms which shall be defined herein.
Numerical values in the specification and claims of this application, particularly as they relate to polymers or polymer compositions, reflect average values for a composition that may contain individual polymers of different characteristics. Furthermore, unless indicated to the contrary, the numerical values should be understood to include numerical values which are the same when reduced to the same number of significant figures and numerical values which differ from the stated value by less than the experimental error of conventional measurement technique of the type described in the present application to determine the value.
All ranges disclosed herein are inclusive of the recited endpoint and independently combinable (for example, the range of “from 2 grams (g) to 10 grams” is inclusive of the endpoints, 2 grams and 10 grams, and all the intermediate values). The endpoints of the ranges and any values disclosed herein are not limited to the precise range or value; they are sufficiently imprecise to include values approximating these ranges and/or values.
As used herein, approximating language may be applied to modify any quantitative representation that may vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term or terms, such as “about” and “substantially,” may not be limited to the precise value specified, in some cases. In at least some instances, the approximating language may correspond to the precision of an instrument for measuring the value. The modifier “about” should also be considered as disclosing the range defined by the absolute values of the two endpoints. For example, the expression “from about 2 to about 4” also discloses the range “from 2 to 4.” The term “about” may refer to plus or minus 10% of the indicated number. For example, “about 10%” may indicate a range of 9% to 11%, and “about 1” may mean from 0.9 to 1.1. Other meanings of “about” may be apparent from the context, such as rounding off, so, for example “about 1” may also mean from 0.5 to 1.4.
As used herein, “Tm” refers to the melting point at which a polymer completely loses its orderly arrangement. As used herein, “Tc” refers to the crystallization temperature at which a polymer gives off heat to form a crystalline arrangement. The terms “Glass Transition Temperature” or “Tg” may be measured using, e.g., a differential scanning calorimetry method and expressed in degrees Celsius.
As used herein, “matrix polymer component”, also referred to as “thermoplastic matrix material”, refers to one or more polymers that are not fibrillated. Examples of suitable matrix polymers include, but are not limited to, amorphous, crystalline, and semi-crystalline thermoplastic materials such as polyolefins (for example, linear or cyclic polyolefins such as polyethylene, chlorinated polyethylene, polypropylene, and the like); polyesters (for example, polyethylene terephthalate, polybutylene terephthalate, polycyclohexylmethylene terephthalate, and the like); arylate esters; polyamides; polysulfones (including hydrogenated polysulfones, and the like); ABS resins; polystyrenes (for example hydrogenated polystyrenes, and atactic polystyrenes, hydrogenated polystyrenes such as polycyclohexyl ethylene, styrene-co-acrylonitrile, styrene-co-maleic anhydride, and the like); polybutadiene; poly(meth)acrylates (for example, poly(methyl methacrylate) (PMMA), methyl methacrylate-polyimide copolymers, and the like); polyacrylonitrile; polyacetals; polycarbonates; polyphenylene ethers (for example, those derived from 2,6-dimethylphenol and copolymers with 2,3,6-trimethylphenol, and the like); ethylene-vinyl acetate copolymers; polyvinyl acetate; liquid crystalline polymers; fluoropolymers such as ethylene-tetrafluoroethylene copolymer, polyvinyl fluoride, and polyvinylidene fluoride, polytetrafluoroethylene (provided that the fluoropolymer has a lower softening temperature than the fluoropolymer component described below); polyvinyl chloride, polyvinylidene chloride; and combinations comprising at least one of the foregoing polymers. The matrix polymer may generally be provided in any form, including but not limited to powders, plates, pellets, flakes, chips, whiskers, and the like. The matrix material is suitably one that has a lower melting temperature than the melting temperature of the reinforcement material.
A variety of reinforcement materials may be used in the disclosed fibers. Some exemplary reinforcement materials include liquid crystalline polymers, polyolefins (e.g., UHMW-PE), carbon fibers, carbon nanotubes, cellulose, fillers, blends (of any of the foregoing), fluoropolymers, and combinations thereof. PTFE is an especially suitable fluoropolymer for use as a reinforcement material. Likewise, UHMW-PE is also a suitable reinforcement material and may be formed into fibrils within the disclosed fibers. UHMW-PE may have a molecular weight in the range of from about 1 million to about 10 million g/mole.
Fluoropolymers and other materials suitable for use as the reinforcement material or fibrillated component of the disclosure are capable of being fibrillated (“fibrillatable”) during mixing with the matrix polymer, the filler, or both simultaneously. “Fibrillation” is a term of art that refers to the treatment of reinforcement materials (e.g., fluoropolymers) so as to produce, for example, a “node and fibril,” network, or cage-like structure.
In one embodiment, the reinforcement material (e.g., fluoropolymer, UHMW-PE) comprises fibrils having an average diameter of 5 nanometers (nm) to 2 micrometers (μm), or from about 5 nm to about 2 μm. The fibril may also have an average fibril diameter of 30 nanometers to 750 nanometers, more specifically 5 nanometers to 500 nanometers. In a further example, the reinforcement material may also have an average fibril diameter of about 30 nanometers to about 750 nanometers, more specifically about 5 nanometers to about 500 nanometers. Field Emission Scanning Electron Microscopy, TEM, SEM, AFM, and STEM are all exemplary techniques for observing the extent of fibrillation of the reinforcement material throughout the matrix polymer in the fibrillated compositions.
Suitable fluoropolymers are described in, e.g., U.S. Pat. No. 7,557,154 and include but are not limited to homopolymers and copolymers that comprise structural units derived from one or more fluorinated alpha-olefin monomers, that is, an alpha-olefin monomer that includes at least one fluorine atom in place of a hydrogen atom. In one embodiment the fluoropolymer comprises structural units derived from two or more fluorinated alpha-olefin, for example tetrafluoroethylene, hexafluoroethylene, and the like. In another embodiment, the fluoropolymer comprises structural units derived from one or more fluorinated alpha-olefin monomers and one or more non-fluorinated monoethylenically unsaturated monomers that are copolymerizable with the fluorinated monomers, for example alpha-monoethylenically unsaturated copolymerizable monomers such as ethylene, propylene, butene, acrylate monomers (e.g., methyl methacrylate and butyl acrylate), vinyl ethers, (e.g., cyclohexyl vinyl ether, ethyl vinyl ether, n-butyl vinyl ether, vinyl esters) and the like. Specific examples of fluoropolymers include polytetrafluoroethylene, polyhexafluoropropylene, polyvinylidene fluoride, polychlorotrifluoroethylene, ethylene tetrafluoroethylene, fluorinated ethylene-propylene, polyvinyl fluoride, and ethylene chlorotrifluoroethylene. Combinations comprising at least one of the foregoing fluoropolymers may also be used. Polytetrafluroroethylene (PTFE) is considered especially suitable.
As is known, fluoropolymers are available in a variety of forms, including powders, emulsions, dispersions, agglomerations, and the like. “Dispersion” (also called “emulsion”) fluoropolymers are generally manufactured by dispersion or emulsion, and may comprise 25 to 60 weight percent (wt. %), or about 25 wt. % to 60 wt. %, fluoropolymer in water, stabilized with a surfactant, wherein the fluoropolymer particles are 0.1 to 0.3 micrometers (microns, μm), or about 0.1 μm to about 0.3 μm in diameter. “Fine powder” (or “coagulated dispersion”) fluoropolymers may be made by coagulation and drying of dispersion-manufactured fluoropolymers. Fine powder fluoropolymers are generally manufactured to have a particle size of 400 to 500 μm, or about 400 μm to about 500 μm. “Granular” fluoropolymers may be made by a suspension method, and are generally manufactured in two different particle size ranges, including a median particle size of 30 to 40 μm, or about 30 μm to about 40 μm and a high bulk density product exhibiting a median particle size of 400 to 500 μm, or about 400 μm to about 500 μm. Pellets of fluoropolymer may also be obtained and cryogenically ground to exhibit the desired particle size.
A fluoropolymer may be at least partially encapsulated by an encapsulating polymer that may be the same as or different from the matrix polymer (hereinafter referred to as an “encapsulated polymer”). Without being bound by theory, it is believed that encapsulation may aid in the distribution of the fluoropolymer within the matrix, and/or compatibilize the fluoropolymer with the matrix.
Suitable encapsulating polymers accordingly include, but are not limited to, vinyl polymers, acrylic polymers, polyacrylonitrile, polystyrenes, polyolefins, polyesters, polyurethanes, polyamides, polysulfones, polyimides, polyetherimides, polyphenylene ethers, polyphenylene sulfides, polyether ketones, polyether ether ketones, acrylonitrile butadiene styrene (ABS) resins, polyethersulfones, poly(alkenylaromatic) polymers, polybutadiene, liquid crystalline polymers, polyacetals, polycarbonates, polyphenylene ethers, ethylene-vinyl acetate copolymers, polyvinyl acetate, liquid crystal polymers, ethylene-tetrafluoroethylene copolymer, aromatic polyesters, polyvinyl fluoride, polyvinylidene fluoride, polyvinylidene chloride, and combinations comprising at least one of the foregoing polymers.
