WO2012078664A1

WO2012078664A1 - High strength and high elasticity composite materials and methods of reinforcing substrates with the same

Info

Publication number: WO2012078664A1
Application number: PCT/US2011/063581
Authority: WO
Inventors: Thomas L. Attard
Original assignee: University Of Tennessee Research Foundation
Priority date: 2010-12-06
Filing date: 2011-12-06
Publication date: 2012-06-14
Also published as: JP2017149149A; EP2648905A4; EP2648905A1; CA2820465A1; KR20130137196A; US20140099496A1; JP2013544688A

Abstract

In accordance with various embodiments of the disclosed subject matter, a composite material is provided. The composite material in accordance with some embodiments of the disclosed subject matter includes a high tenacity fiber reinforced polymer fabric and a polyurea coating layer formed on at least one surface of the polymer fabric. The composite material provides significant strength, flexibility, and energy dissipation. In some embodiments, the composite material can be used to reinforce structural and non-structaral. substrates.

Description

HIGH STRENGTH AND HIGH ELASTICITY COMPOSITE MATERIALS AND METHODS OF REINFORCING SUBSTRATES WITH THE SAME

Cross. Reference to Related A.paUca tioas

[000J I This application claims the benefit of United States Provisional Patent

Application No. 61/420,1.59, Bled December 6, 2010, which is hereby incorporated by reference herein in its entirety.

Cop^yright Notice

[ΘΘ02] A portion of the disclosure of this patent document contains material which is subject to copyright protection. The copyright owner has no objection to the facsimile reproduction by anyone of the patent document or ihe patent disclosure, as it. appears in the Patent and Trademark Office patent file or records, but otherwise reserves all copyright rights whatsoever.

Technical Field

[0003} The disclosed subject matter relates to a composite material comprising a high tenacity fiber reinforced polymer fabric, such as a carbon fiber reinforced polymer, and a poiyu.rea layer coated on at least one surface of the polymer fabric. The disclosed subject matter also relates to reinforcing a substrate, such as a wood, concrete, masonry, steel or other component, with the composite material.

Background

[0004] Earthquakes remain one of nature's deadliest forces. One wa in which earthquakes cause damage is the stress they exert on buildings and other structures due to ground shaking and ground rupture. The damage can render buildings and other structures unusable, or at worst, cause their outright collapse, often resulting in human injury or death. For example, ihe 2010 earthquake in Haiti caused significant damage or destruction to many homes and to the health care infrastructure, resulting in over 170,000 casualties and affecting over 3 million people. (0005} Furthermore, earthquakes, such as, for example, the 1906 San Francisco earthquake, often initiate associated fire disasters (i.e., "fire following earthquake" disasters). The earthquake-associated fires can significantly contribute to the economic losses and to the loss of life related to the original earthquake event. Regions of northern and southern

California thai lie along the San Andreas Fault and its various sister faults are primary candidates for a "fire following earthquake" disaster due to their population, and infrastructure density. Recent modeling of present-day damage resulting from a "fire following

earthquake'^' disaster of the same magnitude as the 1906 San Francisco earthquake and fire estimated that nearly 1 million residents of northern California would be impacted by economic, social, and mortality factors. The overall economic losses were estimated to be about $ 1 50 billion dollars.

{00061 in addi ion to earthquakes and other seismic events, structural damage can also be caused by other natural or non-natural events that exert stresses on buildings and other structures, including, for example, hurricanes, tornados, landslides, flash flooding, tsunamis, and explosions due to warfare or terrorism. Moreo ver, structural damage can occur even in die absence of a particular catastrophic event. For example, damage to structures can be caused by regular long-term use, long-term exposure to environmental factors, and/or increased use and/or loading of structures due to increasing population demands.

|ΘΘ0?! For at least these reasons, various approaches have been made to strengthen structural elements, such as concrete slabs, wails, beams, columns, and foundations. For example, one approach for strengthening new and existing concrete structural eiemenis is by reinforcin them with a variety of steel shapes, such as steel meshes, steel reinforcement bars, and steel grids. However, steel or other suitable metals used for reinforcing these structural elements are subject to corrosion . The products of corrosion result in an expansion of the column of the steel which causes a spelling effect, winch can cause a breakup and

deterioration of the concrete structure. In addition, while other corrosion-resistant materials have been considered, these materials bring about other difficulties, such as delatnin tioti, less ductility, or highe cost.

[0008} Accordingly, it is desirable to provide high strength, highly damped, and/or high elasticity composite materials that overcome these and other deficiencies of the prior art. (0009] For example, there is an ongoing need for protection systems to reinforce structures (e.g., buildings and other infrastructure) against damage due to torsion and or shear and tensile stresses, such as might be experienced, for example, during structural

accelerations and displacements, or to strengthen them following such damage. In addition, there is a need for materials that can also protect buildings and other infrastructure from fire damage and/or that can provide other additional protection, such as from ultraviolet radiation, water damage, and/or environmental pollutants, and/or thai can provide an msulative effect, e.g., to reduce heating and/or cooling costs in the reinforced structures.

Sum ary

(0ΘΙ0] in accordance with various embodiments of the disclosed subject matier, a composite material is provided. The composite material in accordance with some embodiments of the disclosed subject matier includes a high tenacity fiber reinforced polymer fabric and a poiyurea coat ing layer formed on at leas one surface of the poly mer fabri c. The composite material provides significant strength, flexibility, viscous damping, and energy dissipation. In some embodiments, the composite material can also be formed to have additional protecting properties, such as fire resistant properties, UV protective properties, or moisture resistant properties.

[ΘΘ1.1.) The composite material can be used in a variety of applications. For example, the composite material can be used to reinforce structural and/or non-structural substrates to protect them from damage (e.g., due to seismic or wind activity, lire, impact, loading, and/or explosive forces), in another example, the composite materia! can be used to strengthen structural and/or non-structural substrates following damage by forming the composite- material on at least one surface of the substrate (e.g., tightly wrapped around the entire substrate, formed over a crack in the substrate, etc.). in yet another example, the composite material can be used to provide a particular protective property to a substrate, such as UV protection, fire resistance, corrosion resistance, moisture resistance, and/or energy efficiency, in yet another suitable example, the composite material can be used as a stand-alone structure that is strong, stiff and provides significant damping, while also providing one or more protective properties, such as UV protection, fire resistance, corrosion resistance, moisture resistance, and/or energy-efficiency .

(ΘΘ12) In a more particular example, the composite material can be used to provide energy dissipation and sustainable strength properties to light-frame wood construction, concrete and masonry structures, and/or steel structures to save occupant lives and protect infrastructure during extreme loading events (e.g., an earthquake or human-induced hazards having high impact loads involving ballistics or blast loads), in some embodiments, the composite material can be used for the lightweight design of vehicle components, which would improve safety, performance, and fuel efficiency, [0013} in some embodiments, ihe disclosed subject matter can provide a protection system thai reduces structural accelerations and displacements by combining a high strength/high stiffness material with sustainable energy dissipation and ductility. In some embodiments, this protection system can include a composite material that is tightly wrapped around or applied as a ply to (e.g. , adhered to) an exterior .face or surface of a substrate, thereby providing viscoelastic behavior properties that transition to a sustainable elastomeric state by sustaining the interfacial interaction ^'between the composite material and the ^•underlying substrate. The composite material can act as an energy-release valve by providing sustainable energy dissipation and large viscous-type damping during extreme loading events, such as during earthquakes, that minimise structural damage to the substrate. In some embodiments, ihe composite substrate system can allow for a change in viscous damping ratio (e.g., the composite/substrate system has a different viscous damping ratio than the substrate alone).

[0014] In accordance with some embodiments of ihe disclosed subject matter, a composite material is provided, the composite material comprising: a substrate; a fiber reinforced polymer fabric layer attached to at least a portion of the substrate; and a polyurea coating layer formed on an exposed surface of the fiber reinforced polymer fabric layer, |0015 to some embodiments, the substrate is one of; wood, masonry, concrete, steel, and a combination thereof,

[0016] in some embodiments, the substrate lias at least one damaged portion and the fiber reinforced polymer fabric layer and ihe polyurea coating layer are formed on the at leas one damaged portion of the substrate.

[0017] in some embodiments, ihe fiber reinforced polymer fabric layer is a carbon fiber reinforced polymer fabric.

[0018] to some embodiments, the polyurea coating layer is formed by applying an elastomeric polyurea-form ng component solution to the exposed surface of the fiber reinforced polymer fabric layer, wherein the elastomeric polyurea-forming component solution forms an aromatic polyurea coating layer.

[0019] In some embodiments, the polyurea further comprises mi additive component, wherein the additive component is at least one of: an ultraviolet (UV) protective additive, a flame retardant, a corrosion protective additive, a moisture resistance additive, and ceramic microspheres,

[0020] to accordance with some embodiments, a method for reinforcing a substrate is provided, the method comprising: providing a substrate; attaching a high tenacity fiber reinforced polymer fabric to at least a portion of the substrate; applying a saturant composition to an exposed surface of the high tenacity fiber reinforced polymer fabric, wherein the saturant composition comprises a polymer resin; coring the saturant composition to form a tacky surface; applying an elastoinenc polyurea-formmg component solution to the tacky surface; and curing the pclyurea- forming component solution to form a poly area coating layer.

(ΘΘ21) In some embodiments, the method further comprises: applying a primer lay er to a surface of the substrate; and applying another saturant composition to the primer layer. The primer layer can be used to prepare the substrate and/or assist layers to bond with the substrate. The saturant composition can be used to bond the high tenacity fiber reinforced polymer fabric with the substrate.

ft⁾022| In some embodiments, the substrate is one of: wood, masonry, concrete, steel, and a combination thereof.

|ΘΘ23) In some embodiments, the substrate is used in one of: a newly constructed structure and an existing structure.

[0024^'j in some embodiments, the method further comprises performing surface preparation on at least a portion of the substrate, wherein the surface preparation includes at least one of: smoothing the substrate, filling in one or more damaged portions of the substrate with a putty material, and cleaning the substrate.

[0025] In some embodiments, the high tenacity fiber reinforced polymer fabric is wrapped around the substrate.

(0026] In some embodiments, the polyurea-forming component, solution comprises an isocyanate component and a polyamine component, the method further comprising mixing the isocyanate component and the polyamine component prior to applying it to the tacky surface of the saturant to form the polyurea- orming component solution. The polyurea- forming component solution may, in some embodiments, have an excess of the isocyanate component.

(0027] In some embodiments, the method further comprises spraying the polyurea- forming component solution on the tacky surface.

[ΘΘ28] In some embodiments, the method further comprises providing an additive component into the polyurea-forming component solution, wherein the additive component is one of: an ultraviolet (UV) protective additive, a flame retardant, a corrosion protective additive, a moisture resistance additive, and ceramic microspheres.

(0029] In some embodiments, the polyurea coating layer has a thickness, the method further comprising controlling the thickness of the poiyurea coating layer.

[0Θ30] In some embodiments, the method further comprises applying the poiyurea- forming component solution to form the poiyurea coating layer after a given time when the saturant composition on the high tenacity fiber reinforced fabric layer has become tacky and controlling the thickness of the poiyurea coating layer. In some embodiments the given time is between about two hours and about five hours.

(0O31| In some embodiments, the saturant composition is cured for a first time period and wherein the poiyurea-forming component solution, is cured fo a second time period, the method further comprising modifying the first time period and the second time period to obtain material properties of the poiyurea coating layer on the high, tenacity fiber reinforced polymer fabric.

[0032] in some embodiments, a first component of the polyitrea.*formmg component solution and a second component of the tacky surface of the saturant composition applied to the high tenacity fiber reinforced polymer fabric interact to form a sustainable interface between the poiyurea coating layer and the high tenacity fiber reinforced polymer fabric.

[0033] In accordance with some embodiments, a method for reinforcing a substrate having damaged portions is provided, the method comprising: forming a poSyorea-coated high tenacity fiber reinforced polyme fabric, wherein the forming comprises: providing a high tenacity fiber reinforced polymer fabric; applying a saturant composition to a surface of the high tenacity fiber reinforced polymer fabric, wherein the saturant composition comprises a polymer resin; curing the saturant composition to form a tacky surface; applying an elastomerie poiyurea-forming componen solution to the tacky surface; and curing the poiyurea-forming component solution to form a poiyurea coating layer on the high tenacity fiber reiiiforced polymer fabric; preparing at least a portion of the siibstrate for reinforcement prior to positioning the polyiirea-coated high tenacity fiber reinforced polymer fabric on the substrate; and attaching the polyurea-coated high tenacity fiber reinforced polymer fabric to at least the damaged portions of the substrate.

[ΘΘ34] hi some embodiments, the method further comprises applying a ptitty to the substrate ha ving damaged portions to create a smooth surface on the substrate.

[0035] In some embodiments, the method further comprises appl ing another saturant composition to an interface between the substrate and the high tenacity fiber reinforced polymer fabric.

|0036| in some embodiments, the method further comprises forming the poiyurea coating layer of a thickness based at. least in part on an assessment of the damaged portion of the substrate.

|0037| In some embodiments, the method further comprises forming the polyorea coating layer after a given, time when the saturant composition on the high tenacity fiber reinforced fabric layer has become tacky and based at least in part on an assessment of the damaged portion of the subsu me.

