STRUCTURAL COMPOSITE MATERIALS

CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims priority to U.S. Provisional Patent Application No. 62/1 7,964, Filed on My ^' 28., 2015, the entire contents of which are incorporated herein by reference.

TECHNICAL FIELD

This disclosure relates to composite materials that can be used for a variety of applications and products (e.g., on-site co struction, production of pre-cast structural •components) and methods of making composite materials.

BACKGROUND

Materials such, as stone and earth nave been used for thousands of years as structural materials in construction. One of the first cements included limestones and additives such as trass and pozzolanas. In the 1800's, Portland cement was developed. Portland cement is a hydraulic material including, for example, calcium silicates, calcium oxide, silicon dioxide, ahunkrum oxide, ferric oxide, and calcksm sulfate. Processing of these materials to form the cement involves calcination at high temperatures (e.g.. about 1550 <'C). Setting of the cement is accomplished in hours to days using water by means of a series of chemical reactions, with hardening over the course of a few weelks. Portland cement is used in the _. roduction of concrete when mixed with an aggregate (e.g., gravel, stone, or sand) and water.

Each year, approximately 2-4 billion tons of Portland cement are used in the world, of which approximately 80 millio tons are used in the U.S. About 1.5% of toe Portland cement is used to produce precast concrete parts. Precast parts have been widely used in construction and maintenance of buildings and transportation systems as, for example, panels, columns, supports, and pipes. Using precast parts typically reduces the duration of construction projects and simplifies construction procedures.

About 4 GJ of energy is consumed to produce one ton of Portland cement, accounting for 5- 10% of the entire industrial energy consumption. In addition. .Portland cement production accounts for approximately 3-10% of the total human- produced atmospheric carbon dioxide.

Poly mer cements can be used in many applications as substitute for Port land cement and have a high tensile s ren h in addition to a compressive strength that, is comparable to or higher than Portland cement Binders used in polymer cements function to bond together the filler material portion of the cement, and bear much of the load that the cement is subjected to when used in structural applications.

SUMMARY

The "economic and environmental costs of producing structural materials such as cement is significantly attributable to the cost of the binders used in the cements. For example, polymer cements typically cost about §200 per ton to produce, of which greater than 60% of this cost is that of the hinder. Yearly carbon dioxide emissions ftom die manufacture of polymer cement is estimated at about 450 kg per ton of polymer cement produced.

To reduce the costs - both economic and environmental - associated with producing materials suitable for structural use in construction,, batteries, fabrication of pre-cast parts, and a variety of other applications, the present application discloses composite materials and methods of making such materials in which the amount of binder material in the composite is significantly reduced relati ve to conventional structural materials. For example, in the composite materials disclosed herein, the amount of binder material can he less than 9% by weight, less than 18% by volume, or both.

By significantly reducing the amount of binder material in the composite materials, the economic and environmental costs associated with producing ^' Structural materials can be significantly reduced. Accordingly, construction costs can be lowered, energy consumption can be reduced, and carbon dioxide emissions associated with the production "of building materials such as cement can be lowered.

In addition, by applying the processing methods- disclosed herein to produce the composite materials, the binder material - even when present in relativel small amounts can be distributed among the filler material so that composite materials having relatively small amounts of binder material still have pbysical properties, such as relati vely high flexural and compressive .strength, that are favorable for use in structural and/or functional applications.

The processing methods disclosed herein are flexible and can be used to prepare coitrposite niaterials featuring a wide variety of different binder niaterials and filler materials. For example, suitable filler materials can include recycled concrete, sand, soil, rocks, gravels, stones, bricks, metals, alloys, ceramics, glasses, miictional solid or gel fillers, solid waste, carbon materials, polymers, and/or elastomers, and any components of thes materials. The use of recycled waste or other repurposed materials as filler material further highlights the inherent cost-effectiveness and environmental friendliness of the methods and provides, for example, a means for developing countries to foll and efficientl utilize their existing resources.

The methods can be used to produce pre-cast. structural, components from the composite materials for use in construction. In addition, the methods can be used on- site to prepare composite materials for direct use in structural fabrication. The methods can be implemented using conventional, eqisipment and infrastructure that is already in use for the production of widely used cements, concretes, and other aggregate-based materials, and also find wide applications in. other industries such as food production, medicine production, battery and capacitor manufacturing, _, and production of artificial biomaterials. Bio-compatible filler materials and filler materials such .as various glasses can.be used, to fabricate materials with an

aesthetically pleasing appearance, which can be particularly important for biological and therapeutic applications (e.g., fabrication of bio-compa tible prosthe tics) arid in building construction applications.

In first aspect, the disclosure features composite materials that, include a filler material and a binder material disposed between at least some units of the filler material to form a solid, integral composite material, where the composite niaterials include less than 9% by weight of the binder materi al, less than 18% by vol ume of the binder material, or both, mid where the composite materials have a flexural strength of at least 3 MPa.

Embodiments of the composite materials can include an one or more of the following features. The binder material can include at least one material selected from the group consisting of thermoplastic - materials, thermosetting materials, elastomeric materials, polymer materials- ceramic materials, glasses, metals, alloys, salts, carbon materials, and sulfiir-cofttaining materials. The binder material can include, at least one material selected .from, the group consisting of polyesters, polyethersulfbnes, polysulfoaes, polyetherimides, epoxies, fiuoropolyniers, phenolic materials, vinyl esters, carboxyiTiethyleeilulose-basecl materials, polyetherfcetones, cyclic oligomers, polymethyl metliacrylaies, polycarbonates, and polyhwylene terephfhaiates.

The filler material can include at least one material selected . from the group consisting of sand, soil, rocks, gravel, stones, bricks, concrete, cement, wood, metals, alloys, ceramics, polymers, composites, glasses, carbon materials, solid waste, medicine, food, electrod materials, and omponent thereof. The soil can include extraterresti al soil, rocks, and/or minerals. The filler material can include units of at least one material in the form of at least one of powders, beads, dots, grains, particles, chips, cubes, layers, laye stacks, blocks, spheres, fibers, tubes, beams, pipes, rods, threads, platelets, coatings, hollow beads, hollow fibers, hollow blocks, hollow layers, bilayers, porous materials, meshes, fabrics, mats, honeycombs, and three-dimensional forms.

The composite materials can include at least one additive material selected from the group consisting of foaming agents , bubble-generating agents, so l ven ts, and lubricants.

The composite materials can have a compressive strength of at least 10 MPa (e.g., at least 40 MPa). The composite materials can have a flexural strength of at least 5 MPa (e.g., at least 10 MPa).

At least one of the weight percentage of the binder material and the volume percentage of ihe binder mater ial can vary within the composite materials. The composite materials can nclude a first region in which the weight percentage of the binder material has a first value, id a second region in which the weight percentage of the binder material has a second val ue different from the first value. The first and second values can each be less than 9%. The composite materials can include first region in which the volume percentage of ihe binder material has a first value, and a second region in w hich the volume percentage of the binder material has a second value different from he first value. The first and second values can each be less than 18%.

The composite materials ca include a first binder .material, and a second binder .material different from th e first binder material , The second binder material ca t include at least one materia! selected from ^' the gr up consisting -of thermoplastic materials, thermosetting materials, elastoiBeric materials, polymer materials, ceramic materials, glasses, metals, alloys, -salts, carbon materials, and sulfur-containing materials. The second binder material can include at least one material selected from the group consisting of polyesters, polyetliersnlfones, polysiilfones, polyetherimides, epoxi.es, _· fmotopolymers, phenolic materials, vinyl esters, carooxymethyleeiluiose- based materials, ..po!yetherketones, cyclic, oligomers, poly methyl rnethacrylates, polycarbonates, and po!ybutylene tereph h lates.

The composite ^■ ma eriasl can include a first filler material, and a second filler material different from the first filler material The second filler material can include at least one material selected from the group consisting of sand, soil, rocks, gravel, stones, bricks, concrete, cement, wood, metals, alloys, ceramics, polymers, composites, glasses, carbon materials, solid waste, medicine, food, electrode materials, and components thereof.

The composite materials can include less than 5% by weight of the binder material (e.g., less than 3% by weight of the binder material). The composite materials can include less than 10% by volume of the binder material (e.g., less than 5% by volume of the binder material).

Embodiments of the composite materials can also include any of the other features disclosed herein, including 'Combinations of features disclosed in connection with different embodiments, in. any combination as appropriate,

in another aspect, the disclosure features methods of forming ^' a composite material that include forming a mixture that includes a binder material and a filler material, and applying a pressure of at least 10 MPa to the mixture to form the composite material, where the mixture includes less than 9% by. weight of the binder material, less than 18% by volume of the binder material, or both.

Embodiments of the methods can include any one or more of the follo wing features. The methods can include breaking the composite material into a plurality of pieces, and applying a second pressure of at least l MPa ^' to the plurality of pieces. The methods cast include heating the composite ma terial to a temperature of at least 50 °C,

The methods can include forming a pre~east component including the composite material by positioning the -mixture in a mold having a shape conforming to a shape of the -pre-cast component, and applying he pressure to the mixture in the mold. The methods can include applying the pressure to the mixture by contacting the mixture with a compressive load.

The pressure can be applied to the mixture for a duration of at least 1 second.

The methods ca include applying a second pressure of at least 10 MPa to the mixture. Each application of pressure to the mixture can include impacting the mixture with an impact member. Each application of pressure to the mixture can occur for a duration of 1 second or less. During each application of pressure to the mixture, the pressure applied to the mixture can increase from zero to a maximum pressure in a time period of 1.00 microseconds or less.

The pressure can be applied to the mixture by translating a pressurizing member relative to the mixture to apply the pressure to different portions of the mixture at different times. The pressurizing member can include a rolle or a piston.

The mixture can include less than 5% by weight of the binder material (e.g., less than 3% by weight of the binder material, les s than 1 % by weight of the binder material). The mixture can include less than 10% by volume of the binder material (e.g., less than 5% by volume of the binder material).

The binder material can include at least one material selected from the group consisting of thermoplastic materials, thermosetting materials, elastomeric materials, polymer materials, ceramic materials, glasses, carbon materials; metals, alloys, salts, and sulfur-containing materials. The binder material can include at least one material selected from the group consisting of polyesters, polyet ersulfones, polysulfones, ^■ pblyetherimides. epoxies, lluoropo!ymers, phenolic materials, vinyl esters, carboxymethyicellulose-based materials, polyetherketones, cyclic oligomers, polyrnethyl inethaerylaies, .polycarbonates, and poiyburylene terephthalates. The filler material can include at least one m terial selected from the group consisting of sand, soil, rocks, gravel, ^' stones, bricks, metals, alloys, ceramics, polymers, composites, glasses, solid waste, medicine, food, carbon materials, electrode materials, and com onents thereo The: soil can include extraterrestrial soil, rocks, and/or minerals. The filler materia! can include units of one or more materials in the for m of at least one of po wders, beads , dots, grains , particles, chips, c ubes, layers, layer stacks, blocks, spheres, fibers, tubes, beams, pipes, rods, threads, platelets, coatings, hollow beads, hollow fibers, hollow blocks, hollow layers, biiayers, porous materials, meshes, fabrics, mats, honeycombs, and three-dimensional forms. The mixture can include at least one additi ve selected from the group

consisting of foaming agents, bobble-generating agents, solvents, and lubricants.

The applied pressure can be at least 40 MPa (e.g. , at least .100 MPa),

Embodiments of the methods can also incl ude any of the other features disclosed herein, including combinations of features disclosed in connection with different embodiments, in an combination as appropriate.

In a further aspect, the disclosure features composite materials including a filler material, and a binder material disposed between at least some units of the filler material to form a solid, integral composite material, where the composite materials include less than 18% by weight of the binder material, less than 18% by vo lume of the binder materi l, or both, and where for temperature increase of at least 20 °C, an electrical resistance of the composite material increases by at least 20%.

Embodiments of the composi te materi als can include any one or more of the following features.

The electrical resistance of the composite materials can mcrease by at least 100% (e.g. , by at least 1000%),

The binder material can include poiy(vinylidene) fluoride. The filler material can be a first filler material including at least one of silica and motttmooilonite, and the composite material can further include a second filler material including carbon black.

The binder material can include at least one materi al selected from the group consisting of thermoplastic materials, thermosetting materials, eiasfomeric materials, polymer materials, ceramic materials, glasses, metals, alloys, salts, carbon materials. and sulfM-coniaining materials. The binder material can include at least one material selected from the grou consisting of polyesters, polyeUiersuifones, polysulfones, polyetherimides, epoxtes, fl oropo! mers, phenolic materials, vinyl esters, catboxy emyiceilulose-based materials, poiyetfierfeetones, cyclic oligomers, pol niethyl ethaery lares, polycarbonates, a»d poi bi yiene ierephtha!ates.

The filler material can include at least one material selected from the group consisting of sand, soil, rocks, gravel, stones, bricks, concrete, cement, wood, metals, alloys, ceramics, polymers, elastomeric materials, composites, glasses, carbon materials, solid waste, medicine, food, electrode materials, and components thereof. The filler material can include units of at least one material in the form of at least one of powders, beads, dots, grains, particles, chips, cubes, lay ers, lay er stacks, blocks, spheres, fi ers, tubes, beams, pipes, rods, threads, platelets, coatings, hollow beads, hollow fibers, hollow blocks, hollow layers, bilayers, porous materials, meshes, fabrics, mats, honeycombs, and three-dimensional forms.

The composite materials can form a portion of at least one of an electrode, a current collector, a separator, a capacitor, an electrolyte, and a housing within an electrical device.

Embodiments of the composite materials can also include an of the other features disclosed herein, including combinations of features disclosed in connection with different embodiments, in an combination as appropriate,

in another aspect, the disclosure features composite materials including a filler material, and a binder material disposed between at least some - units of the filler material to form a solid, integral composite material, where the composite materials include less than 18% by weight of the binder material, less than 18% by volume of the binder material, or both, and where in response to an applied pressure of at least 0J MPa, as electrical resistance of the composite materials increases by at least 20%.

Embodiments of the composite materials can include any one or more of the followin features.

The electrical resi stance of the composite materials can increase by at least 100% (e.g., by at least 1000%).

The binder material can include poly(vinylidene) fluoride. The filler material can be a first filler material including at least one of silica and montmorillonite, and the composite materials can further include a second filler material including carbon black.

The binder material cart include at least one material selected from the group consisting of thermoplastic materials, thermosetting materials, elastptneric materials, polymer materials, ceramic materials, glasses, metals, alloys, salts, carbon materials, and stilfm'-containing materials. The binder material can include at least one material selected from the group consisting of olyesters, polyethersulfoaes, polysulfones, polyetherimides, epoxies ilnoropolyraers, phenolic materials, viny l esters,

.carboxyinethylcellulose-based materials, polyetherketones. cyclic oligomers, polymethyi .methacryiates, polycarbonates, and pQlybetylene ferephthalates.

