US20140065907A1 - Ballistic Composite Materials, Ballistic Fabrics, and Methods of Making - Google Patents

Ballistic Composite Materials, Ballistic Fabrics, and Methods of Making Download PDF

Info

Publication number
US20140065907A1
US20140065907A1 US13/802,900 US201313802900A US2014065907A1 US 20140065907 A1 US20140065907 A1 US 20140065907A1 US 201313802900 A US201313802900 A US 201313802900A US 2014065907 A1 US2014065907 A1 US 2014065907A1
Authority
US
United States
Prior art keywords
layer
weave pattern
fabric
elastomer
weave
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US13/802,900
Inventor
Tulin Oktem
Andre Beth
Randall Tatham
Original Assignee
Lincoln Fabrics
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US13/672,316 external-priority patent/US20130111640A1/en
Application filed by Lincoln Fabrics filed Critical Lincoln Fabrics
Priority to US13/802,900 priority Critical patent/US20140065907A1/en
Publication of US20140065907A1 publication Critical patent/US20140065907A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D11/00Double or multi-ply fabrics not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H1/00Personal protection gear
    • F41H1/02Armoured or projectile- or missile-resistant garments; Composite protection fabrics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/024Woven fabric
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00Woven fabrics designed to make specified articles
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00Woven fabrics designed to make specified articles
    • D03D1/0035Protective fabrics
    • D03D1/0052Antiballistic fabrics
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06BTREATING TEXTILE MATERIALS USING LIQUIDS, GASES OR VAPOURS
    • D06B1/00Applying liquids, gases or vapours onto textile materials to effect treatment, e.g. washing, dyeing, bleaching, sizing or impregnating
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06NWALL, FLOOR, OR LIKE COVERING MATERIALS, e.g. LINOLEUM, OILCLOTH, ARTIFICIAL LEATHER, ROOFING FELT, CONSISTING OF A FIBROUS WEB COATED WITH A LAYER OF MACROMOLECULAR MATERIAL; FLEXIBLE SHEET MATERIAL NOT OTHERWISE PROVIDED FOR
    • D06N3/00Artificial leather, oilcloth or other material obtained by covering fibrous webs with macromolecular material, e.g. resins, rubber or derivatives thereof
    • D06N3/0002Artificial leather, oilcloth or other material obtained by covering fibrous webs with macromolecular material, e.g. resins, rubber or derivatives thereof characterised by the substrate
    • D06N3/0006Artificial leather, oilcloth or other material obtained by covering fibrous webs with macromolecular material, e.g. resins, rubber or derivatives thereof characterised by the substrate using woven fabrics
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06NWALL, FLOOR, OR LIKE COVERING MATERIALS, e.g. LINOLEUM, OILCLOTH, ARTIFICIAL LEATHER, ROOFING FELT, CONSISTING OF A FIBROUS WEB COATED WITH A LAYER OF MACROMOLECULAR MATERIAL; FLEXIBLE SHEET MATERIAL NOT OTHERWISE PROVIDED FOR
    • D06N3/00Artificial leather, oilcloth or other material obtained by covering fibrous webs with macromolecular material, e.g. resins, rubber or derivatives thereof
    • D06N3/04Artificial leather, oilcloth or other material obtained by covering fibrous webs with macromolecular material, e.g. resins, rubber or derivatives thereof with macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06NWALL, FLOOR, OR LIKE COVERING MATERIALS, e.g. LINOLEUM, OILCLOTH, ARTIFICIAL LEATHER, ROOFING FELT, CONSISTING OF A FIBROUS WEB COATED WITH A LAYER OF MACROMOLECULAR MATERIAL; FLEXIBLE SHEET MATERIAL NOT OTHERWISE PROVIDED FOR
    • D06N3/00Artificial leather, oilcloth or other material obtained by covering fibrous webs with macromolecular material, e.g. resins, rubber or derivatives thereof
    • D06N3/04Artificial leather, oilcloth or other material obtained by covering fibrous webs with macromolecular material, e.g. resins, rubber or derivatives thereof with macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • D06N3/10Artificial leather, oilcloth or other material obtained by covering fibrous webs with macromolecular material, e.g. resins, rubber or derivatives thereof with macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds with styrene-butadiene copolymerisation products or other synthetic rubbers or elastomers except polyurethanes
    • D06N3/106Elastomers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/02Plate construction
    • F41H5/04Plate construction composed of more than one layer
    • F41H5/0471Layered armour containing fibre- or fabric-reinforced layers
    • F41H5/0478Fibre- or fabric-reinforced layers in combination with plastics layers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/02Plate construction
    • F41H5/04Plate construction composed of more than one layer
    • F41H5/0471Layered armour containing fibre- or fabric-reinforced layers
    • F41H5/0485Layered armour containing fibre- or fabric-reinforced layers all the layers being only fibre- or fabric-reinforced layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/022 layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/20All layers being fibrous or filamentary
