US20200024795A1 - Fiber-reinforced composites, methods therefor, and articles comprising the same - Google Patents

Fiber-reinforced composites, methods therefor, and articles comprising the same Download PDF

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US20200024795A1
US20200024795A1 US16/495,890 US201816495890A US2020024795A1 US 20200024795 A1 US20200024795 A1 US 20200024795A1 US 201816495890 A US201816495890 A US 201816495890A US 2020024795 A1 US2020024795 A1 US 2020024795A1
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article
discontinuous
composite
continuous fibers
fibers
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Anvesh Gurijala
Michael Segal
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Boston Materials Inc
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Boston Materials Inc
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    • D—TEXTILES; PAPER
    • D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M10/00—Physical treatment of fibres, threads, yarns, fabrics, or fibrous goods made from such materials, e.g. ultrasonic, corona discharge, irradiation, electric currents, or magnetic fields; Physical treatment combined with treatment with chemical compounds or elements
    • D06M10/04—Physical treatment combined with treatment with chemical compounds or elements
    • D06M10/06—Inorganic compounds or elements
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    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
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    • B29C70/025—Combinations of fibrous reinforcement and non-fibrous material with particular filler
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
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    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
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    • B29C70/14—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of short length, e.g. in the form of a mat oriented
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    • B29C70/887—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced locally reinforced, e.g. by fillers
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    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/06—Reinforcing macromolecular compounds with loose or coherent fibrous material using pretreated fibrous materials
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
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    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/10—Reinforcing macromolecular compounds with loose or coherent fibrous material characterised by the additives used in the polymer mixture
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/248—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using pre-treated fibres
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/20—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads
    • D03D15/242—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads inorganic, e.g. basalt
    • D03D15/275—Carbon fibres
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
    • D04H3/12—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with filaments or yarns secured together by chemical or thermo-activatable bonding agents, e.g. adhesives, applied or incorporated in liquid or solid form
    • D—TEXTILES; PAPER
    • D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M14/00—Graft polymerisation of monomers containing carbon-to-carbon unsaturated bonds on to fibres, threads, yarns, fabrics, or fibrous goods made from such materials
    • D06M14/36—Graft polymerisation of monomers containing carbon-to-carbon unsaturated bonds on to fibres, threads, yarns, fabrics, or fibrous goods made from such materials on to carbon fibres
    • D—TEXTILES; PAPER
    • D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M15/00—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
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    • B29K2105/12—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of short lengths, e.g. chopped filaments, staple fibres or bristles
    • B29K2105/122—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of short lengths, e.g. chopped filaments, staple fibres or bristles microfibres or nanofibers
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    • D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
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Definitions

  • Fiber-reinforced composites are useful in load-bearing components for mechanical systems, and other applications. Also disclosed herein are methods of making and using such composites, articles comprising the same, and the like.
  • FRC fiber-reinforced composites
  • these FRCs are based on polymers, including thermoset polymers, that contain reinforcing fibers.
  • epoxy resins are some of the most popular thermoset polymers in the art, owing to their good adhesive properties and processability. Epoxy resins themselves, however, have relatively low mechanical strength and, therefore, do not effectively facilitate stress in high performance mechanical systems. Consequently, mechanically reinforcing fiber materials such carbon, glass, aramid, basalt, or boron are usually incorporated in the polymer to achieve effective mechanical strength.
  • LFRC Long-fiber reinforced composites
  • SFRC Short-fiber reinforced composites
  • Discontinuous fibers are classified by a general aspect ratio, defined as the ratio of fiber length to diameter, of between 10 and 60. Discontinuous fibers can be randomly or preferentially oriented to yield directionally varying mechanical properties.
  • a high filler loading of reinforcing fiber is required to observe a significant boost in mechanical strength.
  • the continuous fibers in LFRCs are oriented and constructed prior to the dispersion into a polymer matrix.
  • the orientation of discontinuous fibers in SFRCs is modulated after the dispersion into a polymer matrix. Consequently, the high filler loading of discontinuous fibers reduces the processability of the material because the viscosity of the composite increases with the filler volume fraction.
  • Fiber-reinforced composites are useful in load-bearing components for mechanical systems, and other applications. Also disclosed herein are methods of making and using such composites, articles comprising the same, and the like.
  • the subject matter of the present invention involves, in some cases, interrelated products, alternative solutions to a particular problem, and/or a plurality of different uses of one or more systems and/or articles.
  • the present invention is generally directed to an article.
  • the article may be a fiber-reinforced composite in certain embodiments.
  • the article in one set of embodiments, comprises a composite comprising a plurality of continuous fibers defining a substrate, and a plurality of discontinuous agents contained within at least a portion of the substrate. In one embodiment, at least some of the plurality of discontinuous agents have a plurality of magnetic particles adsorbed thereto.
  • the article is generally directed to a composite comprising a fabric defined by a plurality of continuous fibers, and a plurality of aligned discontinuous agents contained within pores within the fabric.
  • the article comprises a layered composite comprising a plurality of plies, at least one ply comprising a plurality of continuous fibers defining a substrate, and a plurality of discontinuous agents contained within the substrate.
  • the article includes a composite comprising a plurality of continuous fibers defining a substrate, and a plurality of discontinuous agents contained within the substrate.
  • at least some of the plurality of discontinuous agents have a plurality of magnetic particles adsorbed thereto.
  • at least 20 vol % of the composite comprises the discontinuous agents.
  • the article in yet another set of embodiments, includes a composite comprising a plurality of continuous fibers defining a substrate, and a plurality of discontinuous agents contained within at least a portion of the substrate.
  • the present invention is generally directed to a method.
  • the method includes providing a liquid comprising a plurality of discontinuous agents having a plurality of magnetic particles adsorbed thereto, exposing the liquid to a plurality of continuous fibers defining a substrate, applying a magnetic field to the liquid to cause alignment of at least some of the plurality of discontinuous agents within the plurality of continuous fibers, and optionally, hardening the liquid to form a composite.
  • the present invention encompasses methods of making one or more of the embodiments described herein, for example, a fiber-reinforced composite. In still another aspect, the present invention encompasses methods of using one or more of the embodiments described herein, for example, a fiber-reinforced composite.
  • FIGS. 1A-1B illustrate composites in accordance with some embodiments of the invention.
  • FIG. 2 is a schematic diagram in accordance with certain embodiments of the invention.
  • fiber-reinforced composites are useful in load-bearing components for mechanical systems, and other applications. Also disclosed herein are methods of making and using such composites, articles comprising the same, and the like.
  • some embodiments of the invention are generally directed to composites comprising discontinuous agents such as fibers or platelets which are positioned within a substrate, e.g., formed from a plurality of continuous fibers.
  • the discontinuous agents may be substantially aligned, for example, by attaching magnetic particles onto the agents and using a magnetic field to manipulate the agents.
  • Other embodiments are generally directed to systems and methods for making or using such composites, kits involving such composites, or the like.
  • certain aspects of the invention are generally directed to fiber-reinforced composite ply with a matrix of discontinuous fibers aligned in the through-plane direction that are fixed in position with a binder and embed a planar fabric of continuous fibers. Aligning particles transversely to the planar fabric can enhance the mechanical, electrical, and/or thermal properties in the transverse direction and interlaminar regions between plies.
  • the discontinuous fibers and similarly sized particles are aligned using a magnetic alignment process in which non-magnetic agents are surface-coated with magnetic particles, allowing the originally non-magnetic particles to exhibit a physical response to magnetic fields.
  • the immediate focus is implementing this alignment method with discontinuous carbon fibers.
  • other agents can also be aligned, including (but not limited to) materials in fiber, platelet, and ellipsoid form, etc.
  • Various embodiments of the invention are generally directed to composite plies with a discontinuous fiber matrix that embed a planar fabric of continuous fibers, regardless of orientation.
  • Other embodiments are generally directed to fiber-reinforced composite plies that do not have oriented, magnetically functionalized particles.
  • Particles typically used in composites are diamagnetic, requiring extremely high magnetic fields for alignment (greater than 1 Tesla).
  • discontinuous carbon fibers and other similarly sized particles can be surface-coated with magnetic nanoparticles make them more responsive to magnetic fields.
  • selection of the proper geometry of particles leads to a magnetic response that may reduce the required magnetic field strength for alignment by over one hundred-fold.
  • sub-millimeter discontinuous carbon fibers can be successfully magnetized to exhibit a suitable magnetic response.
  • the produced magnetically responsive particles can be controlled with magnetic fields to produce composites with tunable orientation and distribution of particles, e.g., as shown in FIG. 1 .
  • Another aspect of the present invention is generally directed to composites comprising substrates having a plurality of discontinuous agents, such as fibers or platelets.
  • the discontinuous agents may be generally substantially aligned within the substrate in some embodiments, for example, substantially orthogonally aligned.
  • the substrate itself may be defined by generally continuous fibers, which may be woven or non-woven to form the substrate. In certain instances, some of the holes or pores created by the continuous fibers may be filled in by the discontinuous agents.
  • the composite may further comprise binders or other materials, such as those discussed herein.
  • magnetic particles can be attached to the discontinuous agents, and a magnetic field may then be used to manipulate the magnetic particles.
  • the magnetic field may be used to move the magnetic particles into the substrate, and/or to align the discontinuous agents within the substrate.
  • the magnetic field may be constant or time-varying (e.g., oscillating), for instance, as is discussed herein.
  • an applied magnetic field may have a frequency of 1 Hz to 500 Hz and an amplitude of 0.01 T to 10 T.
  • Other examples of magnetic fields are described in more detail below.