The filler material can include at least one material selected from the group consisting of sand, soil, rocks, gra vel, stones, bricks, concrete, cement, wood, metals, alloys, ceramics, polymers, elastomeric materials, composites, glasses, carbon materials, solid waste, medicine, food, electrode materials, and components thereof. The fi ller material can include units of at least one material in the form of at least one of powders, beads, dots, grains, particles, chips, cubes, lay ers, lay er stacks, blocks, spheres, fibers, tubes, beams, pipes, rods, threads, platelets, coatings, hollow beads, hollow fibers, hollow blocks, hollow layers, hilayers, porous .materials, meshes, fabrics, mats, honeycombs, and three-dimensional forms.

The composite material s can form a portion of at least one of an electrode, a current collector, a separator, a capacitor, an electrolyte, and a housing within an electrical device.

.Embodiments of the composite materials can also include any of the other features disclosed herein, including combinations of features disclosed in connection with different embodiments, in. any combination as appropriate.

In a further aspect, the disclosure features composite materials including a filler material, and a binder material disposed between at least some units of the filler material to form solid, integral composite material, where the composite materials at least one of: include less than 9% by weight of the binder material and ha ve a.

fiexural strengt that is at least .20% larger than a product of a. fiexural strength of the binder material and a weight percentage of the binder material in the composite materials; and include less than 18% b volume of the binder material and have a flexoral strength that Is at least 20% larger than a product of the flexora! strength of the binder material and a volume percentage of the binder material in the composite materials.

Embodiments of the composite materials can .include any one or more of the fo!lowing features.

The composite materials can include less than 9% by weight of the binder material and can have a flexoral strength that is at least 40% larger than the product of the fkxural strength, of the binder material and the weight percentage of the binder material in the composite materials.

The composite materials; can include less tha .18% by volume of the binder material and can have a fle wal strength that is at least 40% larger than the product, of the flexural strength of the binder material and the volume percentage of the binder -material i the composite materials.

The binder material can includ at least one material selected from the group consisting of thermoplastic materials;, thermosetting materials, elastomeric materials, polymer materials, ceramic materials, glasses, metals, alloys, salts, carbon materials, and siiifttr-containing materials. The binder material can include at least one material selected from the group consisting of polyesters, polyethersulfones, pol sulfoiies, polyetherimid.es, epoxies, fiuoropolysners, phenolic materials, vinyl esters, carboxyrnetl lceilulose-hased materials, pplyetherketones, cyclic oligomers, polymetliyi memacrylates, polycarbonates, and polybutyiene terephthalates.

The filler material can include at least one mateoal selected from the group consistin of: sand, soil, rocks, gravel, stones, bricks, concrete, cement, wood, metals, alloys, ceramics, polymers, composites, glasses, carbon materials, solid waste,

-medicine, food, electrode materials, any components thereof, and any combination thereof. The Slier material can include units of at least one material in the form of at least one of powders, beads, dots, grains, particles, chips, cubes, layers, layer stacks, blocks, spheres, fibers, tubes, beams, pipes, rods, threads, platelets, coatings, hollow beads, hollow fibers, hollow blocks, hollow layers, Mlayers, porous materials, meshes, fabrics, mats, honeycombs, and three-dimensional forms. The composite materials cart include at least one additive selected from the group consisting of foaming agents, babble-generating agents, sol ents, and lubricants.

The composite materials ear have a compressive strength of at least JO MPa (e.g. , at least 40 MPa). The composite materials can have a flexural strengt of a least 5 MPa (e.g., at least JO MPa).

Embodiments of the composi e materials can also include any of the other features disclosed herein, including combinations of features disclosed in connection with different embodiments, in any combination as appropriate,

In another aspect, the disclosure features batteries thai include a negativ electrode, an active materia! layer, a membrane separator disposed betwee the negative electrode and die active material layer, a current collector, and a composite material layer contacting the active- material layer and the current collector, where the composite material layer includes a filler material featuring at least one of ceramic materials and carbon materials, and a binder material featuring poly(vmy iidene) fluoride disposed between at least some units of the filler material to form a solid, integral composite material, where the composite material layer includes 18% or less by weight of tile binder material

Embodiments of the batteries can include any of the features disclosed herein, tnel tiding combinations of features disclosed in connection with different

embodiments, in any combination as appropriate.

In a further aspect the disclosure features medicaments that include a filler material featuring a digestible compound, a binder material includin

cai'boxymethy lce liiiose disposed between at least some units of the fil ler material to form a solid, integral composite material, and a pharmaceutical compound encapsulated by the composite material, where the binder material forms 9% by weight or less of the composite mater ia! .

Embodiments of the medicaments can include any of the features disclosed herein, including .combinations .of -features ^' disclosed in connection with different: embodiments, in any combination as appropriate.

I another aspect, the disclosure features biomimickin composite materials that include a fil ler material featuring particles of calcium c arbonate, and a binder material featuring an epoxy ma erial, disposed between at least som of the particles of calciism carbonate to form a solid, integral composite material, where the composite materials include 15% or less by weight of the binder material, and where the composite materials have a fiexural strength of at least 20 Pa.

Embodiments of the bto imicfctng composite materials can include any of the features disclosed herein, including combinations of features disclosed in connection with different embodiments, in. any combination as appropriate.

Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this disclosure belongs., A Ithoegh methods and materials similar or equivalent to those described herei can be used in the practice or testing of the subject matter herein, suitable methods and materials are described below. All publications, patent applications, patents, and other references mentioned herein are incorporated by reference in their entirety, in case of conflict, the present specification, including definitions, will control, hi addition, the materials, methods, and examples ^' are illustrative only and not Intended to be limiting.

The details of one or more embodiments are set forth in the accompanying drawings and the description below. Other features and advantages will be apparent from the description, drawings, and claims.

Definitions

As used herein, the terms "about" and "approximately" are used

interchangeably, and when used to refer to modify a numerical value, encompass a range of uncertainty of the numerical value of from ½ of the numerical value to twice the numerical value.

As used herein, the singular forms "a," "an," and "the" include plural referents unless the context clearly dictates otherwise.

As used herein, the term "binder materiaF refers to a material or substance that contacts units of a filler material (e g. , grains, particles, fibers, and/or other individual structural entities) and holds the units of the filler material together to form a solid, integral composite material A variety of different substances can be used as hinder materials, including for example thermoplastic materials, thermosetting materials, elastomeric materials, polymer materials (e.g., polyesters, polyethereulfones, poiysiilfones, polyetheri mides, epoxies, fluoropolymers, phenolic materials, vinyl esters, carboxyme by leelluiose-based materials, pol etherketones, cyclic oligomers, pojymethyl methacrylates _. , polycarbonates, and polyhutylene terep halates), ceramic materials, glasses, metals, alloys, salts, carbon materials, composites, and/or saifur-containiag materials.

As used herein, the term "filler material" refers to a material or substance that forms a majority (by percentage weight and/or by percentage volume) of a composite .material, effectively constituting a major portion of the bulk structure of the composite material A. variety of different substances can be used as filler materials, including for example sand, soil, rocks, gravel, stones, bricks, metals, alloys, ceramics, polymers, elastomeric materials, thermosetting materials, thermoplastic materials, composites, glasses, solid waste (e.g., recycled waste), carbon materials, medicine, food, electrode materials, and/or any components .of these materials.

As used herein, the term "compressive strength^ refers to the resistance of a material to a compressive force applied to the aterial and having a tendency to reduce the volume of the material. To determine the compressive strength of a material, a ^' compressive force is applied to the material, with the applied force increasing until the material is crushed (i.e., permanently deforms in a dimension along which the force is applied and/or fractures into multiple pieces due to the applied force). The compressi ve strength of a material, as used herein, is defined as- Fi Ao, where _c i s the compressive force that crashes the material and o is the initial cross-sectional area of the material over which th force is applied.

As used herein, the term ' ^" ftexural strength" refers to the resistance of material to a force applied t the material and .having a tendency to bend or elongate the material. A material's fiexural strength corresponds to the peak stress experienced in a material prior to the material yielding (i.e., fracturing) in a flexure test.

To determine th ftexural strength of a material, a three-point bending test is used.- I a three-point bending test, the material is formed as- a beam and supported at two fixed positions (e.g., near the ends of the material) on the same side of the material, and a piston contacts the opposite side of the material midway between the fixed positions, applying a compressive force that tends to cause a bending deformation of the material The flexura}. strength of a materia!, as used herein, is defined as R ~ (3i2)(PrsmxiJb ), _, where / max is the maximum load applied, during the three-point bending test (i.e., the maximum load that can be sustained by the material without yielding (i.e., fracturing), h Is the sample width, Lis the span length between the fixed supports, and d is the sample height/thickness (i.e., in a . ^' direction along which the force is applied).

As used herein, the term "deformability" refers to the maximu strain present in the composite material before final fracture happens, when the material is subjected to compressive, tensile, bending, or torsion loadings. For a material that deforms along a dimension in response to an applied load, the .material's defcmafalfity is defined as s~ (L-Le)/Le _r where L is the length, of the material along the dimension just befor fracture, and Lo is the length of the material along the dimension prior to the load being applied.

As used herein, the "crushing strength" of a material refers to the maximum compressive load that can be sustained by a material before it fractures into smaller pieces. A material's crushing strength is typically measured by using a piston to apply compressive force to a sam le of the material relatively slowly, noting the applied force j st prior to fracture.

The details of one or more embodiments are set forth i the accompanying drawings and the description below. Other features will be apparent from the description, drawings, and claims.

DESCRIPTION OF DRAWINGS

FIG. 1 is .a schematic diagram showing redistribution of a binder material f om interstitial gaps between filler material particles to regions of contact between the filler material particles during application of pressure to a mixture- of binder and filler materials,

FIG. 2 is a flowchart showing a first series of steps for producing a composite material.

F1G> 3 is a schematic diagram showing an example apparatus used to produce a composite material FIG.4 is a flowchart showing a second series of steps for producing a composite material.

FIG. 5 is a schematic diagram showing another example apparatus used to produce a composite material

FIGS. 6A-6B are schematic diagrams showing -stepwise compression of filler material and hinder materials by a piston and by a roller, respectively.

FIG. 7 is an image showing battery electrodes formed of a composite material

FIG. 8 is a plot, showing a charge-discharge curve of one of the battery elec trodes of FIG. 6.

FIG. 9 is a plot of fiexnral . t engt as a function of polyester binder content for a composite material that includes a sand filler material and a polyester binder material.

FIG. 10 is a plot of fiexnral strength as a function of peak compression pressure for a composite material that includes a sand filler material and a polyester hinder material.

FIG. 11 is art i mage of an example of a composite ma terial that includes a sand filler material and an epoxy binde material.

FIG. 12 is a plot of fiexural strength as a function of peak compression pressure for two composite materials, each including a sand filler material and an epoxy binder material.

FIG. 13 is an image of an example of a composite material that includes a soil filler material and an epoxy binder material

FIG. 14 is a plot of flexural strength as a fonction of peak compression pressure for two examples of composite materials, each including a soil fil ler materia! and an epoxy hinder material

FIG. 15 is a plot of flexural strength as a function of epoxy content for two examples of composite materials, each including a soil filler material and an epoxy binder material.

FIG. 16 is a plot of compressive strength as a function of peak compression pressure for two examples of composi te materials that include a sand fil ler materi a! and an epoxy binder material, in combination with a gravel aggregate material FIG. 17 is an image of an example of a composite ..material that includes a soil filler material and a polyetherketoneketone binder material.

FIG. 18 is a plot: of flexuraS strength as a function of peak compression pressure for an example of a composite material that includes soil fiHex material and a poiyedierketoneketone binder material .

FIG. 19 is a plot of peak compression pressure as a function of the number of impacts fbr an example of a composite material that includes a soil filler material and an epoxy hinder material.

FIG. 20 is a plot of tlexaral strength as a. funct on of the number of impacts for three examples of compos ite material s t hat Incl ude a so il fil ter material and an epoxy binder material,

FIG. 21 is an image of an example composite material that includes a glass filler material and an epoxy binder material,

FIG. 22 is an image of an example composite material thai includes a wood chip filler material and an epox binde material.

FIG. 23 is an image of an example composite material that includes a soil filler material and as epoxy binder material.

FI . 24 i an image of a load cell that includes divider.

FIG. 25 is an image showing examples of composite materials that include -a soil fille material and an epoxy binder material, and featuring voids or recesses.

FIG. 26 is an image showing an. example of an. L-shaped load cell.

FIGS. 27A-27C are schematic diagrams showing cross-sectional views of a coi cell including thermally responsive composite material connected to a battery while atop a heating element, a battery coin cell including a layer .of thermally responsive coniposite material, and a nail penetrating a battery coin cell, respectively.

FIG. 28 is an image showing examples of current collectors coated with a composite materia! before and after abuse testing.

FIG. 29 is a plot of temperature increase as a function of time of a reference battery cell, a battery cell including a composite material that includes

montmorillonite, and a ^' battery cell including a composite material that includes silica. FIGS. 30A-30B are plots of normalized reversible capacity as function of cycle number, and reversible ca ac ty as a function of cycle -number, respectively, of a reference battery cell and battery cell that include a composite material

Like reference symbols in the various drawings indicate like elements.

DETAILED DESCRIPTION

Economic and environmental costs of preparing materials for structural use in construction, batteries, fabrication of pis-cast parts, and a variety of other applications can be _. significantly reduced by reducing the amount of binder used in the materials. In contrast to conventional materials where the binder material fills all of the interstitial spaces between uni ts of the filler material, the composite materials produced by the methods described herein have binder material selecii vely located at the points of contact between units of the fil ler material This allows for a very significant reduction in the amount of binder that is used.

Composite materials for use in structural applications should have suitable physical characteristics, such as flexura! and compressive strength, ft has been discovered that even when the amount of binder material in composite materials is reduced as disclosed herein, advantageous physical properties such as flexural and compressive, strength can still be maintained when the binder material is selectively located at points of contact or c losest approach bet ween units of the filler material Composite materials with properties suitable for structural - applications are also typically produced when filler materials are packed more densel within, the composite structure.

Methods of fabricating the composite materials disclosed herein invol ve the application of relatively high pressures to mixtures of filler and binder materials. Without wishing to be bound by theory, it is believed that applying such high pressures assists both the close packing of the filler material and the location of the binder material. Specifically, it is believed that the application of pressure deforms and/or crushes the filler material into particles of varying size. The crushed filler material forms a denser, close-packed- structure, -reducing- the interstitial gap volume. As the filler material units are compressed, the binder material is squeezed out of the interstitial sites and spread over the filler material unit surfaces. Capillary forces draw the binder material rata the narrowest spaces to form microagglornerations at locations where the filler material units are close to one another,

FIG. 1 is a schematic diagram 100 illustrating the movement of binder material 102 from the interstitial gaps 104 to: contact regions 106 between the units of filler material particles 1 8 whe suitable pressure is applied to the binder and filler materials. This process reduces the amount of binder material used in the composite material while increasing the fraction of binder material that Is utilized to carry mechanical loads within the composite materia! structure. As a result, the composite material can be fabricated at reduced cost (due to the smaller amount of binder material used), while still achieving high material performance, doe to the binder material functioning in a more "intelligent" manner within the composite structure.