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00Coating on the layer surface
    • B32B2255/02Coating on the layer surface on fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00Coating on the layer surface
    • B32B2255/26Polymeric coating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02Composition of the impregnated, bonded or embedded layer
    • B32B2260/021Fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04Impregnation, embedding, or binder material
    • B32B2260/046Synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02Synthetic macromolecular fibres
    • B32B2262/0261Polyamide fibres
    • B32B2262/0269Aromatic polyamide fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/51Elastic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558Impact strength, toughness
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/56Damping, energy absorption
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2571/00Protective equipment
    • B32B2571/02Protective equipment defensive, e.g. armour plates, anti-ballistic clothing
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06NWALL, FLOOR, OR LIKE COVERING MATERIALS, e.g. LINOLEUM, OILCLOTH, ARTIFICIAL LEATHER, ROOFING FELT, CONSISTING OF A FIBROUS WEB COATED WITH A LAYER OF MACROMOLECULAR MATERIAL; FLEXIBLE SHEET MATERIAL NOT OTHERWISE PROVIDED FOR
    • D06N2201/00Chemical constitution of the fibres, threads or yarns
    • D06N2201/02Synthetic macromolecular fibres
    • D06N2201/0263Polyamide fibres
    • D06N2201/0272Aromatic polyamide fibres
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06NWALL, FLOOR, OR LIKE COVERING MATERIALS, e.g. LINOLEUM, OILCLOTH, ARTIFICIAL LEATHER, ROOFING FELT, CONSISTING OF A FIBROUS WEB COATED WITH A LAYER OF MACROMOLECULAR MATERIAL; FLEXIBLE SHEET MATERIAL NOT OTHERWISE PROVIDED FOR
    • D06N2211/00Specially adapted uses
    • D06N2211/10Clothing
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2331/00Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products
    • D10B2331/02Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products polyamides
    • D10B2331/021Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products polyamides aromatic polyamides, e.g. aramides
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2403/00Details of fabric structure established in the fabric forming process
    • D10B2403/02Cross-sectional features
    • D10B2403/021Lofty fabric with equidistantly spaced front and back plies, e.g. spacer fabrics
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T442/00Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/20Coated or impregnated woven, knit, or nonwoven fabric which is not [a] associated with another preformed layer or fiber layer or, [b] with respect to woven and knit, characterized, respectively, by a particular or differential weave or knit, wherein the coating or impregnation is neither a foamed material nor a free metal or alloy layer
    • Y10T442/2615Coating or impregnation is resistant to penetration by solid implements
    • Y10T442/2623Ballistic resistant

Definitions

  • the present invention relates to the field of ballistic materials and methods for making same.
  • Ballistic vests have long struggled with the conflicting priorities of increased bullet resistance and increased comfort and mobility of the wearer. Effective ballistic vests must be manufactured from a material that meets a minimum performance threshold for resistance to ballistic projectiles. Through the years, woven goods have not only provided the necessary ballistic protection, but also have encouraged users to wear the vests due to the relative comfort from the flexibility and reasonable weight. Recent changes in ballistic resistance standards, for example, National Institute of Justice (“NU”) Standard 0101.06, titled “Ballistic Resistance of Body Armor,” have created significant new limitations on vest performance.
  • NU National Institute of Justice
  • Kevlar is spun into fibers, and weaving the fibers (or bundles of Kevlar fibers—“yarns”) causes an impacting bullet to stretch the fibers in order to penetrate.
  • the bullet-stopping power is primarily due to the large amount of energy required to stretch a molecule of Kevlar. Therefore, a bullet's kinetic energy is absorbed in stretching (and breaking) the Kevlar fibers upon impact. Energy is also radially dissipated (radiating through the fabric layer from the point of impact) through the weave structure.
  • the '026 application teaches the use of one or more generally rigid plates of rigid materials to distribute the impact force over an increased amount of the composite material.
  • a composite with rigid plates is taught as useful in using the material in, for example, bulletproof vests.
  • designs of ballistic vests with composite materials include the use of stiffer, rigid materials in response to the backface signature standards of NIJ 0101.06.
  • the usability and comfort of the wearer is affected by such composites due to the stiffness of the fibrous material layer and generally rigid plates.