  • the volume of magnetic particles used to manipulate the magnetic particles may be substantial in some cases.
  • a composite 10 may comprise a plurality of continuous fibers 15 (in this example, woven together to form a substrate). Gaps 25 between the fibers may be empty, or filled with discontinuous agents 30 .
  • the discontinuous agents may be, for example, fibers 35 and/or platelets 40 , and/or may have other shapes such as those discussed herein.
  • the agents may also be aligned, e.g., as is shown with fibers 35 .
  • Some of the discontinuous agents may include magnetic particles 50 that are adsorbed or otherwise attached to the discontinuous agents.
  • An applied magnetic field 55 may in some embodiments be used to manipulate the magnetic particles, e.g., to cause them to align the discontinuous agents, and/or to move them into one or more of the gaps within the substrate.
  • Such composites may find use in a wide variety of applications.
  • such composites may be useful for eliminating or reducing stress concentrations or delamination within materials, stiffening materials, eliminating or reducing surface wear, dissipating electrical shocks, transmitting electrical signals, attenuating or transmitting electromagnetic waves, dissipating thermal shocks, eliminating or reducing thermal gradients, as components for energy storage applications, or as components for carbon fibers or ceramic matrixes. Additional examples are discussed in more detail below.
  • Certain embodiments of the invention are generally directed to composites comprising a plurality of continuous fibers defining a substrate, and a plurality of discontinuous agents contained within the substrate.
  • the plurality of discontinuous agents may be contained within holes or pores of the substrate, e.g., created by spacing between the continuous fibers that define the substrate.
  • the discontinuous agents may be substantially aligned within the holes or pores.
  • the composite may, in some cases, also contain a plurality of particles, such as magnetic particles, adsorbed onto the continuous fibers and/or the discontinuous agents, which may be used to manipulate the agents, e.g., with an applied magnetic field.
  • a binder may be present, for example, to bind the continuous fibers and/or the discontinuous agents within the composite.
  • the composite is generally planar.
  • a substrate need not be a mathematically-perfect planar structure (although it can be); for instance, the substrate may also be deformable, curved, bent, folded, rolled, creased, or the like.
  • the substrate may have an average thickness of at least about 0.1 micrometers, at least about 0.2 micrometers, at least about 0.3 micrometers, at least about 0.5 micrometers, at least about 1 micrometer, at least about 2 micrometers, at least about 3 micrometers, at least about 5 micrometers, at least about 10 micrometers, at least about 30 micrometers, at least about 50 micrometers, at least about 100 micrometers, at least about 300 micrometers, at least about 500 micrometers, at least about 1 mm, at least about 2 mm, at least about 3 mm, at least about 5 mm, at least about 1 cm, at least about 3 cm, at least about 5 cm, at least about 10 cm, at least about 30 cm, at least about 50 cm, at least about 100 cm, etc.
  • the average thickness may be less than 100 cm, less than 50 cm, less than 30 cm, less than 10 cm, less than 5 cm, less than 3 cm, less than 1 cm, less than 5 mm, less than 2 mm, less than 3 mm, less than 1 mm, less than 500 micrometers, less than 300 micrometers, less than 100 micrometers, less than 50 micrometers, less than 30 micrometers, less than 10 micrometers, less than 5 micrometers, less than 3 micrometers, less than 1 micrometers, less than 0.5 micrometers, less than 0.3 micrometers, or less than 0.1 micrometers. Combinations of any of these are also possible in certain embodiments.
  • the average thickness may be between 0.1 and 5,000 microns, between 10 and 2,000 microns, between 50 and 1,000 microns, or the like.
  • the thickness may be uniform or non-uniform across the substrate.
  • the substrate may be rigid (e.g., as discussed herein), or may be deformable in some cases.
  • the pores or holes that are created by the continuous fibers may be relatively small. Some or all of the pores or holes may contain discontinuous agents, which may be aligned in some cases.
  • the pores or holes may have an average size or cross-sectional dimension of no more than 10 cm, no more than 5 cm, no more than 3 cm, no more than 2 cm, no more than 1 cm, no more than 5 mm, no more than 3 mm, no more than 2 mm, no more than 1 mm, no more than 500 micrometers, no more than 300 micrometers, no more than 200 micrometers, no more than 100 micrometers, no more than 50 micrometers, no more than 30 micrometers, no more than 20 micrometers, no more than 10 micrometers, etc.
  • Composites may be used in a wide variety of applications, including those discussed in more detail herein. As non-limiting examples, composites may be used in diverse applications such as reinforcement for pressure vessels, components for wind turbines, shims used in jacking heavy structures, sporting equipment, building or construction materials, laminates or encapsulants for electronic devices, battery components, or panels for vehicles such as automobiles, aircraft, marine vehicles, or spacecraft.
  • one set of embodiments of the invention are generally directed to composites comprising substrates formed from continuous fibers, and containing a plurality of discontinuous agents, e.g., fibers or platelets.
  • the continuous fibers generally have a length that on average is substantially longer than the characteristic dimension of the discontinuous agents.
  • the continuous fibers may have an average length that is greater than 10, greater than 30, greater than 50, greater than 100, greater than 300, greater than 500, or greater than 1,000 times the characteristic dimension of the discontinuous agents.
  • the continuous fibers have an average aspect ratio (e.g., of length to diameter or average cross-sectional dimension) of at least 3, at least 5, at least 10, at least 30, at least 50, at least 100, at least 300, at least 500, at least 1,000, etc.
  • average aspect ratio e.g., of length to diameter or average cross-sectional dimension
  • the continuous fibers may have an average length of at least 1 nm, at least 3 nm, at least 5 nm, at least 10 nm, at least 30 nm, at least 50 nm, at least 100 nm, at least 300 nm, at least 500 nm, at least 1 micrometer, at least 3 micrometers, at least 5 micrometers, at least 10 micrometers, at least 30 micrometers, at least 50 micrometers, at least 100 micrometers, at least 300 micrometers, at least 500 micrometers, at least 1 mm, at least 3 mm, at least 5 mm, at least 1 cm, at least 3 cm, at least 5 cm, or at least 10 cm. Longer average lengths are also possible in some instances.
  • the continuous fibers may be woven together (e.g. bidirectional, multidirectional, quasi-isotropic, etc.), and/or non-woven (e.g., unidirectional, veil, mat, etc.).
  • at least some of the continuous fibers are substantially parallel, and/or orthogonally oriented relative to each other, although other configurations of continuous fibers are also possible.
  • the continuous fibers may together define a fabric or other substrate, e.g., a textile, a tow, a filament, a yarn, a strand, or the like.
  • the substrate may have one orthogonal dimension that is substantially less than the other orthogonal dimensions (i.e., the substrate may have a thickness).
  • the continuous fibers forming the substrate may comprise any of a wide variety of materials, and one type or more than one type of fiber may be present within the substrate.
  • Non-limiting examples include carbon, basalt, silicon carbide, aramid, zirconia, nylon, boron, alumina, silica, borosilicate, mullite, cotton, or any other natural or synthetic fibers.
  • the continuous fibers may have any suitable average diameter.
  • the continuous fibers may have an average diameter of at least 10 micrometers, at least 20 micrometers, at least 30 micrometers, at least 50 micrometers, at least 100 micrometers, at least 200 micrometers, at least 300 micrometers, at least 500 micrometers, at least 1 mm, at least 2 mm, at least 3 mm, at least 5 mm, at least 1 cm, at least 2 cm, at least 3 cm, at least 5 cm, at least 10 cm, etc.
  • the continuous fibers may have an average diameter of no more than 10 cm, no more than 5 cm, no more than 3 cm, no more than 2 cm, no more than 1 cm, no more than 5 mm, no more than 3 mm, no more than 2 mm, no more than 1 mm, no more than 500 micrometers, no more than 300 micrometers, no more than 200 micrometers, no more than 100 micrometers, no more than 50 micrometers, no more than 30 micrometers, no more than 20 micrometers, no more than 10 micrometers, etc. Combinations of any of these are also possible.
  • the continuous fibers may have an average diameter of between 10 micrometers and 100 micrometers, between 50 micrometers and 500 micrometers, between 100 micrometers and 5 mm, etc.
  • the continuous fibers may also have any suitable average length.
  • the continuous fibers may have an average length of at least about 0.5 cm, at least 1 cm, at least 2 cm, at least 3 cm, at least 5 cm, at least 10 cm, etc.
  • the continuous fibers may have an average diameter of no more than 10 cm, no more than 5 cm, no more than 3 cm, no more than 2 cm, no more than 1 cm, no more than 0.5 cm, or the like. Combinations of any of these are also possible; for example, the continuous fibers may have an average length of between 1 cm and 10 cm, between 10 cm and 100 cm, etc.
  • the continuous fibers may comprise a relatively large portion of the composite.
  • the continuous fibers may comprise at least 1%, at least 2%, at least 3%, at least 4%, at least 5%, at least 7%, at least 10%, at least 15%, at least 20%, at least 25%, at least 30%, at least 35%, at least 40%, at least 45%, at least 50%, at least 55%, at least 60%, at least 65%, at least 70%, at least 75%, at least 80%, at least 85%, at least 90%, at least 95%, or at least 97% of the mass of the composite.
  • the continuous fibers comprise no more than 97%, no more than 95%, no more than 90%, no more than 85%, no more than 80%, no more than 70%, no more than 60%, no more than 50%, no more than 40%, no more than 30%, no more than 20%, or no more than 10% of the mass of the composite. Combinations of any of these are also possible.
  • the composite may also contain one or more discontinuous agents in certain embodiments.