[0038] hi some embodiments, at least a first component of the polyurea-forming component solution and a second component of the tacky surface of the saturant composition applied to the high tenacity fiber reinforced polymer fabric interact to form a sustainable interface between the polyurea coating layer and the high tenacity fiber reinforced polymer fabrsc.

[0039] in some embodiments, the method further comprises forming a plurality of poiyurea-coaled high tenacity fiber reinforced polymer fabrics and attaching each of the plurality of polyurea-coated high tenacity fiber reinforced polymer fabrics to a different portion of the substrate.

Brief Description of the .Drawings

ΘΘ40] FIG. 1 is an illustrative cross-section of a composite having at least a high tenacity fiber reinforced polymer fabric layer and a polyurea coating layer formed on a surface of a substrate in accordance with some embodiments of the disclosed subject matter.

[0041] FIG. 2 is an illustrative example of a process for forming a composite having at least a high tenacity fiber reinforced polymer fabric layer and a polyurea coating layer on a. surface of a substrate in accordance with some embodiments of the disclosed subject matter.

[0042] FIG. 3 is an illustrative example of a process for retrofitting a substrate (e.g., a damaged substrate) with a composite having at least a high tenacity fiber reinforced polymer fabric layer and a polyurea coating layer in accordance with some embodiments of the disclosed subject matter.

[0043] FIG. 4 is an illustrative graph of tensile force versus axial displacement that compares the properties of carbon fiber reinforced polymer fabrics with the properties of poly urea-coated carbon fiber reinforced polymer fabrics in accordance with some

embodiments of the disclosed subject matter.

|0044{ FIG. 5 is an illustrative graph, of torque versus angle of twist that compares the torsion properties of a wooden rod wrapped with a carbon fiber reinforced polymer fabric with the torsion properties of a wooden rod wrapped with a polyurea-coated carbon fiber reinforced polymer fabric composite in accordance with some embodiments of the disclosed subject mailer.

(0045} FIG. i>A is an illustrative force-deflection graph showing the results of wood beam bending studies performed on various wood substrates in accordance with some embodiments of the disclosed subject matter.

|0046| FIG, 6B is an illustrative image of testing equipment and a composite-wrapped wood beam during the testing that provided the results shown in FIG. 6A.

(0047) FIG. 6C is an illustrative image of a composite-wrapped wood beam after the testing using the testing equipment shown in FIG. 6B.

|ΘΘ48| FIG. 7 is an illustrative force-deflection graph showing the results of wood beam bending study on a wood beam substrate that was wrapped in a composite having a reinforced polymer fabric layer and a polyurea coating layer (one eighth of an inch thick) in accordance with some embodiments of the disclosed subject matter.

(0049) FIG. 8 is an illustrative graph showing the strain capacities and elastomeric flow of various wood substrates in accordance with some embodiments of the disclosed subject matter.

[ΘΘ50] FIG. 9 is an illustrative graph showing load deflection curves for various wood substrates in accordance wi th some embodiments of the disclosed subject matter,

|ΘΘ51) FIG, IDA is a graph of a simulated accelerat ion-time history of a two-story wooden structure wrapped with a composite in accordance with some embodiments of the disclosed subject matter.

(0052} FIG.1.08 is a graph of a simulated acceleration-time history of a two-story wooden structure wrapped without a composite in accordance with some embodiments of the disclosed subject matter.

[ΘΘ53] FIG.10C are illustrative hysteresis curves of the two-story wooden structure in FIGS. 10A and 10B subjected to forces similar to an earthquake in accordance with some embodiments of the disclosed subject matter.

(0054) FIG. I. LA shows illustrative images of preparing and retrofitting a damaged substrate with a poly urea-coated carbon fiber reinforced polymer fabric composite in accordance with some embodiments of the disclosed subject matter.

[0055] FIG. .1 .IB shows illustrative cross-sections along the retrofitted substrate in accordance with some embodiments of the disclosed subject matter,

|0Θ56) FIG. 1 1C shows illustrative load deflection curves in various retrofitted steel reinforced concrete composite beams in accordance with some embodiments of the disclosed subject matter. |ΘΘ57] FIG. .12A shows illustrative Images of preparing and retrofitting a damaged shear wall substrate with a poiyurea-coated carbon fiber reinforced, polymer fabric in accordance with some embodiments of the disclosed subject matter.

fOOSSJ FIG. 12B shows illustrative force deflection curves in various retrofitted shear wall substrates in accordance with some embodiments of the disclosed subject matter.

[6059] FIG. 1.2C shows images that illustrate the increase in ductility, confinement and compression strength for a damaged shear wall substrate retrofitted with a poiyurea- coated carbon fiber reinforced polymer fabric composite m accordance with some embodiments of the disclosed subject matter.

[0060] FIG. 13 A shows images that illustrate the results of impact testing between a foam core substrate with a carbon fiber reinforced polymer fabric and a poiyurea-coated carbon fiber reinforced polymer composite in accordance with some embodiments of the disclosed subject matter.

[ΘΘ61] FIG, 13B shows an illustrative force versus displacement graph during impact testing of a foam core substrate with a carbon fiber reinforced polymer fabric and a poiyurea- coated carbon fiber reinforced polymer composite in accordance with some embodiments of the disclosed subject matter,

|0062] FIG . 14A shows the viscous damping properties of a thin steel beam substrate with a carbon fiber reinforced polymer fabric and a poiyurea-coated carbon .fiber reinforced polymer composite in accordance with some embodiments of the disclosed subject matter. |ΘΘ63] FIG. 14B shows the power spectrum and model properties of a thin steel beam substrate with a carbon fiber reinforced polymer fabric and a poiyurea-coated carbon fiber reinforced polymer composite in accordance with some embodiments of the disclosed subject matter,

j 0064 FIG. 15 A shows the damping ratio as a function of thickness of the polyurea coating layer for a thin steel beam with a poiyurea-coated carbon fiber reinforced polymer composite, where the damping ratio of a thin steel beam with, a poiyurea-coated carbon fiber reinforced polymer composite is compared, with the damping ratio of a thin steel beam and a thin steel beam with a carbon fiber reinforced polymer fabric, in accordance with some embodiments of the disclosed subject matter.

[0065] FIG. i 5B shows the damping ratio as a function of curing time for thin steel beam with a poiyurea-coated carbon fiber reinforced polymer composite in accordance with some embodiments of the disclosed subject matter.

[0066] FIG. 15C shows the damping ratio as a function of thickness of the polyurea coating layer for a polyurea-coaied carbon .fiber reinforced polymer composite b itself. where the damping ratio of the po!yurea-coated carbon fiber reinforced polymer composite is compared with the damping ratio of a carbon fiber reinforced polymer fabric, in accordance with some embodiments of the disclosed subject matter.

|006?| FIG, S.5D shows the damping ratio as a function of coring time for a po!yurea- coatetl carbon -fiber reinforced polymer composite by itself in accordance with some embodiments of the disclosed subject matter.

(ΘΘ68] The disclosed subject mailer will now be described more fully hereinafter with reference io ihe accompanying examples and drawings, in which representative embodiments are shown. The presently disclosed subject matter can, however, be embodied in different forms and should not be construed as limited to the embodiments set forth herein. .Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the embodiments to those skilled in the art.

j0069j Throughout the specification and claims, a given chemical formula or name shall encompass all optical and stereoisomers, as well as racemic mixtures where such isomers and mixtures exist.

DEFINITIONS

[0070} While the following terms ar believed to be well understood by one of ordinary skill in the art, the following definitions are set forth to faciiitate explanation of the disclosed subject matter.

[0071] Unless defined otherwise, ail. technical and scientific terms used herein have the same meaning as commonly understood to one of ordinary skill in the art to which the presently disclosed subject matter belongs. Although any methods, devices, and materials similar or equivalent to those described herein can be used in the practice or testing of the presently disclosed subject matter, representative methods, devices, and materials are now described.

[0072] Following long-standing patent law convention, the terms "a," "an," and ^**_he" refer to "one or more" when used in this application, including the claims. Thus, for example, reference to "an additive"' includes a plurality of such additives, and so forth.

|0073| Unless otherwise indicated, all numbers expressing quantities of size, amount, elongation percentage, tensile strength, reaction conditions, and so forth used in the specification and claims are to be understood as being modified in ail instances by the term "about." Accordingly, unless indicated to the contrary, the numerical parameters set forth in this specification and attached claims are approximations that can vary depending upon the desired properties sought to be obtained by the presently disclosed subject matter.

(0074) As used herein, the term "about," when referring to a value or to an amount of size, weight, concentration, time, or percentage is meant to encompass variations of, in some embodiments ±20%, in some embodiments ±10%, in some embodiments ±5%, in some embodiments ±1%, and in some embodiments ±0.1% from the specified amount, as such variations are appropriate to perform the disclosed methods.

[ΘΘ75] The term "and/or" when used to describe two or more activities, conditions, or outcomes refers to situations wherein both of the listed conditions are included or wherein only one of the two listed conditions are included.

(0076) The term "comprising " which is synonymous with "including " "containing," or "characterized by" is inclusive or open-ended and does not exclude additional, unrecited elements or method steps. "Comprising" is a term of art used in claim language which means that the named elements are essential, but other elements can be added and still form a construct within the scope of the claim.

|0077) As used herein, the phrase "consisting of excludes any element, step, or ingredient not specified in the claim. When the phrase "consists of appears in a clause of the body of a claim, rather than immediately following the preamble, it limits only the element set forth in that clause; other elements are not excluded from the claim as a whole.

(0078) As used herein, the phrase "consisting essentially of limits the scope of a claim: to the specified materials or steps, phis those that do not materially affect the basic and novel characteristic(s} of the claimed subject matter.

(0079) With respect to the terms "comprising," "consisting of," and "consisting essentially of," where one of these three terms is used herein, the presently disclosed and claimed subject matter ca include the use of either of the other two terms.

(0080) The term "fiber" generally refers to an elongated body the length dimension of which is much greater than the transverse dimensions of width and thickness. The term fiber includes either manufactured or natural ^'monofilament, multifilament, ribbon, strip, staple and other forms of chopped, cut or discontinuous fiber and the like having regular or irregular cross-section. The term "fiber" includes a plurality of any of the foregoing or a combination thereof.

(0081) In some embodiments, the cross sections of the fibers may be circular, flat or

- I I - oblong. They may be irregular or regular mulii-lobaf cross-section having one or more regular or irregular lobes projecting from the linear or longi tudinal axis of the fibers.

[0082] High tenacity fibers are fibers that have high ultimate tensile strength and high modulus of elasticity (e.g., a high Young's modulus or tensile modulus). High tenacity fibers include, but are not limited to, highi oriented, high molecular weight poiyoieiiii fibers, particularly high modulus polyethylene fibers and polypropylene fibers: aramid fibers;

polybei axole fibers such as pol hen/.oxazole (PBO) and polybet othiazole (PBT);

polyvinyl alcohol fibers; polyacrylonitrile fibers; liquid crystal copolyester fibers; glass fibers; carbon fibers; basalt or other mineral fibers; as well as rigid rod polymer fibers; and mixtures and blends thereo In some embodiments, the high tenacity fiber is carbon, fiber, glass fiber (e.g., e-glass or s-glass), aramid (e.g., meta- or para-aramid), liquid crystal copolyester fiber, basalt fiber or a combination thereof.

|00S3j Fabrics comprising high tenacity fibers can include a network of fibers in die form of a woven, knitted or a non-woven fabric. In some embodiments, at least 50% by weight of the fibers in the fabric are high tenacity fibers. n some embodiments, at least about 75% by weight of the fibers in the fabric are high, tenacity fibers. In some

embodiments, substantially all of the fibers in the fabric are high tenacity fibers,

|ΘΘ84] The fabrics of the presently disclosed subject matter can comprise one or more different high tenacity fibers. In some embodiments, the yams in the fabric can be essentially parallel in alignment. In some embodiments, the yarns can be twisted, over-wrapped or entangled. The fabrics of the presently disclosed subject matter can be woven with yams havin different fibers in the warp and weft directions, or in other directions.

[0085] As used herein, a "monomer" refers to a molecule that can undergo polymerization, thereby contributing constitutional units (i.e., an atom or group of atoms) to the essential structure of an oligomer or po ly mer,

|0086| An "Oligomer" refers to a molecule of in termedi ate relative molecular mass, the structure of which comprises a small, pluralit of units (e.g., between about. 2 and about 10 repeating units) derived from molecules o f lower relative molecular mass,

[0087] A "pol ymer" refers io a molecule comprising a plurality of repeating units derived from smaller molecules (e.g., monomers or oligomers). In some embodiments, the polymer has more than 10 repeating units, more than 25 repeating units, more than 50 repeating units, or more than 100 repeating units. In some embodiments, a polymer can have more than 1 ,000, more than 5,000, more than 10,000, mote than 50,000, more than 100,000 repeating units, or more than 250,000 repeating units. (0088} A "copolymer" refers to a polymer derived from more than one species of monomer.