The composite materials fabricated as disclosed herein can be used, for example, in structural materials, pre-cast components, battery electrodes, medicines, particula te composites, foods, and in a variety of other applications.

Fabr i cat ion, of Compost re Mater i als

The composite materials disclosed herein are generally prepared using a technique that is referred to as "pressure-aided self-assembly" (PASA). Units of a

Slier material are combined with a binder material to form a mixture (i.e., with or without a mechanical mixing step) in which the amount of binder material is relatively low, as will be explained further below. Then, relatively high pressure

(e.g., greater than 10 MPa) is applied to the mixture to spread the binder material among the units of the filler material to .fo m., a solid, integral composite material, in. an optional step, the composite material can then be set or cured. Setting or curing the composite material cars include steps such as beating the composite material and or casting/m lding the eomposite material to fabricate pre-cast components formed from the composite material.

Pressure can generally be applied to the mixture of binder and filler materials according to different pressure-loading protocols. FIG. 2 is a flowchart 200 showing a seri es of steps for fabricating eomposite materials according to a _. pressure-loading protocol referred to as quasi-static mixing (QSM). In a first step 202, a mixture of filler material and binder materials is formed. In some embodiments, a foaming agent or bubble-generating agent (e.g.,

tol«enesulfo«yI hydrazkte surfactants, and/or blowing agents) can be added to the mixture of filler and binder materials, it is believed that the addition of the foaming agent to the filler material and binder materials adjusts the properties of the filler and binder materials (e.g., adjusts the effective fluidity and volume of the binder and/or the wettabili ty of the Slier material).

Next, pressure is applied to the mixture in a second step 204. To apply pressure, in certain embodiments,, the filler and binder materials can be placed in a vessel or cavity for this- urpose. However, as wilt he explained in greater detail below, a variety of different methods and appai'ates can be used, to apply pressure to the mixture, and applica tion of pressure in a vessel or cavi ty is only one possibility.

!n some embodiments, the pressure applied is higher than the crushing strength of the filler material As explained above, it is believed that by applying suitable pressure to tbe filler material in the mixture, the filler material is crushed, aid thereby as s umes a closer-packed arrangement of the crushed filler units or particles than prior to the application of pressure, enhancing the physical properties ·- such as compressive strength and flexural strength— of the composite material that is produced.

in some embodiments, the peak applied pressure is at least 10 MPa, for example, at least 20 MPa, at least 30 MPa, at least 40 MPa, at least 50 MPa, at least 70MPa, at least 100 MPa, at least 150 MPa, at least 200 MPa, at least 250 MPa, at least 300 MPa, at least 350 MPa, at least 400 MPa, at least 500 MPa.

In some : embodiments, the duration over which the peak pressure is applied is at least 1 second, for example, at least 2 seconds, at least 5 seconds, at least .10 seconds, at least 30 seconds, at least 1 minute, at least 2 minutes, at least.5 minutes, at least 1.0 minutes, at least 20 minutes, at least 30 minutes, at least 1 hour, at least 2 hours, at least 4 hours, at least 6 hours, at least 12 hours, at least 1 day, at least 2 days, or at least 3 days,

In general, pressure application is initiated and the applied pressure rises to the peak pressure value over a time period, durin which the applied pressure varies. In some embodiments, the time duration between the initiation of pressure and the attainment of peak pressure is at least 1 millisecond, for example, at least 5 milliseconds, at least 10 milliseconds,, at least 50 milliseconds, at least 100 raiSKseeonds, or at least 500 milliseconds, at least 1 second, at least 2 seconds, at least 5 seconds, at least 10 seconds, at least 30 seconds, at least 1 minute, at least 2 minutes, at least 5 minutes, at least 10 minutes, at least 20 minutes, at least 3 minutes, at least 1 hour, at least 2 hours, at least 4 hours, at least 6 hoars, or at least 12 hoars.

In an optional third step 206, the mixture can be broken apart into

particles/pieces and re-mixed. In some embodiments, following break-up of the composite material formed in step 204 into particles pieces, the average particle/piece diameter is at least 1 μηι, for example, at least 5 μιη, at least 10 μηι, at least 50 μιη, at least 100 μιη, at least 1 mm, at least 10 mm, at least 50 mm, at least 100 mm, at least 1 cm,

in an optional fourth step 208, pressure is applied again to the particles/pieces from step 206, in some embodiments, the optional re-applicatio of pressure may be executed at least one time, for example, at least two times, at least three times, at least four times, at least fi ve times, at least 10 times, at least 15 times, least 20 times, at least 30 times, at least 50 times, or at least 1 0 times. As explained above, it is believed t at applying pressure in this manner causes fracture of the particles/pieces of the composite material, yielding smaller pieces that can assemble into a closer- packed arrangement Further, it is believed that the application of pressure causes microaggiomerations of the the binder material to form at critical points between the particles/pieces, preserving the advantageous mechanical properties of the composite materia L

In an optional fifth step 210, a curing operation (e.g., polymerization,, hardening, solidification, or erosslin ng) is performed on the material, resulting in a completed composite material, thus ending the process (at step 212).

Curing operations can be performed in various ways. For example, in some embodiments, curing can be performed in a cast, a mold (e.g. , an open mold or a closed mold), or a container. Curing performed in this manner can be used to prefabricate variety of cast parts and structural components such as support members and decorative elements that can be used in construction applications. In -certain embodiments, curing can be performed on a support surface (e.g. , a planar or a curved surface). Composite materials ^'' cured on. planar or curved surfaces cast be used, for example, as mneticnal material layers in a variety of applications, and as template materials from which various components can be cut or otherwise: mechanically excised,

FIG. 3 is a schematic diagram depicting an example apparatus 300 thai can be used to perform die quasi-static mixing procedures disclosed above. The mixture of binder and filler materials 302 is posi tioned in a cavity of a load cell 304. A piston 306 applies pressure to the binder and the filler materials to form the composite material.

Another pressure-loading protocol that can be used to form the composite materials disclosed herein is referred to impact mixing (ΪΜ). FIG. 4 is a flow chart 400 showing a series of example steps for ^' forming composite materials according to the impact mixing protocol

In a fust step 402, a mixture of filler material and binder materials is formed. In some embodiments, a foaming agent or bubble-generating agent (e.g.,

toluenesnlfonyl liydrazide) is added to the mixture of filler and binder materials. It is believed that the addition of the foaming agent to the filler material and binder mate-rials adjusts the properties of the filler and binder materials (e.g., adjusts the effective fluidity and volume of the binder and/or the wettability of the filler material , as explained above).

Next, impact pressure is applied to the mixture in a second ste 404. For this purpose, in certain embodiments, the mixture of filler and binder materials can be placed in a vessel or cavity-. However, as discussed above, other methods of applying pressure can also be used.

In some embodiments., the impact pressure exceeds the crushing strength of the filler material In certain embodiments, tire peak applied impact pressure can be at least 10 MPa, for example, at least 20 MPa, at least 30 Pa, at least 40 MPa, at least 50 MPa, at least 70MPa, at least 100 MPa, at least 15 M Pa, at least 200 MPa, at least 250 M Pa, at least 300 MPa, at least 350 MPa, at least 400 MPa, at least 500 MPa.

In some embodiments, the duratio over which impact pressure is applied to the mixture is at least 1.0 microseconds, for example, at least 20 microseconds, at least 30 microseconds, at least 50 microseconds,, at least 100 microseconds, at least 200 microseconds,, t least 1 millisecond, at least 5 milliseconds, at least 10 milliseconds, at least 50 milliseconds, at least 100 milliseconds, at least 500 milliseconds, at least 1 second.

When impact pressure is applied to the mixture, the applied pressure rises very quickly from zero to the peak applied pressure, In certain embodiments, for example, the time duration between the initial rise of the applied pressure and the attainment of the peak applied pressure is 1 second or less, for example, 1 millisecond or less, 500 microseconds or less, 300 microseconds or less, 200 microseconds or less, 100 microseconds or less, 50 microseconds or less, 20 microseconds or less, 10

microseconds or less, 5 microseconds or less, 1 microsecond or less,

in an optional third step 406, the composite material formed in step 404 can be broken apart into particles/pieces and re-mixed, Tn some embodiments, following the break-up Of the composite material formed in step 404 into particles/pieces, the average particle/piece diameter is at least I μι», for example, at least 5 μηι, at least 10 μΐΐΐ. at least 50 pm, at least 100 pm, at least 1 mm, at least 10 mm, at least 50 mm, at least 100 mm, at least 1 cm.

in an optional fourth step 408, impact pressure is applied to the

particles pieces of the composite material from step 406. The optional re-application of impact pressure can occur at least one time, for example, at least two times, at least three times, at least four times, at least five times, at least 10 times, at least 15 times, least 20 times, at least 30 times, at least 50 times, at least 100 times. As explained abo ve, it is believed that apply ing pressure in this manner causes fracture of the particles/pieces of th composite-material, yielding smaller pieces that can assemble into a closer-packed arrangement. Former, it is believed that the application of pressure causes mkroaggloraerations of the the binder material to form at critical points between the particles/pieces, preserving the advantageous mechanical properties of the composite material.

in an opti nal fifth step 410, a curing operation can be performed on the composite material, afte which the process (at step 4.12). As discussed above, curing operations can be performed in a variety of ways, including for example curing in a cast* a mold, or a container to fabricate pre- formed parts from composite materials. aiid curing on planar and/or curved surfaces to form functional layers or sheets of the composite material.

FIG. 5 is a schematic diagram depicting an example .apparatus 500 that can be used to perform the impact mixing procedures disclosed herein. The mixture of binder and filler materials 502 is positioned in a cavity of a load cell 504, and a piston. 506 is positioned above the cavity. An impact head 508 (e.g., a hammer) rapidly strikes the piston, driving it into the mixture of hinder and tiller materials and

applying pressure to the mixture to form the composite material

In both the QSM and IM pressitre-loadirtg protocols, pressure can be applied to the .mixture of binder and filler materials in a variety of ways, in general, pressure can be applied in the form of compressive loads, tensile loads, shear loads, vacuum loading, roller loads, bending loads, impact loads,, vibrational (i.e.. dynamic) loads, and combinations of these.

In some embodiments, where pressure is applied via compressive loading, a variety of mechanical devices such as pistons, hydraulic machines, mechanical presses, weights, rollers, calendaring systems, extrusion systems, molding systems (e.g., injection molding systems «1.4 compression molding systems), and

'combinations of such systems can be used.

In certain embodiments, where pressure is applied via one or more impacts on the mixture of binder and filler materials (e.g., a compressive load that increases in magnitude over a relatively short duration), the impact pressure can applied by an impact head (e.g., a hammer), a. dro tower, art iropactor, a weight, a blast loading, an explosive compression, a high-speed roller, a high-pressure gas system, a hydraulic system, and via combinations of these methods.

in some embodiments, rather than applying pressure to the entire volume o the mixture of filler and binder materials, processing methods can be used in which portions of the mixture are selectively pressurized. In this manner, mixtures having different compositions, as will he discussed later, can be formed into single, integral, solid .composite material, in which the composition of the material vari es as a function of position within the material That is, different portions of the material can have different compositions for different functional and/or structural applications. Further, selective fabrication methods in which different portions of the mixture are pressurized at different times permit fabrication that is akin to 3D printing, in which layers or portions of a final composite material are selectively formed or built up to yield a final product. These methods can be referred to collectively as "sectioned" processing of the composi te materi als.

FIGS. 6A and 6B are schematic diagrams showing two examples of sectioned processing. la FIG. ^' 6A _> the binder and the filler materials are compressed in portions or stages in apparatus 600, Composite material 604 has already been formed by the application of pressure via piston 602. Piston 602 is in. the process of pressurizing- section of binder and filler materials 606, while binder and filler materials 608 have not yet been pressure-treated.

In FIG. 6B„ a mixture of binder and filler materials 612 is compressed by a roller 614 as part of a processing apparatus 610. Roller 614 selecti vely applies pressure to only that portion of the mixture under the roller. As such, the portion of the mixture to the left of roller 614 in FIG, 6B has already be pressure treated, while porti on 612 of the -mixture h as not yet been pressure treated.

These examples illustrate how the binder and filler mixture can be compressed section by section, with various pressures, loading rates, loading modes, loading methods, loading directions, and loading times. Each section can be compressed either once o multiple times. Different sections may overlap, aad at different steps of the pressure ^■ application, the section boundaries may change.

In certain embodiments, different regions of the composite material can have different compositions. By using the sectioned processing methods discussed above, mi tures w th different combinations or binder materials and/or filler materials can be pressurized to form a single, integral, solid composite material For example, composite materials formed by successive layers with different combinations of binder materials and/or filler materials can be combined into a single composite material using techniques such as rolling, as shown in FIG. 6B, Composition variations can occur in an of three spatial dimensions.

Variations in material composition can even be introduced during _.

pressurization, as additional filler and/or binder materials can he added to

unpressurized portions of the composite material while other portions of the ma terial are being pressurized. Further, different pieces or particles of once-pressurized composite materials can be. subjected to further pfess«ma.tio» cycles,, thereby combining the pieces info a single composite material with composition variations.

In general, within different regions, the composite material can include d fferent binder materials, different filler materials, or both different binder and different filler materials. Any of the binder a d filler materials (and combinations thereof) that are disclosed herein can be used to form these structurally complex compos i te mater i ais.

In some embodiments, features such as voids or surface features can be created in the composite material using molding techniques and/or by varying the composition of the composite materials. For example, a void can he created in a composite materia! by adding only filler material to the region, or filler material with a very small amount- of binder material The resulting composite materia! will lack ^' Structural integrity in that region, allowing the filler material or low-binder composite portion to: be separated from the remainder of the ^' Composite material using techniques such as polishing, extraction, washing, and/or sonieation. The resulting composite material will include voids corresponding to the former locations of the filler material or low-binder composite portion. FIG. 25 shows an image of a composite material with voids 2502.

In both the QS and IM protocols, depending on the binder material used, the specific conditions of the curing step may or may not involve the application of heat, hi some embodiments, the curing step is per formed at a peak temperature of about 0 *G or higher, for example, at about 10 °C. or higher, at about 20 «C or higher, at about 30 ^ft C or higher, at about 50 ^<S C or higher, at abou 100 °C or higher, at about 200 °C or higher, at about 300 °C or higher, at about 400 °C or higher, at about 500 °C or higher, at about 800 °C or higher, at about 1000 °C or higher, at about .1200 * or higher, at about 1 00 € or higher, at about 1600 °C or higher, at about 1800 °C or higher, or at about 2000 ^f 'C or- higher. In some embodiments, the setting step is performed at a peak temperature at about room temperature, at about 80 '·€, at about 100 °C, or -at about 200 ^< .