The encapsulating polymers may be obtained by polymerization of monomers or mixtures of monomers by methods known in the art, for example, condensation, addition polymerization, and the like. Emulsion polymerization, particularly radical polymerization may be used effectively. In one embodiment, the encapsulating polymer is formed from monovinylaromatic monomers containing condensed aromatic ring structures, such as vinyl naphthalene, vinyl anthracene and the like. Examples of suitable monovinylaromatic monomers include styrene, 3-methylstyrene, 3,5-diethylstyrene, 4-n-propylstyrene, alpha-methylstyrene, alpha-methyl vinyltoluene, alpha-chlorostyrene, alpha-bromostyrene, dichlorostyrene, dibromostyrene, tetra-chlorostyrene, and the like, and combinations comprising at least one of the foregoing compounds. Styrene and/or alpha-methylstyrene may be specifically mentioned. Other useful monomers for the formation of the encapsulating polymer include monovinylic monomers such as itaconic acid, acrylamide, N-substituted acrylamide or methacrylamide, maleic anhydride, maleimide, N-alkyl-, aryl-, or haloaryl-substituted maleimide, and glycidyl (meth)acrylates. Other monomers include acrylonitrile, ethacrylonitrile, methacrylonitrile, alpha-chloroacrylonitrile, beta-chloroacrylonitrile, alpha-bromoacrylonitrile, acrylic acid, methyl (meth)acrylate, ethyl (meth)acrylate, n-butyl (meth)acrylate, t-butyl (meth)acrylate, n-propyl (meth)acrylate, isopropyl (meth)acrylate, 2-ethylhexyl (meth)acrylate, and the like, and combinations comprising at least one of the foregoing monomers.
Mixtures of the foregoing monovinylaromatic monomers and monovinylic monomers may also be used, for example mixtures of styrene and acrylonitrile (SAN). The relative ratio of monovinylaromatic and monovinylic monomers in the rigid graft phase may vary widely depending on the type of fluoropolymer, type of monovinylaromatic and monovinylic monomer(s), and the desired properties of the encapsulant. The encapsulant may generally be formed from up to 100 wt. %, or up to about 100 wt. %, of monovinyl aromatic monomer, specifically 30 to 100 wt. %, more specifically 50 to 90 wt. % monovinylaromatic monomer, with the balance being comonomer(s). In further examples, the encapsulant may generally be formed from up to about 100 wt. % of monovinyl aromatic monomer, specifically about 30 to about 100 wt. %, more specifically about 50 to about 90 wt. % monovinylaromatic monomer, with the balance being comonomer(s).
Elastomers may also be used as the encapsulating polymer, as well as elastomer-modified graft copolymers. Suitable elastomers include, for example, conjugated diene rubbers; copolymers of a conjugated diene with less than 50 wt. %, or less than about 50 wt. %, of a copolymerizable monomer; olefin rubbers such as ethylene propylene copolymers (EPR) or ethylene-propylene-diene monomer rubbers (EPDM); ethylene-vinyl acetate rubbers; silicone rubbers; elastomeric C1-8 alkyl (meth)acrylates; elastomeric copolymers of C1-8 alkyl (meth)acrylates with butadiene and/or styrene; or combinations comprising at least one of the foregoing elastomers.
Examples of conjugated diene monomers that may be used are butadiene, isoprene, 1,3-heptadiene, methyl-1,3-pentadiene, 2,3-dimethyl-1,3-butadiene, 2-ethyl-1,3-pentadiene; 1,3- and 2,4-hexadienes, and the like, as well as mixtures comprising at least one of the foregoing conjugated diene monomers. Specific conjugated diene homopolymers include polybutadiene and polyisoprene.
Copolymers of conjugated diene rubbers may also be used, for example those produced by aqueous radical emulsion polymerization of a conjugated diene and up to 10 wt. %, or up to about 10 wt. %, of one or more monomers copolymerizable therewith.
(Meth)acrylate monomers suitable for use as an elastomeric encapsulating monomer include the cross-linked, particulate emulsion homopolymers or copolymers of C4-8 alkyl (meth)acrylates, in particular C4-6 alkyl acrylates, for example n-butyl acrylate, t-butyl acrylate, n-propyl acrylate, isopropyl acrylate, 2-ethylhexyl acrylate, and the like, and combinations comprising at least one of the foregoing monomers. Exemplary comonomers include but are not limited to butadiene, isoprene, styrene, methyl methacrylate, phenyl methacrylate, phenylethyl methacrylate, N-cyclohexylacrylamide, vinyl methyl ether or acrylonitrile, and mixtures comprising at least one of the foregoing comonomers. Optionally, up to 5 wt. % of a polyfunctional crosslinking comonomer may be present, for example divinylbenzene, alkylenediol di(meth)acrylates such as glycol bisacrylate, alkylenetriol tri(meth)acrylates, polyester di(meth)acrylates, bisacrylamides, triallyl cyanurate, triallyl isocyanurate, allyl (meth)acrylate, diallyl maleate, diallyl fumarate, diallyl adipate, triallyl esters of citric acid, triallyl esters of phosphoric acid, and the like, as well as combinations comprising at least one of the foregoing crosslinking agents.
Suitable elastomer-modified graft copolymers may be prepared by first providing an elastomeric polymer (for example, as described above), then polymerizing the constituent monomer(s) of the rigid phase in the presence of the fluoropolymer and the elastomer to obtain the graft copolymer. The elastomeric phase may provide 5 to 95 wt. % of the total graft copolymer, more specifically 20 to 90 wt. %, and even more specifically 40 to 85 wt. % of the elastomer-modified graft copolymer, the remainder being the rigid graft phase. In further examples, the elastomeric phase may provide about 5 to about 95 wt. % of the total graft copolymer, more specifically about 20 to about 90 wt. %, and even more specifically about 40 to about 85 wt. % of the elastomer-modified graft copolymer, the remainder being the rigid graft phase. Depending on the amount of elastomer-modified polymer present, a separate matrix or continuous phase of ungrafted rigid polymer or copolymer may be simultaneously obtained along with the elastomer-modified graft copolymer.
Specific encapsulating polymers include polystyrene, copolymers of polystyrene, poly(alpha-methylstyrene), poly(alpha-ethylstyrene), poly(alpha-propylstyrene), poly(alpha-butylstyrene), poly(p-methylstyrene), polyacrylonitrile, polymethacrylonitrile, poly(methyl acrylate), poly(ethyl acrylate), poly(propyl acrylate), and poly(butyl acrylate), poly(methyl methacrylate), poly(ethyl methacrylate), poly(propyl methacrylate), poly(butyl methacrylate); polybutadiene, copolymers of polybutadiene with propylene, poly(vinyl acetate), poly(vinyl chloride), poly(vinylidene chloride), poly(vinylidene fluoride), poly(vinyl alcohols), acrylonitrile-butadiene copolymer rubber, acrylonitrile-butadiene-styrene (ABS), poly(C4-8 alkyl acrylate) rubbers, styrene-butadiene rubbers (SBR), EPDM rubbers, silicon rubber and combinations comprising at least one of the foregoing encapsulating polymers. A preferred fluoropolymer is polytetrafluoroethylene.
Preferably, the encapsulating polymer comprises a styrene-acrylonitrile copolymer, an acrylonitrile-butadiene-styrene copolymer, alpha-alkyl-styrene-acrylonitrile copolymer, an alpha-methylstyrene-acrylonitrile copolymer, a styrene-butadiene rubber, a methyl methacrylate copolymer, or a combination thereof. In another embodiment, the encapsulating polymer comprises SAN, ABS copolymers, alpha-(C1-3)alkyl-styrene-acrylonitrile copolymers, alpha-methylstyrene-acrylonitrile (AMSAN) copolymers, SBR, and combinations comprising at least one of the foregoing. In yet another embodiment the encapsulating polymer is SAN or AMSAN. A preferred fluoropolymer encapsulated by an encapsulating polymer is styrene acrylonitrile encapsulated polytetrafluoroethylene.
Suitable amounts amount of encapsulating polymer may be determined by one of ordinary skill in the art without undue experimentation, using the guidance provided herein. In one embodiment, the encapsulated fluoropolymer comprises 10 to 90 weight percent (wt. %), or about 10 to about 90 wt. %, fluoropolymer and 90 to 10 wt. %, or about 90 wt. % to about 10 wt. %, of the encapsulating polymer, based on the total weight of the encapsulated fluoropolymer. Alternatively, the encapsulated fluoropolymer comprises 20 to 80 wt. %, or about 20 to about 80 wt. %, more specifically 40 wt. % to 60 wt. %, or about 40 to about 60 wt. % fluoropolymer, and 80 wt. % to 20 wt. %, or about 80 to about 20 wt. %, specifically, 60 wt. % or 40 wt. %, or about 60 about 40 wt. % encapsulating polymer, based on the total weight of the encapsulated polymer.