  • the agents may include agglomerated agents or individual agents.
  • the agents may have a variety of shapes, including discontinuous fibers or platelets. Other shapes include, but are not limited to, nanotubes, nanofibers, nanosheets, or the like.
  • the discontinuous agents are not spherical.
  • a fiber has a shape such that one orthogonal dimension (e.g., its length) is substantially greater than its other two orthogonal dimensions (e.g., its width or thickness).
  • the fiber may be substantially cylindrical in some cases.
  • a platelet may have a shape such that two orthogonal dimensions (e.g., its diameter) are substantially greater than its other orthogonal dimension (e.g., its width or thickness).
  • a platelet may be substantially cylindrical or disc-shaped in some cases, although it may have other shapes as well.
  • both platelets and fibers may be present in some cases, and/or that other shapes besides platelets and/or fibers may be present in certain embodiments (e.g., instead of or in addition to platelets and/or fibers).
  • discontinuous agents such as platelets and/or fibers may be relatively stiff, or may be curved or flexible in some cases, or adopt a variety of other shapes.
  • a fiber need not be perfectly straight (e.g., its length may still be determined along the fiber itself, even if it is curved).
  • a platelet need not be perfectly disc-shaped.
  • the discontinuous agents may have a dimension (e.g., a characteristic dimension) that is substantially the same, or smaller, than the thickness of the substrate.
  • a dimension e.g., a characteristic dimension
  • at least some discontinuous fibers within a composite may have an average length that substantially spans the thickness of the substrate.
  • the dimension may be greater than the thickness.
  • certain embodiments of the invention are generally directed to composites comprising discontinuous fibers.
  • the discontinuous fibers within a composite may have an average length, or characteristic dimension, of at least 1 nm, at least 3 nm, at least 5 nm, at least 10 nm, at least 30 nm, at least 50 nm, at least 100 nm, at least 300 nm, at least 500 nm, at least 1 micrometer, at least 3 micrometers, at least 5 micrometers, at least 10 micrometers, at least 20 micrometers, at least 30 micrometers, at least 50 micrometers, at least 100 micrometers, at least 200 micrometers, at least 300 micrometers, at least 500 micrometers, at least 1 mm, at least 2 mm, at least 3 mm, at least 5 mm, at least 1 cm, at least 1.5 cm, at least 2 cm, at least 3 cm, at least 5 cm, at least 10 cm, etc.
  • the discontinuous fibers may have an average length, or characteristic dimension, of no more than 10 cm, no more than 5 cm, no more than 3 cm, no more than 2 cm, no more than 1.5 cm, no more than 1 cm, no more than 5 mm, no more than 3 mm, no more than 2 mm, no more than 1 mm, no more than 500 micrometers, no more than 300 micrometers, no more than 200 micrometers, no more than 100 micrometers, no more than 50 micrometers, no more than 30 micrometers, no more than 20 micrometers, no more than 10 micrometers, no more than 5 micrometers, no more than 3 micrometers, no more than 1 micrometers, no more than 500 nm, no more than 300 nm, no more than 100 nm, no more than 50 nm, no more than 30 nm, no more than 10 nm, no more than 5 nm, etc. Combinations of any of these are also possible.
  • the discontinuous fibers within a composite may have
  • the discontinuous fibers may also have any suitable average diameter.
  • the discontinuous fibers may have an average diameter of at least 10 micrometers, at least 20 micrometers, at least 30 micrometers, at least 50 micrometers, at least 100 micrometers, at least 200 micrometers, at least 300 micrometers, at least 500 micrometers, at least 1 mm, at least 2 mm, at least 3 mm, at least 5 mm, at least 1 cm, at least 2 cm, at least 3 cm, at least 5 cm, at least 10 cm, etc.
  • the discontinuous fibers may have an average diameter of no more than 10 cm, no more than 5 cm, no more than 3 cm, no more than 2 cm, no more than 1 cm, no more than 5 mm, no more than 3 mm, no more than 2 mm, no more than 1 mm, no more than 500 micrometers, no more than 300 micrometers, no more than 200 micrometers, no more than 100 micrometers, no more than 50 micrometers, no more than 30 micrometers, no more than 20 micrometers, no more than 10 micrometers, etc. Combinations of any of these are also possible.
  • the discontinuous fibers may have an average diameter of between 10 micrometers and 100 micrometers, between 50 micrometers and 500 micrometers, between 100 micrometers and 5 mm, etc.
  • the discontinuous fibers may have a length that is at least 10 times or at least 50 times its thickness or diameter, on average.
  • the fibers within a composite may have an average aspect ratio (ratio of fiber length to diameter or thickness) of at least 3, at least 5, at least 10, at least 30, at least 50, at least 100, at least 300, at least 500, at least 1,000, at least 3,000, at least 5,000, at least 10,000, at least 30,000, at least 50,000, or at least 100,000.
  • the average aspect ratio may be less than 100,000, less than 50,000, less than 30,000, less than 10,000, less than 5,000, less than 3,000, less than 1,000, less than 500, less than 300, less than 100, less than 50, less than 30, less than 10, less than 5, etc. Combinations of any of these are also possible in some cases; for instance, the aspect ratio may be between 5, and 100,000.
  • a composite is not limited to only discontinuous fibers.
  • a composite may include platelets, e.g., instead of or in addition to discontinuous fibers.
  • a platelet may be disc-shaped, although other shapes may be possible as well.
  • the platelet may have a maximum dimension or a characteristic dimension of at least 10 micrometers, at least 20 micrometers, at least 30 micrometers, at least 50 micrometers, at least 100 micrometers, at least 200 micrometers, at least 300 micrometers, at least 500 micrometers, at least 1 mm, at least 2 mm, at least 3 mm, at least 5 mm, at least 1 cm, at least 1.5 cm, at least 2 cm, at least 3 cm, at least 5 cm, at least 10 cm, etc.
  • the platelet have a maximum dimension or a characteristic dimension of no more than 10 cm, no more than 5 cm, no more than 3 cm, no more than 2 cm, no more than 1.5 cm, no more than 1 cm, no more than 5 mm, no more than 3 mm, no more than 2 mm, no more than 1 mm, no more than 500 micrometers, no more than 300 micrometers, no more than 200 micrometers, no more than 100 micrometers, no more than 50 micrometers, no more than 30 micrometers, no more than 20 micrometers, no more than 10 micrometers, etc.
  • the characteristic dimension may be taken as a diameter of a perfect circle having the same area as the face of the platelet. Combinations of any of these dimensions are also possible.
  • the maximum dimension or a characteristic dimension may be between 5 mm and 15 mm, or between 1 mm and 5 mm, between 1 mm and 1 cm, etc.
  • the platelet may have an average aspect ratio (ratio of largest dimension to smallest dimension or thickness) of at least 3, at least 5, at least 10, at least 30, at least 50, at least 100, at least 300, at least 500, at least 1,000, etc.
  • the average aspect ratio may be less than 1,000, less than 500, less than 300, less than 100, less than 50, less than 30, less than 10, less than 5, etc. Combinations of any of these are also possible in some cases; for instance, the aspect ratio may be between 5, and 1,000.
  • the discontinuous agents may be formed or include any of a wide variety of materials, and one or more than one type of material may be present.
  • the discontinuous agents may comprise materials such as carbon (e.g., carbon fibers), basalt, silicon carbide, silicon nitride, aramid, zirconia, nylon, boron, alumina, silica, borosilicate, mullite, nitride, boron nitride, graphite, glass, or the like.
  • the discontinuous agents may include any natural and/or any synthetic material, and may be magnetic and/or non-magnetic.
  • the discontinuous agents may comprise a relatively large portion of the composite.
  • the discontinuous agents may comprise at least 1%, at least 2%, at least 3%, at least 4%, at least 5%, at least 7%, at least 10%, at least 15%, at least 20%, at least 25%, at least 30%, at least 35%, at least 40%, at least 45%, at least 50%, at least 55%, at least 60%, at least 65%, at least 70%, at least 75%, at least 80%, at least 85%, at least 90%, at least 95%, or at least 97% of the mass of the composite.
  • the discontinuous agents comprise no more than 97%, no more than 95%, no more than 90%, no more than 85%, no more than 80%, no more than 70%, no more than 60%, no more than 50%, no more than 40%, no more than 30%, no more than 20%, or no more than 10% of the mass of the composite. Combinations of any of these are also possible.
  • the discontinuous agents may be at least substantially aligned within the composite.
  • Methods for aligning discontinuous agents, such as fibers, are discussed in more detail herein.
  • Various alignments are possible, and in some cases, can be determined optically or microscopically, e.g., as is shown in FIG. 1B .
  • the alignment may be determined qualitatively. However, it should be understood that the alignment need not be perfect.
  • At least 50%, at least 75%, at least 85%, at least 90%, or at least 95% of the discontinuous agents within a composite may exhibit an alignment that is within 20°, within 15°, within 10°, or within 5° of the average alignment of the plurality of the discontinuous agents, e.g., within a sample of the composite.
  • the alignment of the discontinuous particles is substantially orthogonal to the substrate.
  • the average alignment may be oriented to be at least 60°, at least 65°, at least 70°, at least 75°, at least 85°, or at least 87° relative to the plane of the substrate at that location.
  • the substrate itself may not necessarily be planar, but may also be curved, etc.
  • alignment of the discontinuous particles substantially orthogonal to the substrate may serve to provide reinforcement of the substrate. This may improve the strength of the substrate, e.g., when subjected to forces in different directions. For instance, fibers within the substrate may run in substantially orthogonal directions in 3 dimensions, thereby providing strength to the substrate regardless of the direction of force that is applied.