When the coring step occurs with the application of heat, there may be a desired rate of equilibration to the peak temperature, in some embodiments, the rate at which equilibration to the peak . temperature of the curing step occurs is 0.1 °C per minute or higher, for e ample, 0.2 °C per minute or higher, 0.5 °C per minute or higher, 1 "C per minute or higher, 2 ⁴ *G per minute or higher, 5 "C per minute or higher, 1.0 °C per minute -or higher, 1.5 °C per minute or higher, 20 -°C per minute or higher, 50 °C per minute or higher, 100 ^a C per minute or higher, 200 ^a C per minute or higher, 500 °C per minute or higher.

in general, the duration of the curing step depends upon the binder materialCs) that are used to form the composite material For example, the curing step can be performed for at least 5 minutes, for at least 10 minutes, for at least 20 minutes, for at least 30 mimites, for at least 40 minutes, for at least 1 hour, for at least 2 hours, for at least 3 hours, for at least 6 hours, for at least 12 hours, for at least 24 hours, for at least 36 hours, for at least 2 days, for at least 3 days, for at least 4 days, for at least 6 days, for at least 7 days, for at least 10 days , for at least 2 weeks, for at least I month .

!n some embodiments, the crying step can be performed under air or in an inert atmosphere (e.g., a nitrogen atmosphere or an argon atmosphere), depending upon, fo example, the moisture and/or oxygen sensitivity of the binder material(s} in the composite materials.

Composite. Material . C omposi tion . and r perties

As discussed above, the composite materials disclosed herein include a filler material and a. binder material disposed between at least some units of the filler material to form an integral composite material

In general, the composite materials disclosed herein include relatively small amounts of the binder niateriai(s). .However, pressure-based processing ^: of the.

mixtures of binder and filler materials yields composite materials , whic ^' nonetheless retain advantageous mechanical and fun.ctio.na! properties.

in some embodiments., the composite materials include less than 18% by weight of the binder material (e.g. , less than 1.4% by weight of the binder material, less than 10% by weight of the binder material,, less than 9% by weight of the hinder material, less than 8% by weight of the binder material, less .than 7% by weight of the binder material, less than 6% by weight of the binder material, less than 5% by weight of the binder material less tha -4% by weight of the binder material less than 3% by weiaht of the binder material, less than 2% b v weight of the binder material, less than .1 % by weight of the binder material, less than 0.5% by weight of the binder material, less than 0.2% by wei ght of the binder materiai). In some embodiments, the composite materials include less than. 18% by weight of the binder material

In certain embodiments., the composite materials include less than 20% by volume of the binder material (e.g., less than 19% by volume of the binder material, less than 18 by volume of the binder material, less than 17% by vol ume of the binder material, less than 16% by vol erne of the binder material less than 15% by vol ume of the binder material, less than 14% by volume of the binder material, less than 13% by volume of the binder material, less than 12% by volume of the binder material, less than 11% by volume of the binder material less than 10% by volume of the binder material, less than 9% by volume of the binder materia less than 8% by volume of the binder material less than 7% by volume of the bi nder material less than 6% by volume of the binder material, less than 5% by volume of the binder material, less than 4% by volume of the binder material, less than 3% by volume of the binder material, less than 2% by volume of the binder material, less than 1% by volume of the binder material). In some embodiments, the composite materials include less than 10% by weight of the binder materiai and less tha 20% by volume of the binder material

In general the composite materials include one or more binder materials. The binder material content of the composite material typically infiiiences the composite material's compressive strength, flexural strength, or both, as mieroagglomerations of the binder material are positioned between units of the filler material and can support a variety of material loads. Accordingly,, properties of the composite materials can be modified by including particular binder materials within the composite materials. Example binder materials that can be used include thermoplastics, thermosetting materials, elastomers, natural polymers, synthetic .polymers, ceramics, glasses, metals, alloys, salts, soJfor-containing compositions, chemical precursors of the foregoing materials, id combinations of the foregoing materials (e.g., polyesters, epoxies, ifcoropolyrners, phenolic compounds, vinyl esters, carboxymefhylcel In loses, poiyetherketonekfitones, cyclic oligomers, poiy(mefhyl mefhaer Sates),

polycarbonates, and polybutyleae terephthalates). In some embodiments, the binder material can be diluted with at least one _; o.f solid, a liquid, or a gas. Example diluents include, but are not limited to, water, aqueous solutions, organic solvents (e.g., ethanol), solutions including organic .solvents, surfactants, surfkctant-ieleasing solids or gels, gas abbies, gas■generation, agents, inorganic solvents, solutions including inorganic solvents, lubricants, and/or solid particles. In some embodiments, the binder material includes chemical precursors (e.g., resins, initiators, or hardeners) that react and/or harden during fabrication (e.g., during the curing step) t form, for example, various polymers.

In general, the composite materials include one or more filler materials.. The filler materials also influence the physical properties of the composite materials, and therefore adjustment of the properties of the composi te ma terial can be achieved through selection of ^' suitable filler materials. Example filler materials include wood, fabrics, mats, sand, sod, rocls, concrete, cement, minerals, inorganic compounds, organic compounds, gravels, stones, bricks, metals, alloys, ceramic materials, polymers, elastomeric materials, thermosetting materials ^' , thermoplastic materials, composites, glasses, aerogels, porous materials, cellular materials, aerogels, solid waste, recycled materials, medicine, food, carbon materials, electrode materials, ^' components of these materials, and combinations of these materials. In certain embodiments, when the filler material is soil, the soil can include various different types of soil, including terrestrial soils and/or extraterrestrial soils (e.g., lunar soil). I some embodiments, the soil includes extraterrestrial soil, rocks, and/or minerals. In some embodiments, whe the filler includes rocks and/or minerals, the rocks and or minerals can be extraterrestrial rocks and/or minerals: (e.g., lunar rocks and/or minerals ^' ).

In some embodiments, the size distribution of units of the filler materials can be random. In certain embodiments, the size distribution of units of the filler materials can be controlled, using, for example, sieve analysis, size selection, size exclusion, and/Or size promotion.

In some embodiments, the at least one filler material can be subjected to a surface treatment or coating. Without wishing to be bound by theory, it is believed that the surface treatment or coating promo tes bonding of the bi nder r»aterial(s) to the IHier material(s), .thereby enhancing the mechanical properties of the composite material.

in general, the units of the filler masem! cars include materials in various morphological. forms. For example, the filler material can incl de un ts in the form of one .or more of powders, beads , dots, grains, particles, chips, cubes, layers, layer stacks, blocks, spheres, fibers, tubes, beams, pipes, rods, threads, platelets, coatings, hollow beads, hollow fibers, hollow blocks, hollow layers, bilayers, porous materials, meshes, fabrics, mats _. , honeycombs, and three-dimensional forms.

The composite materials disclosed herein can also include other types of materials for structural, and functional applications. For example, the composite materials can include at least one aggregate material to add mechanical strength to the composite material structure. The composite materials can also include at least one reinforcing material to augment the structural integrity of the composite materials. These additional materials can generally be added at any time during fabrication of the composite materials, for examp le, during the formation of the mixture of filler material and binder material, or before, between, or after the application of pressure to the mixture.

Example aggregate materials that can be used ^' include any of th filler materials disclosed herein. In some embodiments, aggregate materials can be subjected to a surface treatment or coating prior to inclusion in the composit material The surface treatment or coating adjusts the bonding strength of the aggregate material.

Example reinforcing materials include any of the filler materials described herein. Reinforcing materials can also fee subjected to surface treatments or coatings to adjust the bonding strength of the reinforcing materials.

in some embodiments, the composite materials can include at least one additive. Additives can, for example, adjust the properties of the composite material or aid in the preparation of the composi te material. Example additives include, but are not limited to, foaming agents, bubble-generating agents, solvents, lubricants, components of the foregoing materials, and combinations of the foregoing materials. Additives can be combined with other components of the composite materials at various stages of fabrication, includin prior to applying pressure to the composite materials. and between pressurization cycles. In addition, additives can be added to only certain regions of a mixture or a composite material so that ^' the properties of the composite material are different at different locations within the material.

in certain embodiments., the composite materials disclosed herein can include more than one binder material and/or more than one filler material Combinations of multiple binder materials and/or multiple fil ler materials can be used to prepare composite materials with particular physical properties (e.g., fiexural strength, compressive strength) and/or particular functional properties (e.g., electrical resistance). In general,, .a wide variety of different combinations of filler materials and binder materials can be used, including combinations of any of the filler materials and any of the binder materials disclosed herein, in some embodiments, the composite materials disclosed herein can include 2 or more different filler materials (e.g., 3 or more different filler materials, 4 or more different filler materials, 5 or more different filler materials, or even more different-filler materials). In certain embodiments, the composite materials disclosed herein can include 2 or more different binder materials (e.g., 3 or more different binder materials, 4 or more different binder materials, 5 or more different binde materials, or even more different binde materials).

in some embodiments, the distribution of one or more filler materials and/or one or more binder materials can be heterogeneous within the composite materials. By varying .the distribution of filler material(s) and/or binder niaterial(s) within the composite materials, the materials can be manipulated to have spatially varying, physical and/or functional properties. As such, the methods disclosed herein permit in situ fabrication of functional materials with controlled variations in. properties, suitable for a variety of applications, in particular, selective or sectioned processing methods, examples of whic are shown in FIGS, 6A and 6B, can be used to fabricate composite materials in whic the distributions of one or more binder materials and/or one or more filler materials are non-uniform.

For example, in certain composite materials, the distribution of a binder material withi the composite material is non-uniform. Suc materials can include distinct regions in which the hinder material distribution or concentration is constant, but where the binder distribution or concentration differs among at least some of the regions, in some examples, the distribution or concentration of the binder material varies continuously from one location ^' to ^■ ■another within the material.

Similar considerations apply to filler materials, in certain composite materials, the distribution of a filler material is non-uniform. The concentration or 'distribution of the filler material can vary in step- wise fashion between different regions of the composite material, or in a smoothly varying continuous or semi- continuous fashion through the composite material.

In addition, for composite materials that include two or more filler materials and/or two or more binder materials, the. distribution or concentration of each of the binder materials and/or each of the filler materials can var as discussed above.

T!ie effect of a non-homogeneous distribution of one or more filler or binder materials within the composite material is that the weight percentage of the hinder material and or the volume percentage O the binder ^" material can vary within ^" the composite material. For example, in some composite materials fabricated as disc losed herein, the weight percentage of a binder material can ha ve a first value at one location or region in the composite material, and a second, differen value at another location or region in the material. T he weight percentage at any location or region can have value as discussed previously, for example.

Similarly, in certain composite materials, the volume percentage of a binder material can have first value at one location or region in the composite material, and a second, different value at another location or region in the material. The volume percentage at any location or region can have a value as discussed previously, for example. Where composite materials include more than one binder material, the weight and/or volume percentages of each of the binder materials can vary ¹ independently of the other hinder materials. Simila considerations apply to the distribution of filler materials within the composite materials.

As discussed previously, although the materials disclosed herein include binder materials in smaller concentrations than is typical for structural materials, the compressive strength of the composite materials is higher than man structural materials such as cement that are currently tn use. In some embodiments, the composite materials prepared by the methods described herein have a compressive strength of I MPa or higher, for example, 3 MPa or higher, 5 MPa or higher, 10 MPa or higher,.15 MP or higher, 20 MPa or higher, 25 MP or higher, 30 MPa or higher, 35 MPa or higher, 40 MPa or higher, 50 MPa or higher, 60 MPa or higher, 70 MPa or higher, 100 MPa or higher. It has been, observed that when the form of the applied pressure is impact pressure d r ng fabrication, the compressive strength of the composite materia! correlates with the number .of impacts.

The composite materials disclosed herein also have advantageous flexura! properties, despite the relatively low concentration of binder materials therein, I» some embodiments, the composite materials prepared by the methods described herein have a fiexural strength of 0.1 MPa or higher, for example., 1 MPa or higher, 3 MPa oy. higher, 5 MPa or higher, 10 MPa or higher, 1 S MPa or higher, 20 MPa or higher, 25 MP or higher, 30 MPa or higher, 35 MPa or higher, 40 MPa or higher, 50 MPa or higher,. 60 MPa or higher,. 70 MPa or higher, 100 MPa or higher.

Because the composite materials disclosed herein include relatively small amounts of binder materials) and comparatively larger amounts of filler materials), wh ere th e flexura! strength of the binder materia S(s) is/are less than the flexura! strength of the filler materials), the composite materials will generally have flexura! strengths that are greater than the flexura! strengths of the binder material alone. In som embodiments, For example, th composite materials hav a flexura! strength that is at least 20% larger (e.g., at least 30% larger, at least 40% larger, at least 50% larger, at least 60% larger, at least 70% larger, at least 80% larger, at least 90% larger, at least 100% larger, at least 200% larger, at least 300% larger, at least 500% larger, at least 700% larger, at least 1000% larger) than a product of the flexura! strength of the binder material and a weight percentage of the binder material in the composite material,

In certain embodiments, the composite material has a flexura! strength that i at least 20% larger (eg., at least 30% larger,, at least 40% larger, at least 50% larger, at least 60% larger, at least 70% larger, at least 80% larger, at least 90% larger, at least 100% larger, at least 200% larger, at least 300% larger, at least 500% larger, at least 700% lamer, at least 1000% larger) tha a product of the flex oral strength of the binder materia! and a volume percentage of the binder material in the composite ^■ material Composite materials prepared according to the methods disclosed herein, also h w high deformabilify. In some embodiments, for example, the composite materials disclosed herei have a def rmability of 0.1% or higher, 1% or higher, 5% or higher, 10% or higher, 15% or higher, 20% or higher, 25% or higher, 30% or higher, 35% or higher, 40% or higher, 50% or higher.

Filler and binder materials can be selected to impart a variety of physical properties to the composi te materials. Among these are exuraJ and compressive strength, as discussed above. Control over other physical properties can also be achieved. For example, in some embodiments, the choice of filler and binder materials, as well as the relati ve amounts of each and the processing steps used to form the composite material, can be used to produce composite material with advantageous electrical properties.

Resistive heating in electrical devices occurs when large currents ^' flow through circuit elements ^' that, are not designed to handle such currents; the elements overheat, leading to failure of the elements and potentially, catastrophic damage to other device components. Excess heating ca also result from physical abuse or mishandling of electrical devices, which can cause damaae to circuit elements, increasing their resistance" and leading to resistive heating.

The methods disclosed herein can be used to fabricate (e.g., used to form) composite materials thai function as sacrificial elements within eiectrical devices suc as electrodes, current collectors, batteries, voltage sources, and current sources. The composite materials have temperature-dependent and/or pressure-dependent resistance profiles such that when the temperature and/or pressure applied to the composite materia! increases significantly, the resistance of the composite material also increases significantly. Thus, when current flows within a device that contains, such a material, it is the composite material that undergoes resisti ve heating and subsequent failure, due to the increased resistance of the composite material. In this fashion, the composite .materia! may be rendered inoperable. However, tire failure of the composite material interrupts current How within the device, ensuring that resistive heating within other device-elements and components does not occur. As such, the composite material acts as a sacrificial element to prevent more significant thermally- and/or mechanicaliy-induced damage to the device's components. In some embodiments, when the temperature of the composite material increases by 20 °C, the electrical resistance of the composite material increases by at least 20% (e.g., at least 3 ⁽ %, at least 40%, at least 50%, at least 6 ⁽ %, at least 70%, at least 80%, at least 90%, at least 95%, at least 99%, at least 100%, at least 200%, at least 500%, or at least 1.000%). In certain embodiments, when the temperature of the composite material increases by 30 °C, the electrical resistance of the composite material increases by at least 40% (e.g. , at least 60%, at least 80%, at least 100%, at least 200%, at least 400, or at least 1000%). ). In some embodiments, when the temperature of the composite materia! increases by 50 °€, the eiectrical resistance of the composite material increases by at least 70% (e,g. , at least 200%, at least 300%, at least 500%, at least 1000%). In some embodiments, when the temperature of the composite material increases by 70 °C (e.g., at least 80 °C, at least 90 ^' °C, at least 100 °G, at least 1 10 C, at least 120 °C), the eiectrical resistance of the composite material increases by at least 100% (e.g., at least 200%, at least 300%, at least 500%, at least 1000%).