Additives
The disclosed compositions may include one or more other additives may be present in the compositions described herein, as desired. Exemplary additives include: one or more polymers, ultraviolet agents, ultraviolet stabilizers, heat stabilizers, antistatic agents, anti-microbial agents, radiation stabilizers, pigments, dyes, fillers, plasticizers, flame retardants, antioxidants, lubricants, and combinations thereof.
Exemplary polymers that can be mixed with the compositions described herein include elastomers, thermoplastics, thermoplastic elastomers, and impact additives. The compositions described herein may be mixed with other polymers such as a polyester, a polyestercarbonate, a bisphenol-A homopolycarbonate, a polycarbonate copolymer, a tetrabromo-bisphenol A polycarbonate copolymer, a polysiloxane-co-bisphenol-A polycarbonate, a polyesteramide, a polyether, a polyepoxide, a polylactide, a polylactic acid (PLA), an acrylic polymer, polyacrylonitrile, a polystyrene, a polyolefin, a polysiloxane, a polyurethane, a polyamide, a polyamideimide, a polysulfone, a polyphenylene ether, an acrylonitrile-butadiene-styrene (ABS) resin, an acrylic-styrene-acrylonitrile (ASA) resin, a poly(alkenylaromatic) polymer, a polybutadiene, a polyacetal, a polycarbonate, an ethylene-vinyl acetate copolymer, a polyvinyl acetate, a liquid crystal polymer, an ethylene-tetrafluoroethylene copolymer, an aromatic polyester, a polyvinyl fluoride, a polyvinylidene fluoride, a polyvinylidene chloride, tetrafluoroethylene, or any combination thereof.
The additional polymer can be an impact modifier, if desired. Suitable impact modifiers may be high molecular weight elastomeric materials derived from olefins, monovinyl aromatic monomers, acrylic and methacrylic acids and their ester derivatives, as well as conjugated dienes that are fully or partially hydrogenated. The elastomeric materials can be in the form of homopolymers or copolymers, including random, block, radial block, graft, and core-shell copolymers.
A specific type of impact modifier may be an elastomer-modified graft copolymer comprising (i) an elastomeric (i.e., rubbery) polymer substrate having a Tg less than 10° C., or less than about 10° C., less than 0° C. or less than about 0° C., less than −10° C. or less than about −10° C., or between −40° C. to −80° C. or between about −40° C. to −80° C., and (ii) a rigid polymer grafted to the elastomeric polymer substrate. Materials suitable for use as the elastomeric phase include, for example, conjugated diene rubbers, for example polybutadiene and polyisoprene; copolymers of a conjugated diene with less than about 50 wt. % of a copolymerizable monomer, for example a monovinylic compound such as styrene, acrylonitrile, n-butyl acrylate, or ethyl acrylate; olefin rubbers such as ethylene propylene copolymers (EPR) or ethylene-propylene-diene monomer rubbers (EPDM); ethylene-vinyl acetate rubbers; silicone rubbers; elastomeric C1-C8 alkyl(meth)acrylates; elastomeric copolymers of C1-C8 alkyl(meth)acrylates with butadiene and/or styrene; or combinations comprising at least one of the foregoing elastomers. Materials suitable for use as the rigid phase include, for example, monovinyl aromatic monomers such as styrene and alpha-methyl styrene, and monovinylic monomers such as acrylonitrile, acrylic acid, methacrylic acid, and the C1-C6 esters of acrylic acid and methacrylic acid, specifically methyl methacrylate.
Specific impact modifiers include styrene-butadiene-styrene (SBS), styrene-butadiene rubber (SBR), styrene-ethylene-butadiene-styrene (SEBS), ABS (acrylonitrile-butadiene-styrene), acrylonitrile-ethylene-propylene-diene-styrene (AES), styrene-isoprene-styrene (SIS), methyl methacrylate-butadiene-styrene (MBS), and styrene-acrylonitrile (SAN). Exemplary elastomer-modified graft copolymers include those formed from styrene-butadiene-styrene (SBS), styrene-butadiene rubber (SBR), styrene-ethylene-butadiene-styrene (SEBS), ABS (acrylonitrile-butadiene-styrene), acrylonitrile-ethylene-propylene-diene-styrene (AES), styrene-isoprene-styrene (SIS), methyl methacrylate-butadiene-styrene (MBS), and styrene-acrylonitrile (SAN).
The compositions described herein may comprise an ultraviolet (UV) stabilizer for dispersing UV radiation energy. The UV stabilizer does not substantially hinder or prevent cross-linking of the various components of the compositions described herein. UV stabilizers may be hydroxybenzophenones; hydroxyphenyl benzotriazoles; cyanoacrylates; oxanilides; or hydroxyphenyl triazines. Specific UV stabilizers include poly[(6-morphilino-s-triazine-2,4-diyl)[2,2,6,6-tetramethyl-4-piperidyl) imino]-hexamethylene [(2,2,6,6-tetramethyl-4-piperidyl)imino], 2-hydroxy-4-octyloxybenzophenone (Uvinul™ 3008); 6-tert-butyl-2-(5-chloro-2H-benzotriazole-2-yl)-4-methylphenyl (Uvinul™ 3026); 2,4-di-tert-butyl-6-(5-chloro-2H-benzotriazole-2-yl)-phenol (Uvinul™ 3027); 2-(2H-benzotriazole-2-yl)-4,6-di-tert-pentylphenol (Uvinul™ 3028); 2-(2H-benzotriazole-2-yl)-4-(1,1,3,3-tetramethylbutyl)-phenol (Uvinul™ 3029); 1,3-bis[(2′-cyano-3′,3′-diphenylacryloyl)oxy]-2,2-bis-{[(2′-cyano-3′,3′-diphenylacryloyl)oxy]methyl}-propane (Uvinul™ 3030); 2-(2H-benzotriazole-2-yl)-4-methylphenol (Uvinul™ 3033); 2-(2H-benzotriazole-2-yl)-4,6-bis(1-methyl-1-phenyethyl) phenol (Uvinul™ 3034); ethyl-2-cyano-3,3-diphenylacrylate (Uvinul™ 3035); (2-ethylhexyl)-2-cyano-3,3-diphenylacrylate (Uvinul™ 3039); N,N′-bisformyl-N,N′-bis (2,2,6,6-tetramethyl-4-piperidinyl)hexamethylenediamine (Uvinul™ 4050H); bis-(2,2,6,6-tetramethyl-4-pipieridyl)-sebacate (Uvinul™ 4077H); bis-(1,2,2,6,6-pentamethyl-4-piperdiyl)-sebacate+methyl-(1,2,2,6,6-pentamethyl-4-piperidyl)-sebacate (Uvinul™ 4092H); or combinations thereof. Other UV stabilizers include Cyasorb 5411, Cyasorb UV-3638, Uvinul 3030, and/or Tinuvin 234.
The compositions described herein may comprise heat stabilizers. Exemplary heat stabilizer additives include, for example, organophosphites such as triphenyl phosphite, tris-(2,6-dimethylphenyl)phosphite, tris-(mixed mono- and di-nonylphenyl)phosphite, or the like; phosphonates such as dimethylbenzene phosphonate or the like; phosphates such as trimethyl phosphate, or the like; or combinations thereof.
The compositions described herein may comprise an antistatic agent. Examples of monomeric antistatic agents may include glycerol monostearate, glycerol distearate, glycerol tristearate, ethoxylated amines, primary, secondary and tertiary amines, ethoxylated alcohols, alkyl sulfates, alkylarylsulfates, alkylphosphates, alkylaminesulfates, alkyl sulfonate salts such as sodium stearyl sulfonate, sodium dodecylbenzenesulfonate or the like, quaternary ammonium salts, quaternary ammonium resins, imidazoline derivatives, sorbitan esters, ethanolamides, betaines, or the like, or combinations comprising at least one of the foregoing monomeric antistatic agents.
Exemplary polymeric antistatic agents may include certain polyesteramides polyether-polyamide (polyetheramide) block copolymers, polyetheresteramide block copolymers, polyetheresters, or polyurethanes, each containing polyalkylene glycol moieties polyalkylene oxide units such as polyethylene glycol, polypropylene glycol, polytetramethylene glycol, and the like. Such polymeric antistatic agents are commercially available, for example PELESTAT™ 6321 (Sanyo) or PEBAX™ MH1657 (Atofina), IRGASTAT™ P18 and P22 (Ciba-Geigy). Other polymeric materials may be used as antistatic agents are inherently conducting polymers such as polyaniline (commercially available as PANIPOL™ EB from Panipol), polypyrrole and polythiophene (commercially available from Bayer), which retain some of their intrinsic conductivity after melt processing at elevated temperatures. Carbon fibers, carbon nanofibers, carbon nanotubes, carbon black, or a combination comprising at least one of the foregoing may be included to render the compositions described herein electrostatically dissipative.