  • the discontinuous particles may also limit degradation of the surface, e.g., with interlaminar micro-cracks, through-ply fissures, or the like.
  • the discontinuous particles may enhance other properties of the substrate, e.g., electrical and/or thermal properties within the composite, in addition to or instead of its mechanical properties.
  • the discontinuous agents may be uncoated. In some cases, however, some or all of the discontinuous agents may be coated.
  • the coating may be used, for example, to facilitate the adsorption or binding of particles, such as magnetic particles, onto the agents.
  • the agents may be coated with a surfactant, a silane coupling agent, an epoxy, glycerine, polyurethane, an organometallic coupling agent, or the like.
  • surfactants include oleic acid, sodium dodecyl sulfate, sodium lauryl sulfate, etc.
  • Non-limiting examples of silane coupling agents include amino-, benzylamino-, chloropropyl-, disulfide-, epoxy-, epoxy/melamine-, mercapto-, methacrylate-, tertasulfido-, ureido-, vinyl-, isocynate-, and vinyl-benzyl-amino-based silane coupling agents.
  • organometallic coupling agents include aryl- and vinyl-based organometallic coupling agents
  • Particles such as magnetic particles may be adsorbed or otherwise bound to at least some of the discontinuous agents.
  • the particles may coat some or all of the discontinuous agents and/or the continuous fibers. This may be facilitated by a coating of material as discussed above, although a coating is not necessarily required to facilitate the adsorption of the particles.
  • the particles may comprise any of a wide variety of magnetically susceptible materials.
  • the magnetic materials may comprise one or more ferromagnetic materials, e.g., containing iron, nickel, cobalt, alnico, oxides of iron, nickel, cobalt, rare earth metals, or an alloy including two or more of these and/or other suitable ferromagnetic materials.
  • the magnetic particles may have a relative permeability of at least 2, at least 5, at least 10, at least 20, at least 40, at least 100, at least 200, at least 500, at least 1,000, at least 2,000, at least 5,000, or at least 10,000.
  • non-magnetic particles may be used, e.g., in addition to and/or instead of magnetic particles.
  • Non-limiting examples of nonmagnetic particles include glass, polymer, metal, or the like.
  • the particles may be spherical or non-spherical, and may be of any suitable shape or size.
  • the particles may be relatively monodisperse or come in a range of sizes.
  • the particles may have a characteristic dimension, on average, of at least 10 micrometers, at least 20 micrometers, at least 30 micrometers, at least 50 micrometers, at least 100 micrometers, at least 200 micrometers, at least 300 micrometers, at least 500 micrometers, at least 1 mm, at least 2 mm, at least 3 mm, at least 5 mm, at least 1 cm, at least 1.5 cm, at least 2 cm, at least 3 cm, at least 5 cm, at least 10 cm, etc.
  • the particles within the composite may also have an average characteristic dimension of no more than 10 cm, no more than 5 cm, no more than 3 cm, no more than 2 cm, no more than 1.5 cm, no more than 1 cm, no more than 5 mm, no more than 3 mm, no more than 2 mm, no more than 1 mm, no more than 500 micrometers, no more than 300 micrometers, no more than 200 micrometers, no more than 100 micrometers, no more than 50 micrometers, no more than 30 micrometers, no more than 20 micrometers, no more than 10 micrometers, etc. Combinations of any of these are also possible.
  • the particles may exhibit a characteristic dimension of or between 100 micrometer and 1 mm, between 10 micrometer and 10 micrometer, etc.
  • the characteristic dimension of a nonspherical particle may be taken as the diameter of a perfect sphere having the same volume as the nonspherical particle.
  • the particles may comprise a relatively large portion of the composite.
  • the particles may comprise at least 1%, at least 2%, at least 3%, at least 4%, at least 5%, at least 7%, at least 10%, at least 15%, at least 20%, at least 25%, at least 30%, at least 35%, at least 40%, at least 45%, at least 50%, at least 55%, at least 60%, at least 65%, at least 70%, at least 75%, at least 80%, at least 85%, at least 90%, at least 95%, or at least 97% of the volume of the composite.
  • the particles comprise no more than 97%, no more than 95%, no more than 90%, no more than 85%, no more than 80%, no more than 70%, no more than 60%, no more than 50%, no more than 45%, no more than 40%, no more than 35% no more than 30%, no more than 25%, no more than 20%, no more than 15%, no more than 10%, no more than 7%, no more than 5%, no more than 4%, no more than 3%, no more than 2%, or no more than 1% of the volume of the composite. Combinations of any of these are also possible.
  • a binder is also present within the composite, e.g., which may be used to bind the continuous fibers and the discontinuous agents, e.g., within the composite.
  • the binder may facilitate holding the continuous fibers and the discontinuous agents in position within the composite.
  • the binder is optional and not required in all cases.
  • the binder may comprise a resin.
  • the binder may include a thermoset or a thermoplastic.
  • the binder may comprise a thermoplastic solution, a thermoplastic melt, thermoplastic pellets, a thermoset resin, a volatile compound such as a volatile organic compound, water, or an oil.
  • binders include an epoxy, polyester, vinyl ester, polyethylenimine, polyetherketoneketone, polyaryletherketone, polyether ether ketone, polyphenylene sulfide, polyethylene terephthalate, a polycarbonates, poly(methyl methacrylate), acrylonitrile butadiene styrene, polyacrylonitrile, polypropylene, polyethylene, nylon, a silicone rubber, polyvinylidene fluoride, styrene butadiene rubber, or a pre-ceramic monomer, such as a siloxane, a silazane, or a carbosilane.
  • the binder may also include mixtures including any one or more of these materials and/or other materials, in certain embodiments.
  • the binder may comprise at least 1%, at least 2%, at least 3%, at least 4%, at least 5%, at least 7%, at least 10%, at least 15%, at least 20%, or at least 25% of the mass of the composite, and/or no more than 25%, no more than 20%, no more than 15%, no more than 10%, no more than 7%, no more than 5%, no more than 4%, no more than 3%, no more than 2%, or no more than 1% of the mass of the composite.
  • composites can be prepared from a liquid, such as a slurry, containing a plurality of discontinuous agents and a plurality of magnetic particles, to which a suitable substrate is exposed to.
  • the discontinuous agents can include fibers, platelets, or the like, e.g., as discussed herein.
  • a magnetic field can be applied to manipulate the magnetic particles and the discontinuous agents, for example, to move the magnetic particles into the substrate, and/or to align the discontinuous agents. Excess material can be removed.
  • the composite can be set or hardened, e.g., with a binder, which may be used to immobilize or fix the discontinuous agents within the substrate.
  • the binder may, in certain embodiments, be infused or impregnated into the substrate.
  • a liquid such as a slurry
  • the slurry may include discontinuous agents and/or magnetic particles.
  • the liquid phase may include, for example, a thermoplastic or a thermoset, e.g., a thermoplastic solution, thermoplastic melt, thermoset, volatile organic compound, water, or oil.
  • thermosets include polyethylenimine, polyetherketoneketone, polyaryletherketone, polyether ether ketone, polyphenylene sulfide, polyethylene terephthalate, a polycarbonates, poly(methyl methacrylate), acrylonitrile butadiene styrene, polyacrylonitrile, polypropylene, polyethylene, nylon, polyvinylidene fluoride, phenolics, epoxies, bismaleimides, cyanate esters, polyimides, etc.
  • elastomers include silicone rubber and styrene butadiene rubber, etc.
  • thermoplastics include epoxy, polyester, vinyl ester, polycarbonates, polyamides (e.g., nylon, PA-6, PA-12, etc.), polyphenylene sulfide, polyetherimide, polyetheretherketone, polyetherketoneketone, etc.
  • ceramic monomers include a siloxane, a silazane, or a carbosilane, etc. In some cases, for example, one or more of these may be added to assist in homogenously dispersing the discontinuous agents and/or magnetic particles within the liquid.
  • volatile organic compounds include, but are not limited to, isopropanol, butanol, ethanol, acetone, toluene, or xylenes.
  • the magnetic particles may be adsorbed or otherwise bound to the discontinuous agents within the liquid.
  • the magnetic particles may be added to the discontinuous agents prior to introduction into the liquid, or the discontinuous agents and magnetic particles may be separately added to the liquid and at least some of the magnetic particles may spontaneously adsorb onto the discontinuous agents.
  • any suitable amount of discontinuous agents and/or magnetic particles may be present in the slurry or other liquid. For instance, at least 10%, at least 15%, at least 20%, at least 25%, at least 30%, at least 35%, at least 40%, at least 45%, at least 50%, at least 55%, at least 60%, at least 65%, at least 70%, at least 75%, or at least 80% of the volume of the slurry may be discontinuous agents and/or magnetic particles.
  • no more than 85%, no more than 80%, no more than 75%, no more than 70%, no more than 65%, no more than 60%, no more than 55%, no more than 50%, no more than 45%, no more than 40%, no more than 35%, no more than 30%, no more than 25%, no more than 20%, no more than 15%, or no more than 10% may be discontinuous agents and/or magnetic particles. Combinations of any of these are also possible in some cases.
  • a slurry or other liquid may contain between 70% and 80%, between 75% and 85%, between 50% and 90%, etc. discontinuous agents and/or magnetic particles.
  • the substrate After preparation of the slurry or other liquid, it may be applied to or exposed to the substrate, e.g., comprising the continuous fibers.
  • the substrate may be placed on a surface such as a polymer foil, metal foil, or paper, e.g., for application of liquid, a magnetic field, mechanical vibration, heating, and/or the like, e.g., as discussed herein.