In some embodiments, when the temperature of the composite material increases by at least 20 ⁶ C, the electrical resistance of the composite material increases by at least 20% (e.g., at least 30%, at least 40%, at least 50%,: at least 60%, at least 70%, at least 80%, at least 90%, at least 95%, at least 99%, at least 100%, at least 200%, at least 500%, or at least 1000%). In certai embodiments, when the temperature of the composite m terial increases by at least 30 °C, the electrical resistance of the composite material increases by at least 40% (e.g., at least 60%, at least 80%, at least 100%, at least 200%, at least 400, or at least 1000%). In some embodiments, when the temperature of the composite mater ial increases by at least 50 °C, the electrical resistance of the composite material increases by at least 70% (e.g., at least 200%, at least 300%, at least 500%, at least 1000%). In some embodiments, when the temperature of the composite material increases by a least 70 "C (e.g., at least 80 °C, at least 90 °C, at least 100 °C, at least 1 10 °C, at least 120 °€) _J: the electrieai esistan.ee of the composite material increases by at least 100% (e.g., at least 200%, at least 300%, at least 500%, at least 1000%).

In certain embodiments, when the composite material is subjected to a pressure of 0.1 MPa, an electrical resistance of the composite material increases by at least 20% (e.g., at least 30%, at least 40%, at least 50%, at least 60%, at least 70%, at least 80%, at least 90%, at least 100%, at least 200%, or at least 1000%). In some embodiments, when the composite material is subjected to a pressure of 0.5 MPa, the •electrical resistance of the composite materia! increases by at least 30% (e.g.. at least 40%, at least 50%, at least 70%, at least 100%, at least 200%, at least 300%, or at least 1000%). la certain embodiiBents, when the composite material is subjected to a pressure of I MPa, the electrical resistance of the composite material increases by at least 40% (e.g.. at least 50%, at least 100%, at least 150% _. , at least 200%,. at least 300%, at least 500%, at least 700%, at least 1000%). In some embodiments, when tire composite material is subjected to a pressure of 5 MPa (cvg., , at least 10 MPa, at. least 20 MPa, at least 50 MPa, at least 100 MPa, at least 20 MPa, at least 500 MPa), the electrical resistance of the composite material increases by at least 50% (e.g., at least 100%, at least 1 0%, at least 200%, at. least 300%, at least 500%, at least 700%, at least 1000%).

In certain embodiments, whe the composite material is subjected to a pressure of at least 0.1. MPa, an electrical resistance of the composite material increases by at least 20% (e.g., at least 30%, at least 40%, at least 50%, at least 60%,. at least 70%, at least 80%, at least 90%, at least 100%, at least 200%, or at least .1000%). la some embodiments, when the composite materia! is subjected to a pressure of at least 0,5 MPa, the electrical resistance of the composite material increases by at least 30% (e.g., at least 40%, at least 50%, at least 70%, at least 100%, at least 200%, at least 300%, or at least 1000%). In certain embodiments, when the composite material is subjected to a pressure; of at leas 1 MPa, the electrical resistance of the composite material increases by at least 40% (e.g. , at l east 50%, at least 100%, at least 150%, at least 200%, at least 300%, at least 500%, at least 700%, _. at least 1000%). [ft some embodiments, when tire composite material is subjected to a pressure of at least 5 MPa (e.g ., at least 10 MPa, at least 20 MPa, a t least 50 MPa, at least 100 MPa, at least 200 MPa, at least 500 MPa), the electrical resistance of the composite material -increases- by at least 50% (e.g., at least 100%, at least 150%, at least 200%, at least 300%, at least 500%, at least 700%, at least 1000%). Applications

The composite materials disclosed herein, owing to their reduced cost of production, "greener" methods of fabrication, and favorable physical properties, can he used in a number of applications, including as substitutes for conventional cement or concrete in structural materials (e.g., lunar infrastrueteral materials), in batteries (e.g., electrodes), as medidnes, and in foods. A number of examples of such applications are described below.

(i) Comfructiau

hen used in the context of construction, the composite materials can, for example, be prepared on-site using existing equipment and infrastructure already used in the preparation of Portland cement, concrete, and other structural materials. The composite materials can be formed or cured in a variety of shapes as desired for use as Structural elements, reinforcing members, and decorative elements in building construction.

(U) Pr -C M Components

The composites can also be prepared by setting the mixture in a cast or simila cavity or surface that allows manufacture of parts and components with desired shapes and contours. These cast parts can include structural members and decorative elements for use in construction, electrical device fabrication., and other applications,

(m) ThfW-Dim.emk>nal Printing and Additive Manufacturing

In some embodiments, the composite materials are produced using three- dimensional printing techniques or additive manuftcturing. The material can, for example, be processed layer by layer, section by section, or part by part, over multiple steps, as discussed above in connection with FIGS, 6 A and 6B. For example, the mix ture of the filler and binder materials can be gradually added to a working station in ba tches: after each ba tch of mixture is .added, the batch is compressed, follo wed by. addition of the next batch. In some embodimen ts, curing of the materi al is performed after each batch of mixture lias been compressed, after several batches of the mixture have been compressed, or after all of the batches of the mixture have been compressed. In some embodiments, compression and breaking apart of the COBiposi le material can be performed one or more times. In some embodiments, ^' the identity and/or content of toe filler and/or binder materials is different between different hatches. Likewise, m.ceitain embodiments:, the applied pressure and/or type of pressure ad is different between different batches.

(iv) ThermcMy-fcespomive Coatings that Mitigate Thermally-Related Damage

In some embodiments the methods disclosed herein can be used to produce thermally responsive composite materials (TRCMs) for electric energy storage or energy conversion devices (e.g., batteries, lithium-ion batteries, capacitors, psendo- supercapacitors, and energy conversion devices that contain electrodes). The TRCMs can be formed as coatings, mixed components, aggregated components, fibers, layers, blocks, particles, beads, grains, or any combinatio thereof, in an energy storage or conversion device.

When electric energy storage or conversion devices are used and a

Bia!tknction or damage occurs, the temperature in the devices, for example, can rise to above the working temperature range. In such cases, a TRCM coating (TRCMC) acts as a "sacrificial element" that is damaged by the high temperature, resulting in an increase in the impedance of the component that is coated with the TRCMC. T he increase in impedance of the coated component reduces the current that flows in the device, reducing short-circuit current and mitigating thermal runaway (i.e.. preventing the overheating of one or more parts of the electric energy storage or conversion device). B sustaining damage to increase its electrical resistance, TRCM protects the ^■ components it is applied to or associated with.

(v) ne alty-R spottsrve Coatings that Mifig te Mechanical!y-Triggerecl Damage

In some. embodiments _. , when mechanical abuse is inflicted on an electric energ storage or conversion device that contains a TRCMC applied to a component of the device, the resistivity of the TRCM increases in response t the mechanical perturbation, thereby reducing the current that flows through the device and preventing the device from overheating. Here again, the TRCM acts as a sacrificial element to protect the device, in this case from failure due to physical handling. Composite materials that function as T C s can generally be fabricated using the methods disclosed herein by ^' preparing mixtures that contain a relatively Sow binder material concentration and/or mixtures in which a relatively large mismatch in properties exists between the filler and binder materials. Various physical responses of the composite materials can lead to sacrificial, damage to the .materials. In some embodiments, for example, swelling of the TRCM in response to elevated

temperature and or mechanical perturbation can lead to irreversible structural damage and increased resistivity .

Themiaily-responsive composite materia! coatings can be applied inside, next to, or associated with various functional, components of electric energy storage and conversion devices, including electrodes, current collectors, anodes, cathodes, separators, cell cases, spacers, wires, electrolytes, module cases, battery pack eases, capacitor pack cases, and to other locations inside of, next to, or near such devices. fvi) Biomimickmg Materials

Tile methods disclosed herein can also be used to fabricate a variety of biomimicking materials. Biomimicking materials have nano- or micro-structures similar to those of biomaterials including, for example, natural or ^■ man-made materials that contain a large amount of fi ller and or reinforcing material and a reiatively small amount of binder materials. Example biomimicking materials that can be prepared using the methods described herein include, but are not limited to, artificial teeth, bones, nails, shells, scales, skins, muscles, tendons, nacre, ivory, hooves, horns, and/or other animal bod parts.

(vii) mi Liquefaction

Soil liquefaction is a phenomenon in which soil loses structural integrit o stiffness, losing some or all of its load-bearing capacity. Soil liquefaction, when it occurs underneath or in close proximity to structures, can be extremely troublesome if it leads to loss of underlying support for the structures. For example, buildings that have foundations built directly on sand that liquefies will experience an abrupt loss of support, resulting in extreme and irregular settling of the building structure, potentially causing extensi ve damage. The fabrication methods disclosed herein. can be used with earth as the filler material in the composite materials. When the filler material earth is located beneath or around structures, the formation of composite materials incorporating the earth can significantly increase ground-level .support provided to the structures, reducing the potential for cosily damage arising from the loss of structural support due to soil liquefaction. For example, a solution of a binder material (e.g., an epoxy material) can be added directly to soil and allowed to stand until it hardens. This increases the resistance of the soi l-based composite material to liquefaction or mechanical erosion.

(v i) Eleci tdes

In some embodiments, the methods disclosed herein, can be used to produce electrodes that contain a large amount of active material grains and a relatively small amount of binder material. Electrodes fabricated using these methods typically have a greater strength, toughness, and long-term durability than electrodes produced according to conventional, methods. Accordingly, the performance of de vices that use such electrodes is also typically improved. In addition, electrode fabrication in accordanc with these methods, in many cases, does not use solvent, thus simplifying the process and reducing its cost.

0x) food and Medici m

In some embodiments, the methods disclosed herein are used in the manufacture of foods or medicines. When used to manufacture foods, such as cookies, the composite food materials produced can be resistant to breaking apart during handling, packaging, and or shipping, an important advantage to reduce waste during manufacturing. During consumption _^ such food products typically exhibit improved "cruuchiness" when eaten and produce less debris (i.e., crumbs) than products produced conventionally.

Pharmaceutical and other compounds can be packaged in pill form, with the pill casing made from the composite materials disclosed herein. The composite materials typically yield pill casings with improved structural integrity relative to con ventional medications. Further, on account of the control over the selection of binder and filler materials allowed by the methods, in addition to control over the fabrication process (i.e., .control over the magnitude and manner of pressurizatios to form the composite materials), a significant degree of control can be achieved over the porosity of the pill casings. Adjustment; of the porosity cm be used to control the release profile for active pharmaceutical ingredients within the casing,

EXAMPLES

This section provides a number of specific examples to further illustrate the foregoin disclosure, hut which are not intended to limit the scope of the disclosure in any manner.

Example 1 ; Battery Electrodes

Battery electrodes were fabricated using the methods disclosed herein. The active material fille (NCM - provided by TODA AMERICA, with a product number of NCM-04ST), carbon black (CB - TJMCA.L C-NERGY SUPER C6S), and polyCvhiyiidene fluoride) (PVDF; provided b SIGMA-ALDR3CH, with a product number of 182702 -250G) were mixed in a 50 mL beafcer in a 93:3:4 ratio with a lab spatula for 5 minutes . The collective weight of the particles was 150 nig. The .mixture was then transferred to a cylindrical load cell. The load cell was mads of stainless steel and measured 3/4" in inner diameter, 2" in height, and 1" in outer diameter. It was equipped with a top piston and a bottom piston; both of the pistons were made of stainless steel, measuring 3/4" in diameter and 1" in height. The bottom piston was mserted in the cell, and the NCM-GB-PVDF mixture was placed on top of the bottom piston, inside the steel cell. No solvent was used. The top piston was compressed into the load cell by a type-5582 Instron machine and was used to apply pressure on the CM-CB-PVDF mixture. The maximum compression, pressure was 350 MPa>

Then, the load cell, including the NCM-CB-PVDF mixture inside and the two pistons, was moved into a CA BOLITE CTF quartz tube furnace. The material was heated up with a heating rate of 20 °C/niin. to 200 °C _} and this temperature was maintained for 1 hour before the material was air-cooled in the furnace. The heating was performed in an inert atmosphere by purging, nitrogen through the quartz tebe from an open end. The material in the load cell was taken out. It was a structurally integral disk, arid was employed as the. electrode m a. Type 20.16 half-cell FIG, 7 shows two battery electrodes prepared using this method.

A Celgard 2320 trtlayef polypropy lese-polyetriylene (PP PE PP) membrane was sandwiched in between the electrode and a 1.1 mm thick, i 5. . un diameter lithium disk. The membrane thickness was 20 μιη. About 30 μΐ BASF electrolyte (1M L1PF6 in 1 ; .1 EC-EMC) was added into the cell. The assembled battery cells were charged to 4.6 V by a MTi BST8-3 batter analyzer, with a charging rate of C/10. FiQ, 8 shows charge-discharge . curves of this electrode. The data show that the batteries could be charged and re-charged for ultip I e cycles, since in each cycle, the battery cell demonstrated a capacity to store and release electric energy.

Example 2 : Sand-Pol este Composite Materials ~- Quasi-Static M ixing

Sand samples wer harvested from the Black Beach, San Diego, United States; polyester was purchased from US composites (404 tooling polyester resin- Isophtha!ie).

The resin and the initiator were mixed with a lab spatula in a 50 mL beaker, ^• with the initiator making up 1.25 weight percent of the mixture. After mixing, a small amount of the polyester resin binder material-initiator mixture was added to 5 g of air- dried sand grains. The resin binder material content was between 2 weight percent to 5 weight percent of the total weight The sand grains and the resi n binder material were premixed for a few minutes in a 50 mi, beaker by a Lab ^' spatula, and the resulting mixture was transferred into a cylindrical load cell. The load cell was made of stainless steel, with measurements of "3/4" inner diameter, 2" height, and 1 " oute diameter. It was equipped with a top piston and a bottom piston; both of the pistons were made of stainless steel and had a diameter of 3/4" and a height of I". The bottom piston was inserted m the cell, and the sand-resin mixture was placed on top of the bottom piston, inside the steel cell. The to piston was compressed into the load cell by a type-5582 Lnstron machine and was used to apply a pressure on the sand- resin binder material mixture. The maximum compression pressure was in the range of 30 M Pa to 350 MPs. The compression time was 5 minutes.