The compositions described herein may comprise a radiation stabilizer, such as a gamma-radiation stabilizer. Exemplary gamma-radiation stabilizers include alkylene polyols such as ethylene glycol, propylene glycol, 1,3-propanediol, 1,2-butanediol, 1,4-butanediol, meso-2,3-butanediol, 1,2-pentanediol, 2,3-pentanediol, 1,4-pentanediol, 1,4-hexandiol, and the like; cycloalkylene polyols such as 1,2-cyclopentanediol, 1,2-cyclohexanediol, and the like; branched alkylenepolyols such as 2,3-dimethyl-2,3-butanediol (pinacol), and the like, as well as alkoxy-substituted cyclic or acyclic alkanes. Unsaturated alkenols are also useful, examples of which include 4-methyl-4-penten-2-ol, 3-methyl-pentene-3-ol, 2-methyl-4-penten-2-ol, 2,4-dimethyl-4-penten-2-ol, and 9 to decen-1-ol, as well as tertiary alcohols that have at least one hydroxy substituted tertiary carbon, for example 2-methyl-2,4-pentanediol (hexylene glycol), 2-phenyl-2-butanol, 3-hydroxy-3-methyl-2-butanone, 2-phenyl-2-butanol, and the like, and cyclic tertiary alcohols such as 1-hydroxy-1-methyl-cyclohexane. Certain hydroxymethyl aromatic compounds that have hydroxy substitution on a saturated carbon attached to an unsaturated carbon in an aromatic ring can also be used. The hydroxy-substituted saturated carbon can be a methylol group (—CH2OH) or it can be a member of a more complex hydrocarbon group such as —CR24HOH or —CR242OH wherein R24 is a complex or a simple hydrocarbon. Specific hydroxy methyl aromatic compounds include benzhydrol, 1,3-benzenedimethanol, benzyl alcohol, 4-benzyloxy benzyl alcohol and benzyl alcohol. 2-Methyl-2,4-pentanediol, polyethylene glycol, and polypropylene glycol are often used for gamma-radiation stabilization.
The term “pigments” means colored particles that are insoluble in the resulting compositions described herein. Exemplary pigments include titanium oxide, carbon black, carbon nanotubes, metal particles, silica, metal oxides, metal sulfides or any other mineral pigment; phthalocyanines, anthraquinones, quinacridones, dioxazines, azo pigments or any other organic pigment, natural pigments (madder, indigo, crimson, cochineal, etc.) and mixtures of pigments. The pigments may represent from 0.05% to 15%, or from about 0.05% to about 15%, by weight relative to the weight of the overall composition. The choice of pigments may depend on the composition of particular fibers being used for a given application.
The term “dye” refers to molecules that are soluble in the compositions described herein and that have the capacity of absorbing part of the visible radiation.
Pigments, dyes or fibers capable of absorbing radiation may be used to ensure the heating of an article based on the compositions described herein when heated using a radiation source such as a laser, or by the Joule effect, by induction or by microwaves. Such heating may allow the use of a process for manufacturing, transforming, or recycling an article made of the compositions described herein.
Suitable fillers for the compositions described herein include: silica, clays, calcium carbonate, carbon black, kaolin, and whiskers. Other possible fillers include, for example, silicates and silica powders such as aluminum silicate (mullite), synthetic calcium silicate, zirconium silicate, fused silica, crystalline silica graphite, natural silica sand, or the like; boron powders such as boron-nitride powder, boron-silicate powders, or the like; oxides such as TiO2, aluminum oxide, magnesium oxide, or the like; calcium sulfate (as its anhydride, dihydrate or trihydrate); calcium carbonates such as chalk, limestone, marble, synthetic precipitated calcium carbonates, or the like; talc, including fibrous, modular, needle shaped, lamellar talc, or the like; wollastonite; surface-treated wollastonite; glass spheres such as hollow and solid glass spheres, silicate spheres, cenospheres, aluminosilicate (armospheres), or the like; kaolin, including hard kaolin, soft kaolin, calcined kaolin, kaolin comprising various coatings known in the art to facilitate compatibility with the polymeric matrix, or the like; single crystal fibers or “whiskers” such as silicon carbide, alumina, boron carbide, iron, nickel, copper, or the like; fibers (including continuous and chopped fibers) such as asbestos, carbon fibers, glass fibers, such as E, A, C, ECR, R, S, D, or NE glasses, or the like; sulfides such as molybdenum sulfide, zinc sulfide or the like; barium compounds such as barium titanate, barium ferrite, barium sulfate, heavy spar, or the like; metals and metal oxides such as particulate or fibrous aluminum, bronze, zinc, copper and nickel or the like; flaked fillers such as glass flakes, flaked silicon carbide, aluminum diboride, aluminum flakes, steel flakes or the like; fibrous fillers, for example short inorganic fibers such as those derived from blends comprising at least one of aluminum silicates, aluminum oxides, magnesium oxides, and calcium sulfate hemihydrate or the like; natural fillers and reinforcements, such as wood flour obtained by pulverizing wood, fibrous products such as cellulose, cotton, sisal, jute, starch, cork flour, lignin, ground nut shells, corn, rice grain husks or the like; organic fillers such as polytetrafluoroethylene; reinforcing organic fibrous fillers formed from organic polymers capable of forming fibers such as poly(ether ketone), polyimide, polybenzoxazole, poly(phenylene sulfide), polyesters, polyethylene, aromatic polyamides, aromatic polyimides, polyetherimides, polytetrafluoroethylene, acrylic resins, poly(vinyl alcohol) or the like; as well as additional fillers and reinforcing agents such as mica, clay, feldspar, flue dust, fillite, quartz, quartzite, perlite, tripoli, diatomaceous earth, carbon black, or the like, or combinations comprising at least one of the foregoing fillers or reinforcing agents. The choice of filler may be influenced by the materials of the fiber, and not all filler may be optimal for all applications.
Plasticizers, lubricants, and mold release agents can be included. Mold release agent (MRA) will allow the material to be removed quickly and effectively. Mold releases can reduce cycle times, defects, and browning of finished product. There is considerable overlap among these types of materials, which may include, for example, phthalic acid esters such as dioctyl-4,5-epoxy-hexahydrophthalate; tris-(octoxycarbonylethyl) isocyanurate; tristearin; di- or polyfunctional aromatic phosphates such as resorcinol tetraphenyl diphosphate (RDP), the bis(diphenyl) phosphate of hydroquinone and the bis(diphenyl) phosphate of bisphenol-A; poly-alpha-olefins; epoxidized soybean oil; silicones, including silicone oils; esters, for example, fatty acid esters such as alkyl stearyl esters, e.g., methyl stearate, stearyl stearate, pentaerythritol tetrastearate (PETS), and the like; combinations of methyl stearate and hydrophilic and hydrophobic nonionic surfactants comprising polyethylene glycol polymers, polypropylene glycol polymers, poly(ethylene glycol-co-propylene glycol) copolymers, or a combination comprising at least one of the foregoing glycol polymers, i.e., methyl stearate and polyethylene-polypropylene glycol copolymer in a suitable solvent; waxes such as beeswax, montan wax, paraffin wax, or the like.
Various types of flame retardants can be utilized as additives. In one embodiment, the flame retardant additives include, for example, flame retardant salts such as alkali metal salts of perfluorinated C1-C16 alkyl sulfonates such as potassium perfluorobutane sulfonate (Rimar salt), potassium perfluoroctane sulfonate, tetraethylammonium perfluorohexane sulfonate, potassium diphenylsulfone sulfonate (KSS), and the like, sodium benzene sulfonate, sodium toluene sulfonate (NATS) and the like; and salts formed by reacting for example an alkali metal or alkaline earth metal (for example lithium, sodium, potassium, magnesium, calcium and barium salts) and an inorganic acid complex salt, for example, an oxo-anion, such as alkali metal and alkaline-earth metal salts of carbonic acid, such as Na2CO3, K2CO3, MgCO3, CaCO3, and BaCO3 or fluoro-anion complex such as Li3AlF6, BaSiF6, KBF4, K3AlF6, KAlF4, K2SiF6, and/or Na3AlF6 or the like. Rimar salt and KSS and NATS, alone or in combination with other flame retardants, are particularly useful in the compositions disclosed herein. In certain embodiments, the flame retardant does not contain bromine or chlorine.