  • any suitable method may be used to apply the slurry or other liquid to the substrate.
  • the liquid may be poured, coated, sprayed, or painted onto the substrate, or the substrate may be immersed partially or completely within the liquid.
  • the liquid may be used to wet, coat, and/or surround the continuous fibers.
  • a magnetic field may be applied to manipulate the magnetic particles.
  • the magnetic field may also be used to manipulate the discontinuous agents, e.g., due to the magnetic particles that are adsorbed or otherwise bound to the discontinuous agents.
  • the magnetic field may be used to move the magnetic particles into the substrate, e.g., into pores or holes within the substrate.
  • the magnetic field may be used to at least substantially align the discontinuous agents within the substrate, e.g., as discussed herein.
  • the magnetic field may be used to align at least 50%, at least 75%, at least 85%, at least 90%, or at least 95% of the discontinuous agents to within 20°, within 15°, within 10°, or within 5° of the average alignment.
  • the magnetic field in some embodiments, may be used to align the magnetic particles and/or the discontinuous agents within the substrate, e.g., in the direction of the magnetic field, and/or within the substrate in a through-plane direction.
  • the magnetic field is a constant magnetic field.
  • the magnetic field may be time-varying; for example, the magnetic field may oscillate or periodically change in amplitude and/or direction, e.g., to facilitate manipulation of the discontinuous agents.
  • the oscillation may be sinusoidal or another repeating waveform (e.g., square wave or sawtooth).
  • the frequency may be, for example, at least 0.1 Hz, at least 0.3 Hz, at least 0.5 Hz, at least 1 Hz, at least 3 Hz, at least 5 Hz, at least 10 Hz, at least 30 Hz, at least 50 Hz, at least 100 Hz, at least 300 Hz, at least 500 Hz, etc., and/or no more than 1000 Hz, no more than 500 Hz, no more than 300 Hz, no more than 100 Hz, no more than 50 Hz, no more than 30 Hz, no more than 10 Hz, no more than 5 Hz, no more than 3 Hz, etc.
  • the frequency may be between 1 Hz to 500 Hz, between 10 Hz and 30 Hz, between 50 Hz and Hz, or the like.
  • the frequency may be held substantially constant, or the frequency may vary in some cases.
  • the magnetic field may have any suitable amplitude.
  • the amplitude may be at least 0.001 T, at least 0.003 T, at least 0.005 T, at least 0.01 T, at least 0.03 T, at least 0.05 T, at least 0.1 T, at least 0.3 T, at least 0.5 T, at least 1 T, at least 3 T, at least 5 T, at least 10 T, etc.
  • the amplitude in some cases may be no more than 20 T, no more than 10 T, no more than 5 T, no more than 3 T, no more than 1 T, no more than 0.5 T, no more than 0.3 T, no more than 0.1 T, no more than 0.05 T, no more than 0.03 T, no more than 0.01 T, no more than 0.005 T, no more than 0.003 T, etc.
  • the amplitude may also fall within any combination of these values. For instance, the amplitude may be between 0.01 T to 10 T, between 1 T and 3 T, between 0.5 T and 1 T, or the like.
  • the amplitude may be substantially constant, or may vary in certain embodiments, e.g., within any range of these values.
  • the magnetic field direction (i.e., direction of maximum amplitude) may vary by +/ ⁇ 90°, +/ ⁇ 85°, +/ ⁇ 80°, +/ ⁇ 75°, +/ ⁇ 70°, +/ ⁇ 65°, +/ ⁇ 60°, +/ ⁇ 55°, +/ ⁇ 50°, +/ ⁇ 45°, +/ ⁇ 40°, +/ ⁇ 35°, +/ ⁇ 30°, +/ ⁇ 25°, +/ ⁇ 20°, +/ ⁇ 15°, +/ ⁇ 10°, +/ ⁇ 5° about a mean direction.
  • a variety of different devices for producing suitable magnetic fields may be obtained commercially, and include permanent magnets or electromagnets.
  • an oscillating magnetic may be created by attaching a magnet to a rotating disc and rotating the disc at an appropriate speed or frequency.
  • permanent magnets include iron magnets, alnico magnets, rare earth magnets, or the like.
  • mechanical vibration may be used to manipulate the particles, e.g., in addition to and/or instead of magnetic manipulation.
  • mechanical vibration can be used to move particles into the substrate, e.g., into pores or holes within the substrate, and/or at least substantially align the discontinuous agents within the substrate, e.g., as discussed herein.
  • vibration may be used to align the particles within the substrate and/or move the particles into holes or pores within the substrate, which may be used, for example, to correspondingly manipulate the discontinuous agents and/or eliminate voids.
  • mechanical vibration may be applied to cause motion of the particles and/or discontinuous agents of at least 1 micrometer, at least 2 micrometers, at least 3 micrometers, at least 5 micrometers, at least 10 micrometers, at least 20 micrometers, at least 30 micrometers, at least 50 micrometers, at least 100 micrometers, at least 200 micrometers, at least 300 micrometers, at least 500 micrometers, at least 1,000 micrometers, at least 2,000 micrometers, at least 3,000 micrometers, at least 5,000 micrometers, or at least 10,000 micrometers.
  • the mechanical vibrations may be time-varying; for example, the mechanical vibrations may periodically change in amplitude and/or direction, e.g., to facilitate manipulation of the discontinuous agents.
  • the oscillation may be sinusoidal or another repeating waveform (e.g., square wave or sawtooth).
  • the frequency may be, for example, at least 0.1 Hz, at least 0.3 Hz, at least 0.5 Hz, at least 1 Hz, at least 3 Hz, at least 5 Hz, at least 10 Hz, at least 30 Hz, at least 50 Hz, at least 100 Hz, at least 300 Hz, at least 500 Hz, etc., and/or no more than 1000 Hz, no more than 500 Hz, no more than 300 Hz, no more than 100 Hz, no more than 50 Hz, no more than 30 Hz, no more than 10 Hz, no more than 5 Hz, no more than 3 Hz, etc.
  • the frequency may be between 1 Hz to 500 Hz, between 10 Hz and 30 Hz, between 50 Hz and Hz, or the like.
  • the frequency may be held substantially constant, or the frequency may vary in some cases. If applied in conjunction with an oscillating magnetic field, their frequencies may independently be the same or different.
  • the discontinuous agents within the substrate may be set or fixed in some embodiments, e.g., to prevent or limit subsequent movement of the discontinuous agents and form a relatively hard composite.
  • techniques to form the composite include, but are not limited to solidifying, hardening, gelling, melting, evaporating, freezing, or lyophilizing the liquid or the slurry.
  • a material, such as a thermosetting polymer may be cured to harden the composite.
  • the substrate may thus form a composite that is a solid, a gel, or the like.
  • the liquid may comprise a relatively volatile solvent, which can be removed by heating and/or evaporation (e.g., by waiting a suitable amount of time, or allowing the solvent to evaporate, e.g., in a fume hood or other ventilated area).
  • volatile solvents include isopropanol, butanol, ethanol, acetone, toluene, or xylenes.
  • methods of removing solvents include applying vacuum, lyophilization, mechanical shaking, or the like.
  • heating may be applied to the substrate, for example, to remove a portion of the solvent.
  • the substrate may be heated to a temperature of at least about 30° C., at least about 35° C., at least about 40° C., at least about 45° C., at least about 50° C., at least about 55° C., at least about 60° C., at least about 65° C., at least about 70° C., at least about 75° C., at least about 80° C., at least about 90° C., at least about 100° C., at least about 125° C., at least about 150° C., at least about 175° C., at least about 200° C., at least about 250° C., at least about 300° C., at least about 350° C., at least about 400° C., at least about 450° C., at least about 500° C., etc.
  • thermoelectric transducer any suitable method of applying heat may be used, for example, a thermoelectric transducer, an Ohmic heater, a Peltier device, a combustion heater, or the like.
  • the viscosity of the liquid may decrease as a result of heating.
  • the heating may be applied, for example, prior, concurrent or subsequent to the application of magnetic field and/or mechanical vibration.
  • heating may be used to prevent or initiate cross-linking or curing of a thermosetting prepolymer.
  • a binder may also be applied in one set of embodiments, e.g., before, during, and/or after hardening of the composite and/or removal of at least a portion of the liquid.
  • the binder may be used to produce a pre-impregnated composite ply material, e.g., by wetting dry ply material.
  • the binder may be a liquid in some cases, and may be caused to harden after application to the composite.
  • the binder is permeated into at least a portion of the composite.
  • Non-limiting examples of permeation techniques include using gravitational and capillary forces, by applying pressure to the binder to force it into the composite, or the like.
  • the binder is used to coat all, or only a portion of, the substrate, e.g., without necessarily requiring permeation.
  • suitable binders include resins or other materials such as those discussed herein.
  • the binder may be hardened.
  • the binder may harden spontaneously, e.g., upon evaporation of a solvent.
  • heat may be applied to harden the binder, e.g., by exposing the composite to temperatures such as those described above.
  • the binder may be hardened upon exposure to light or a catalyst, e.g., to facilitate or promote a chemical or polymerization reaction to cause the binder to polymerize.
  • a thermosetting polymer may be cured upon exposure to suitable temperatures.
  • a polymer may be exposed to ultraviolet light to cause polymerization to occur.
  • Composites such as those discussed herein may be used in a wide variety of applications, in various aspects. Composites such as those described herein may exhibit a variety of different features in various embodiments of the invention.