[0089] The term "prepolymer" refers to a monomer, oligomer or short chain polymer with reactive terminal groups (e.g., epoxy, ester, carboxylie acid (or carbox late), hydroxy!, vinyl, or amine groups) that can react to form a larger (e.g., higher molecular weight) polymer or copolymer. In some embodiments, "short chats polymer" refers to a polymer with 1,000 repeating units or less (e.g., 1,000, 750, 500, 400, 300, 200, 150, 1 0, 75, 60, 50, 40, or 30 repeating units or less). In some embodiments, a short chain polymer has molecular weight of less than 10,000 g/moS (e.g., less than 10,000, 7,500, 5,000, 4,000, 3,000, 2,000, or 1 ,000 g/mol),

jO09 | The term "resin" or "polymer resin" as used herein refers to a composition comprising one or more polymeric, oiigomeric or monomeric materiais thai can be hardened by polymerization. Thus, in some embodiments, a resin is a viscous liquid composition that can be polymerized to form a solid. Suitable resins include, but are not limited to, epoxy resins, vinyl ester resins, polyester resins and methylnieihacrySale resins.

[ΘΘ Ι.] The hardening (or farther polymerization) of the resin can also he referred to as "curing." in some embodiments, the curing requires a polymerisation initiator, e.g., an organic peroxide. In some embodiments, the level of curing is dependent on time and temperature. In some embodiments, "curing" refers to partial curing, e.g., wherein tire further polymerization of the resin is allowed to proceed to about .1 %. 20%, 30%, 40%, 50%, 60%, 70%, 80%, or 90% completion (i.e., leaving about 90, 80, 70, 60, 50, 40, 30, 20, or about 10% unreacted polymerizabie groups as compared to the percentage of polymeri abie groups present in the resin prior to curing).

[0092] The term "tacky" as used herein refers to a partially cured resin, e.g., a resin or saturant wherein some level of polymerization of the original resin has occurred, but wherein there are still urtreacted, po!ymerizabie groups available.

|0093] The term "polyurea" refers to a polymer comprising multiple urea bonds (i.e., bonds having the structure - -C(=0)- R-, wherein R is H, alkyt, or aryl). Polyureas can be formed by the reaction of isocyanate-ierminaied prepolymers and amine-containing components (e.g., amine-tenninaied polymer resins,, amine-termiiiaied oligomers, or amine- containing monomers).

fi⁾094 The term "isocyanate" refers to the group -3N OQ,

|0095] The term "amine" refers to the group -NR R", wherein R' and R" are independently H, alkyt, or aryl. "Primary amines" are compounds wherein both R' and R" are H. "Secondary amines" are compounds wherein one of " and R" is H and the other is alky! or aryl.

[0096] As used herein, the terra "al^'k i" refers to C;_^y inclusive, linear (i.e., "straight- chain"), branched, or cyclic, saturated or at least partially and in some cases fully unsaturated (i.e., alkenyl and alkynyl) hydrocarbon chains, including for example, methyl, ethyl, propyl, isopropyl, butyl, isobutyl, w jutyl, pentyi hexyl, octyl, ethen l. propenyJ, hutenyl, pentenyl, bexenyi, oeteoyl, butadienyl, propynyl, butynyl, pentynyl, hexynyi, heptynyl, and alleny! groups. "Branched" refers to an a!kyl group in which a lower alky! group, such as methyl, ethyl or propyl, is attached to linear aikyl chain. "Lower aikyl" refers to an aikyl group having .1 to about 8 carbon atoms (i.e., a Cj.§ aikyl), e.g., 1 , 2, 3, 4, 5, , 7, or 8 carbon atoms, "Higher aikyl" refers io an aikyl group having about 10 to about 20 carbon atoms, e.g., 10, 1 1 , 12, 13, 14, 1.5, 16, .17, 18, 19, or 20 carbon atoms. In certain embodiments, "aikyl" refers, in particular, to straight-chain alkyls. in other embodiments, "aikyl" refers, in particular, to C_\-$ branched-chain alkyls.

[0097] Aikyl groups can optionally be substituted with one or more aikyl group substitueots, which can be the same or different. The term "aikyl group substitueni" includes but is not limited to aikyl, halo, ary^'Iamino, acyl, hydroxyl, ary!oxyi, alkoxyl, alkyithio, arylthio, aralkyloxyl, aralkylthio, carboxyl, alkoxycarbonyl, oxo, and cycioalkyl. There can be optionally inserted along the aikyl chain one or more oxygen, sulfur or substituted or unsubsti luted nitrogen atoms, wherein the nitrogen substituent is hydrogen, lower aikyl (also referred to herein as "alk iarainoalkyr), or aryl.

[0098] The term "aryl" is used herein to refer to an aromatic substituent which can he a single aromatic ring or multiple aromatic rings which are fused together, linked covalently, or linked to a common group such as a methylene or ethylene moiety. The common linking group can also be a carbonyl as in benzophenone or oxygen as in diphenylether or nitrogen in diphenySamine. The aromatic ring(s) can include phenyl, naphthyl, biphenyl, diphenylether, dipheuylamine and benzophenone among others. In particular embodiments, the term "aryl" means a cyclic aromatic comprising about 5 to about 1 carbon atoms, including 5- and 6- membered hydrocarbon and heterocyclic aromatic rings,

[ΘΘ ] The aryl group can be optionally substituted with one or more aryl group substituents which can be the same or different, where "aryl group substituent" includes alkyi, aryl, aralkyl, hydroxy, alkoxyl, aryloxy, aralkoxyl, carboxy, acyl, halo, nitro, alkoxy carbony I , ary to ycarbonyi, aralkoxycarbony 1, acy loxyl, acy laini.no, aroy lamino, carbamoyl, alkylcarbamoyl, diaikylcarbamoyl, arylthio, alkyithio, alkyiene and ~NR:R.", where R' and R" can he each independently ^'hydrogen, alky I, aryl. aod anilkyl.

[01.00] Specific examples of aryl groups include but are not limited to

eyclope adienyf phenyl, furan, thiophene, pyrrole, pyrao, pyridine, imidazole, isothiazole, isoxaxole, pyra¾ole, pyrazine, pyriniidine, and the like,

10101 T e terra "microspheres" refers to particles having at least one dimension less than about .1 00 microns. In some, but not all, embodiments, microspheres are essentially spherical and have a diameter of less than about 1000, 750, 500, 400, 300, 200, 100, 75, 50, 25, 10, 5, or 1 microns, in some embodiments, microspheres can be irregular in shape, or have a rod-like, disc, or cubic shape.

GENERAL CONSIDERATIONS

(t)102| Generally speaking, the disclosed subject matter provides a composite material that includes a high tenacity fiber reinforced polymer fabric and a poiytsrea coating layer formed on the high tenacity fiber reinforced polymer fabric. The composite material can he formed on any suitable substrate (e.g., wood, reinforced concrete, steel, any other suitable substrate, and/or any combination thereof)- The composite material provides a material that integrates viscoelaslic behavioral properties via sustainable inierfacial interaction between the composite material and the underlying substrate.

10103] The composite material can be used in a variety of applications. For example, the composite material can be used to reinforce structural and/or non-structural substrates to protect them from damage (e.g., due to seismic activity, fire, impact, loading, and/or explosive forces). In another example, the composite material can be used to strengthen structural and/or non-structural substrates following damage by forming the composite material on at. ^'least one surface of the substrate (e.g., tightly wrapped around the entire substrate, formed over a crack in the substrate, etc.). In yet another example, the composite material can be used to provide a particular protective property to a substrate, such as UV protection, fire resistance, corrosion resistance, moisture resistance, and/or energy efficiency.

[0104] in a more particular embodiment, the disclosed subject matter can provide a protection system that reduces structural accelerations and displacements by combining a high strength/high stiffness material with sustainable energy dissipation and ductility, in some embodiments, this protection system can include a composite materia] that is tightly wrapped around or applied as a ply (e.g., adhered to) an exterior face or surface of a substrate, thereby providing viscoelaslic behavior properties that transition to a sustainable elastomeric state by sustaining the interfacial interaction between the composite material and the underlying substrate. The composite material can act as an energy-release valve by providing sustainable energy dissipation and large viscous-type damping during extreme loading events, such as during earthquakes, that minimize structural damage to the substrate, in some embodiments, the composite/substrate system can allow for a change in viscous damping ratio (e.g., the composite/substrate system has a different viscous damping ratio than the substrate alone),

(0.105) in another suitable embodiment, the composite material of the disclosed subject matter can be used to construct a stand-alone structure having high strength, high stiffness, and provides significant damping. In addition, the composite material can provide one or more protective properties, such as UV protection, fire resistance, corrosion resistance, moisture resistance, and or energy-efficiency. For example, the composite material can be used to manufacture automotive parts, spotting goods equipment, and bicycle frames, among others. In a more particular example, each of these parts or structures may have a desirable set of properties, such as a damping ratio greater than a given percentage. As explained hereinbelow, the composite material can be modified by varying curing times and/or varying the thickness of the polyurea coating layer to achieve particular properties.

[0106] As described herein, the composite material can include a layer of high tenacity fiber reinforced polymer (FRP) and a layer of elastoraerk polyurea formed on the layer of high tenacity fiber reinforced polymer. In a more particular embodiment, a high tenacity fiber reinforced polymer fabric can be attached to a substrate using a first saiurant composition, a second saiurant can be applied to the exposed surface of the high tenacity fiber reinforced polymer fabric and cured until forming a tacky surface, and an elastomeric polyurea can be formed on the tacky surface. Use of the polyurea coating layer can increase ductility and energy dissipation by about 100% in a composite as compared to that of the relatively stiff and brittle FRP alone.

(0107] in some embodiments, the properties of the composite material can be described as a function of time-related ( and volume- fraction (h_p) polymeric properties. For example, it has been determined that time-related factors in the preparation of the composite material (e.g., time fac tors related to the reaction of the precursors of the polyurea layer and the precursors of the polymer of the FRP) can affect the viscous properties and/or elongation percentage of the FRP and/or composite as a whole, thereby enabling the strength of the resulting load-bearing composite to be sustained at large deformations,

[0108] For example, as described herein, studies of the disclosed composites and of composite-wrapped wood-frame structures indicate that wrapping substrates with the presently disclosed composite material can synergisiically confine the substrate and provide a continuous .load path, for example, between the foundation of the wrapped wood-frame structure and its roof. Moreover, no de-bonding was exhibited between the individual composite wrap constituents or between the wrap and the wood frame substrate.

Accordingly, the interaction, or synergy, of the exterior composite tight-wrap and the frame can be used to replace the interaction of an exterior wood sheathing diaphragm and the frame, for example, via the fasteners typically used in traditional wood structures. The integration of large viscous-type damping can preclude reliance on the hysteretic damping of the shear wall fasteners, which can pull through or withdraw from the framing during ground .motions, or the minimal viscous damping that is ordinarily provided by structural and non-structural components in traditional wood structures.

[0109] in another example, as described ^'herein, the disclosed composites can be applied to reinforced concrete beams, shear walls, and other structures. More particularly, a structure or structural element can be retrofitted with the composite material. A damaged structural element having .multiple cracks such that the after-test load capacity dropped, to approximately 40% of its peak value can be retrofitted with the composite material. Upon forming the composite material over portions of the damaged, structural element, the

reinforced structural element recovered its original load capacity and received a significant increase in the ductility of the structural element. The ductility of the composite material formed on the structural element allows the structural element to experience large

deformations. That is, the energy after the formation of cracks can be readily dissipated, thus inhibiting the formation of new crack surfaces and inhibiting further damage from occurring.

[01.10] in some embodiments, the composite material wrapped around a substrate can reduce accelerations and elastic displacements in wrapped substrates up until their peak loading stress via an increase in strength, stiffness and viscous properties. During extreme loading, where an unwrapped substrate would have been loaded ineiastically and beyond its maximum strength, the composite wrap can. provide, in some embodiments, a "sustainable negative stiffness" to help minimize damages by inducing a viscous damping mechanism to stabilize crack substrate growth (by invoking stable crack energy release) and dissipate strain energy, allowing the wrapped substra te to sustain a high level of strength. Models of the viscoelastic behavior of the wrapped substrates can be developed based, for example, on existing nonlinear constitutive material models formulated on continuum mechanics theory. See, e.g., Atiard. T.I, et aL J. of Eng. Mechanics, ASCE, 134(10), 881 (2008), which is incorporated by reference herein in its entirety. COMPOSITES

[01.11 j in some embodiments, the disclosed subject matter provides a composite comprising a fabric that is coated on at least one surface with a coating layer comprising an elastomeric polyurea, where the fabric is a high tenacity fiber reinforced by a polymer matrix (sometimes referred to herein as a fiber reinforced polymer (FRP) fabric). The composite is sometimes referred to herein as CarbonFlex.

[0112] ^'Referring to FIG. 1, a cross-section of a substrate surface reinforced with a composite in accordance with some embodiments of the disclosed subject matter is provided. As shown in cross-section of FIG. 1 , a. substrate 1.00 can be provided. As generally described herein, substraie 1 0 can. be made of an suitable materia]., such as, for example, wood, masonry (e.g., brick, stone, stucco, tile), concrete (including concrete reinforced with steel or other meiaS), steel, or combinations thereof.

[Θ 113] It should be noted that the composite can be formed without a substrate. That is, the composite can be used to construct a stand-alone structure. Alternatively, the composite can be formed without a substrate and, at a later time, attached to a substraie.