The flame retardant additives may include organic compounds that include phosphorus, bromine, and/or chlorine. In certain embodiments, the flame retardant is not a bromine or chlorine containing composition. Non-brominated and non-chlorinated phosphorus-containing flame retardants can include, for example, organic phosphates and organic compounds containing phosphorus-nitrogen bonds. Exemplary di- or polyfunctional aromatic phosphorus-containing compounds include resorcinol tetraphenyl diphosphate (RDP), the bis(diphenyl) phosphate of hydroquinone and the bis(diphenyl) phosphate of bisphenol-A, respectively, their oligomeric and polymeric counterparts, and the like. Other exemplary phosphorus-containing flame retardant additives include phosphonitrilic chloride, phosphorus ester amides, phosphoric acid amides, phosphonic acid amides, phosphinic acid amides, tris(aziridinyl) phosphine oxide, polyorganophosphazenes, and polyorganophosphonates.
Some suitable polymeric or oligomeric flame retardants include: 2,2-bis-(3,5-dichlorophenyl)-propane; bis-(2-chlorophenyl)-methane; bis(2,6-dibromophenyl)-methane; 1,1-bis-(4-iodophenyl)-ethane; 1,2-bis-(2,6-dichlorophenyl)-ethane; 1,1-bis-(2-chloro-4-iodophenyl)ethane; 1,1-bis-(2-chloro-4-methylphenyl)-ethane; 1,1-bis-(3,5-dichlorophenyl)-ethane; 2,2-bis-(3-phenyl-4-bromophenyl)-ethane; 2,6-bis-(4,6-dichloronaphthyl)-propane; 2,2-bis-(2,6-dichlorophenyl)-pentane; 2,2-bis-(3,5-dibromophenyl)-hexane; bis-(4-chlorophenyl)-phenyl-methane; bis-(3,5-dichlorophenyl)-cyclohexylmethane; bis-(3-nitro-4-bromophenyl)-methane; bis-(4-hydroxy-2,6-dichloro-3-methoxyphenyl)-methane; 2,2-bis-(3,5-dichloro-4-hydroxyphenyl)-propane; and 2,2-bis-(3-bromo-4-hydroxyphenyl)-propane. Other flame retardants include: 1,3-dichlorobenzene, 1,4-dibromobenzene, 1,3-dichloro-4-hydroxybenzene, and biphenyls such as 2,2′-dichlorobiphenyl, polybrominated 1,4-diphenoxybenzene, 2,4′-dibromobiphenyl, and 2,4′-dichlorobiphenyl as well as decabromo diphenyl oxide, and the like.
The flame retardant optionally is a non-halogen based metal salt, e.g., of a monomeric or polymeric aromatic sulfonate or mixture thereof. The metal salt is, for example, an alkali metal or alkali earth metal salt or mixed metal salt. The metals of these groups include sodium, lithium, potassium, rubidium, cesium, beryllium, magnesium, calcium, strontium, francium and barium. Examples of flame retardants include cesium benzenesulfonate and cesium p-toluenesulfonate. See e.g., U.S. Pat. No. 3,933,734, EP 2103654, and US2010/0069543A1, the disclosures of which are incorporated herein by reference in their entirety.
Another useful class of flame retardant is the class of cyclic siloxanes having the general formula [(R)2SiO]y wherein R is a monovalent hydrocarbon or fluorinated hydrocarbon having from 1 to 18 carbon atoms and y is a number from 3 to 12. Examples of fluorinated hydrocarbon include, but are not limited to, 3-fluoropropyl, 3,3,3-trifluoropropyl, 5,5,5,4,4,3,3-heptafluoropentyl, fluorophenyl, difluorophenyl and trifluorotolyl. Examples of suitable cyclic siloxanes include, but are not limited to, octamethylcyclotetrasiloxane, 1,2,3,4-tetramethyl-1,2,3,4-tetravinylcyclotetrasiloxane, 1,2,3,4-tetramethyl-1,2,3,4-tetraphenylcyclotetrasiloxane, octaethylcyclotetrasiloxane, octapropylcyclotetrasiloxane, octabutylcyclotetrasiloxane, decamethylcyclopentasiloxane, dodecamethylcyclohexasiloxane, tetradecamethylcycloheptasiloxane, hexadecamethylcyclooctasiloxane, eicosamethylcyclodecasiloxane, octaphenylcyclotetrasiloxane, and the like. A particularly useful cyclic siloxane is octaphenylcyclotetrasiloxane.
Exemplary antioxidant additives include organophosphites such as tris(nonyl phenyl)phosphite, tris(2,4-di-t-butylphenyl)phosphite (“IRGAFOS 168” or “1-168”), bis(2,4-di-t-butylphenyl)pentaerythritol diphosphite, distearyl pentaerythritol diphosphite or the like; alkylated monophenols or polyphenols; alkylated reaction products of polyphenols with dienes, such as tetrakis[methylene(3,5-di-tert-butyl-4-hydroxyhydrocinnamate)] methane, or the like; butylated reaction products of para-cresol or dicyclopentadiene; alkylated hydroquinones; hydroxylated thiodiphenyl ethers; alkylidene-bisphenols; benzyl compounds; esters of beta-(3,5-di-tert-butyl-4-hydroxyphenyl)-propionic acid with monohydric or polyhydric alcohols; esters of beta-(5-tert-butyl-4-hydroxy-3-methylphenyl)-propionic acid with monohydric or polyhydric alcohols; esters of thioalkyl or thioaryl compounds such as distearylthiopropionate, dilaurylthiopropionate, ditridecylthiodipropionate, octadecyl-3-(3,5-di-tert-butyl-4-hydroxyphenyl)propionate, pentaerythrityl-tetrakis[3-(3,5-di-tert-butyl-4-hydroxyphenyl)propionate or the like; amides of beta-(3,5-di-tert-butyl-4-hydroxyphenyl)-propionic acid or the like, or combinations comprising at least one of the foregoing antioxidants.
As described, the disclosed compositions may include PTFE, which has anti-drop properties. The disclosed compositions may include additional anti-drip agent, depending on the user's needs.
Further Aspects
The following aspects are illustrative only, and do not serve to limit the scope of the present disclosure.
Aspect 1. A composite fiber, comprising: a thermoplastic matrix polymer, the composite fiber having a diameter in the range of from about 2 micrometers to about 4 millimeters, and the composite fiber comprising a plurality of fibrillated reinforcement material regions disposed within the thermoplastic matrix polymer, and the melting temperature or Tg of the thermoplastic matrix material, whichever is higher, being below the melting temperature or Tg, whichever is lower, of the fibrillated reinforcement material.
The thermoplastic matrix polymer, the plurality of fibrillated reinforcement material regions, or both, may, in some embodiments, be oriented. By “oriented” is meant an element sharing an alignment (or nearly sharing an alignment) with another element. As one example, an element (e.g., a fibril) may have a major axis that is within about, e.g., 20 degrees of parallel to the corresponding major axis of another fibril. As another example, a region may comprise a plurality of oriented fibrils, the fibrils all having major axes that are aligned to within about 20 degrees of a particular line in space. It should be understood that in some embodiments, the fibrils are not oriented relative to one another and may, in some embodiments, be essentially randomly oriented.
A fiber may have a diameter in the range of from about 2 micrometers to about 4 mm, e.g., from about 2 micrometers to about 200 micrometers, from about 0.1 mm to about 4 mm, and all intermediate values. The length of a fiber according to the present disclosure may be according to the needs of the user. A fiber may have a length of, e.g., 1-100 mm and all intermediate values. A fiber may have a diameter in the range of about 2 to about 200 micrometers, depending on the user's needs.
It should be understood that a fiber may be circular in cross-section, but may also be rectangular, ovoid, polygonal, or otherwise shaped. Rectangular fibers may be termed “tapes,” in some embodiments. Tapes according to the present disclosure may have a cross-sectional aspect ratio in the range of from about 1 to about 100, e.g., about 2 to about 90, about 3 to about 80, about 5 to about 75, about 10 to about 65, about 20 to about 50, about 30 to about 40, or even about 35. Aspect ratios of 1, 2, 3, 4, 5, 6, 7, 8, 9, and 10 are all considered suitable.
Aspect 2. The composite fiber of aspect 1, wherein the thermoplastic matrix polymer comprises a polyalkylene terephthalate, a polyalkylene napthalate, poly(phenylene oxide), polycarbonate, poly(styrene), poly(amide), a polyolefin, or any combination thereof.
Aspect 3. The composite fiber of aspect 2, wherein the polyalkylene terephthalate comprises polybutylene terephthalate.
Aspect 4. The composite fiber of any of aspects 1-3, wherein the plurality of fibrillated reinforcement material regions are present at, e.g., about 0.01 to about 15 wt % of the fiber (e.g., from about 0.25 wt % to about 5 wt %), or from about 1 to about 14 wt % or from about 2 to about 13 wt %, or from about 3 to about 12 wt %, or from about 4 to about 11 wt %, or from about 5 to about 10 wt %, or from about 6 to about 9 wt % or from about 7 to about 8 wt %. The reinforcement material may be present in fibril form, but may also be present in other forms, e.g., strands, aggregates, agglomerates, and the like.
Aspect 5. The composite fiber of aspect 4, wherein the plurality of fibrillated reinforcement material regions are present at from about 0.25 wt % to about 5 wt % as measured against the weight of the composite fiber.