  • composites such as those discussed herein may be useful for reducing or eliminating stress concentrations, reducing or eliminating delamination, increasing planar strength and/or stiffness, reducing or eliminating surface wear, dissipating electricity (e.g., in electrical shocks), transmitting electrical signals, attenuating electromagnetic waves, transmitting electromagnetic waves, dissipating heat (e.g., in thermal shocks), reducing or eliminating thermal gradients, storing energy, synthesizing ex-PAN carbon fibers, synthesizing ceramic matrix composites (CMC), or the like.
  • a composite ply with at least three-axes of fiber orientation may be produced.
  • This fiber structure may allow the composite ply to distribute stresses between subsequent plies and adjacent components, which may reduce or eliminate stress concentrations. This may significantly improve the strength of a laminated composite structure under dynamic loads, e.g., when a laminated composite structure is formed with small features or mates with a material with drastically different stiffness (e.g. metal alloys or plastics).
  • Another set of embodiments is generally directed to a composite ply with through-plane reinforcement of the interlaminar region.
  • This fiber reinforcement allows the composite ply to efficiently distribute stresses between adjacent layers to hinder the formation of cracks and prevents a crack from propagating in the interlaminar region.
  • the targeted reinforcement of the interlaminar region can significantly improve the strength of a laminated composite structure under shock and cyclic loads.
  • This formulation may be useful when a laminated composite structure is formed with long sheets of composite ply, for example, where a single crack in the interlaminar region between the plies can potentially compromise the structural integrity of the overall structure.
  • Yet another set of embodiments is generally directed to a composite ply with through-plane reinforcement, e.g., a through-plane uni-directional fabric.
  • This fiber reinforcement may reinforce target through-plane loads (e.g. point loads and high-pressure loads).
  • the targeted through-plane reinforcement can significantly improve the strength and stiffness of a laminated composite structure under expected through-plane mechanical loads. This may be useful for effectively handling a composite ply with through-plane reinforcement that can easily deform during handling in an un-cured state while forming an exterior shell for a laminated composite structure.
  • Still another set of embodiments is generally directed to a composite ply with through-plane oriented particles with hardness and/or chemical stability.
  • the through-plane reinforcement can significantly improve the polymer matrix's resistance to damage from mechanical wear (e.g. abrasion) and/or chemical corrosion (e.g. oxidization).
  • This formulation may be useful, for example, for forming surfaces that protect structures from mechanical and chemical wear.
  • a composite ply having enhanced through-plane electrical conductivity. This can significantly improve the resistance to damage caused by localized heat generation induced by charge accumulation upon rapid discharge of electrical energy (e.g. lightning). This formulation is particularly useful for forming surfaces that protect structures from damage from electrical discharge.
  • a composite ply with enhanced near-isotropic electrical conductivity is provided. This may effectively conduct electrical signals.
  • a composite ply is provided with enhanced isotropic electrical conductivity. This material may effectively attenuate incident electromagnetic waves.
  • a composite ply is provide having low radio-frequency interference and enhanced through-plane thermal conductivity to effectively transmit electromagnetic waves without overheating.
  • Another set of embodiments is generally directed to a composite ply with enhanced through-plane thermal conductivity for sufficient structural integrity under heating. This may be useful in some embodiments for increasing structural integrity under rapid temperature fluctuations. Still another set of embodiments is generally directed to a composite ply with through-plane thermal conductivity and low electrical conductivity. This formulation may be useful for effectively moving and distributing heat flux, e.g., in electronics.
  • Yet another set of embodiments is generally directed to a carbon-based composite ply with through-plane electrical conductivity. This may be useful for adsorbing ionic species from an electrolyte and efficiently distributing electrical charge.
  • One set of embodiments is generally directed to a composite ply with through-plane carbon fiber catalysts. At appropriate temperatures, a PAN (polyacrylonitrile) matrix may be oxidized and carbonized to form a carbon matrix.
  • Another set of embodiments is generally directed to a composite ply with through-plane carbon fiber or silicon carbide catalysts. At appropriate temperatures, the polymer matrix may be oxidized to form a ceramic matrix.
  • the present invention is generally directed to the following:
  • a process for making a fiber-reinforced composite comprising providing continuous fibers, or a combination comprising at least one of the foregoing: combining continuous fibers, or a combination comprising at least one of the foregoing, in a dispersed phase within discontinuous fibers, inorganic crystals or a combination comprising at least one of the foregoing particulate filler including, without limitation, uncoated, silane coupling agent coated, organometallic coupling agent coated, ferromagnetic material, specifically containing oxides of iron, nickel, cobalt, an alloy of a rare earth metal, or a combination comprising at least one of the foregoing coated discontinuous fibers and inorganic crystals and compounds with a thermosetting prepolymer and an optional volatile organic compound to provide a curable mixture; forming the curable mixture with a dispersed phase in the form of continuous fibers, or a combination comprising at least one of the foregoing into a layer material comprising opposing first and second layer surfaces; and applying a magnetic
  • thermoelectric transducer including, without limitation, an Ohmic heater, a Peltier device, or a combination comprising at least one of the foregoing decreases the viscosity of the curable mixture.
  • a mechanical system subassembly comprising of a single layer or multiple layers of a fiber-reinforced composite, comprising providing continuous fibers; combined the continuous fibers, in a dispersed phase within discontinuous fibers, inorganic crystals or a combination comprising at least one of the foregoing particulate filler including, without limitation, uncoated, silane coupling agent coated, organometallic coupling agent coated, ferromagnetic material, specifically containing oxides of iron, nickel, cobalt, an alloy of a rare earth metal, or a combination comprising at least one of the foregoing coated discontinuous fibers and inorganic crystals and compounds with a thermosetting prepolymer and an optional volatile organic compound to provide a curable mixture; forming the curable mixture with a dispersed phase in the form of continuous fibers into a layer material comprising opposing first and second layer surfaces; applying a magnetic field in the presence of a static electromagnet to the layer material; mechanically vibrating the layer material in the parallel, orthogonal
  • Fiber-reinforced composites are typically constructed with continuous fibers that are bundled into tows, assembled into woven or non-woven fabrics, and encased in a resin matrix.
  • carbon fiber composites formed into layers or plies offer exceptional strength in the direction of the strong-axis of the carbon fibers (e.g. in-plane) but are drastically weaker when loads are applied perpendicular to the fibers (e.g. through-plane). While, these composite plies are laminated to create a structure with excellent bulk in-plane properties, the lack of through-thickness reinforcement makes the laminated composite structure especially prone to interlaminar micro-cracks and through-ply fissures. These cracks and fissures degrade the integrity of the component and can eventually result in the delamination and catastrophic failure of the carbon fiber composite structure.
  • Magnetized particles e.g. discontinuous fibers of carbon, basalt, silicon carbide, silicon nitride, aramid, zirconia, nylon, boron, alumina, silica, borosilicate, or mullite or platelets of alumina, boron nitride, or graphite with at least one long axis less than 1 millimeter
  • a liquid-phase solvent of volatile organic compound e.g. isopropanol, butanol, ethanol, acetone, toluene, or xylenes
  • the magnetized particles account for at most 85 percent by volume of the slurry in this example.
  • the slurry is deposited onto a woven (e.g. bi-directional, multi-directional, or quasi-isotropic) or non-woven (e.g., uni-directional, veil, or mat) fabric of carbon, basalt, silicon carbide, aramid, zirconia, nylon, boron, alumina, silica, borosilicate, mullite, cotton, or any natural or synthetic long-fibers.
  • the slurry wets, coats, and/or surrounds the continuous fibers of the fabric.
  • the fabric containing the slurry is then exposed to a magnetic field of at most 10 teslas in field strength in this example.
  • the magnetic field aligns the magnetized particles within the fabric in the direction of the magnetic field.
  • the fabric is heated to evaporate the bulk solvent of the slurry, resulting in dry ply material with through-plane aligned particles embedding and/or coating the fabric.
  • the dry ply material is coated with a liquid-phase binder (e.g. epoxy, polyester, vinyl ester, polyethylenimine, polyetherketoneketone, polyaryletherketone, polyether ether ketone, polyphenylene sulfide, polyethylene terephthalate, polycarbonates, poly(methyl methacrylate), acrylonitrile butadiene styrene, polyacrylonitrile, polypropylene, polyethylene, nylon, silicone rubbers, polyvinylidene fluoride, styrene butadiene rubber, or pre-ceramic polymer).
  • the liquid-phase binder effectively wets the dry ply material to produce a pre-impregnated composite ply material.
  • This process may result in a high aligned particle content (up to 85 percent of total composite ply volume). Additionally, the solvent of the slurry can be removed prior to application of the liquid-phase binder, which may avoid issues with chemical incompatibility between the binder and the solvent. In some cases, this process may be useful for certain types of precursor dry ply material that is weak and brittle prior to the application of the liquid-phase binder.
  • Magnetized particles e.g. discontinuous fibers of carbon, basalt, silicon carbide, silicon nitride, aramid, zirconia, nylon, boron, alumina, silica, borosilicate, or mullite or platelets of alumina, boron nitride, or graphite with at least one long axis less than 1 millimeter
  • a liquid-phase binder e.g.
  • the magnetized particles account for at most 80 percent by volume of the slurry in this example.
  • an additional solvent thinner comprised of liquid-phase of volatile organic compound (e.g. isopropanol, butanol, ethanol, acetone, toluene, or xylenes), oil and/or water can be introduced to the slurry to assist in homogenously dispersing the magnetized particles into the liquid-phase binder.