After the first loading, the top piston was removed and the compressed sand- resin mixture was transferred into a 50 mL beaker, broken apart, by a lab spatula into small grain clusters having a cluster size below 100 μηχ The sand-resin binder material mixture was then placed back into the load cell and compressed again by a similar procedure as was used on the first loading.

The compacted material was kept in the load cell, and cured in a■ ^' VWR.

(1330GM) box furnace at 215 *C in air for an hour. After curing, the sample was removed from the load eel! and cut into beam ^' samples using an MTI high speed diamond cut-off saw. The sample surfaces were polished by a 320 grit sand paper to eliminate surface cracks and roughness.

The tlexura! strength was measured in a three-point bending setu on the type- 5582 InstroH machine, in the displacement control mode. The crosshead speed was set to 3.0 mm min and the span length, £ ₅ was set to 19,05 mm. The ^· tlexura! strength was defined as R - (3/2)(Λ«ί«Ι ¾/ ² } _! where Pmx is the maximum load, b is the sample width, and d is fee sample heigh FIG. 9 shows a plot 802 of the fiexural ^' strength of the composite material as a function of polyester binder material content, showing a positive correlation between, the two. FIG. .10 shows a plot 902 of the flexum! strength of the composite material as a function of peak compression pressure. FIG. 10 show's posi tive correlation between the two variables until about 200 MPa, then exhibited no change with increasing pressure. Example 3: Sand-Epoxy Composite Material - Quasi-Static Mixing

Composite materials were produced. y using epoxy as the binder material . The epoxy resin binder material was EPON S28 provided by Miller-Stephenson Chemical; the hardener was ¾-xyiylenedianiine provided by Sigma-Aldricb; the sand sample was collected from the Black Beach, San Diego, ^' United States,

The resin binder material and the hardener were first mixed thoroughly with a lab spatula in a 50 mL beaker, at weight ratio, of 5; 1. After mixing, a. small amount of the resin binder material -hardener mixture was added to 5 g of air-dried soil grains. The resin binder material content was either 4 weight percent er 5 weight percent of the total weight. The sand grains and the resin binder material were premised for a few minutes in a 50 mL beaker by a lab spatula, and the resulting mixture was transferred into a cylindrical load cell. The load cell was made of stainless steel, measuring 3/4" in inner diameter, 2" in height, and i" in outer diameter. It was equipped with a top piston aad a bottom piston; both of the pistons were mad of stainless steel, measuring 3/4" ia diameter and 1 " in height. The bottom piston was insetted in the ce ll, and the sand-resin binder material mixture was placed on top of the bottom piston, inside the steel cell The top piston was quasi-statlcail

compressed into the load cell by atype-5582 Instxon machine and was used to apply a pressure on the sand-resin mixture, with the loading rate of 0.3 mm/aim. The maximum compression pressure was either 100 MPa or 350 MPa. The compression rime was 5 minutes.

After the first loading, the top piston was removed aid the compressed material was transferred into a 50 t«L beaker and broken apart by a lab spatul into small grain clusters. The mixture was then placed back int the load cell and compressed again, with the same loading rate, maxininm pressure, and compression time as the first loading. The compacted material was kept in the load cell, and cured in a VW (1330GM) box furnace at 100 ^i! C in air for an hour.

After curing, the material was removed from the load cell and cut into beam samples using an MTi high speed diamond cut-off saw. The sample su ces were polished by a 320 grit sand paper to eliminate surface cracks and roughness. FIG. 11 shows an image of the composite material sample produced. The flexural strength was measured it* a three-point bending setup on the type~S5S2 instron machine, in the displacement control mode, similar with the testing procedure in Example 2. The crosshead speed was set to 3.0 mm/min and the span length, L, was set to 1 .05 ram. FIG. 12 shows plots of flexural strength as a function of peak pressure used in the method. n FIG. 12, plot 1 02 represents tie composite material including 5 weight percent binder; and plot 1204 represents the composite material including 4 weight percent binder, FIG. 12 shows that the flexural strength of the composite material had a higher positive correlation with peak pressure with. the higher epoxy hinder material content.

Example .4 : . Soil-Epo y. Composite . Material - .Quasi-Static _ Mixing

.Another composite material was produced, using soil as the filler material. The soil was collected from the Merriam Crater, Arizona, and air-dried. The epoxy binder mater ial and tire hardener were the s-arae as that of Example 3. The resin- hardener mixing, filler material-binder material premising, ..first compression, breaking apart of the composiie material, second compression, curing, cutting, polishing, and f!exural strength measurement procedures were the same as thai of Example 3. The resin binder material content was either 2.5 weight percent or 4 weight percent -of the total mass; the compression pressure was in the range from 10 Pa to 350 MPa.

FIG. 13 is an image of the composiie materia! produced, FIG, 1.4 shows the flexural strength of the composite material as a function of compression pressure. I» FIG. 1 , plot 1402 represents the composite material that includes 4 weight percent binder material and plot 1404 represeiits composite material that includes 2-5 weight, percent binder material. Overall, a higher epoxy binder material content and a higher compression pressure result in composite materials with higher flexural strength.

Distribution

Another composite material was produced, using the same soil epoxy resin binder material, and hardener as were used in Example 3.

Three groups of soils (designated A, B, and C) of different grain size distributions were tested. A sieve analysis was performed by using a W.S. Tyler Ro~ Tap R3 29 machine, with shake table, a sieve holder, and a fo I dable protective case. The shake frequency was -278 per minute, with a two-dimensional circular displacement of 1" by 0.75", at 150 taps pet minute. The hammer weight was 5 lbs.

The sieves stack consisted of 6 sieves with top cover and a bottom pan. The grid sizes of the sieves were 560 pro, 500 μιη, 1 12 μιιι, 90. pm, 25 pm, and 20 pm, respectively, ordered from the top to the bottom. Thas, three different size ranges of soil grains were obtained: 500-560 pm, 90-112 pm, and 20-25 pm.

Group A contained only the soil grains with the grain sizes of between 500- 550 pm. Group B filler material contained, soils within grain sizes ranging from 500- 560 μηι, 90-112 μηι, and 20-25 μηι (two stepped particle gradation), with a mass ratio of 67:219:714. Group C contained original soil grains without sieve analysis (i.e., the grain size distribution was as-received and with random particle size). The soils were air-dried. The .resin-hardener mixing, mixing -of the filler material and the binder material,, first compression, breaking apart of mixture, second compression, curing, cutting, polishing, and flexura! strength measurement procedures were the same as in. Example 3. The resin content was in the range of 2-7 weight percent of the total mass and the compression pressure was 350 MPa. FIG. 15 shows plots of the tlexural strength as a function of epoxy content for the composite materials prepared. Plot 1502 represents the composite material made with sod filler material having 500 pm uniform particle size, plot 1504 represents the composite material made with sod filler material having two-stepped particle size gradation, and plot 1506 represents the composite material made with soil filler material having random particle size.

Overall, incorporatin ^' more -epoxy .binder material resulted in materials with a higher i!exurai strength.

Example 6: Sa&d-Epoxy Composite Material with Aggregates

Another composite material was produced, using the same soil and binder material as was used in Example 4 was used. Gravel purchased commercially was employed as the aggregate. The average gravel particle size was ground 3/8 inch. The gravels were air-dried. Two groups of gravels were tested. Group A was brush- coated by a ihin layer of epoxy-hardener mixture; the epoxy-hardener mixture was the same as the resin premked with the filler material ^' soil; the amount of the resin coating was around 5 mg/cm ² . Group B gravels were nncoated.

The procedures of resin-hardener mixing, filler material-binder material premixing, first compression, and breaking part of mixture were the same as in Example 4. The compression pressure was 350 MPa. The soil-resin mixture was then mixed for one minute with 9 g of Group A or Group B gra vels using a lab spatula. The mixture was placed back into the load cell and compressed again at the same loading rate, the same maximum pressure, and die same compression time as the first loading. The compacted material was kept in the load cell and cured in a VWR- 1330GM box furnace at 100 °C in air for an hour. The overall binder material content was 2.6 weight percent of the total mass of the material containing Group A gravels, and 1.4 weight percent for the material containing Group B gra vels. After -curing, the samples were removed from the il cell and air-cooled to room temperature. The samples were cylinders having a diameter of 3/4" and a height ^' of -1.5". The compressive strength was measured by crushing the cylinder using a Type-5582 Instron machine,- at a loading rate of 1..mm/irr . The -compressive strength was defined as Fms Aa, where F x is die peak compressiv force at which the cy linder fails, -and Λ& is the initial cross-sectional area of the cylinder. FIG. 16 shows plots of the compressi ve strength as a function of peak pressure. Plot 1602 represents the composite material that includes surface resin on the aggregate (Group A), and plot 1604 represents the composite material that includes no surface resin on the aggregate (Group B). The plots hidkaie a higher positive correlation between compressi ve strength and peak pressure of the composite material that incl udes surface resin on the aggregate relati e to di composite material with no surface resin on the aggregate . Example 7: Soii-PEKK Composite material

Another composite material was produced, using the same soil as was used in Example 4 as the filler material. The binder material was a thermoplastic material, polyetherketoneketo e (PEKK) (K.EPSTAH 60O2PL), which was provided by

Arkema in powder form, having a particle size of -SO μηι.

The PEK powders were mixed with about -5 g of air-dried soil grains in a 50 mL beaker with a lab spatula. The polymer content was set as 4 weight percent of the total weight. The mixture was then moved into the same steel cell as was used in Example 4. At room temperature, the top piston was compressed into the steel cell -by a type-5582 stron machine, with a loading rate of 0.3 mtn min. The maximum compression pressure varied m the range from 10 to 350 MPa. After holding the

^• pressure for 5 minutes, the steel ceil, including the material inside and the two pistons, was moved into a quartz tube furnace. The material was heated at a heating rate of 20 "C/ffiin to the set point, and this temperature was maintained for 1 hour. The heating was performed in an inert atmosphere by purging nitrogen through the quartz tube froiii an open end. The set point was 400 °C. Then, the material was fumace-cooled to room temperature , taken out of the steel cell, and cut into beam samples using an MTI high speed diamond cut-off saw. The sample surfaces were polished by 320 grit sand paper to reduce surface cracks and roughness. FIG. .17 shows an image of the PE K-based sample. The ilexural strength was measured in a three -point bending setup, similar to the procedure it* Example 5. Plot 1802 in FIG. 18 shows that the flexural s trength i ncr eases as a function of peak pressure in the composite material having 4 weight percent of binder material.

Example 8: Impact jyf ixing IIM)

.Another composite material was produced, using impac mixing (ΪΜ) and the same soil filler materia! and epoxy binder material as was used in Example 4.

The epoxy resin, binder material and the hardener were first mixed together with a lab spatula in a 50 mL beaker with a weight ratio of 5:1. After mixing, a small amount of epoxy-hardener mixture was added to about 5 g of air-dried soil grains. The resin content was 4 weight percent of the total weight of the epoxy-hardener mixture. The simulant-resin mixture was transferred into the steel cell the same as was used in Example 4. The steel cell was placed into an instron CEAST 9350 impact machine, where a hammer was dropped to impact the soil-epox binder material mixture through the top piston. The hammer mass was in the range from 2.77 kg to 5.77 kg, adjusted by 0.5 kg and 1 kg weights. An aeeelerometer embedded in the hammer measured the deceleratio of the hammer, from which the impact force could be calculated. The drop distance of the hammer was in a range of 20 cm to 1 m.

Multiple impacts were conducted on the soil-epoxy binder material mixture. Between two impacts, the top piston of the steel cell was removed and the compressed material was transferred into a 50 mL beaker, broken apar by a lab spatula into small pieces with the size belo 100 μηι, and placed back into the steel cell; then, the top piston was placed back and the steel cell was placed into the drop tower again. The number of impacts ranged from 2 to 5,

After completing the impacts, the material was kept in the steel cell and cured in a VW - 1330GM box furnace at 1 0 ^l 'C i air for one hour. After coring, the sample was removed from the steel cell and cut into beam samples using an M l high speed diamond cut-off saw. The sample surfaces were polished by a 320 grit sand paper. The flexttral strength was measured in a three-point bending .setup, similar to how it was measured i¾ Example 4, FIGS. 1 and 20 show the peak compression strength arid the fiexural strength, respectively, as a function of the number of strikes. FIG, 1 is a plot 1 02 of peak compression strength of the composite material after repeated pressuri aiion, as a fonction of imber of impacts. According to FIG, 19, there is a positive .correlation between peak compression ..pressure and the number of impacts up until 4 impacts, after which a low correlation or a slight negati ve correlation, was observed. In FIG. 20, plot 2002 represents the fiexural strength of a composite material following fabrication by repealed cycles of impact pressurizaiion with a hammer velocity of 2.0 m s, a hammer mass of 5.77 kg, and 1 1.5 J/strike. Plot 2004 represents the f!e-xural strength _, of a composite material following fabrication by repeated cycles of impact pressuriza iion with a hammer velocity of 3.0 /s, a hammer mass of 2.77 kg, and 12.5 J/strike. Plot 2006 represents the fiexural strength of a composite material made using a hammer velocity of 2.4 m/s, a hammer mass of 4,27 kg, and 12.3 J/sfrlke, All three plots show a positive correlation between fiexural Strength and number of pressuiization strikes.

EM.mp.le 9: Gl ass-Hpoxy ..Cprnpo sit . Material

Another composite material was produced using the same binder .material as in Exampl 4. The resinTiardener mixing, premising, first compression, breaking apart of m ixture, second compression , and curing procedures were the same as those in Example 4, except that the filler material was glass beads obtained from Sigma-

Aldrich (Product No. G9268). The glass particle size was 425-600 μη¾. The epoxy binder material content was 4 weight percent of the total mass; the compression pressure was 350 MPa. FIG. 21 shows an image of the composite material produced by this method.

During the prefixing and pressure application steps of the methods disclosed herein, the fluidity of the binder material can be improved b adding a diluent that includes, for example, a solid, a liquid, a gas, a foaming agent, and or a bubble- generating agent. A composite material was produced using the same sand and epoxy binder material as in Example 3, incorporating the use of a diluent The epoxy resin binder material and the hardener were first mixed with a lab spatula i a 50 mL beaker at a weight ratio of 5: L Then, ethane! was added to the resin-hardener mixture, and mixed with a lab spatula for 1 minute. The ethanoi was obtained Irani Fisher Scientific (Product o, A407-4). The volumetric ratio of epoxy to ethanol was 1:1. After mixing, a small amount of the epoxy-ethanol mixture was added to about 5 g of air-dried sand grains. The epoxy binder material content was 2 weight percent of the total weight of the resulting mixture. The sand grains and the epoxy-ethanol mixture were mixed fox a few minutes m a SO txiL beaker by a lab spatula, and then transferred into the same steel ceil as was used in Example 3. The quasi-static mixing, curing, cutting, polishing, and fiexurai strength measurement procedures were performed the same way as in Example 3. The quasi-static mixing pressure was 350 MPa. The fiexurai strength of the resulting composite material was 12 MPa,

Example 1 1 : Usin Recyei ed Materials as Filler MateriaJs Reinf rce e»ts

As discussed previously, a wide variety of different tiller materials can b used in the composite materials disclosed herein. For example, in some

embodiments, the filter materials can be recycled materials. Recycled materials can also be used as reinforcing materials in. the composite materials.