Aspect 6. The composite fiber of any of aspects 1-5, wherein the reinforcement material comprises a polyolefin, a fluoropolymer, or any combination thereof.
Aspect 7. The composite fiber of aspect 6, wherein the fluoropolymer comprises polytetrafluoroethylene.
Aspect 8. The composite fiber of any of aspects 1-7, wherein the plurality of fibrillated reinforcement material regions comprises a first group of fibrillated reinforcement material regions having major axes that are oriented to within about 20 degrees of one another and a second group of fibrillated reinforcement material regions having major axes that are oriented to within about 20 degrees of one another.
Aspect. 9. The composite fiber of aspect 8, wherein the first group of fibrillated reinforcement material regions having major axes defines a first average major axis, wherein the second group of fibrillated reinforcement material regions having major axes defines a second average major axis, and wherein the first and second average major axes differ from one another by at least about 10 degrees.
Aspect 10. The composite fiber of any of aspects 1-9, wherein the fiber has a diameter in the range of from about 2 to about 200 micrometers.
Aspect 11. The composite fiber of any of aspects 1-9, wherein the fiber has a diameter in the range of from about 0.3 to about 4 mm.
Aspect 12. The composite fiber of any of aspects 1-13, wherein the fiber has a modulus in the range of from about 0.5 to about 6 GPa. A fiber according to the present disclosure may have a modulus in the range of at least about 0.5 GPa, e.g., about 0.6, 0.7, 0.8, 0.9, 1.0, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6, 1.7, 1.8 or even about 1.9, 2, 2.5, 3, 3.5, or even about 4 GPa. Modulus may be measured according to ASTM D3822.
Aspect 13. The composite fiber of aspect 12, wherein the fiber has a modulus in the range of from about 1 to about 4 GPa.
Aspect 14. An article, the article comprising a plurality of composite fibers according to any of aspects 1-13, the article being characterized as a woven article, a non-woven article, or any combination thereof.
Aspect 15. The article of aspect 14, wherein the article comprises a carpet.
Aspect 16. A method, comprising: using a composite fiber according to any of aspects 1-13 in additively manufacturing at least a portion of an article.
Aspect 17. The method of aspect 19, wherein the additively manufacturing comprises fused filament fabrication.
The methods include essentially any additive-manufacturing process that uses a fiber or filament as a build material, e.g., FFF. In these techniques, a single filament or a threaded spools of a thermoplastic filament is introduced into a heating chamber. The thermoplastic is melted and then exerted through a nozzle (the size and shape of which will vary according to the user's needs and the application) onto a substrate, where the exerted thermoplastic solidifies. The nozzle may be moveable in one or more of the x, y, and z axes, and may also be rotatable. Similarly, the substrate (sometimes termed the “build surface” or platform) may also be moveable and/or rotatable. The relative motion of the nozzle and substrate (as well as the deposition of the thermoplastic) is suitably controlled by software. Additional background on these techniques may be found in U.S. Pat. No. 5,121,329, incorporated herein by reference.
Although additive manufacturing techniques are known to those in the art, the present disclosure will provide some further background on such techniques for convenience.
Suitable additive manufacturing processes include other processes that use filaments, pellets, and the like, and suitable processes will be known to those of ordinary skill in the art; the disclosed compositions may be used in virtually any additive manufacturing process that uses filament or even pellet build material.
In exemplary additive manufacturing techniques, a plurality of layers is formed in a preset pattern by an additive manufacturing process. “Plurality” as used in the context of additive manufacturing includes 2 or more layers. The maximum number of layers can vary greatly, determined, for example, by considerations such as the size of the article being manufactured, the technique used, the capabilities of the equipment used, and the level of detail desired in the final article. For example, 20 to 100,000 layers can be formed, or 50 to 50,000 layers can be formed.
As used herein, “layer” is a term of convenience that includes any shape, regular or irregular, having at least a predetermined thickness. In some embodiments, the size and configuration of two dimensions are predetermined, and on some embodiments, the size and shape of all three dimensions of the layer is predetermined. The thickness of each layer can vary widely depending on the additive manufacturing method. In some embodiments the thickness of each layer as formed differs from a previous or subsequent layer. In some embodiments, the thickness of each layer is the same. In some embodiments, the thickness of each layer as formed is 0.5 millimeters (mm) to 5 mm. In other embodiments, the article is made from a monofilament additive manufacturing process. For example, the monofilament may comprise an thermoplastic polymer with a diameter of from 0.1 to 5.0 mm.
The preset pattern can be determined from a three-dimensional digital representation of the desired article as is known in the art and described in further detail below.
Any additive manufacturing process can be used, provided that the process allows formation of at least one layer of a thermoplastic material that is fusible to the next adjacent layer. The plurality of layers in the predetermined pattern are fused to provide the article. Any method effective to fuse the plurality of layers during additive manufacturing can be used. In some embodiments, the fusing occurs during formation of each of the layers. In some embodiments the fusing occurs while subsequent layers are formed, or after all layers are formed.
In some embodiments, an additive manufacturing technique known generally as material extrusion can be used. In material extrusion, an article can be formed by dispensing a material (“the build material”, which may be rendered flowable) in a layer-by-layer manner and fusing the layers. “Fusing” as used herein includes the chemical or physical interlocking of the individual layers, and provides a “build structure.” Flowable build material can be rendered flowable by dissolving or suspending the material in a solvent. In other embodiments, the flowable material can be rendered flowable by melting. In other embodiments, a flowable prepolymer composition that can be crosslinked or otherwise reacted to form a solid can be used. Fusing can be by removal of the solvent, cooling of the melted material, or reaction of the prepolymer composition.
In particular, an article can be formed from a three-dimensional digital representation of the article by depositing the flowable material as one or more roads on a substrate in an x-y plane to form the layer. The position of the dispenser (e.g., a nozzle) relative to the substrate is then incremented along a z-axis (perpendicular to the x-y plane), and the process is then repeated to form an article from the digital representation. The dispensed material is thus also referred to as a “modeling material” as well as a “build material.” In some embodiments a support material as is known in the art can optionally be used to form a support structure. In these embodiments, the build material and the support material can be selectively dispensed during manufacture of the article to provide the article and a support structure. The support material can be present in the form of a support structure, for example, a scaffolding that can be mechanically removed or washed away when the layering process is completed to the desired degree. The dispenser may be movable in one, two, or three dimensions, and may also be rotatable. Similarly, the substrate may also be moveable in one, two, or three dimensions, and may also be rotatable.
Systems for material extrusion are known. One exemplary material extrusion additive manufacturing system includes a build chamber and a supply source for the thermoplastic material. The build chamber may include a build platform, a gantry, and a dispenser for dispensing the thermoplastic material, for example an extrusion head.
The build platform is a platform on which the article is built, and desirably moves along a vertical z-axis based on signals provided from a computer-operated controller. The gantry is a guide rail system that can be configured to move the dispenser in a horizontal x-y plane within the build chamber, for example based on signals provided from a controller. The horizontal x-y plane is a plane defined by an x-axis and a y-axis where the x-axis, the y-axis, and the z-axis are orthogonal to each other.
Alternatively, the platform can be configured to move in the horizontal x-y plane and the extrusion head can be configured to move along the z-axis. Other similar arrangements can also be used such that one or both of the platform and extrusion head are moveable relative to each other. The build platform can be isolated or exposed to atmospheric conditions. The distance between the platform and head may be adjustable, as may be the orientation of the head and platform relative to one another. It should be understood that the platform may be heated, cooled or maintained at ambient temperature, depending on the user's needs.
In some embodiments, both the build structure and the support structure of the article formed can include a fused expandable layer. In other embodiments, the build structured includes a fused expandable layer and the support material does not include an expandable layer. In still other embodiments, the build structure does not include an expandable layer and the support structure does include a fused expandable layer. In those embodiments where the support structure includes an expandable layer, the lower density of the expanded layer can allow for the support material to be easily or more easily broken off than the non-expanded layer, and re-used or discarded.
In some embodiments, the support structure can be made purposely breakable, to facilitate breakage where desired. For example, the support material can have an inherently lower tensile or impact strength than the build material. In other embodiments, the shape of the support structure can be designed to increase the breakability of the support structure relative to the build structure.
For example, in some embodiments, the build material can be made from a round print nozzle or round extrusion head. A round shape as used herein means any cross-sectional shape that is enclosed by one or more curved lines. A round shape includes circles, ovals, ellipses, and the like, as well as shapes having an irregular cross-sectional shape. Three-dimensional articles formed from round shaped layers of build material can possess strong structural strength. In other embodiments, the support material for the articles can be made from a non-round print nozzle or non-round extrusion head. A non-round shape means any cross-sectional shape enclosed by at least one straight line, optionally together with one or more curved lines. A non-round shape can include squares, rectangles, ribbons, horseshoes, stars, T head shapes, X shapes, chevrons, and the like. These non-round shapes can render the support material weaker, brittle and with lower strength than round shaped build material.