  • volatile organic compound e.g. isopropanol, butanol, ethanol, acetone, toluene, or xylenes
  • the slurry is deposited onto a woven (e.g. bi-directional, multi-directional, or quasi-isotropic) or non-woven (e.g., uni-directional, veil, or mat) fabric of carbon, basalt, silicon carbide, aramid, zirconia, nylon, boron, alumina, silica, borosilicate, mullite, cotton, or any natural or synthetic long-fibers.
  • the slurry wets, coats, and surrounds the continuous fibers of the fabric.
  • the fabric containing the slurry is then exposed to a magnetic field of at most 10 teslas in field strength in this example.
  • the magnetic field aligns the magnetized particles within the fabric in the through-plane direction.
  • the fabric is heated to evaporate the bulk solvent thinner, resulting in a composite ply material with a liquid-phase binder.
  • the composite ply material is either further heated or cooled to consolidate the composite ply material by solidifying, hardening, gelling, or freezing the liquid-phase binder to produce a pre-impregnated composite ply material.
  • This process may result in a low aligned particle content (up to 20 percent of total composite ply volume). Additionally, the lack of a solvent during processing of low particle loading slurries may allow streamlined manufacturing with minimal solvent fume management and lower emissions. A solvent thinner may be used to disperse particles into the liquid-phase binder. This process also may use heating of the produced material after the liquid-phase binder has been added to remove the solvent.
  • Particles e.g. discontinuous fibers of carbon, borosilicate, or nylon with at least one long axis less than 1 millimeter
  • a woven fabric comprised of carbon, borosilicate, or nylon and embedded in a matrix of epoxy, polyester, vinyl ester, polyether ether ketone (PEEK), acrylonitrile butadiene styrene (ABS), high-density polyethylene (HDPE), or nylon.
  • PEEK polyether ether ketone
  • ABS acrylonitrile butadiene styrene
  • HDPE high-density polyethylene
  • This formulation may be used to provide a composite ply with at least three axes of fiber orientation.
  • This fiber structure allows the composite ply to efficiently distribute stresses between subsequent plies and adjacent components, which may reduce or eliminate the accumulations of stress concentrations. The reduction or elimination of stress concentrations can significantly improve the strength of a laminated composite structure under dynamic loads.
  • This formulation may be useful when a laminated composite structure is formed with small features or mates with a material with drastically different stiffness (e.g. metal alloys or plastics).
  • Example applications include dome reinforcement for Type III, IV, and V pressure vessels, wing tips and trailing/leading edges for wind turbines, hydrofoils for marine vehicles, aerodynamic winglets for automobiles, and aerostructure bolt/rivet fastener attachments for aircrafts.
  • Particles e.g. discontinuous fibers of carbon, borosilicate, or nylon with at least one long axis less than 1 millimeter
  • a non-woven fabric comprised of carbon, borosilicate, or nylon and embedded in a matrix of epoxy, polyester, vinyl ester, polyether ether ketone (PEEK), acrylonitrile butadiene styrene (ABS), high-density polyethylene (HDPE), or nylon.
  • the particles are transversely oriented to the continuous fibers of the fabric.
  • This formulation may provide a composite ply with through-plane reinforcement of the interlaminar region.
  • This fiber reinforcement allows the composite ply to efficiently distribute stresses between adjacent layers to hinder the formation of cracks and prevents a crack from propagating in the interlaminar region.
  • the targeted reinforcement of the interlaminar region can significantly improve the strength of a laminated composite structure under shock and cyclic loads.
  • This formulation may be useful when a laminated composite structure is formed with long sheets of composite ply, for example, where a single crack in the interlaminar region between the plies can compromise the structural integrity of the overall structure.
  • Example applications include over-wraps for Type III, IV, and V pressure vessels, spars for wind turbines, hulls for marine vehicles, chassis panels for automobiles, and wings, and turbine fan blades for aircrafts.
  • Particles e.g. discontinuous fibers of carbon or borosilicate with at least one long axis less than 1 millimeter
  • a woven fabric comprised of borosilicate or nylon and embedded in a matrix of epoxy, polyester, vinyl ester, polyether ether ketone (PEEK), acrylonitrile butadiene styrene (ABS), high-density polyethylene (HDPE), or nylon.
  • the particles comprise over 50 percent by volume of the overall composite and are transversely oriented to the continuous fibers of the fabric in this example.
  • This formulation provides a composite ply with through-plane reinforcement, e.g., as a through-plane uni-directional fabric.
  • This fiber reinforcement targets through-plane loads (e.g. point loads and high-pressure loads) and the scrim fabric offers minimal in-plane reinforcement.
  • the targeted through-plane reinforcement can significantly improve the strength and stiffness of a laminated composite structure under expected through-plane mechanical loads.
  • This formulation may be useful for effectively handling a composite ply with through-plane reinforcement that can easily deform during handling in an un-cured state while forming an exterior shell for a laminated composite structure.
  • Example applications include repairs to the interior features of tooling for injection molding, shims used in jacking heavy structures, and surfaces of bats and sticks for sports.
  • Particles e.g. discontinuous fibers of silicon carbide, silicon nitride, zirconia, boron, alumina, silica, or micro-platelets of alumina, boron nitride with at least one long axis less than 1 millimeter
  • a woven e.g.
  • bi-directional, multi-directional, or quasi-isotropic fabric comprised of carbon, borosilicate, or nylon and embedded in a matrix of epoxy, polyester, vinyl ester, polyether ether ketone (PEEK), acrylonitrile butadiene styrene (ABS), high-density polyethylene (HDPE), or nylon.
  • the particles are transversely oriented to the continuous fibers of the fabric.
  • This formulation provides a composite ply with through-plane oriented particles with excellent hardness and/or chemical stability.
  • the through-plane reinforcement can significantly improve the polymer matrix's resistance to damage from mechanical wear (e.g. abrasion) and/or chemical corrosion (e.g. oxidization).
  • This formulation may be useful for forming surfaces that protect structures from mechanical and chemical wear.
  • Example applications include Class A surfaces for automobiles, skins for aircrafts, and panels for buildings.
  • Particles e.g. discontinuous fibers of carbon or micro-platelets of graphite with at least one long axis less than 1 millimeter
  • a woven fabric comprised of carbon and embedded in a matrix of epoxy, polyester, vinyl ester, polyether ether ketone (PEEK), acrylonitrile butadiene styrene (ABS), high-density polyethylene (HDPE), or nylon.
  • PEEK polyether ether ketone
  • ABS acrylonitrile butadiene styrene
  • HDPE high-density polyethylene
  • the particles are transversely oriented to the fibers of the fabric.
  • the particles comprise over 50 percent by volume of the overall composite and are transversely oriented to the continuous fibers of the fabric.
  • This formulation provides a composite ply with enhanced through-plane electrical conductivity and can significantly improve the resistance to damage caused by localized heat generation induced by charge accumulation upon rapid discharge of electrical energy (e.g. lightning).
  • This formulation may be useful for forming surfaces that protect structures from damage from electrical discharge.
  • Example applications are skins and leading/trailing edges for aircrafts and wind turbines.
  • Particles e.g. discontinuous fibers of carbon or micro-platelets of graphite with at least one long axis less than 1 millimeter
  • a non-woven fabric comprised of carbon and embedded in a matrix of epoxy, polyester, vinyl ester, polyether ether ketone (PEEK), acrylonitrile butadiene styrene (ABS), high-density polyethylene (HDPE), or nylon.
  • the particles are transversely oriented to the continuous fibers of the fabric.
  • This formulation provides a composite ply with enhanced near-isotropic electrical conductivity and can effectively conduct electrical signals across long and through thick composite structures.
  • Example applications are aircraft and wind turbine de-icing systems that implement ohmic heating to prevent accumulation of ice and composite health monitoring systems that implement electrical signals to detect delamination within thick and/or long laminated composite structures.
  • Particles e.g. discontinuous fibers of carbon or micro-platelets of graphite with at least one long axis less than 1 millimeter
  • a woven fabric comprised of carbon and embedded in a matrix of epoxy, polyester, vinyl ester, polyether ether ketone (PEEK), acrylonitrile butadiene styrene (ABS), high-density polyethylene (HDPE), or nylon.
  • the particles are transversely oriented to the continuous fibers of the fabric.
  • This formulation provides a composite ply with enhanced isotropic electrical conductivity and can effectively attenuate incident electromagnetic waves.
  • Example applications are skins for aircrafts that absorb radar signals for stealth.
  • Particles e.g. micro-platelets of alumina or boron nitride with at least one long axis less than 1 millimeter
  • a woven fabric comprised of borosilicate and embedded in a matrix of polypropylene (PP) and polyethylene (PE).
  • PP polypropylene
  • PE polyethylene
  • This formulation provides a composite ply with low radio-frequency interference and enhanced through-plane thermal conductivity to effectively transmit electromagnetic waves without overheating.
  • Example applications include radomes for telecommunications.
  • Particles e.g. e.g. discontinuous fibers of carbon, silicon carbide, silicon nitride, alumina, or micro-platelets of alumina, boron nitride, or graphite with at least one long axis less than 1 millimeter
  • a woven fabric comprised of carbon and embedded in a matrix of epoxy, polyester, vinyl ester, polyether ether ketone (PEEK), acrylonitrile butadiene styrene (ABS), polypropylene (PP), polyethylene (PE), nylon.
  • the particles are transversely oriented to the continuous fibers of the fabric.
  • This formulation provides a composite ply with enhanced through-plane thermal conductivity sufficient structural integrity. This formulation may be useful to increase structural integrity under rapid temperature fluctuations.
  • Example applications are skins for spacecraft during atmospheric re-entry and brake discs for vehicles.