[01.1.4] In some embodiments, substrate 100 may be damaged and include cracks, pits, chips, and/or grooves in the surface of substrate 1 0. To provide a uniform and/or a smooth surface, substrate 100 can be prepared by using a putty material. As shown in FIG. 1 , putty material 1.05 has been applied to provide a smooth surface for reinforcement with the composite. Alternatively, any suitable procedure may be performed to prepare substrate 100. For example, abrasive blasting can be performed to remove loose material from the surface of substrate 100. hi another example, epoxy resin and/or cementiiious mortars can be applied to repair portions of the surface of substrate i 00.

[01.15] ft should be noted that putty material 105 applied to substrate 1 0 may not be used for a newly constructed structure or substrate that is generally undamaged.

Jul 16} m some embodiments, s bstrate 100 (and its prepared surface) can be in contact with a primer 1 1.0 and a first saturant composition 120. Primer 1 10 can be also in contact with one side of a high tenacity fiber reinforced polymer fabric 130 (e.g., the high tenacity fiber fabric with the polymeric matrix formed by curing of, for example, the first saturant composition 120). Attachment of the fiber reinforced polymer fabric 104 can be performed such that during curing of the polymer matrix in fabric 130 an interaction or bonding (e.g., covalent bonding) takes place between the polymeric components of primer 1 10, saturant composition 120, and/or the fiber reinforced polymer fabric 130. For example, primer .1 1 and/or first saturant composition 120 can improve the bonding of the gh tenacity fiber reinforced polymer fabric 130 with substrate 100. In another example, primer 1 10 can improve the bonding of first saturant composition 120 with substrate 100. In yet another example, a predetermined amount of time ma elapse before forming additional layers to allow the high tenacity fiber reinforced polymer fabric 130 to bond or interact with substrate 100.

[6117] in some embodiments, the exposed side of the fiber reinforced polymer fabric

130 can be in contact with a poly urea coating layer 150, at interface i 35. More particularly, a second saturant composition 140 cart be applied to the exposed surface of the fiber reinforced polymer fabric 130. When a tack surface is formed by at least partially curing the second saturant composition 140 for a given, period of time (e.g., about two hours to five hours), a polyurea coating layer 150 can be formed on the high tenacity fiber reinforced polymer fabric 130. Polymeric components from both fiber reinforced polymer fabric 130 with second saturant composition 140 and polyurea coating layer 140 can interact (e.g., via covalent bonding) at interface 135 to prevent separation of fiber reinforced polymer fabric 1 0 and polyurea coating layer 140 following complete curing of the composite. It should also be noted that curing the second saturant composition can, in some embodiments, cure the first saturant composition applied between substrate 1 0 and fiber reinforced polymer fabric 130. J01 IS] it should be noted that the thickness of the polyurea coating layer 1 SO can be varied based on the desired properties of the composite-coated substrate. It should also be noted that the properties of the composite (e.g., viscous damping properties versus stiffness properties) can. generally be modified by modifying time-related ( and volume-fraction (h_p) polymeric properties. For example, the time related to the reaction, of the precursors of the polyurea coating layer 150 and the polymer of the fiber reinforced polymer fabric 1 0 can affect the viscous properties and/or elongation percentage of the composite as a whole.

[6119] in some embodiments, if desired, an additive layer 1 10 can be formed on one side of the polyurea coating layer 1 8. Additi ve layer 1 10 can contain, for example, ceramic microspheres or an additional protectant layer (e.g., a moisture resistance layer, a TJV protective layer, a corrosion resistance layer, a flame retardant layer, etc.). in some

embodiments, optional additive layer 110 is absent.

[6120] Accordingly, the interaction, or synergy, of various components within the primer layer 1 10, the first saturant. composition layer 120, the fiber reinforced polymer fabric layer 130, the second saturant composition layer 140, the polyurea. coating layer 150, and/or the additive layer 160 form the composite having desirable strength, stiffness, and damping properties. The strength, stiffness, and damping properties of the composite can be modified based on lime-related ( ) and volume-fraction (h_p) polymeric properties. For example, lime- related factors in the preparation of the composite material (e.g., the time to ewe the second saturant compo ition, which creates an interaction between components of the polyurea coating layer 150 and the precursors of the polymer of the fiber reinforced polymer fabric layer 130) can affect the viscous properties and/or elongation percentage of the composite, thereby enabling the strength of the resulting load-bearing composite to be sustained at large deformations,

[012J } As described above, the composite or composite material can be used in a variety of applications. For example, the composite can be used to wrap substrates including buildings, building components and other structures and parts or elements thereof in order to reinforce the substrates following damage or to prevent damage from occurring in the future. The composite can also be used to provide reinforcing inserts for building materials. For example, in addition to being used as a wrap for concrete structures, materials comprising the composite can be embedded within the concrete structure. In some embodiments, the composite materials can be used as a wrap for armored vehicles, such as military txanspori or weapons vehicies. Additional uses also include protective clothing (e.g., bullet proof vests and the like) or bio-medical applications, such as in the fabrication of prosthetics or parts for prosthetics. Even further, the composite can be used in high-vibration or high impact or shock load applications, uch as bicycles, helmets, etc. For example, the composite material can be .formed around a foam core to impart impact resistance properties to the foam core.

[0122} in some embodiments, the composite can be used as a building material itself.

For example, the composite can be used to construct bicycie frames, automotive pans, and/of protective clothing. In a more particular example, the composite can be used for the

lightweight design and manufacftirmg of vehicle components, which would improve safety, performance, and fuel efficiency.

|0123| it should be noted that, for the polyurea coating layer, any suitable elastomeric polyurea can be used. The polyurea can be selected based, on any suitable factors including, but not limited to, cost, abrasion resistance, flexibility, chemical resistance, toxicity volatility of chemicals given off by the polyurea over time, UV resistance, moisture resistance, and the like. In some embodiments, the polyurea has an elongation (i.e., an elongation at break) of at least about 100%. in some embodiments, the polyurea can have an elongation of about 600% or more. In some embodiments, the polyurea has a tensile strength of between about 1500 and about 2000 pounds per square inch (psi) (e.g., about 1500, about 1600, about 1700, about 1800, about .1 00, or about 2000 psi). The properties of many polyureas are known in the art and/or can be measured by techniques kno wn m the art, such as ASTM D412.

(0124} Pofyureas suitable for use In the disclosed subject matter can be prepared by mixing (e.g., reacting or polymerizing) isocyanates and amines. In some embodiments, the isocyanate is a di-isocyanate- terminated prepoiymer (i.e., a compound having the formula 0^:::C^::::N- -N^:::C^::::0, wherein R can comprise aliphatic or aromatic groups and can be polymeric or non-polymeric). For example, in some embodiments, the isocyanate can be a compound based on the structure of methylene diphenyi diisocyanate. Thus, in some embodiments, the isocyanate includes, but is not limited to, 4,4'-diphenylmethane

diisocyanate (MDJ), p-phenylene diisocyanate (P Di), m-phenylene diisocyanate (MPDI), toluene diisocyanate (TDI), or a mixture thereof Suitable isocyanai.es can also comprise backbones based on polyethers. Additional examples of suitable isocyanates are described in, for example, U.S. Patent No. 5.415,499, which is hereby incorporated by reference herein in its entirety.

(0125} Typically the amine-containing component comprises at least two reactive amine groups. The reactive amine groups can be primary or secondary amines. In some embodiments, the amine-coniaimng component comprises an amine-iermm ted prepol mer, such as an amine-terminated polymer resin and/or a monomeric aliphatic or aromatic

po^'lyamine (e.g., a diamine, triaraine, tetraamine, etc.). Exemplary amine-terminated polymer resins include blends comprising polyoxyalkylene di- and/or triamnies and aromatic polya ines, such as diethyltomenediamine and dimethyltliiotoluenediamine (DMTDA). In some embodiments, the po!yurea can include an amine-containing component such as, but not limited to, amine-termtnated polypropylene glycols (e.g., JEFFAMINE# D2000 and JEFFAMINE® T5 00, available from Huntsman Corporation, The Woodlands, Texas, United States of America), diethyltoluenediamine (i.e., ETHACU .E® 100, available from Albemarle Corporation, Baton Rouge, Louisiana, United States of America), or a diamine comprising seobut l groups (e.g., UNILINK 4200™, Dorf Kelal Chemicals LLC, Stafford, Texas, United States of America), The amine- terminated compounds suitable for use in the present subject matter generally have a mean functionality of about 2,0 to 3,0 and an average molecular weight of about 150 to 6000. Additional examples of suitable amine-contahiing components are described in, for example, U.S. Patent No. 5,415,499, which is incorporated by reference herein in its entirety.

f i)126 Thus, in some embodiments, the poiyurea layer is provided by mixing and reacting an isocyanate-tenninated compound or polymer with an amine-terminated polymer and/or an aliphatic or aromatic diamine compound and then essentially immediately applying the resultant reacting mixture to the surface (e.g., of the fabric) to be coated. The mixing of the two reactants can. be effected directly within a spray gun. used to apply the mixture (i.e., impingement mixing). Of course, mixtures of suitable isocyanate-terromated compounds aad mixtures of suitable aoune-terarioaied compounds can be used, x some embodiments, a slight excess of isocyanate equivalents can be used. For example, ihe components can be mixed such that there are slightly more reactive isocyanate groups than reactive amine groups. In some embodiments, there is between about a 1% and about a 10% excess of isocyanate equivalents. In some embodiments, there is about a 5% excess of isocyanate equivalents.

10J.27J It should be noted that providing an isocyanale-rich polyurea layer (e.g., 5%- rich isocyanate) can, in some embodiments, enhance the molecular reactivity between a component of the polyurea layer and a component of the fiber reinforced polymer layer, it should also be noted that providing an. isoeyanate-rieh polyurea layer can, in some embodiments, create non-contaminated state, thereby creating a no-slip condition between the polyurea layer and the fiber reinforced polymer layer.

[0128] in some embodiments, the polyurea is aromatic. Accordingly, in some embodiments, cither or both of the isocyanate and amine components comprise an aromatic moiety.

|0129| In some embodiments, the polyurea is a fire-resistant polyurea. Use of a fire- resistant polyurea can provide fire-resistive properties to the composite material and to substrates reinforced with the composite material For example, use of a fire-resistant polyurea can reduce the intensity of heat to the polyurea and to the composite materia! and/or reduce toxic outgassing. in some embodiments, the fire-resistant polyurea is also

iiitumeseent. Accordingly, in some embodiments, the composite combines in a single reinforcing material, high strength, high energy dissipation, and fire-resistivity.

|O130] Fire resistant properties of poiyureas or other materials can be tested by methods known in the art, such as for example, ASTM E84- 5 (Standard Test Method for Surface Burning Characteristics of Materials). In some embodiments, the poly urea has a flame spread classification of about 50 or less and/or a smoke developed classification of about 200 or less as measured using ASTM ES4-05. In some embodiments, the polyurea has a flame spread classification of about 20 and/or a smoke developed classification of about 1 15. in some embodiments, the polyurea is the polyurea sold as System 550D-F by Quantum Coatings (Edmonton, Alberta, Canada).

f0131] In some embodiments, various additives can be included in the polyurea layer. For example, the additives can be added to either the isocyanafe reactaats a»d or the amine reaciants when the polyurea is prepared.. Additives include, .for example, organic and inorganic colorants or dyes, UV protective agents, adhesion promoters, fillers, and other processing aids or enhancers.

|0132| UV protective agents can include light stabilizers, UV absorbers, and antioxidants. Examples of suitable light stabilizers include hindered amines, such as bis- ( 1 _s2,2,6,6-pentajnTethyl-4-piperidmyi>sebacate and bis-(2_!2,6_!6-tetram.enthyl-4- piperidyi)sebacaie,

101.33] UV absorbers can protect against photodegradation by competing with the polyurea for absorption of ultraviolet, light, in some embodiments, the UV absorber has broad absorption over the UV range from about 290 nm to about 400 nm. Suitable UV absorbers can include, but are not limited to, triazines, ben oxaatinones, benzotria/oles, benzophenones, bertzoates, formamldmes, cinuamaies/propenoates, aromatic propanediones, benzimidazoles, cycloaiiphatic ketones, f rmauiiides (including oxamides), cyanoacrylates, benzopyranones, and mixtures thereof.

[01.34] Antioxidants, on the other band, can interrupt the degradation process in different ways according to their structure. The major classifications of antioxidants are primary antioxidants and secondar antioxidants. Primary antioxidants, such as sierically hindered phenols, react rapidly with peroxy radicals to break the degradation cycle.

Secondary antioxidants, such as arylaniines, are more reactive toward oxygen-centered radicals than are hindered phenols. The secondary antioxidants react with hydroperoxide to yield non-radical non-reactive products, and are frequently called hydroperoxide decomposers. Multifunctional antioxidants, such as hindered amine stabilizers ("HAS"), combine the functions of primary and secondary antioxidants.

[0135] Exam les of adhesion promoters include, but are not limited to, titanates and zireonates, as well as various organofunctional silanes (especially the aniiuo-functional si!anes). Examples of useful fillers include, but are not limited to, zinc oxide ("ZnO"), barium sulfate, calcium oxide, calcium carbonate, and silica, as well as any salts and oxides thereof. Additional fillers and/or additives also include, but are not limited to, foaming agents, glass, ceramic, and/or plastic microspheres, and. various metals.