The above material extrusion techniques include techniques such as fused deposition modeling and fused filament fabrication as well as others as described in ASTM F2792-12a. In fused material extrusion techniques, an article can be produced by heating a thermoplastic material to a flowable state that can be deposited to form a layer. The layer can have a predetermined shape in the x-y axis and a predetermined thickness in the z-axis. The flowable material can be deposited as roads as described above, or through a die to provide a specific profile. The layer cools and solidifies as it is deposited. A subsequent layer of melted thermoplastic material fuses to the previously deposited layer, and solidifies upon a drop in temperature. Extrusion of multiple subsequent layers builds the desired shape. In some embodiments at least one layer of an article is formed by melt deposition, and in other embodiments, more than 10, or more than 20, or more than 50 of the layers of an article are formed by melt deposition, up to and including all of the layers of an article being formed by melt deposition.
In some embodiments the thermoplastic polymer is supplied in a melted form to the dispenser. The dispenser can be configured as an extrusion head. The extrusion head can deposit the thermoplastic composition as an extruded material strand to build the article. Examples of average diameters for the extruded material strands can be from 1.27 millimeters (0.050 inches) to 3.0 millimeters (0.120 inches).
So-called large format additive manufacturing (LFAM) systems are also within the scope of the present disclosure, as such systems may utilize pellets of polymeric material according to the present disclosure to form parts.
In a LFAM system, a comparatively large extruder converts feed material to a molten form that is then deposited on a table. A LFAM system may comprise a frame or gantry that in turn includes a print head that is moveable in the x, y and/or z directions. Alternately, the print head may be stationary and the part (or the part support) is moveable in the x, y and/or z axes.
The print head may have a feed material in the form of pellets and/or filament and a deposition nozzle. The feed material may be stored in a hopper (for pellets) or other suitable storage vessel nearby to the print head or supplied from a filament spool.
An LFAM apparatus may comprise a nozzle for extruding a material. The polymeric material is heated and extruded through the nozzle and directly deposited on a building surface, which surface may be a moveable (or stationary) platform or may also be previously-deposited material. A heat source may be positioned on or in connection with the nozzle to heat the material to a desired temperature and/or flow rate. The bed may be heated or at room temperature.
In one non-limiting embodiment, a nozzle may be configured to extrude molten polymeric material (from melted pellets) at about 1 to about 50 kg/hr through a nozzle onto a print bed. The size of a print bed may vary depending on the needs of the user and can be room-sized. As one example, a print bed may be sized at about 400×200×86 inches. A LFAM apparatus may have one, two, or more heated zones.
One exemplary LFAM method is known as big area additive manufacturing (BAAM; e.g., Cincinnati Incorporated, http://www.e-ci.com/baam/). LFAM systems may utilize filaments, pellets, or both as feed materials. Exemplary description of a BAAM process may be found in, e.g., US2015/0183159, US2015/0183138, US2015/0183164, and U.S. Pat. No. 8,951,303, all of which are incorporated herein by reference in their entireties. The disclosed compositions are also suitable for droplet-based additive manufacturing systems, e.g., the Freeformer™ system by Arburg (https://www.arburg.com/us/us/products-and-services/additive-manufacturing/).
Additive manufacturing systems may use materials in filament form as the build material. Such a system may, as described, effect relative motion between the filament (and/or molten polycarbonate) and a substrate. By applying the molten material according to a pre-set schedule of locations, the system may construct an article in a layer-by-layer fashion, as is familiar to those of ordinary skill in the art. As described elsewhere herein, the build material may also be in pellet form.
The disclosed technology may include methods of forming a three-dimensional objects. These methods may include depositing a layer of thermoplastic material (e.g., a material according to the disclosed compositions) through a nozzle onto a platform to form a deposited layer. A user may then deposit subsequent layers onto the first deposited layer and repeat the preceding steps to form the three-dimensional object. A related apparatus for forming such three-dimensional objects may comprise a platform configured to support the three-dimensional object; an extrusion head arranged relative to the platform and configured to deposit a thermoplastic material in a preset pattern to form a layer of the three-dimensional object; and a controller configured to control the position of the extrusion head and the energy source relative to the platform. The vertical distance between the platform and the extrusion head is adjustable; the extrusion head may be moveable in one, two, or three dimensions and may also be rotatable.
The foregoing description is illustrative only and does not necessarily limit the scope of the present disclosure or the appended claims.
In a particular embodiment, the thermoplastic matrix polymer comprises >90.0 wt % of a polyalkylene terephthalate, with regard to the total weight of the thermoplastic matrix polymer. Preferably, the thermoplastic matrix polymer comprises >95.0 wt %, more preferably >98.0 wt %, of a polyalkylene terephthalate. Particularly preferably, the thermoplastic matrix polymer comprises a polyalkylene terephthalate as the only thermoplastic material. For example, the thermoplastic matrix polymer may consist of a polyalkylene terephthalate and optional additives.
The polyalkylene terephthalate may for example be a polyalkylene terephthalate selected from a polyethylene terephthalate, polybutylene terephthalate, polycyclohexylmethylene terephthalate. Preferably, the polyalkylene terephthalate is polybutylene terephthalate.
Preferably, the thermoplastic matrix polymer comprises >90.0 wt % of a polyalkylene terephthalate wherein the polyalkylene terephthalate is polybutylene terephthalate, with regard to the total weight of the thermoplastic matrix polymer. Preferably, the thermoplastic matrix polymer comprises >95.0 wt %, more preferably >98.0 wt %, of a polyalkylene terephthalate wherein the polyalkylene terephthalate is polybutylene terephthalate. Particularly preferably, the thermoplastic matrix polymer comprises a polyalkylene terephthalate as the only thermoplastic material, wherein the polyalkylene terephthalate is polybutylene terephthalate. For example, the thermoplastic matrix polymer may consist of a polyalkylene terephthalate and optional additives, wherein the polyalkylene terephthalate is polybutylene terephthalate.
In particular, the poly(butylene terephthalate) may be a homopolymer comprising polymeric units derived from 1,4-butanediol and terephthalic acid or a diester thereof, such as dimethyl terephthalate.
The polymeric units derived from 1,4-butanediol and terephthalic acid or a diester thereof, such as dimethyl terephthalate may for example be polymeric units according to the formula:
Alternatively, the poly(butylene terephthalate) may be a copolymer comprising ≥90 wt % with regard to the total weight of the poly(butylene terephthalate) of polymeric units derived from 1,4-butanediol and terephthalic acid or a diester thereof, such as dimethyl terephthalate.
In the case that the poly(butylene terephthalate) is a copolymer, it may for example comprise ≤10.0 wt % of polymer units derived from further monomers. Suitable further monomers may for example be selected from isophthalic acid, naphthalene dicarboxylic acid, ethanediol, 1,3-propanediol, cyclohexanedimethanol, or combinations thereof.
For example, the poly(butylene terephthalate) may comprise ≤10.0 wt % of polymeric units derived from further monomers, preferably ≤5.0 wt %, such as ≥0.5 and ≤5.0 wt %, with regard to the total weight of the poly(butylene terephthalate).
In a particular embodiment, the poly(butylene terephthalate) comprises polymeric units derived from 1,4-butanediol and terephthalic acid or dimethyl terephthalate, and further ≥0.5 and ≤5.0 wt % polymeric units derived from isophthalic acid.
It is preferred that the poly(butylene terephthalate) has an intrinsic viscosity of ≥0.50 and ≤2.00 dl/g, for example ≥0.70 and ≤1.30 dl/g, as determined in accordance with ASTM D2857-95 (2007).
The invention further also relates to a composite fiber comprising a thermoplastic matrix polymer, the composite fiber having a diameter in the range of from about 2 micrometers to about 4 millimeters, and the composite fiber comprising a plurality of fibrillated reinforcement material regions disposed within the thermoplastic matrix polymer, and the melting temperature or Tg of the thermoplastic matrix polymer, whichever is higher, being below the melting temperature or Tg, whichever is lower, of the fibrillated reinforcement material, wherein the thermoplastic matrix polymer is a polybutylene terephthalate.
Further, the invention also relates a composite fiber comprising a thermoplastic matrix polymer, the composite fiber having a diameter in the range of from about 2 micrometers to about 4 millimeters, and the composite fiber comprising a plurality of fibrillated reinforcement material regions disposed within the thermoplastic matrix polymer, and the melting temperature or Tg of the thermoplastic matrix polymer, whichever is higher, being below the melting temperature or Tg, whichever is lower, of the fibrillated reinforcement material, wherein the thermoplastic matrix polymer is a polybutylene terephthalate, wherein the fibrillated reinforcement material is polytetrafluorethylene. In the context of the present invention, Tg may be understood as determined in accordance with ISO 11357-2 (2013). Particularly, the invention also relates to a composite fiber comprising a thermoplastic matrix polymer, the composite fiber having a diameter in the range of from about 2 micrometers to about 4 millimeters, and the composite fiber comprising a plurality of fibrillated reinforcement material regions disposed within the thermoplastic matrix polymer, wherein the thermoplastic matrix polymer is a polybutylene terephthalate, and wherein the fibrillated reinforcement material is polytetrafluorethylene.