Another composite material -was produced, using the same epoxy binder material as in Example 3, with recycled wood chips as filler materials. T he wood chips were generated from sawing pine wood, and had a size of about 1/4" to 3/4", The premixing, pressure step, curing, cutting, polishing, and fiexurai strength measurement procedures were performed in the same way as in Example 3. The pressure was 350 MPa; the hinder material content was 5 weight percent FIG. 22 shows a photo of thie composite material produced. The fiexurai strength of the ^■ material was 11 MPa.

Exampl 12. B inder Material Formed Throug iti lti Pol y men zatjon

As discussed above, various polymers can be used as binder materials i the composite materials disclosed herein. When polymers are used as binder materials, monomer precursors can be added to the mixture containing the filter matenais, and the monomers can be polymerized in situ to form the binder materials during fabrication. Another composite material was produced, using .methyl methacr i te (M A) provided by Sigma-Aidrich (Product Ho. M5590 ), and the free radical initiator benzoyl peroxide (Sigma-A!dr ich Luperox; product .no. 51/7909). The filler material was the same soil as in Example 4.

The MM A and initiator were first mixed by a lab spatula in a 50 ml. beaker, at a weight ratio of 50 : 1. After mixing, a small amount of the MMA nitiaior mixture was added, to about 5 g of air-dried soli grains. The binder material content was 4 weight percent, 6 weight percent or 8 weight percent of the total weight. The soil grains and the MMA -initiator mixture were _. .mixed for I minute in a 50 mL beaker by a lab spatula, and this resulting .mixture was transferred Into the same steel cell as in Example 4, The quasi-static mixing procedure was the same as in Example 4. The applied pressure was 350 MPa,

The compacted material was kept in the steel cell, with the piston remaining in place, and cured in a VW ( 1330GM) box furnace at 80 *'€ in air for 36 hours in order to polymerize the MMA into poly(meihyj metliacrylaie) (PMMA).

After curing, the sample was removed from the load cell and cut .brio beam samples using an ΜΤΪ high speed diamond cut-off sa w. The sample surfaces were polished with 320 grit sand paper. The flexurai strength measurement procedure was the same as in Example 4. At 4, 6, and S weight percent binder material, the flexurai strengths of the materials were 20 MPa, 3.3 MPa and 3? MPs, respectively.

Example 1 : Thermally -Responsive Coatings for Electrodes

Thermally-responsive coatings were produced for battery electrodes. The thermally-responsive composite material coatings (TRCMCs) included about 90% by weight of particle filler material, about 1% by weight of conductive additive filler material, and about 9% by weight of polymer binder material. Th particle .filler material was silica (Sigma- Aldrich S563 h Silicon Dioxide) or montmorilloni e (Alfa Aesar L i 5160, Montmorilloaite .10). The conductive additive filler material was carbon black (TIMCAL CrNlRGY Super~C65 ). The polymer binder material was. polyvinyl ί dene fluoride) (Sigma-Aidrich 4271.52, PVDF). The three components were first mixed together in an agate mortar at room temperature for 40 minutes. After mixing, A^meilryl-2-pyrroSidone (2 mL per gram of filler material-binder material .mi tore, Stgma-A!dnch 270458) was added. Slurry mixin was performed by a Qsonica Q55 ultrasonic probe for 10 minutes. The resulting stony was spread onto an aluminum current collector using a doctor blade. The ^■ aluminum current collector was obtained from MTX (Product No,: EQ-bcaf-15u-280), had a thickness of 15 μηχ and had been cleaned beforehand with acetone. The initial thickness of the slurry was -25 μηι. The slurry was then dried in vacuum oven at 80 °C for 20 hours, resulting in. a reduction of th thicknes of the slurry layer to 7-8 μιτι, The coated curreni collector was compressed by a hardened steel double-roller under a pressure exceeding 10 MPa, with the final TRCMC thickness being -4 μηχ

The TRCM C-coated current collector was cut into 9/16— diameter discs, and directly assembled into CR2016 coin cells. FIG , 27 shows a schematic diagram of a coin celt 2704 in contact with a heat source 2718 and a -voltage source 2720, An. exploded view 2702 of the coin cell is also shown in FTG. 27A, In the exploded view, the C 2016 iop case 2706 and bottom ease 2708 house aluminum current collector 2710, which is covered with the TRCMC composite .material. The mass of th

TRCMC composite material was approximately .1 mg in each cuitenfcHDollector cell sample. About 5 ,uL electrolyte (BASF LPS0 Selectilyte) was added to each cell. A stainless steel space 2712 and a spring 2714 were used to stabilize the current collectors. A reference sample was prepared with a similar structure, except that the current collector was not coated with the TRCMC material.

The coin cell sample was placed on a steel rod 2716 on heat source 2718 (a hot plate), and voltage source 2720 ( CR1060 commercial battery cell) was connected to it. Voltage source 2720 applied a voltage of about 4.2 V across current; ^■ collector 2710. Coin cell 2704 was connected to a ΜΤΪ BST8-3 Battery Analyzer, and was heated to 140 °C, while the temperature was measured si the bottom surface of the coin cell by an Omega TT- -40-25 type- gage-40 thermocouple connected to an Omega QM-EL-USB-TC temperature logger; the ti of the thennocouple was affixed to the center of the bottom surface of the coin cell

The temperature, and the voltage were maintained f r about 5 ruin. Then, the cell was ai r-coo led and opened . FIG, 28 is an image of three curreni coil ectors before (row 2702) and after (row 2704) the thermal testing. In the reference sample (the current collector without the TRCMC material, column 2706), the current collector showed no discernible changes after me test. Both current collectors with

mommorillonite- (column 2708) and siliea-based (column -2710) TRCMCs were disintegrated after the test, indicating that the damage to the T CMC materials was thermally triggered, and therefore that the TRCMC materials function as current limiting sacrificial materials when the cell is exposed to elevated temperatures.

To produce battery cells, active electrode material (AEM) layers were coated on top of TR CMC-coated current, coileclors. The AEM layer (middle layer inside housing) Consisted of 93% by weight of active material (NCM - provided by TODA AMERJCA, with a product number of NCM-04ST), 4% by weight of polymer binder material, and 3% by weight of conductive additive. The active material was Li- NiCoMn. (TODA America NCM-04ST). The polymer binder material was poly(vi»ylidene fluoride) (Sigma- Aldrich 182702). The conductive additive was carbon black (TIMCAL C-NERGY Super-C65).

The slurry processing of the AEM layers was performed in t he same manner to the TRCMC. The wet AEM slurry was first coated on top of clean current collectors (for reference samples) or TR CMC-coated current collectors (for TRCMC- modified samples). The initial layer thickness of the AEM was about 220 μη¾. After drying at 80 "C in a vacuum oven for 20 hours, the dried electrode film thickness was about 100 μηι The dried electrode film was the compressed by a hardened steel double-roller, similar to the TRCMC layer processing. The final layer thickness of the AEM was about 80 μηι. The electrode film was cut into 9/16' ⁵ -dia.meier discs, and assembled into CR2016 coin cells. The mass of active material was approximately 35 mg In each coin cell.

FIG. 27B shows a. schematic diagram of a coin cell 2730 produced as described above. In. FIG, 2?B, the top case 2732 and bottom case 2734 house the inner components. The negative electrode 2736 was a 1. l-min-thick lithium, foil, with a diameter of 1/2". The membrane separator 2738 was a 25-^i.m-thick porous trilayer polymer film (Product No. 2325 from Celgard). The active material 2740 layer was positioned between■ ^■ membrane separator 2738 and TRCMC layer 2742. Current collector 2744 was positioned on the opposite side of TRCMC layer 2742.

The battery coin cell was first cured for 5 hours. Then, the battery coin cell was cycled between 4,3-3.0 V at C/10 in an MIT BST8-3 Batter Analyzer for one cycle and between 4.2-3.0 V for 15 additional cycles at G'2, and finall charged to 4.6 V at C/ ^' O. The charged batter coin-cells were pre-heated on a hot plate at 1 10 "C for 1. minute, air-cooled to room temperature, and fully charged to 4.6 V again at C/10.

To evaluate the response of the coil cell to mechanical abuse, the coil cell was subjected to penetration by a nail. FIG. 27C is a schematic diagram of a pre-heated coin cell 2762 durin penetration by a stainless steel nail 2764. The radius of curvature of nail tip was 0.8 mm, and the nail was driven through the center of the coin cell by a Pahngren bench vise. The temperature was measured b an Omega TT- K-40-25 type- gage-40 thermocouple connected to an Omega QM-EL-USB-TC temperature logger, with the tip of the thermocouple affixed on fee top surface of the coin cell 2762, 2.5 mm displaced from the center. The coin cell was insulated, by a polyorethane bolder 2766 and cover 2768 during the nail penetration test. Insulating tape 2770 was placed over the coin cell 2762, and the thermocouple 2772 used for temperature 'measurement contacted the top surface of the coin ceil.

FIG . 29 shows plots of temperature increase as function of time for a reference battery cell without a TRCMC (plot 2902), a battery cell with

motitmorillonite-based TRCMC -{plot 2904), and a battery cell with, silica-based

TRCMC (plot 2906). The plots show that the battery cells with TRCMCs, upon nail penetration, exhibit much lower temperature increases, indicating that TRCMCs can be used in battery .cells and other electronic devices to mitigate excess internal tempera tures than might otherwise occur as a result of mechanical perturbations.

FIG. 30A shows plots of normalized reversible capacity as a function of cycle number for a reference battery cell without a TRCMC (plot 3002), a battery cell with mo!itraori!ionite-based TRCMC (plot 3004), aid a battery cell with silica-based TRCMC (plot 3006). F I G. 30A shows that the cycling performance of TRCMC- modified battery coin cell was comparable with that of reference coin cells without TRCMCs. The data shown in FIG, 3QA were measured without pre~heating the cells. The first-cycle reversible capacities of the reference cell and the ce lls with

moniniorillonlte-based and silica-based TRCMCs were respectively 1 14 rnAh, 133 nxAk and 82 mAh per gram of active material.

FIG. 30B depicts plots of reversible capacity as a function of cycle number for a reference battery cell without a TRCMC (plot 3022) and a battery cell with .montmorilfonite-based T CMC (plot 3024). Comparison of the plots in FIG . SOB shows that after pre-heating, the T CMC-modified coin cell could not be charged or discharged, indicating that internal damage had taken place at the pre-heating temperature. These results demonstrate that TRC Cs are thermally responsive, and can prevent damage to other components of the cells b undergoing a large increase in their effective internal impedance upon exposure to excessive temperatures (i.e., daring pre-heating). When the impedanc of the TRCMCs increases, large- currents cannot flow within the battery cell, and the cell's other components are thereb protected from temperature-related damage.

Example 1 ; Mitigatin Li nef ction

Soil liquefaction can result in significant damage to buildings and structures that are suppoited by the liquefying soil. By using a small amount of polymer binder material, the soil can be significantly strengthened, thus mitigating soil liquefaction and helping to prevent associated structural damage to the buildings.

The same soil and the same epox -hardener binder .material mixture as in Example 4 were used to fabricate another composite material. The epoxy resin binder material and the hardener were first - mixed by means of a lab spatula in a 50 mt beaker, at a weight ratio of 5: 1. After mixing, 35 grams of the soil was placed into a 50 mL beaker. The soil was separated from the inner wall of the beaker by aluminum foil. A small amount of epox -hardener mixture was diluted by eihanol, and poured onto the soil from the top, The polymer content was 5 weight percent of the soil, weight; the polymer-ethanol volume ratio was 1:1. The soaked soil was at rest in air for 2 days at room terapemtisre.

FIG. 23 shows an image of the resulting composite material, which was structurally integral. Beam samples were cut, polished, and their ftexuraS strengths were measured, following the same procedure as in Example 4. The flexural strength was 2 MPa. The hardened soil was also tested under simulated environmental conditions by washing it in a stream of water for 10 mm. The flow rate of the stream was 1 IJm and the soil composite material sample mass was 35 g. The weight loss of the soil wa less than 1%. Example 15 : Sol vent- Aided Binder Material Mixture and Food/M edicme Production

Carboxymethyicellulose (CMC) is used in the harmaceutical industry as a water-soluble and biocompatible binder material for medications. Composite materials can readily be produced us ng the methods disclosed herein . using earhoxyraethylcellulose s dium as the binder material. In this example, a filler material consisting of powder ground and harvested from an, Oreo* cookie was used.

Carboxymethyicellulose. sodium was first mixed wit water at a 50:50 mass ratio in a 50 m.L beaker. A small amount of this mixture was applied to S g. of ground cookie pow ^r der. The binder material content was 5 weight percent .of the total weight. The cookie powder and the binder material were thoroughly raised for a few minutes in a 5 niL beaker by a lab spatula, and then transferred int a load cell. The load cell was made of stainless steel and was 3/4" in inner diameter and 2" in height. It was equipped w th a top piston and a bottom piston; both of the pistons were 3/4" in diameter and 1" in height. The load cell was compressed through the top and bottom pistons by a type-5582 Instron machine, with a loading rate of 0.3 rnm/min. The maximum compression pressure was 350 MPa. After the first loading, the top piston was removed and the compressed material was transferred into a 50 raL beaker and broken apart by a lab spatul into aggregates having si es below 1 0 μηι. The mixture was placed back into the load cell and compressed again at the same loading rate and maximum pressure. The compacted material was kept in the load cell, with the pistons remaining hi place but not compressed, and the mixture was cured and dried in a VW (1330GM) box furnace at 100 °C in air fo 24 hours.

After curing, the samp le was removed from the load eel! and cut into beam samples using an MTI high speed diamond cut-off saw. The sample surfaces were polished by 320 grit sand paper. The flexural strength was measured in a three-point bending setup on the type-5582 Instron -machine, in the displacement .control mode. The cross-head speed was set to 3.0 mm min and the span length, .£-. was set to 19.05 mm. The flexural strength i defined as R - (3iQ,)(PmsJJh(fi , where / is the maximum load; h is the sample width, an d is the sample height. The- average flexural strength was 3 MPa. E le: .16..€ omposi te. Material Fabr ieation . wi th . Po amin , A gents

Foaming agents can be added into the filler material- nder material mixture to generate bubbles to adjust the binder- material and filler material properties (e.g., the effecti ve fluidity aid v olume of binder material, and/or the wettability of filter materials), In general, a variety of different foaming agents can be used, id can be added at v arious stages of the fabrication process (e.g., foaming agents can be added to start the foaming process before, during, or after the compression of the mixture).