[0136] The various additives are generally present (individually or as a whole) at less than about 1 % by weight of the total polyurea composition, in some embodiments, the polyurea layer contains about 5% by weight or less of one or more additives, in some embodiments, the polyurea layer contains about 1 % by weight or less of one or more additives,.

[^'0137} In some embodiments, the properties of the composit e can b e control Led by controlling the thickness of the polyurea coating layer. Controlling the thickness of the coating layer can alter the volume fraction of elastomeric polyurea in the composite as a whole. Typically, the polyurea coating layer is thicker than the fabric (e.g., at least about 5, 10, 20, 30, 40, 50, 100, 250, or 500 times thicker than the fabric when the fabric thickness is measured before the application of the saturant). In some embodiments, the coating layer has a thickness of between about: 1/16*^* of an inch (i.e., about 0.0625 inches) and about i/8* of an inch (i.e., 0.125 inches). Accordingly, in some embodiments, the coating layer has a thickness of about 0.0625, about.0.0675, about 0.0725, about 0.0775, about 0.0825, about 0.0875, about 0.0925, about 0.0975, or about 0.125 inches. In contrast, the fabric typically has a thickness of less than about 0,01 inches, in some embodiments,, the fabric has a thickness (prior to the addition and curing of saturant composi tion) of between about 0.0013 inches and about 0,0065 inches (e.g., about 0,0013, about 0.0017, about 0.0021, about 0,0025, about 0.0029, about 0.0033, about 0.0037, about 0.0041 , about 0.0045, about 0.0049, about 0.0053, about 0.0057, about 0.0061, or about 0.0065 inches).

[0138] The fabrics of the presentl disclosed composites comprise a network of hi gh tenacity fibers. The fabric can be woven, knitted, or non-woven. In some embodiments, the high tenacity fibers are uni-directional such that the fibers are generally aligned in a parallel fashion, in some embodiments, the high tenacity fibers are bi-directional such that the fibers are aligned in both parallel and perpendicular directions.

[0139} it should be noted that any suitable high tenacity fiber or combination of fibers can be used. For example, m some embodiments, the high tenacity fiber is carbon fiber, glass fiber (e.g., e-gtass or s-glass), aramid (e.g., meta- or para-aramid), liquid crystal eopolyester fiber, basalt fiber, or any suitable combination thereof. In some embodiments, the high tenacity fiber includes carbon fiber and the fabric comprises a carbon fiber reinforced polymer (CFR.P) fabric. CFRPs are relatively inexpensive compared to other FRPs and have excellent strength and durability. More particularly, suitable high tenacity fiber fabrics include, but are not limited to, MBraCffD cloths, commercially available from BASF

Construction Chemicals, LLC (Shakopee, Minnesota, United States of America).

[01.40] High tenacity fiber fabrics are generally reinforced by thermosetting polymer matrix based on a polymeric resin, such as, but not limited, to, epoxy resins, vinyl ester resins, and polyester resins. In some embodiments, the disclosed composites comprise a carbon fiber reinforced polymer (CFR.P) fabric reinforced with a polymer .matrix based on an epoxy resin.

[0:1.41] The fabric can be obtained with at least same polymeric resin pre-embedded

(or pre-irnpregnsted) in the fabric and then treated further to cause coring of the resin when desired. Alternatively, the fabric can be obtained free of polymeric resin and the polymeric resin can be applied as part of a saturant composition.. Accordingly, in some embodiments, the presently disclosed composite comprises a CF P fabric that has been treated with a mixture (e.g., a saturant composition.) comprising a polymeric resin, (e.g., an epoxy, vinyl ester, or polyester resin). The mixture can also inchide additional chemicais or additives, as desired, such as to promote the curing of the resin (e.g., polymerization initiators or curing accelerators) and or a diluent. Additional additives can further include one or more of a filler, a colorant, a UV protectant, a viscosity modifier, a defoaming agent, and a surface drying agent or the tike.

|Θ142| Typically, epoxy resins can include an epoxy~ter.min.ated prepolymer (e.g., an epoxy-terminated monomer, oligomer, or short chain polymer) and a hardener comprising a polyamine (e.g., triemylenetelramme). Epoxy-terminated prepolymers can be prepared, for example, from the reactio of epichlorohydrin and bisphenol A. Thus, suitable epoxy resins include, but are not limited ^'to, glycidyl ethers of polyvalent phenols such as bisphenol A epoxy resins, bisphenol F epoxy resins, bisphenol S epoxy resins, phenolic novolak epoxy resins, cresol novolak epoxy resins, brornmated bisphenol A epoxy resins, and bromuiated phenolic novolak epoxy resins; glycidyl esters such as diglycldyl phthalate. diglycidyl hexahydrophthalate, diglycidyl tetrahydrophihaiate, and benzoic acid or dimer acid glycidyl esters; heterocyclic epoxy resins such as ^S-diglycidyi-S.S-dtinetliylhydantoin and triglydicyl isocyanurate; and. alicyclic epoxy resins such as naphthalene-based epoxy resins and 2,2\4,4'~ tetraglycidoxybiphenyt These epoxy resins can be used either singly or as a mixture of two or more particular resins.

|0143] in some embodiments, the epoxy resin is provided as part of a saturant composition or compositions comprising, for example, Bisphenol A epoxy resin, alky! glycidyl ether, amorphous silica, isophoronediamine, benzyl alcohol, and salicylic acid. In some embodiments, the epoxy resin is provided as part of a commercially avaiiable MBrace Saturant, such as MBraee¾ Saturant LTC (available from BASF Construction Chemicals, LLC; Shakopee, Minnesota, United States of America).

fi⁾144j Vinyl ester resins typically include an epoxy resin and a monocarboxylic acid.

Examples of monocarboxylic acids include, but are not limited to, acrylic acid, methacryiic acid, crotonic acid, cinnamic acid, sorbitamc acid, acrylic dimers, monomethyl maiate. monopropyl roaiate, monobutyi malate, .ra «o(2-ethyliiexyl.)malale and the like.

|014S} Polyester resins can be prepared by the reaction of a dt- or polycarboxylic acid and a polyvalent alcohol (i.e., a polyoi, a compound comprising at least two hydroxy! groups). Polycarboxylic acids include, but are not limited to, mma!ic acid, maleic anhydride, maleic acid, iiaconic acid, isophtha!ic acid, terephtha!ic acid, tefrahydrophthalic acid, adipk acid and sebacic acid. Polyvalent alcohols include, but are not limited to, ethylene glycol, propylene glycol diethyiene glycol, dipropylene glycol, 1 ,2-biuanediol, 1 ,3- butaaediol, 1 ,5-petitanedioi, L6-hexanediol, 2 -methyl- 1 ,3-propanediol, 2,2-dimethyi-I,3- proparsediol, cyclohexane- i ,4-dimethanol. ethylene oxide adducts ofbisphenol A, and propylene oxide adducts of bisphenol A.

10 i 61 in some embodiments, the polymer matrix reinforced fabric ⁽e.g., the cured

FRP in the absence of the poiyirrea coating layer) has an ultiraate tensile strength of at least abou t 145 ksi (1.0 GPa) and a tensile modulus of at least about 20,000 ksi ( 138 GPa) measured in the direction along the length of the fabric. In some embodiments, the fabric has an ultimate tensile strength, of at least about 500 ksi (3.45 GPa) and a tensile modulus of at leasi about 30,000 ksi (207 GPa). In some embodiments, the fabric ha an ultimate tensile strength of at least about 550 ksi (3.79 GPa) and a tensile modulus of at least about 33,000 ksi (228 GPa). In some embodiments, the fabric has an ultimate tensile strength of between about 1.90 GPa and about 5,74 GPa (e.g., about 1,90, 2.40, 2.90, 3.40, 3,90, .40, .90, 5.40, or about 5.74 GPa) with elongation percentages varying between about 0,5% and 2.0% (e.g., about 0.5, ,0, .1 ,5, or about.2.0 %) beyond yield. In some embodiments, the fabric has an ultimate tensile strength per unit width of about 3.575 kips per inch (per ply). In some embodiments, the fabric has an ultimate modulus of about 21 .5 kips per inch (per ply per unit width). Tensile properties can be measured by any suitable approach know in the art, such as, for example, AST D3039,

f0147| By combining the FRP fabric with the elastonieric poiyurea layer, the elastic and inelastic properties and viscous properties of the composiie material as a whole can be significantly enhanced, in some embodiments, the composite has an elongation of about 100% or more (e.g., about 100%, about: 150%, about 200%, about 250%, about 300%, or about 400% or more). In some embodiments, th composite has an elongation of about 600%.

f 0148 in addition to providing a combination of strength and energy dissipation, the presentl y disclosed composites can be free of carcinogenic toxici ty . By "free o f carcinogenic toxicity," it is meant, that the composites are essentially free of volatile carcinogenic chemicals and, if used in long-term proximity io humans, such as when the composite is used as a wrap for a building or as protective clothing, the humans exposed to the composite do not experience a statistical increase in cancer incidence compared to humans not exposed to the composite.

|0149| in some embodiments, in addition to the FRP fabric and the at least one po!yurea coating layer, the composite can include additional components. For example, the composite can include a FRF fabric that is coated on both sides with a polyure coating layer. Additionally or alternatively, the composite can be coated with n adhesive, e.g., to enhance the attachment of the composite to various other materials.

[01.50] In some embodiments, the composite can further include microspheres, such as ceramic microspheres, that are embedded into the polyurea coating layer or added in a separate layer on a surface of the polyurea coating layer (e.g., on the surface of the polyurea coating layer not in contact with the FRP fabric). For example, ceramic microspheres can add additional insulating properties to the composite material. Accordingly, in some embodiments, the composi te can be used to increase the energy efficiency rating of a structure, for example, a wood-constructed home, in some embodiments, the use of a composite comprising ceramic microspheres can increase the energy efficiency of a structure from about 2 to about 4 times (e.g., about 2, 3, or 4 times) that of the corresponding structure where the composite is not used.

METHODS FOR REINFORCING SUBSTRATES

[0151 j FIG. 2 is an illustrative method for reinforcing a substrate, such as a substrate from a newly constructed structure) with a composite material that includes a high tenacity fiber reinforced polymer fabric and a polyurea layer is provided. It should be noted that, in the illustrative method of FIG, 2 and other flow charts described herein, some steps can be added, some steps can be omitted, the order of the steps can be re-arranged, and/or some steps can be performed simultaneously.

[0152] As shown, method 200 begins by providing a substrate at 21 , It should be noted that the composite material in accordance with the disclosed subject matter can be used with any suitable substrate. Suitable substrates can include, but are not limited to, wood, masonry (e.g., brick, stone, stucco, tile), concrete (including concrete reinforced with steel or other metal), steel, or combinations thereof Alternatively, as shown in embodiments described herein, a suitable substrate can be a foam (e.g., expanded polystyrene, expanded po!yurethane, etc). It should also be noted that, the substrate can be any suitable shape (e.g., a wall, a beam, a slab, a bar, a column, a rod, a support strut) or size. For example, in some embodiments, the substrate is a building component intended for rise in new construction of a house or other building (e.g., an office building, a hospital, a school, a store, a power plant, an airport, etc.), a bridge, a roadway, a dam, a tunnel, a retaining wall, a dock, or a wharf. |0153| At 220, a first saturant composition can be applied to the surface of the substrate prior to attaching the high tenacity fiber reinforced polymer fabric. Upon applying the first saturant composition at 220, a high tenacity fiber reinforced polymer fabric can be attached to at least a portion of the substrate at 230. As described previously, any suitable high tenacity fiber fabric can be used . For example, in some embodiments, the fabric can include at least some carbon fibers. In a mor particular embodiment, the hi gh, tenacity fiber reinforced polymer fabric is a carbon fiber reinforced polymer fabric.

|t)154| Attaching the high tenacity fiber reinforced polymer fabric to the substrate can be done by any suitable method. For example, the high tenacity fiber reinforced polymer fabric can be attached to the substrate surface by stapling or nailing. In another suitable embodiment, the attaching can be performed by coating at least a portion of a surface of the substrate with a primer composition and/or the first saturant composition to provide a coated substrate and contacting the coated substrate with the high tenacity fiber fabric. The primer composition and/or the first saturant composition can comprise an adhesive and/or a polymer resin that can Interact (e.g., via covalent bonding or non-covalent bonding) with the high tenacity fiber reinforced polymer iabric and, in some cases, the second saturant composition that is applied to the fabric after the fabric is contacted to the coated surface.

[0155] it should be noted that any suitable polymer resin can be used in the primer or the saturant composition. Suitable polymer resins for use in the primer can include, but are not limited to, epoxy resins, vinyl ester resins, polyester resins, and methylmethacrylate resins. If a primer comprising a polymer resin is used, it can be the same resin or type of resin as the polymer resin in the saturant composition (the polymer resin in 230) or it can be a different type of polymer resin. Accordingly, in some embodiments, die polymer resin in the saturant and the polymer resin in the primer can both be epox resins.