In particular, the invention also encompasses an embodiment relating to a composite fiber comprising a thermoplastic matrix polymer, the composite fiber having a diameter in the range of from about 2 micrometers to about 4 millimeters, and the composite fiber comprising a plurality of fibrillated reinforcement material regions disposed within the thermoplastic matrix polymer, and the melting temperature or Tg of the thermoplastic matrix polymer, whichever is higher, being below the melting temperature or Tg, whichever is lower, of the fibrillated reinforcement material, wherein the thermoplastic matrix polymer is a polybutylene terephthalate, wherein the fibrillated reinforcement material is polytetrafluorethylene, wherein the composite fiber comprises 0.01 wt % to 15.0 wt %, preferably 0.25 wt % to 5.0 wt %, more preferably 0.50 wt % to 2.50 wt %, of the fibrillated reinforcement material, as measured against the total weight of the composite fiber.
Even further particularly, the invention also encompasses an embodiment relating to a composite fiber comprising a thermoplastic matrix polymer, the composite fiber having a diameter in the range of from about 2 micrometers to about 4 millimeters, and the composite fiber comprising a plurality of fibrillated reinforcement material regions disposed within the thermoplastic matrix polymer, and the melting temperature or Tg of the thermoplastic matrix polymer, whichever is higher, being below the melting temperature or Tg, whichever is lower, of the fibrillated reinforcement material, wherein the thermoplastic matrix polymer is a polybutylene terephthalate having an intrinsic viscosity of ≥0.50 and ≤2.00 dl/g, for example ≥0.70 and ≤1.30 dl/g, as determined in accordance with ASTM D2857-95 (2007), wherein the fibrillated reinforcement material is polytetrafluorethylene, wherein the composite fiber comprises 0.01 wt % to 15.0 wt %, preferably 0.25 wt % to 5.0 wt %, more preferably 0.50 wt % to 2.50 wt %, of the fibrillated reinforcement material, as measured against the total weight of the composite fiber.
In the context of the present invention, polytetrafluorethylene is also referred to as PTFE.
The fibrillated reinforcement material may be present in the composite fiber of the present invention in the form of a fibrillated reinforcement material encapsulated with a further thermoplastic material. For example, the fibrillated reinforcement material may be a polytetrafluorethylene encapsulated with a styrene-acrylonitrile copolymer. Such polytetrafluorethylene encapsulated with a styrene-acrylonitrile copolymer may also be referred to as TSAN. For example, the fibrillated reinforcement material may be a TSAN wherein the TSAN comprises 10-90 wt % of polytetrafluorethylene and 10-90 wt % of styrene-acrylonitrile copolymer, with regard to the total weight of the TSAN, preferably 20-80 wt % of polytetrafluorethylene and 20-80 wt % of styrene-acrylonitrile copolymer, more preferably 30-70 wt % of polytetrafluorethylene and 30-70 wt % of styrene-acrylonitrile copolymer, even more preferably 40-60 wt % of polytetrafluorethylene and 40-60 wt % of styrene-acrylonitrile copolymer.
Such fibrillated reinforcement material is understood to contribute to the degree of dispersion of the regions of fibrillated material in the thermoplastic matrix polymer, and thereby to contribute to the improvement of the mechanical properties and the melt processing properties of the material that forms the composite fiber.
The invention in a certain embodiment relates to a composite fiber having a diameter in the range of 2.0 μm to 4.0 mm, wherein the fiber comprises a thermoplastic matrix polymer, and a plurality of fibrillated reinforcement material regions disposed within the thermoplastic matrix polymer, wherein the melting temperature of the thermoplastic matrix polymer is lower than the melting temperature of the fibrillated reinforcement material.
For example, the thermoplastic matrix polymer is selected from a polyalkylene terephthalate, preferably a polyethylene terephthalate or a polybutylene terephthalate, a polyalkylene naphthalate, preferably a polyethylene naphthalate, a polyphenylene oxide, a polycarbonate, a polystyrene, a polyamide, a polyolefin, or a combination thereof. Preferably, the thermoplastic matrix polymer is selected from a polyalkylene terephthalate, preferably a polyethylene terephthalate or a polybutylene terephthalate, a polyalkylene naphthalate, preferably a polyethylene naphthalate, a polyphenylene oxide, a polycarbonate, a polystyrene, a polyamide, or a polyolefin.
Particularly, it is preferred that the thermoplastic matrix polymer is polybutylene terephthalate. Further particularly, it is preferred that the fibrillated reinforcement material is a thermoplastic material, preferably an ultra-high molecular weight polyethylene (UHMWPE) or a polytetrafluorethylene (PTFE). It is particularly preferred that the fibrillated reinforcement material is a thermoplastic material encapsulated in a further thermoplastic material. It is preferred that the melting temperature of the further thermoplastic material is lower than the melting temperature of the thermoplastic material.
Particularly, it is preferred that the melting temperature of the further thermoplastic material is <20° C., more preferably <10° C., above the melting temperature of the thermoplastic matrix polymer. Even more particularly, it is preferred that the melting temperature of the further thermoplastic material is <20° C., more preferably <10° C., above the melting temperature of the thermoplastic matrix polymer, and the melting temperature of the fibrillated reinforcement material is >30° C., preferably >50° C., even more preferably >70° C. above the melting temperature of the thermoplastic matrix polymer.
In the context of the present invention, a UHMWPE is to be understood to be a polyethylene having a weight average molecular weight (Mw) of >1000 kg/mol, preferably >1000 and <10000 kg/mol, as determined in accordance with ISO 11542-1 (2001).
In the context of the present invention, the melting temperature may be understood as the peak melt temperature Tp,m as determined in accordance with ISO 11357-3 (2011), first heating run.
The invention will now be elucidated by the following non-limiting examples.
The following materials were used in the experiments according to the present invention:
The PFTE has a melting temperature of 326° C. The SAN has a melting temperature of 230° C. Both PBT1 and PBT2 have a melting temperature of 223° C.
Formulations of the above materials were compounded according to the following table:
Wherein the numbers indicate the parts by weight of each of the materials used in the tested formulations. Example 1 was included for comparative purposes.
Compounding was performed by extruding a dry blend of the formulations of the above table using a 25 mm twin screw extruder. The temperature of extrusion was 250° C. (melt temperature), with a screw rpm of 200. Prior to extrusion the mixture was dried at 120° C. for 4 hours. After compounding, the obtained material was cooled and shaped to pellets.
Of the compounded formulations according to examples 1-9, a number of parameters were tested as presented in the table below.
Wherein:
Of the material of each of the examples 1-9, fibers were spun by feeding pellets into a capillary rheometer (Gottfert, RG50) having a 15 mm diameter channel. The material was them pushed out of a die of diameter 0.3-2 mm (depending on the final diameter of fiber required) and length 10-30 mm at a shear rate of 100 s−1 and temperature of 250 C. The melt coming out of the die was then spun using a haul-off unit (Gottfert) at speeds from 10 mm/s-2000 mm/s. Prior to spinning the mixture was dried at 120 C for 4 hours.
Further, material of each of the examples 1-9 were converted to tapes by feeding pellets into a capillary rheometer (Gottfert, RG50) having a 15 mm diameter channel. The material was them pushed out of a die having a rectangular cross section (0.5*1 mm) and a shear rate of 100 s−1 at 250 C. The melt coming out of the die had similar cross-section to that of the die. Prior to extrusion the mixture was dried at 120 C for 4 hours.
Certain material properties were further determined using the tapes and fibers prepared as above. Results thereof are presented in the table here below.
Wherein μ is the coefficient of friction as determined using a Favimat+friction testing device, wherein the lower clamp is a friction clamp, using as conditions a starting gauge length of 5 mm, test speed of 20 mm/min, elongation of 300%, and a pretention weight of 1.0 g.
During downward movement of the friction clamp, the force F is measured that is required to displace a calibrated pretension weight that applies a pulling force Fp to the testing device in the regime of 10-90% of the total elongation of the fiber. The coefficient of friction is calculated using the Euler-Eytelwein equation:
Wherein α is the wrapping angle of the fiber in the friction device.
The above presented examples demonstrate fibers according to the invention to have improved fiber processability properties and improved mechanical properties, thereby rendering them suitable for use in applications where high durability of the fibers and good process economics in the fiber production stage are critical requirements.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/EP2017/083975 | 12/21/2017 | WO | 00 |
| Number | Date | Country | |
|---|---|---|---|
| 62439243 | Dec 2016 | US |