  • Textiles used in ballistic resistant materials may be configured in weave patterns which have ballistic resistant qualities.
  • the weave pattern should be resistant to penetration of a ballistic projectile by causing the energy to be transformed into stretching and/or breaking fibers. This is best performed when the weave is capable of maintaining its configuration without, for example, spreading yarns apart to allow passage of the projectile without sufficient energy transferred into stretching fibers (or conversely being forced together by a passing projectile).
  • a primary technique previously used to maintain the configuration of a weave is to create a textile with a tight weave (i.e., having low air permeability). However, such a tight weave typically increases the stiffness of the fabric—negatively impacting usability and comfort.
  • a composite material of the present invention is comprised of a textile layer of woven fabric and a first elastomer layer disposed on a first side of the textile layer.
  • the textile layer may comprise a compound fabric such as a double-layer fabric.
  • the double-layer fabric may have a first layer woven as a plain weave and a second layer woven as a crowfoot weave (3/1 twill weave).
  • the composite material may further comprise a second elastomer layer disposed on the second side of the textile layer.
  • the present invention may be embodied as a method of manufacturing a composite material comprising the steps of coating a compound fabric with an elastomer material and allowing the elastomer material of the coating to cure.
  • the present invention may further be embodied as a method of making a composite ballistic fabric, including weaving a first ballistic woven layer having a first weave pattern with a second ballistic woven layer having a second weave pattern to form the composite ballistic fabric.
  • the second weave pattern can have a different weave pattern than the first weave pattern.
  • the present invention can be embodied as a composite ballistic fabric including a first ballistic woven layer having a first weave pattern woven to a second ballistic woven layer having a second weave pattern.
  • the second weave pattern can have a different weave pattern than the first weave pattern.
  • FIG. 1A depicts a cross-sectional diagram of a material having a double-layer compound fabric according to an embodiment of the present ;
  • FIG. 1B depicts a cross-sectional diagram of a material having a triple-layer compound fabric according to another embodiment of the present
  • FIG. 2 depicts the weave structures of two fabrics, a plain weave and a crowfoot weave, suitable for use in embodiments of the present invention
  • FIG. 3 is another view of the two fabrics of FIG. 2 ;
  • FIG. 4 depicts a double-layer fabric for use in an embodiment of the present invention
  • FIG. 5 is another view of the double-layer fabric of FIG. 4 ;
  • FIG. 6 is another view of the double-layer fabric of FIGS. 4 and 5 ;
  • FIG. 7 depicts the structure of two fabrics, a plain weave and a crowfoot weave, suitable for use in embodiments of the present invention, wherein the yarns of the fabrics are thicker than those used in other embodiments;
  • FIG. 8 is another view of the two fabrics of FIG. 7 ;
  • FIG. 9 depicts a double-layer fabric for use in another embodiment of the present invention, wherein the yarns of the fabrics are thicker than those used in other embodiments;
  • FIG. 10 is another view of the double-layer fabric of FIG. 9 ;
  • FIG. 11 is another view of the double-layer fabric of FIGS. 9 and 10 ;
  • FIG. 12 is a flowchart showing a method according to another embodiment of the present invention.
  • FIG. 13 is a flowchart showing a method according to another embodiment of the present invention.
  • the present invention may be embodied as a composite material 10 comprising a woven fiber layer (“textile” layer).
  • the textile layer may preferably be a compound fabric layer 11 woven from a plurality of warp and weft yarns.
  • a compound fabric is a fabric having more than one interlaced layer of woven fabric (further described below).
  • the yarns of the fabric are assembled from a plurality of fibers—multifilament yarns.
  • the fiber may be an aramid fiber. More specifically, the fiber may be a para-aramid, such as, for example, Kevlar® brand fiber.
  • the yarns may be of any linear density, and preferably from approximately 200 denier to 3,000 denier.
  • the composite material 10 of the present invention further comprises a first elastomer layer 12 disposed on a first side of the compound fabric layer 11 .
  • the elastomer layer 12 may be described as a coating on the compound fabric layer 11 .
  • the elastomer layer 11 may be disposed on the compound fabric layer 11 such that a portion of the material forming the elastomer layer 11 impregnates at least a portion of the weave of the compound fabric layer 11 .
  • the elastomer layer 12 may function to hold the weave configuration of the compound fabric layer 11 together near the point of impact of a ballistic object (e.g., a bullet) and throughout a radial distance from the point of impact.