[0156] At 240, a second saturant composition can be applied to an exposed surface of the fabric. As described above, the second saturant composition can comprise an adhesive and/or a polymer resin that can interact (e.g., via covalent bonding or non-covalent bonding) with the high tenacity fiber reinforced polymer fabric. After the saturant is applied to an exposed surface of the fabric (e.g., by painting or spraying) at 240, it can be cured at 250 for a suitable period of lime to provide a tacky surface (a tacky outer surface to the fabric). It should be noted, thai (he time to cure the second saturant composition can. be varied based on the chemical composi tion, of the saturant, temperature, and/or humidity. In. some

embodiments, the second saturant composition can be cured for between about. 2 hours and. about 3 hours (e.g., about 120, 130, 140, 150, 160, 170, or about 180 minutes), in some embodiments, the saturant composition can be partially cured, in some embodiments, the second saturant composition can be cored as long as about free hours.

(0.157) When the saturant is partially cured at 250, an elastomeric polyurea-forming component solution can be applied to the tacky surface at 260. Applying the poiyurea- forming component solution while the surface is tacky can allow for interaction (e.g., eovalent or nott-covalent bonding) between the chemicals or components in the polyurea- forming component solution and the resin or other components in the saturant composition. This interaction during preparation can allow for sustained interfacial interaction, between the polyurea coating layer and the fiber reinforced polymer fabric layer when, for example, the reinforced substrate is subjected to various stresses or events, in some embodiments, the elastomeric po!yurea-fonning solution can be sprayed or brushed onto the tacky surface.

[0158] in some embodiments, the polyurea- forming component solution comprises materials that form an aromatic polyurea layer. In some embodiments, the polyurea layer is fire-resistant. For example, the polyurea layer can have a flame spread classification as determined using ASTM E84-05 of about 50 or less (e.g., about 50, about 40, about 30, or about 20 or less). In some embodiments, the polyurea layer can .have a smoke developed classification of about. 200 or less (e.g., about. 200, about 180, about 1.60, about 140, or about 120 or less) as measured by AST E84-05. In some embodiments, the polyurea layer has a. flame spread classification of about 20 and a smoke developed, classification of about 1. 15 In some embodiments, the fire-resistant polyurea layer is intnmescent, A suitable fire-resistant, iotumescent polyurea. includes, for example, the polyurea sold as System 550D-FR by Quantum Coatings (Edmonton, Alberta, Canada).

10159] in some embodiments, the polyurea- forming component solution comprises a first component that is an isocvanate (e.g., an isocvanate prepolymer) and a second component comprising an amine (e.g., an amine-terminaied prepolymer). in some embodiments, the isocyanate is a di-isocyanate-terminated prepolymer (i.e., a compound having the formula 0^™C N^f-R-N==C==0, wherein R can comprise aliphatic or aromatic groups and can be polymeric or non-polymeric). For example, in some embodiments, the isocyanate can be a compound based on the structure of methylene diphenyl diisocyanaie. Thus, in some embodiments, the isocyanate includes, but is not limited to, 4.4'-chp.henyimethane diisoeyanate (MDI), p-phenylene diisoeyanate (PPDI), m-phenylene diisoeyanate (MPDI), toluene diisocyanate (TDt), or a. mixture thereof. Suitable isocyanates can also comprise backbones based on polyeihers. Addi tional examples of suitable isocyanates are described in, for example, U.S. Patent No. 5,415,499, which is hereby incorporated by reference herein in its entirety.

10160] The amine-terminated prepolymercan comprise at least two reactive amine groups. The reactive amine groups can be primary or secondary amines, to some

embodiments, the amine-terminated prepoly.ra.er comprises an amine-terminated polymer resin and/or .monomelic aliphatic or aromatic polyamine (e.g., a diamine, triamine, tetraaniine, etc.). Exemplary amine-terminated polymer resins can include blends comprising polyoxyalkyiene di- and or trianiines and aromatic polyamines, such as

diethylioiaeiiediamme and dimethyi iotoluenediamine (DMTDA). In some embodiments, the polyurea can include an a ine-containing component such as, but not limited to, amine- tenninated polypropylene glycols (e.g., JEFFAMINE- D2000 and JEFFAMINE® T5000, available from Huntsman Corporation, The Woodlands, Texas, Unit ed States of America), diethyltoluenediamme (i.e., ETHACURH® 100, available from Albemarle Corporation, Baton Rouge, Louisiana, United States o f America) , or a diami ne comprising seobutyl groups (e.g., U ILINK 4200™, DorfKetal Chemicals LLC, Stafford, Texas, United States of America), The amine-terminated compounds suitable for use in the present subject matter generally have a mean functionality of about 2.0 to 3.0 and a average molecular weight of about 150 to 6000. Additional examples of sui table amine-terminated prepolymers are described in, for example, U.S. Patent No. 5,415,499.

|Θ:161] The components of the pol la-ea- forming component solution can be typically mixed immediately prior to application io the tack surface. For example, the components can be mixed in a spray gun as they are being sprayed. In some embodiments, the components of the polyorea-fomiing component solution can be mixed in a ratio where there is a slight: excess of isocyanate equivalents (.i.e., reactive isocyaaate groups). In some embodiments, the components can be mixed such that there is between an about 1 % and an about 10% excess of isocyanate equivalents (e.g., an about 1%, 2%, 3%, 4%, 5%, 6%, 7%, 8%, 9%, or 10% excess of isocyanate equivalents), in some embodiments, there is a 5% excess of isocyanate equivalents. In some embodiments, the use of a slight excess of isocyanate can enhance interaction of the polyurea layer with the fiber reinforced polymer fabric, due to interaction of the isocyanate component from the polyurea-forrning solution with unreacted. polymeric groups in the saturant of the fiber reinforced polymer fabric. |θ:162] In some embodiments, (he polyurea-forming component solution can comprise one or more additi es to enhance the functionality or appearance of the reinforced substrate, in some embodiments, the polynrea-forming component solution can comprise a UV

protective additive, such as, but not limited to an organic pigment. In some embodiments, the polyurea-fbnning component solution can comprise between about 1% and about 10% by volume of the UV protective additive (e.g., about ? %, about 2%, about 3%. about. 4%, about 5%, about 6%, about 7%, about 8%, about 9% or about 10%). In some embodiments, the polyurea-forming component solution can comprise about 5% by volume of the UV protective additive.

[01.63] Following application of the polyurea-forming component solution, the polyurea component solution can be allowed to cure to form a coating layer at 270. li should be noted that some pol ureas can cure relatively rapidly. In some embodiments, the polyurea component solution can be allowed to cur for about I to 5 minutes (e.g., about 60, 90, 120, 150, 1 80, 210, 240, 270, or 300 seconds) and while the polyurea is still tacky, an additive is applied to the coating layer (e.g., to lite exposed surface of the coating layer), in some embodiments, the additive comprises ceramic microspheres.

[0164] As described herein, properties of the composite (e.g., viscous damping properties, strength properties, and/or stiffness properties) can. be modified by controlling the thickness of the polyurea coating layer. Controlling the thickness of the polyurea coating layer can alter the volume fraction of elastomeric polyurea in the composite, which can alter the properties of the resulting composite. In another example, the time related to the reaction between polyurea coating layer and the polymer of the fiber reinforced polymer fabric can affect the viscous properties of the resulting composite. Accordingly, when presented with particular material specifications (e.g., an installation requires a highly damped material), the composite can be made to accommodate such specifications.

|0165| hi some embodiments, the approach for reinforcing substrates can be applied to a previously constructed structure and, more particularly, an already damaged structure. Referring to FIG. 3, an illustrative method for reinforcing a substrate having damaged portions with a composite material that includes a high tenacity fiber reinforced polymer fabric and a polyurea layer is provided.

[0166] As shown, method 300 begins by providing a substrate having damaged portions at 310, in some embodiments, the substrate can be already present in a previously constructed building or other structure. In some embodiments, the previously constructed building o other structure can be a building or other structure that has been damaged due to a catastrophic event, such as an earthquake, a fire, a tornado, a hurricane, a typhoon, flooding, or an explosion. Alternatively, in some embodiments, the building or other structure is present in a region where there is an increased likelihood of such an event. For example, the building or structure can be located near a fault line, near the coastline, in a war zone, and/or be a building or structure having an increased risk ofa ierrorist attack, such as a building of economic or government importance or a building related to high population density events (e.g., sporting arenas, theaters, etc.).

(0167] In some embodiments, the previously constructed building can be damaged or be suspected of having damage due to normal wear and tear and/or related to age. For example, concrete is relatively alkaline, preventing the corrosion of any reinforcing metal bars present within concrete structures. Over time, however, concrete can become neutralized due to the action of carbon dioxide in the air. Once the concrete becomes neutralized, the metal bars can become susceptible to corrosion and an increase in volume, causing cracks in the structure. In some embodiments, the concrete is already cracked, and the metal bars are susceptible to corrosion. I some embodiments, older structures can become candidates for damage because the use of the structure changes over time. For example, bridges can become candidates of damage due to increases in traffic above levels accounted for during the design of the bridge, in such an embodiment, the building or other structure can be 10 or more years old (e.g., 10, 20, 30, 40, 50, 60, 70, 80, 90, or .100 or more years old).

|Θ 168] Alternatively, in some embodiments, the building or other structure can be newly constructed (e.g., within the last 1 , 5, 4, 3, or 2 years) such that the reinforcement, is performed to prevent damage. In some embodiments, the newly constructed building or other structure is a structure built within the last 1.2 months.

10 i 691 In some embodiments, the building or other structure is under construction or the substrate is intended for use in future construction.

(6170] With a substrate having damaged portions (or suspected damage due to, for example, wear and tear), the substrate can be prepared at 320. This can include, for example, selecting the substrate and preparing it by one or more of cleaning the surface of the substrate, smoothing the surface of the substrate, and filling in cracks, pits, chips, and or grooves in the surface of the substrate prior to attaching the fabric. Cleaning can be done by any suitable method, such as power washing or any other method to remo ve surface dirt and/or other non-substrate matter. In some embodiments, providing the substrate can comprise filling in and/or smoothing out the surface of the substrate with a putty material . Smoothing can be performed by sanding or any other suitable method. Cracks, pits, chips, grooves or other indentations or disfigurements in the surface of the substrate can he .filled in with any suitable materia!, such as, but not limited to wood filler, cement, concrete, or mortar. Generally, the fill material should be such that it does not interfere with the attachment of the fabric. Thus, in some embodiments, the fill material is a material that can interact (e.g., via covalent or non-covalent bonds) with a polymer resin applied to the surface of the substrate as part of a primer for attaching the high tenaci ty fiber fabric, or with a polymeric component present in or added to (e.g., in a satnrant) the high tenacity fiber fabric. 101.71] Steps 330 through 380 of FIG. 3 are similar t steps 220 through 270 of

FIG. 2. In particular, the composite material can be prepared by applying a first satnrant composition to a surface of the substrate (at 330); attaching a high tenacity liber reinforced fabric to at ieast a portion of the substrate with the use of the first satnrant composition (at 340); coating the high tenacity fiber fabric with a second satnrant composition comprising a polymer resin (at 350); curing the second saturant composition for a period of time (e.g., about two hours to five hours) to provide a tack surface (at 350); applying an elastomeric ^•polyorea-forming component solution to the tacky surface (at 360); and curing the polyurea- forming component solution to provide a composite material (370),

|*11 ^"2| In some embodiments, the substrate can be reinforced b attaching a previously prepared composite to the substrate, wherein the previously prepared composite includes a high tenacity fiber reinforced polymer fabric and a po!yurea coating layer. Thus, in some embodiments, the method of reinforcing the subs trate comprises preparing a composite material and attaching the composite material to the substrate. The previousl prepared composite material can be attached to the substrate via any suitable method, such as, but no limited to, stapling or nailing the composite material to the substrate and/or adhering the composite material to the siibstraie via an adhesive and/or polymeric resin coated on the substrate and/or on the composite materia!.

[6173] It. should be noted that reinforcing a substrate (e.g., a wood home, a reinforced concrete bridge, a steel structure, an automobile, an aircraft structure, etc.) inhibits or reduces damage to the siibstraie due to seismic activity (e.g., earthquakes), fire, and/or explosive forces (e.g., due to ballistics). In some embodiments, reinforcing the substrate can also provide resistance to water damage ⁽e.g., due to mechanical stresses from flash flooding or by reducing mold or other damage due to water saturation into the substrate), environmental pollutants and/or sun damage. In some embodiments, the protective properties can relate, at least in part, to a specific additive (e.g., a UV protectant, a flam retardant, moisture resistance, etc) added to the fiber reinforced polymer fabric or the poiyurea layer. In some embodiments, the protecti e property is related to the chemical composition of the fiber reinforced polymer fabric and/or the poiyurea layer. For example, polyureas can be moisture and/or mold resistant. In some embodiments, such as when a microsphere additive is used, the reinforcing can provide an insulati ve effect to the substrate, thereby making the reinforced substrate a more energy efficient building materia! than the non-reinforced substrate. In some embodiments, the reinforcing can increase the energ efficiency to between about 2 and 4 times (e.g., about 2, 3, or 4 times) that of the non-reinforced substrate.

EXAMPLES

[0174] The following examples farther illustrate s me embodiments of the present invention, but should not be construed as in any way limiting the scope.