  • Particles e.g. e.g. micro-platelets of alumina or boron nitride with at least one long axis less than 1 millimeter
  • a woven fabric comprised of carbon and embedded in a matrix of epoxy, polyester, vinyl ester, polyether ether ketone (PEEK), acrylonitrile butadiene styrene (ABS), high-density polyethylene (HDPE), nylon, or silicone rubbers.
  • PEEK polyether ether ketone
  • ABS acrylonitrile butadiene styrene
  • HDPE high-density polyethylene
  • nylon or silicone rubbers.
  • the particles are transversely oriented to the continuous fibers of the fabric.
  • the particles comprise over 50 percent by volume of the overall composite
  • This formulation provides a composite ply with excellent through-plane thermal conductivity and low electrical conductivity. This formulation may be useful for effectively moving and distributing heat flux, e.g., in electronics.
  • Example applications include printed circuit board laminates, gap fillers, and encapsulants for electronic devices.
  • Particles e.g. discontinuous fibers of carbon or micro-platelets of graphite with at least one long axis less than 1 millimeter
  • a non-woven fabric comprised of carbon embedded in a matrix of polyvinylidene fluoride (PVDF) or styrene butadiene rubber (SBR).
  • PVDF polyvinylidene fluoride
  • SBR styrene butadiene rubber
  • This formulation provides a carbon-based composite ply with excellent through-plane electrical conductivity. This formulation may be useful for adsorbing ionic species from an electrolyte and/or efficiently distributing electrical charge.
  • Example applications include anodes for electrochemical batteries (e.g. lithium-ion and sodium-ion cells) and electrodes for supercapacitors.
  • Particles e.g. discontinuous fibers of carbon with at least one long axis less than 1 millimeter
  • PAN polyacrylonitrile
  • This formulation provides a precursory composite ply with through-plane carbon fiber catalysts. At appropriate temperatures, the PAN matrix may oxidize and carbonize into a carbon matrix. This formulation may be useful for creating ex-PAN carbon-carbon composites with isotropic grains.
  • This prophetic example illustrates formulations for ceramic matrix composites (CMCs).
  • Particles e.g. discontinuous fibers of carbon and silicon carbide with at least one long axis less than 1 millimeter
  • preceramic monomers e.g. siloxane, silazane, or carbosilane
  • thiol thiol
  • vinyl acrylate
  • methacrylate methacrylate
  • epoxy R-groups epoxy
  • This formulation may provide a precursory composite ply with through-plane carbon fiber or silicon carbide catalysts. At appropriate temperatures, the polymer matrix can oxidize into a ceramic matrix. This formulation may be useful for creating ceramic matrix composites with isotropic grains.
  • a reference to “A and/or B”, when used in conjunction with open-ended language such as “comprising” can refer, in one embodiment, to A only (optionally including elements other than B); in another embodiment, to B only (optionally including elements other than A); in yet another embodiment, to both A and B (optionally including other elements); etc.
  • the phrase “at least one,” in reference to a list of one or more elements, should be understood to mean at least one element selected from any one or more of the elements in the list of elements, but not necessarily including at least one of each and every element specifically listed within the list of elements and not excluding any combinations of elements in the list of elements.
  • This definition also allows that elements may optionally be present other than the elements specifically identified within the list of elements to which the phrase “at least one” refers, whether related or unrelated to those elements specifically identified.
  • “at least one of A and B” can refer, in one embodiment, to at least one, optionally including more than one, A, with no B present (and optionally including elements other than B); in another embodiment, to at least one, optionally including more than one, B, with no A present (and optionally including elements other than A); in yet another embodiment, to at least one, optionally including more than one, A, and at least one, optionally including more than one, B (and optionally including other elements); etc.
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Publication number Priority date Publication date Assignee Title
WO2022101003A1 (fr) * 2020-11-11 2022-05-19 Coeus Limited Enveloppe structurale
CN114633493A (zh) * 2022-01-21 2022-06-17 南京航空航天大学 一种新型磁引导层间颗粒增强复合材料及其制备方法
US11479656B2 (en) * 2019-07-10 2022-10-25 Boston Materials, Inc. Systems and methods for forming short-fiber films, composites comprising thermosets, and other composites
US11840028B2 (en) 2018-12-10 2023-12-12 Boston Materials, Inc. Systems and methods for carbon fiber alignment and fiber-reinforced composites

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7149577B2 (ja) * 2018-10-15 2022-10-07 有限会社ヒロセ金型 炭素繊維強化樹脂成形品の製造方法、及び炭素繊維強化樹脂成形品
CN112466681B (zh) * 2020-11-20 2022-01-14 东莞东阳光科研发有限公司 一种电极及其制备方法
FR3118096B1 (fr) * 2020-12-18 2023-11-17 Safran Aircraft Engines Aube en materiau composite a matrice au moins partiellement ceramique
FR3118030B1 (fr) 2020-12-18 2023-09-01 Safran Ceram Procédé de fabrication d’une pièce en matériau composite à matrice céramique
US20230272256A1 (en) 2022-02-28 2023-08-31 Boston Materials, Inc. Thermally conductive aligned materials and methods of making and use thereof
US20240052558A1 (en) 2022-08-15 2024-02-15 Boston Materials, Inc. Thermal interface materials comprising aligned fibers and materials such as solder, alloys, and/or other metals
TWI821018B (zh) * 2022-11-14 2023-11-01 天下長榮科技有限公司 交織纖維複合材料

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050239948A1 (en) * 2004-04-23 2005-10-27 Yousef Haik Alignment of carbon nanotubes using magnetic particles
US20110186775A1 (en) * 2010-02-02 2011-08-04 Applied Nanostructured Solutions, Llc. Carbon nanotube-infused fiber materials containing parallel-aligned carbon nanotubes, methods for production thereof, and composite materials derived therefrom

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5432000A (en) * 1989-03-20 1995-07-11 Weyerhaeuser Company Binder coated discontinuous fibers with adhered particulate materials
JP3362493B2 (ja) * 1993-12-28 2003-01-07 日本エクスラン工業株式会社 磁性繊維およびその製造方法
JP3461054B2 (ja) * 1994-04-04 2003-10-27 株式会社豊田中央研究所 複合材料
WO2001025514A1 (fr) * 1999-10-04 2001-04-12 Insung Powdertech Co., Ltd. Fibre et tissu renfermant un materiau magnetique
US8173857B1 (en) * 2000-12-20 2012-05-08 Patrick Yananton Adhesion of particles of active ingredients to an open pore substrate
US7935415B1 (en) * 2002-04-17 2011-05-03 Conductive Composites Company, L.L.C. Electrically conductive composite material
EP2013408B2 (fr) * 2006-05-02 2016-09-28 Rohr, Inc. Nacelles et ses composants utilisant des nanorenforcements
US20080145647A1 (en) * 2006-12-13 2008-06-19 Rahul Ganguli Metal impregnated composites and methods of making
DE102007042554B4 (de) * 2007-09-07 2017-05-11 Carl Freudenberg Kg Vliesstoff mit Partikelfüllung
US20120289107A1 (en) * 2011-04-22 2012-11-15 OSUS, Inc. Metal/polymer composite fibers
US20130252497A1 (en) * 2011-11-14 2013-09-26 Faserinstitut Bremen E.V. Thermoplastic fibre, hybrid yarn, fibre perform and method for producing fibre performs for fibre composite components, in particular high performance fibre composite component, using the same, fibre composite component and method for producing fibre composite components, in particular high performance fibre composite components
JP6392027B2 (ja) * 2013-08-30 2018-09-19 株式会社東芝 タービン翼
US10096396B2 (en) * 2014-08-25 2018-10-09 The Boeing Company Composite materials with improved electrical conductivity and methods of manufacture thereof
US10472472B2 (en) * 2014-09-23 2019-11-12 The Boeing Company Placement of modifier material in resin-rich pockets to mitigate microcracking in a composite structure
GB201522393D0 (en) * 2015-12-18 2016-02-03 Rolls Royce Plc Composite component forming method
CN105690802B (zh) * 2016-02-06 2018-06-26 陕西科技大学 一种碳纤维增强高分子基复合材料的制备方法及应用
CN105734535B (zh) * 2016-03-18 2019-03-05 大连理工大学 一种提高复合材料镍镀层结合强度的方法

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050239948A1 (en) * 2004-04-23 2005-10-27 Yousef Haik Alignment of carbon nanotubes using magnetic particles
US20110186775A1 (en) * 2010-02-02 2011-08-04 Applied Nanostructured Solutions, Llc. Carbon nanotube-infused fiber materials containing parallel-aligned carbon nanotubes, methods for production thereof, and composite materials derived therefrom

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11840028B2 (en) 2018-12-10 2023-12-12 Boston Materials, Inc. Systems and methods for carbon fiber alignment and fiber-reinforced composites
US11479656B2 (en) * 2019-07-10 2022-10-25 Boston Materials, Inc. Systems and methods for forming short-fiber films, composites comprising thermosets, and other composites
US11767415B2 (en) 2019-07-10 2023-09-26 Boston Materials, Inc. Systems and methods for forming short-fiber films, composites comprising thermosets, and other composites
US11820880B2 (en) 2019-07-10 2023-11-21 Boston Materials, Inc. Compositions and methods for carbon fiber-metal and other composites
WO2022101003A1 (fr) * 2020-11-11 2022-05-19 Coeus Limited Enveloppe structurale
CN114633493A (zh) * 2022-01-21 2022-06-17 南京航空航天大学 一种新型磁引导层间颗粒增强复合材料及其制备方法

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