.Another composite materia! was produced, using the same sand and epox binder material as in Example 3. The foaming agent was toluenesttlfonyi hydrazide iTSi ), provided by SigflWrAl.dri.cb (Product No.1.32004). The resin and the hardener were first mixed thoroughly with a lab spatul in a 50 mL beaker, at weight ratio of 5: 1. Then, TSFt was added into the resin-hardener mixture, and mixed with a lab spatula for 1 minute. The TSFf was either 5 weight percent or 10 weight percent of the total binder material mass. After mixing, a small amount of epoxy-TSH mixture was added to 5 g of air-dried sand grains. The resin binder material content was 4 weight percent of the total weight. The sand grains and the resin binder material were thoroughly mixed for a few minutes in a 50 mL beaker b a lab spatula, and the resulting mixture was transferred into the same steel cell as in Example 3. The pressure application, curing, cutting, polishing, and flexural strength measurement procedures were- the same as in Example 3. The applied pressure was 350 MPa. The samples with 5 weight percent TSH had an average flexural strength of 30 MPa; the samples with 10 weight percent TSH had an average flexural strength of 26 MPa,

Example 17: Ncm-Uniforro Distribution of Binder- Material

As discussed above, composite materials can be produced that can vary in composition at different locations within the material, for a variety of structural or functional applications. When the binder material includes a polymer, the polymer need not be uniforml distributed within the composite m terial. For example, critical load-carrying regions may have a higher local polymer binder material content, while regions where local loadings are relatively small may have lower local binder -material content. Different sections of materials can be added and processed in a stepwise manner, in an additive manufacturin or 3D printing process. For example, a portion of a composite materia! can be added, compressed, and/or cured, before the next portion of material is added mid processed.

Another composite material was prepared by mixing resits and hardener ^• thoroughly with a lab spatula in a 50 mL beaker, at a weight ratio of 5:1. After mixing, a small amount of epoxy resin hinder material-hardener mixture was deposited onto 5 g of air-dried soil grains.

The resin binder material content, was 2 weight percent or 4 weight percent of the total weight for different hatches. Each batch of soil-resin binder material mixture was thoroughly mixed for a few minutes in a 50 mL beaker by a lab spatula, and was transferred into a load cell The load cell was made of stainless steel and was 3/4" in inner diameter and 2" in height, it was equipped wit a top piston and a bottom piston; both of the pistons were 3/4" in diameter and I " in height. The load cell was compressed through the top and bottom pistons by a type-5582 Instron machine, with a loading rate of 0.3 mm/min. The maximum compression pressure was 350 MPa. After the first loadings the top piston was removed and the compressed soil-resin binder material .mixture was transferred into a 50 mL beaker, and broken apart by lab spatula into small pieces. Next, the bottom one quarter volume of the load cell was filled:- with 1.25 g of soil-resin mixture of 4 weight percent resin hinder material content; the soil-resin mixture was slightly condensed by the upper piston, by using the Instron machine under a pressure of 10 M Pa. The upper pis on was removed after compression. The middle half of the load cell was then filled with 2.5 g of soil-resin hinder material mixture of 2 weight percent resin content, followed by slight compression by the upper piston, using the Instron .machine under the pressure of 10 MPa, The upper piston was removed after compression. Finally, the top quarter of the load cell w ^; as filled by 1 ,25 g of soil-resin binder material mixture of 4 weight percent binder material content. The entire sample was compressed by the upper piston in the Instron machine, at the loading rate of 0.3 mm/min. The maximum compression pressure was 350 MPa. The compacted material was kept in the load cell and cured in a VW - 1.-330GM box furnace at- 100 °C in a for one hoar. After curing, the sample was removed from the load cell and cut into beam .samples using an Mil high speed diamond cut-off saw. The sample surfaces were polished using 320 grit sand paper. The flexura! strength was measured in a three-point bending setup on the lype-5582 Instron machine, in the displacement control mode. The erosshead speed was set to 3.0 mrn/mhi and the span length, / _· , was set to 19.05 mm. The ilexural strength is defined as .R ~ ^' (3 2%PtmJJhtP), where is the maximum load, b is the sample width, and d is the sample height. The average fiexural strength was 22 MPa,

Example 18.: Ste ped Proees si n of Composite M a teriajs

As discussed above, the fabrication methods disclosed herein permit step-wise or segmented processing of mixtures of binder and filler materials to form composite materials. When pressure is appl d to the mixtures., compaction ca be -performed, section by section, sfep-by~step, area by area, or layer b layer. The compression pressure, rate, area, direction, and mode ma vary in each operation. Different sections of materials can be added and processed step-by-step, in an additive manufacturing -or three-dimensional printing process (i.e., a. portion of material can be added, compressed, and/or cured, before next portion of material is added and processed).

.Another composite material was produced, using the same soil and polymer binder material as in Example 4. The resin and the hardener were first raised thoroughly with a Sab spatul in a 50 mL beaker, at a weight ratio of 5:1. After mixing, a smal l amount of resin-hardener mixture was appli ed to 5 g of air-dried soil grains. The resin binde -material content was 4 weight percent ofthe total weight, for different batches. The soil grains and the resin were thoroughly mixed for a few minutes in a SO ml, beaker by a lab spatula, and the resulting mixture was transferred into a load cell The load cell was made of stainless steel and was 3/4" in inner diameter and 2" in height. It was equipped with a top piston and a bottom piston; both of the pistons were 3/4" in diameter and l ^M in height. The load cell was quasi- statical !y compressed through the top and bottom pistons by a type-5582 Instron machine, with the loading rate of 0.3 mm/mm. The maximum compression pressure was 350 MPa. After the first loading, the top piston was removed and the compressed material was transferred into 50 nil, beaker, broken apart b a lab spatula into small aggregates. A third of the mixture was placed back into t e load cell and compressed again at the same loading rate but only to 200 MPa. After maintaining the pressure on the mixture, for 2 minutes, the to piston was removed and another 1/3 of the mixture was placed into the load ceil and compressed again at the same loadin rate at 200 MPa, After maintaining the pressure for another 2 minutes, the top piston was removed again and the final 1/3 of the mixture was placed into the load cell and compressed at the same loading rate at 350 MPa, The ^■ .compacted material was kept in the load cell and cured in a YWR-1330GM box furnace at 100 °C in air for one hour.

After curing, the composite material was removed from the load cell and cut into beam samples using an Mil high speed diamond cut-off saw. The composite .material surfaces were polished using 320 grit sand paper. The. flexural strength was .measured In a three-point bending setup on. the type-5582 Instron machine, in the displacement control mode. The crosshead speed was set to 3,0 mtn min and the span length, L, was set to 1 .05 mm. The flexural strength is defined as R

(3/2)(/Via.¾/./&?-), where -is the maximum load, b is the sample width, and t is the sample height The measured, flexural strength was 25 MPa,

Example J .9: C omposite M aterial s w i t in er or Snrfac e Features

Another composite material was produced, using the same resin binder material and hardener as in Example 4. The binder material and hardener were first mixed thoroughly with a lab spatula in 50 mL beaker, at a weight ratio of 5:1. After mixing, a smal l amount of resin-hardener mixture was added to 5 g of air-dried soil grains. The resin binder material content was 4 weight percent ofthe total weight. The soil grains and the resin were thoroughly mixed for a few minutes in a 50 mL beaker b a lab spatula, and the resulting mixture was transferred into a cylindrical load cell. The load cell was made of stainless steel, . measuring 3/4" in inner diameter, 2" In height, and 1 " in outer diameter. It was equipped with top piston and a bottom piston; both of the pistons were made of stainless steel, 3/4" in diameter and 1 " in lieight. The bottom piston was inserted in the cell, and the soil-resin binder material mixture was placed on top of he bottom piston, inside the steel cell The top piston was compressed into the load cell by a type-5582 instron. machine and pressure was applied to the sand-resin binder .material msxiure, with a loading rate of 0.3 mm/min. The maximum compression pressure was 350 MPa. The compression time was 5 minutes. After the first loading, the to piston was removed id the compressed material was transferred into a 50 mL beaker, and broken apart by a lab spatula into small pieces.

FIG. 24 shows an image of the apparatus that was used, to prepare the composite material A divider 2402 was placed into the em ty load ceil 2406, _: onthe bottom, piston, 2404 as shown in FIG. 24. I n genera ^' the divider can ha ve various shapes, according to the intended design of the inner features of the resulting composite material The divider divided the load cell into different zones; each zone was filled with either a compressed soil-resin binder material mixture, or with air- dried soil without binder material The mixture in each zone was compressed, with the same loading rate, maximum pressure, and compression time as was -used with ike first, loading. The compacted material was kept in the load cell and .cared in a VWR- 1.330GM box furnace at 100 °C in air for one hour.

After curing, ^' the sample was removed from the load ceil and put into a 50 mL beaker filled with water. The beaker and the materia! was then placed in a VWR- 50BT ukrasonieatot, and vibrated for 1 hour at 60 Hz. The regions With no resin binder ma terial were removed during sonication. Zones that previously contained on ly filler material defined the voids 2502 of the resulting composite material, as shown in FIG. 25. Example 20; Additional Filler Materials/Reinforcements

Another composite material was produced, using the same filler material polymer binder materia], and preparative procedures used in Example 4, The resin binder material and the hardener were first mixed thoroughly with a lab spatula in a 50 mL beaker, at a weight ratio of 5:1, Next, a small amount of resin-hardener mixture was added to 5 g of air-dried soil grains. The resin, binder material content was 4 weight percent of the total weight. The soil grains and the resin binder material were thoroughly mixed for a few minutes in a 50 mL beaker by a lab spatula, and the .resulting mixture was transferred into a cylindrical load cell. The load celt was made of stainless steel, measuring 3/4" in inner diameter, 2" in height, and I" in outer diameter, it was equipped with a top piston and a bottom piston; both of the pistons were, made of stainless steel, measuring 3/4" in diameter and 1 " in height. The bottom piston was inserted in the cell, and the soil-resin hinder material mixture was placed on top of the bottom piston, inside the steel cell The top piston was compressed into the load ceil by a type-5582 Instron mac ine and applied a pressure -on the sand-resin bidder material .mixtore, with the loading rate of 0.3 n m . The maximum compression pressure was 350 MPa. The compression time was 5 minutes. After the first loadiag, the top piston was removed and the compressed material, was transferred into a 50 mL beaker, and broken apart by a Sab spatula into small pieces. About 0.1 g of glass fibers, which were approximately 0.08· mm in diameter and approximately I mm in length, were added into the mixture and mixed thoroughly with a lab spatula. The soil-resin binder material mixtitre with glass fibers was then placed back into the load cell and compressed again, with the same loading rate, ma imum -pressure, ^' nd compression time as was used in the first loading. The compacted material was ke t in the load cell and cured i a VWR- 1330GM bo ftiruace at 100 °C in air for one hour.

After curing, the material was removed from the load cell and cut into beam samples using an Mil high speed diamond cut-off saw. The sample surfaces were polished using 320 grit sand paper. The .fiexural strength measurement procedure was the same as in Example 4. The material had a measured fiexural strength of 31 MPa.

Example 211 Sectioned Processin of Composite Material s

As discussed above, during fabrication of the composite materials, the mixture of binder and filler materials does not have to be compacted simultaneously. Further, composite materials produced according to the methods disclosed herein can be fabricated in stages rather than in a single pressiuization step. Instead, pressure treatment can be performed section b section, step-hy-step, are by area, or layer by layer. The compression pressure, rate, area, direction, and mode may vary in each operation. Different sections of materials can be added and processed step-by-step, in a additive manufacturing or three-dimensional printing process (i.e.. a portion of material can be added, compressed, and/or cured, before the next portion of material is added and processed) .

.Another composite material was produced, using the same er material and binder material used in Example 4. The resin and the hardener were first mixed thoroughl with a lab spatula in a 50 rhL beaker, at a weight ratio of 5:1. After mixing, a small amount of resin-hardener mixture was deposited onto 8 g of air-dried soil grains. The resin binder material content was 4 weight percent of the total weight. The soil grains and the resin binder material were thoroughly mixed for a few minutes in a 50 mL beaker by a lab spatula, and the resulting mixture was transferred into an L-shaped load cell, as shown in FIG. 26, formed of hardened steel. The l.~ shaped load cell was 4 inches long on each side, with a hollow inne channel in the middle measuring 0.5" by 0,5". Two pistons were designed to fit the inner channel. The piston position could be fixed by loading pins during compression.

The soil-resin binder material mixture was compressed in th L-shaped load cell by a type-5582: insiron machine, through piston 2602. The posi ion of the ther piston 2604 was fixed. The loading rate was 0.3 mm/min. The maximum

compression pressure was 350 MPa. After the peak pressure was reached and maintained for 5 minutes, piston 2602 was locked and fixed in place. The ^' L-shaped load cell was flipped over, and material insid was compressed through piston 2604 with the same loading rate and maximum compression pressure. After holding the peak pressure for 5 .minutes, the compacted material was kept in the load cell and cured in a VWR-1.33QGM box furnace at 100 °C in air for one hour.

After curing, the sample was removed from the L-shaped load cell and cut into beam samples using an M il high speed diamond cut-off saw. The sample surfaces were polished using 320 grit sand paper. The flexural strength was measured in the same three-point bending setup as was used in Example 4. The composite material had a flexural strength of 30 MPa.

Example 22: Curing at Room Temperature

Another composite material was produced, using the same filler material as was used in Example 4. The epox resin binder material was the same as that used in Example 3, but the hardener was EPi URE-3072 (obtained from Momentive). The resin binder material preparation, soil-resin premising, compression, re-mixing, and re-compression process were the same -as in Example 4. The compacted material was kep in the load cell and cured- at room temperature in air for 1-7 days.

After curing, the composite material was removed from the load cell and cut into beam samples using an MTi hig speed diamond cut-off saw. The sample surfaces were polished using 320 gilt sand paper. The fiexural strength measurement process was the same as that, used in Example 4, The testing data showed that the material had a fiexural strength of 8 MPa whets the curing time was 24 hours. The fiexural strength increased to 15 MPa when the curing time was 48 hours, and to 22 MPa when the curing time was 168 hours-.

Example 23: B ioroimiek? Composite . Mate ials

The methods disclosed herein can be used to fabricate hiomimiekmg

.materials, _, including natural or man-made materials that contain a large amount of filler material and/or reinforcemen t componen ts and a small amount of binder material,

A composite material was produced using calcium carbonate (provided by Acres Orga cs) as a filler material. The epoxy and tlie hardener were the sam as those used in Example 4. Th resin and the hardener were first mixed tiioroiighly with a lab spatula in a 50 mL beaker, at a weight ratio of 5: L After mixing, a small amount of resin-hardener mixture was added onto 2.5 g of calcium carbonate. The resin binder material content was 15 weight percent of the total weight. The calcium carbonate and the resifi binder material were premixed for a few minutes in a 50 mL beaker by a lab spatula. The first compression, re-mixing, second compression, curing, and testing procedures were the same as those used in, Example 4. The maximum compression pressure was 350 MPa. The material, which may be viewed as an artificial nacre, had a fiexural strength of 23 MPa.

OTHER EMBODIMENTS

A number of embodiments have been described. Nevertheless, it will b understood that various modifications ma be made without departing from the spirit and scope of the disclosure. Accordingly, other embodiments are within the scope of the following claims.