BXAMFLE i : Tensile Compost te Coupon Res pits

}01?5| Coupons of composite were prepared using MBrace® F P cloth (about 0,068 inch thick x about 1 inch wide: available from BASF Construction Chemicals, LLC, Sfaafcopee, Minnesota, United States of America) saturated with a saturant prepared, by mixing a. composition comprising Bisphenol A epoxy resin, alky! glycidyi ether, and amorphous silica with a composition comprising isophoranediaraine, benzyl alcohol, and salicylic acid; and coated with a non-fire resistant polyurea-fonumg composition. Coupons were prepared wit two different poiyurea layer thicknesses (e.g., either about one eighth of an inch thick or about one sixteenth of an inch thick), providing final composite dimensions of about 0.5 in. thick x about 5 in. wide or about 0.32 in. thick x about 1 in, wide.

|0176| FIG. 4 is an illustrative graph of tensile force versus axial displacement that compares the elastic properties of carbon fiber reinforced polymer fabrics (as indicated by CFRP - Test 1 curve 420 and C FP - Test 2 curve 430) with the elastic properties of a polyurea-coated carbon fiber reinforced polymer fabric having a poiyurea coating layer with a thickness of either one sixteenth of an inch fas indicated by CarbonFlex, I Poly - Text 1 curve 410 and CarbonFlex, I x Poly - Test 2 curve 440) or one eighth of an inch (as indicated by CarbonFlex, 2x Poly - Test 1 curve 450), As shown in curves 410 and 440 of FIG. 4, the displacement of the polyurea-coated tensile coupon having i/T6^i:! of one inch thick poiyurea. coating layer on each side was about 3.75 times larger than that of the non-coated CFRP coupon (as compared to curves 420 and 430). Moreover, the displacement of the poiyurea- coated tensile coupon having a 1 8^U! of one inch thick poly rea coating layer per side (curve 450) was about 6.25 limes larger than that of the non-coated CFRP coupon (carves 420 and 430). it should also be noted that the continuous nat ure of the curves in FIG. 4 suggests that no interfacial s ip had occurred between the polyurea and the CFRP.

EXAMPLE 2: Torsion Results of Composite Wrapped Wood

[0177] FIG. 5 is an illustrative graph showing the results of a torsion study that was conducted on a white pine wood rod that 12 inches long and 1/2 of an inch in diameter. In this embodiment, the rod was wrapped with a polyurea coated ( 1/16 inch) CFRP composite according to above-described method of the disclosed subject matter. As shown in FIG. 5, the composite wrap was able to provide the necessary energy dissipation and strength components, as implied by the highly nonlinear response of the specimen, to enable the polyurea-coated composite wrapped wooden structure to attain a maximum torque reading of 80,0 pound inches (Ibs-in). This maximum torque reading is nearly font' times the torsional strength of unwrapped white pine at about 22.9 pound inches. It should be noted that the continuity of the curve shown in FIG, 5 and visual inspection o f several cross-sectioned, slices of the wrapped rod indicate that no bond sli occurred between the composite and the wood structure.

EXAMPLE 3; Bending Results of Composite Wrapped Wood

[0178] Three 2 x 4 wood beams of white pine, each with a 28 inch span, were subjected to wood beam bending studies. Each of the wood beams was prepared differently - as shown in FIG. 6A, curve 61.0 corresponds to the wood beam by itself (labeled by Wood only), curve 620 corresponds to the wood beam wrapped with a carbon fiber reinforced polymer fabric (labeled by Wood + CFRP), and curve 630 corresponds to the wood beam wrapped in a polyurea-coated carbon liber reinforced polymer composite of the disclosed subject matter. Each of these wood beams was subjected to concentrated mid-span forces as indicated on the force axis of FIG. 6A. For example, FIG. 6B shows an illustrative testing setup that subjected these wood beams to concentrated mid-span forces. The results, as shown in FIG. 6 A, indicate significant increases in displacemeiu, shear strength, and energy dissipation in the polyurea-coated carbon fiber reinforced polymer composite wrapped beam. The polyurea-coated carbon fiber reinforced polymer composite wrap was able to hold the damaged wood beam together well after the sudden strength drop, which, without being bound to any one theory, enabled the load to re-distribute to the wrap while energy was steadily dissipated.. Tests have shown that the displacement ductility and energy dissipation values can exceed those of a beam wrapped only with a carbon fiber reinforced polymer fabric by more than 100%. FIG. 6C illustrates an example of shows a photograph of a polyurea-coated carbon fiber reinforced polymer composite wrapped wood beam following testing with the testing setup shown in FIG. 613,

(0.179) Similarly, FIG. 7 shows a graph showing the results of a wood beam bending study of a wood beam wrapped with a polyurea-coated carbon fiber reinforced polymer composite, where the polyure layer is one eighth of an. inch thick. Also similar to FIG. 6 A, the circled portion of the graph indicates a strength drop. It should be noted thai, for the wood beam wrapped with a composite comprising an eighth of an inch thick layer of polyurea, the strength drop was immediately followed by a recovery stress (hardening). This behavior is at least due in part to the viscoelastic nature of the polyurea-coated carbon fiber reinforced pol mer composite and its interfacial chemical interaction. It should also be noted that the thicker coat of polyurea (e.g., one sixteenth of a inch versus one eighth of an inch) provides greater support and stiffness to the carbon, fiber reinforced polymer fabric (as well as to the entire system), thereby providing adjustable desirable properties upon load

redistribution and greater energy dissipation and ductility.

| 180] Turning to FIG. 8, FIG, 8 is a graph showing the strain capacities and elastomeric flo of polyurea-coated carbon fiber reinforced polymer fabric composites applied to a wooden substrate. As shown, curve 830 shows the data related to the strain at the interface between the polyurea and the carbon fiber reinforced polymer fabric components of the composite material and curve 840 shows the data related to th strain at the interface between the composite material and the wooden substrate, in addition, FIG.. 8 includes curve 10, which shows the data related to the strain for a non-wrapped wooden substrate, and curve 820, which shows the data related to the strain for a woode substrate wrapped only with a carbon fiber reinforced polymer fabric, It should be noted that, similar to FIG. 7, the open circles indicate a strength drop. It should also be noted that the closed circles indicate a yield point.

[0181] As indicated, FIG. 8 shows parallel strains on the wood and polyurea interfaces at quarter span locations, implying that there is no de-bonding, while the negligible strain rate indicates that there is no deformation in the polyurea. Again, without being bound to any one theory, the data shown in FIG. 8 supports the existence of a purel elastomeric poSyurea-carbon fiber reinforced polymer system after the wood substrate reaches its strength drop and the existence of a viscoe!astic energy dissipative sy stem prior to that point (but after yield).

[01.82] FIG. 9 shows the results of additional studies of composite wrapped wood beams under static load and indicates that the composite wrapped beams (curves 930 and 940) have a significant increase in ductility of 150% as compared to wood beams wrapped in carbon fiber reinforced polymer alone (curve 920). The carbon fiber reinforced polymer alone has an elongation of only .5%. Further, compared to the unwrapped wood beam (curve 10), the composite wrapped beams have a significant increase in ductility of 800%. FIG. 9 shows various load-deflection curves and indicates that two composite wrapped beams (one ^'having about 2 tiroes the amount of polyurea by volume and/or thickness; see

CarbonFlex x Wood Bead 2xY curve 940) exhibit a sustainable negative stiffness and strength over prolonged deflections and continued substrate cracking, relative to a carbon fiber reinforced polymer-wrapped wood beam.

|Θ183) It should be noted that the 2xV beam shown by curve 940 depicts an elastic- plastic like region after the final strength drop. Accordingly, curing time and polyurea volume fractions can be tailored to design the tight-wrap to satisfy specific structural performance demands.

|0J84] In addition, a comparison of the load-deflec tion curves of the IxV and 2xV beams in FIG. 9 suggest that the negative stiffness becomes less negative as cracks in the damaged wood member propagate and the load gradually transfers to the composite.

Following the final strength drop shown in FIG. 9, where the substrate fails, a strain

hardening region ensues that actually restores stress. The increasing nature of the negative slope of the stiffness indicates that the composite stabilizes wood crack growth as the composite transitions to a nearly purel viscous material.

EXAMPLE 4; Simulations of Acceleration and Hysteresis in Wrapped Wood Structure fftlSS] As shown in FIGS. iOA-iOC, computational simulations were performed to compare the performance of a two-story composite wrapped wood structure (indicated by CF in FIG. 1(C) to thai of a non-wrapped structure (indicated by W in FIG. 10C) subjected to conditions similar to the 1 94 Northridge earthquake, interior gypsum board wall sheathing and stucco finishes were not included in the model and neither was pinching of the hysterets. The post-yield viscoelastic portion of the CF tight- wrap was based on previously described models (see e.g., Attard. International Journal of Solids and Simeiwes., 42(21 -22), 5656- 5668 (2005); and Attard and Mknolet . Engineering Mechanics, 134(10), 881-891 (2008))

- '7 ~ and the sustainable negative stiffness region was modeled using a regression of experimental data. The confinement of the CF structure was modeled as a nonlinear "tight-fit" element, and the viscous-plus-hysteretic damping was calculated as ¾ ^::: 32% using experimental data, with 13% calculated from viscous-type damping. For the Ws structure, 20%, of which viscous damping contributed 2%. See Filiatranlt et aL Engineering Structures, 25, 461-47.1 (2003 ). The "deep shear" displacements were estimated as a function of a changing shear modulus in the negative stiffness region of the CF mode! . The CF and Ws models were embedded into a comprehensive nonlinear time-history code, HONOR See Attard. T.L.. "Modeling of Higher-Mode Effects in Various Structures Using a ^'Pushover Analysis "

Doctoral Dissertation, Arizona State University, Tempe, Arizona (2003); and Attard and Fafitis. Engineering Structures, 29(8), 1977-1989 (2007).

[0186] For comparison, FIG. 50A shows an illustrati ve graph of a simulated acceleration time-history of a two-story wooden structure that is wrapped wi th a polyurea- coated carbon fiber reinforced polymer fabric composite and FIG. iOB shows an illustrative graph of a simulated acceleration time-history of a two-story wooden structure without the composite described herein. An analysis of the acceleration results of the simulations in FIGS, IDA and J OB reveals significantly larger stiffness and viscous-type damping in the CF structure, which enabled the peak, accelerations in the CF structure to be 25% and 35% smaller than those in the Ws structure on the top and bottom stories, respectively. The standard deviations of the acceleration time histories were 39% and 47% smaller, which represent a substantia] across-the-board reduction. FIG. IOC shows the hysteresis and inter- story drifts (in %) in the two structures, indicating significant reduction in building damage to the bottom story using the poly urea-coated carbon fiber reinforced polymer fabric composite and no damage to the top story, which remained elastic. In comparison to the Ws structure, which experienced significant damage to both stories, the polyurea-coated carbon fiber reinforced polymer fabric composite wrapped structure was able to reduce the maximum post-elastic inter-story drift by 81%, where the post-elastic drift is defined here as the post- yielding drift, per cycle,

EXAMPLE 5; Retrofitting a Steel Reinforced Concrete Composite Beam (SRCC) j0187| As described herein, the approach for reinforcing substrates can be applied to a previously constructed structure and, more particularly, to art alread damaged structure. |θ :188] As shown in FIG. 1 1 A, the substra te can be prepared before retrofitting the substrate with the disclosed composite by, for example, re-shaping the substrate, steel shape welding, and grouting. As also shown in FIG, i 1 A, in this example, two concrete beams were prepared and retrofitted - one with only a carbon fiber reinforced polymer fabric and one with the polyurea-eoated carbon fiber reinforced polymer composite.

[6189] FIG. I I B shows various cross-sections along the concrete beam retrofitted with the carbon fiber reinforced polymer fabric. For example, section Al-Ai illustrates the three- layer bottom laminate used to cany tensile forces and section A2-A2 illustrates the three-layer composite formed around, the bottom portion of the beam and the polyurea-eoated carbon fiber reinforced polymer fabric formed around all four sides of the beam, in addition, the polyurea-eoated carbon fiber reinforced polymer fabric can be formed around particular portions of the beam. For example, section A3^» A3 shows that polyurea-eoated carbon fiber reinforced polymer fabric can be attached to opposing sides of the beam such that, in combination with the composite formed around the bottom portion of the beam, a "U" shaped composi te jacket is formed.

[01.90] FIG. I IC shows the results of force-deflection response studies along different beams - as shown, curve 1 1 10 corresponds to s steel reinforced concrete composite (SRCC) beam retrofitted with polyurea-eoated carbon fiber reinforced polymer composite portions (labeled BS ), curve 1 120 corresponds to a SRCC beam retrofitted with only carbon fiber reinforced polymer fabric portions (labeled B2), and curve 1 .130 corresponds to a SRCC beam retrofitted with polyurea-eoated carbon fiber reinforced polymer composite portions having no steel welded (labeled Bl). The results indicate thai the use of polyurea-eoated carbon fiber reinforced polymer composite portions allow the SRCC beam to experience significant increases in displacement and energy dissipation. The composite wrapped SRCC beams in 1 1 10 and 1 130 exhibit large viscous damping, a sustainable negative stiffness, and strength over prolonged deflections under stabilized substrate cracking, relative to a carbon fiber reinforced polymer-wrapped wood beam io. 1 120.

EXAMPLE 6: Retrofitting a Seismic Damaged Reinforced Concrete Shear Wall

[01.91] Similar to the above-mentioned example, the approach for reinforcing substrates can be applied to a previously constructed structure and, more particularly, to an already damaged structure, in this example, a reinforced concrete shear wall was damaged under a cyclic load. The cyclic testing resulted in severe damage to the reinforced concrete- shear wall that included a three millimeter wide cross-crack and concrete crush at two of the botiom comers of the wail. The after-test load capacity of the wall dropped to approximately 40% of its peak value,

[0192] As shown in portion 12 ! 0 of FIG. J 2 A, the shear wail substrate can. be prepared before retrofitting the substrate with the disclosed composite by, for example, grouting and crack injection. As shown in portion 1220 of FIG, 12A. various portions of the shear wall substrate, such as the cracked, crushed, and/or damaged portions of the substrate, can be retrofitted and reinforced with the poiyurea-coated carbon fiber reinforced polymer composite. In particular, particular portions of the shear wall substrate and reinforced with the composite before the entire substrate is wrapped around with the composite. As described previously, the composite can be prepared and then attached to the substrate or, alternatively, the composite can be formed direciiy on the surface of the substrate.

[0193] Taming to FIGS. 12B and 12C, the results of the force-deflection response studies along the retrofitted and reinforced shear wall indicate that the use of poiyurea-coated carbon fiber reinforced polymer composite portions allow the shear wall to recover about 80% of the shear wall's original load capacity. In addition, as shown in the illustrative images of FIG. 12C, the poiyurea-coated carbon fiber reinforced polymer composite provides a substantial increase in ductility. This increase in ductility allows the reinforced concrete shear wall to experience large deformations, where the energy dissipation properties of the poiyurea-coated carbon fiber reinforced polymer composite stabilized crack growth and sustained the high strength of the structure even after the concrete was crushed. By readily dissipating the energy after the formation of cracks, the formation of new crack surfaces and/or further damage can be prevented from occurring. As also shown in the images of FIG. 12C, it should be noted that there is significant confinement and a substantial increase in compression strength in this retrofitted wall.

EXAMPLE 7: Viscous Damping and Impact Resistance of Composite Wrapped. Substrates [ft 194] In this example, foam core substrates were used, where one foam core substrate was wrapped only with a carbon fiber reinforced polymer fabric and one foam core substrate was wrapped with a poly urea-coated carbon fiber reinforced polymer composite of the disclosed subject matter . These foam core substrates were then subjected to impact resistance testing, where a high loading speed (a shock load) or 4 meters per second was used.

|01 5] As shown in FIGS. 13 A and 13B, the amount of load handled by the poiyurea- coated carbon fiber reinforced polymer composite wrapped around the foam core substrate is in stark contrast to the foam core substrate wrapped with only the carbon fiber .reinforced polymer fabric. As shown in images 1310 and 13 1.5, upon performing the impact test, the carbon fiber reinforced polymer fabric de-bonds from she foam core substrate, in comparison, images 1320 and 325 illustrate that the poiy rea-coated carbon fiber reinforced polymer composite can absorb much more energy from the impact and dissipate the energy. As a result, the polyurea-coated carbon fiber reinforced polymer composite allows the foam core to experienc significant increases in displacement and energy dissipation, it should be noted that there is no debonding in the foam core wrapped with the polyurea-coated carbon fiber reinforced polymer composite.

[0196] Turning to FIGS, 14A and 148, the two thin steel beam substrates were subjected to high vibration tests. As described above, the polyurea-coated carbon fiber reinforced polymer composite transitions from a viscoelastic material to a nearly viscous material. The composite can act as an energ -release valve by providing sustainable energy dissipation and large viscous-type damping during extreme loading events, such as during earthquakes. In some embodiments, the composite/substrate system can allow for a change in viscous damping ratio (e.g., the composite/substrate system has a different viscous damping ratio than the substrate alone).

|0J97 As shown, when comparing the results between the steel beam substrate that was wrapped only with a carbon fiber reinforced polymer fabric and the steel beam substrate that was wrapped with a polyurea-coated carbon, fiber reinforced polymer composite of the disclosed subject matter, the polyurea-coated carbon fiber reinforced polymer composite provides viscous-typ damping to minimize vibrations during the testing.

EXAMPLE 8: Damping Ratio of the Composite

|«T9S] It should be noted that, in some embodiments, the properties of the composite material can be modified by varying time-related (t_e) and volume- fraction (h_p) polymeric properties. For example, as shown in F GS. 15.4 and 15C, properties of the composite, such as damping ratio, can be modified by controlling the thickness of the polyurea coating layer. Controllin the thickness of the polyurea coating layer can alter the volume .fraction of elasiomeric polyurea in the composite, which can. alter the properties of the resulting composite. In another example, as shown in FIGS. 15B and 1 SO, time-related factors in the preparation of the composite material (e.g., time factors related- to the reaction of the precursors of the polyurea layer and the precursors of the polymer of the FRP) can affect the damping ratio of the composite as a whole, {hereby enabling the strength of the resulting load-bearing composite to be sustained at large deformations. Accordingly, the composite material may be modified during the fabrication of the composite material (e.g., method 200 of FIG. 2, method 300 of FIG. 3, etc.) to achieve desired properties.

S0199J Turning to FIG. ISA, thin steel beams were used. The dampin ratio determination included a steel beam by itself, a steel beam wrapped only with a carbon fiber reinforced -polymer fabric, a steel beam wrapped with a polyurea-coated carbon -fiber reinforced poly mer composite ( where the poly urea layer is 1/32 of an inch), and a steel beam wrapped with a polyurea-coaied carbon fiber reinforced polymer composite (where the polyurea layer is .1/16* of an inch). As shown in FIG. 15A, the damping ratio is significantly greater for steel beams wrapped with the polyurea-coated carbon fiber reinforced polymer composite. In addition, FIG. I SA shows that the damping ratio of a steel beam wrapped with the polyurea-coaied carbon fiber reinforced polymer composiie can vary as a function of the thickness of the polyurea layer. Increasing the thickness of the polyurea layer (e.g., from l/32^isi of an inch to 1 /16'" of art inch), substantially increases the damping ratio.

[0200] As shown in FIG. 1 SB, the curing time for forming the polyurea layer on the carbon fiber reinforced polymer fabric, where the composite was formed on a steel beam, was varied between two hours and five hours. The damping ratio can vary as a function of time- related factors in the preparation of the composite material (t_e). It should be noted, however, that other properties, such as slightly greater stiffness, may be achieved by increasing the curing time.

[0201} In this example, these tests were conducted with the polyurea-coated carbon fiber reinforced polymer composite by itself. This can, for example, remove any contributing effects from the thin steel beam. As shown in FIG. 15€, the damping ratio was determined for a carbon fiber reinforced polymer fabric, a polyurea-coated carbon fiber reinforced polymer composite (where the polyurea layer is 1/16 of an inch), and a polyurea-coated carbon fiber reinforced polymer composite (where the polyurea layer is ί/8* of an inch). As shown in FIG. 15C, the damping ratio is significantly greater for the polyurea-coated carbon fiber reinforced polymer composite than with the carbon fiber reinforced polymer fabric by itself. Similar to FIG. ISA, FIG, 1 SC shows that the damping ratio the polyurea-coaied carbon fiber reinforced polymer composite can vary as a function of the thickness of the polyurea layer, increasing the thickness of the polyurea layer (e.g., from l/16^to of an inch to I/8^a of an inch), substantially increases the damping ratio, in addition, die greater the thickness of the polyurea layer, the greater the strength and stiffness properties of the composite material. Accordingly, the thickness of the polyurea layer can be modified based o the desired properties of the resulting composite.

|02 2 j Similar to FIG. 158, FIG. J 5D shows that the curing time for forming the polyurea layer on the carbon, fiber reinforced pol mer fabric affects the damping ratio, it should be noted, however, that although FIG. 15D shows that damping ratio decreases as curing time increases, curing time can be modified to achieve a composite material having a desired range of damping ratio. Again, the curing times used in making the composite can be modified based on the desired properties of the resulting composite.

(0203] Accordingly, high strength and high elasticity composite materials and methods of reinforcing substrates with the same are provided.

[0204] Although the invention has been described and illustrated in the foregoing iilustraiive embodiments, it is understood that the present disclosure has been made only by way of example, and that numerous changes in the details of implementation of the invention can be made without departing from the spirit and scope of the invention, which is only limited by the claims which follow. Features of the disclosed embodiments can be combined and rearranged in various ways.

Claims

What is claimed is;

! , A composite comprising:

a substrate;

a fiber reinforced polymer fabric layer attached to at least a portion of the substrate; and

a polyurea coating layer formed on an exposed surface of the fiber reinforced polymer fabric layer,

2. The composite of claim L wherein the substrate is at least one of: wood, masonry, concrete, steel and a combination thereof.

3. The composite of claim 1 , wherein the substrate has at least one damaged portion and the fiber reinforced polymer fabric iayer and the polyiirea coating layer are formed on the at least one damaged portion of the substrate.

4. The composite of claim 1 , wherein the fiber reinforced poly mer fabric iay er is a carbon fiber reinforced polymer fabric.

5. The composite of claim I , wherein the poly area coating layer is formed by applying an elastomeric polyurea-forming component solution to the exposed surface of (he fiber reinforced polymer fabric layer, wherein the elastomerk polyurea-forming component solution forms an aromatic polyiire coating Iayer.

6. The composite of claim 1 , wherein the polyurea further comprises an additive component wherein the additi ve component is at least one of: an ultraviolet (UV) protective additive, a flame retardant, a corrosion protective additive, a moisture resistance additive, ceramic microspheres, and a combination thereof.

7. A method for reinforcing a substrate, the method comprising:

providing a substrate;

attaching a high tenacity fiber reinforced polymer fabric to at least a portion of the substrate;

applying a saturant composition to an exposed surface of the high tenacity fiber reinforced polymer fabric, wherein the saturant composition comprises a polymer resin; curing the saturant composition to form a tacky surface;

applying an eiastonierie polyorea-forimng component solution to the tacky surface; and

curing the polyurea-foraurig component solution to form, a polyurea coating layer.

8. The method of claim 7, wherein the substrate is at least one of; wood, masonry, concrete, steel, an a combination thereof.

9. The method of claim ?, wherein the saturant composition is cured for a first time period and wherein the polyurea-formiiig component solution is cured for a second time period, the method further comprising modify ng the first time period and the second time period to obtain material properties of the polyurea coating layer on the high tenacity fiber reinforced polymer fabric.

.

10. The method of claim 7, further comprising performing surface preparation on at least a portion of the substrate, wherein the surface preparation includes at least one of: smooihing the substrate, filling in one or more damaged portions of the substrate- with a putty material, and cleaning the substrate.

1 1. The method of claim 7, wherein the high tenacity fiber reinforced polymer iabric is wrapped around the substrate.

12. The method of c laim ?, wherein the polyurea-forming component solution comprises an isocyanate component and a poiyaniine component, the method further comprising mixing the isocyanate component and the polyamine component prior to the applying to the tacky surface to form the polyurea-forming component solution, wherein the polyurea-forming component solution has an excess of the isocyanate component.

13. The method of claim 7, further comprising spra ng the polyurea-forming component solution on the tacky surface.

14, The method of claim 7, fo mer comprising providing an additive component into the polyurea-forming component solution, wherein the additive component is at Least one of: an. ultraviolet (tiY) protective additive, a flame retardant, a corrosion protective additive, a moisture resistance additive, ceramic microspheres, and a combination thereof.

1.5. The method of claim 7, wherein the polyurea coating layer has a thickness, the method further comprising controlling the thickness of the polyurea coating layer.

16. The method of claim 7, wherein at least a first component of the polyurea- forming component solution and a second component of the tacky surface of the saturaiii composition applied to the high tenacity fiber reinforced polymer fabric interact to form an sustainable interface between th polyurea coating layer and the high tenacity fiber reinforced polymer fabric.

.

17. A method for providing a composite, the method comprising:

forming a, polyurea-eoated high tenacity fiber reinforced polymer fabric, wherein the forming comprises:

providing a high tenacity fiber reinforced polymer fabric;

applying a saturant composition to a surface of the high tenacity fiber reinforced polymer fabric, wherein the saturant composition comprises a polymer resin;

curing the saturant composi tion to form a tack surface;

applying an elastomeric polyurea-fo ming component solution to the tacky surface; and

curing the polyurea-forming component solution to form a polyurea coating layer on the high tenacity fiber reinforced polymer fabric,

18. The method of claim 17, further comprising:

preparing at least a portion of a substrate for reinforcement, prior to positioning the polyurea-eoated high tenacity fiber reinforced polymer fabric on the substrate: and

attaching the poly urea-coated high tenacit fiber reinforced polymer fabric to a damaged portion of the substrate.

19. The method of claim 17, wherein the saturant composition is cured, for a first time period and wherein the polyurea-forming component solution, is cured for a second time period, die method further comprising modifying the first time period arid the second time period to obtain the polyurea coating layer of a thickness based at leas!, in part on an assessment of the damaged portion of the substrate.

20, The method of claim 17, wherein at least a first component of the polyurea- forming component solution and a second component of the tacky surface of the saturant composition applied to the high tenacity fiber reinforced polymer fabric interact to form an sustainable interface between the polyurea coating layer and the high tenacity fiber reinforced polymer fabric.