  • a ballistic object e.g., a bullet
  • the elastomer layer 12 may act as a shock absorber between yarns of the weave, absorbing the tendency to of the yarns to move relative to each other. In this way, the kinetic energy of the movement of yarns is transferred into heat energy by the elastic property of the elastomer used in the elastomer layer 12 . Where the extent of the elasticity of the elastomer is reached, energy may be absorbed by the localized tearing (failure) of the elastomer.
  • the elastomer coating 12 may be formed from any elastomer.
  • the elastomer may be urethane rubber, silicone rubber, nitrile rubber, butyl rubber, acrylic rubber, natural rubber, styrene-butadiene rubber, and the like.
  • any elastomer material can be used to form the first elastomer layer without departing from the scope of the present invention.
  • the elastomer layer may be a thermoset elastomer layer.
  • the elastomer layer 12 can be a thermoplastic or any material suitable for thermoforming An interface layer may be used between the elastomer layer 12 and the compound fabric layer 11 .
  • Such an interface layer improves the bond between the chosen elastomer and the fibers of the fabric.
  • the interface layer may be, for example, an adhesive or a primer.
  • the elastomer used in the elastomer layer 12 may require a drying or curing operation step during manufacturing, depending on the chosen elastomer.
  • a second layer 18 of elastomer may be disposed on a second side of the compound fabric layer 11 (opposite the first side of the compound fabric layer 11 ). Similar to the first elastomer layer 12 , described above, the second elastomer layer 18 may be constructed from any elastomer. The elastomer of the second elastomer layer 18 may be the same elastomer as that of the first elastomer layer 12 . The elastomer of the second elastomer layer 18 may be different than that of the first elastomer layer 12 .
  • FIG. 1A An embodiment of a composite material 10 according to the present invention is depicted in FIG. 1A .
  • the composite material 10 comprises a first elastomer layer 12 and a second elastomer layer 18 .
  • the compound fabric layer 11 of the depicted embodiment is a double-layer fabric comprising a first layer 14 and a second layer 16 .
  • the double-layer fabric may be a plain weave 22 fabric tied to a crowfoot weave 26 (3/1 twill weave) using a plurality of the yarns of one or both weaves 22 , 26 to connect (tie) the weaves 22 , 26 together into a single, compound (double-layer) fabric.
  • FIGS. 4-6 depict an example of such a double-layer fabric 30 .
  • the double-layer fabric 30 may be constructed of the two layers of fabric 22 , 26 tacked together by tack points 32 formed by picking certain warp yarns 34 of one layer with certain weft yarns 36 of the other layer.
  • the first and/or second elastomer layers 12 , 18 may be made from elastomers which are foamed—e.g., elastomer materials incorporating a plurality of gas bubbles within the material.
  • the elastomer of the elastomer layers 12 , 18 may comprise a chemical blowing agent which causes foaming upon certain conditions as is known in the art.
  • a double-layer fabric (a fabric having a first layer and a second layer) may comprise two plain weave layers.
  • the double-layer fabric comprises a plain weave layer 22 and a twill weave layer, such as, for example, a crowfoot weave layer 26 (e.g., a 3/1 twill weave).
  • a crowfoot weave layer 26 e.g., a 3/1 twill weave.
  • Compound fabric layers 11 made from double- and triple-layer fabrics according to the present disclosure have been shown to enhance the performance of rubber (elastomer)-coated fabrics.
  • the weaves according to the present invention may also comprise additional layers (e.g., more than three).
  • the structure of one woven layer is considered to enhance the integrity of another layer.
  • one layer may be thought of as holding the other layer together.
  • This effect may be even more synergistic where the weave structures of the layers are not the same.
  • a plain weave may “open up” (spread apart upon impact of a projectile) in a characteristic way (along force vectors) which is different from the way in which a twill weave opens up.
  • the integrity of the weave structure of each layer may be increased without adding a significant amount of rigidity.
  • FIGS. 7-8 depict two fabrics—plain weave 50 and crowfoot weave 55 —which comprise yarns thicker than those used in the fabrics of FIGS. 2-3 (e.g., having a higher denier value).
  • FIGS. 9-11 depict the formation of a double-layer fabric 60 used in another embodiment of a material according to the present invention using the thicker yarns. The number of tack points 62 is greater than the number used in embodiments using “thinner” yarns.
  • Composite materials of the present invention may be used to manufacture garments according to another embodiment of the present invention.
  • the garments may be, for example, vests, jackets, pads, braces, etc.
  • the materials may also be used to enhance objects such as cars, briefcases, backpacks, etc.
  • the present invention may be embodied as a method 100 of manufacturing a composite material such as those materials described above.
  • the method 100 comprises the step of applying 103 an elastomer coating to a first side of a compound fabric.
  • the elastomer coating may be applied 103 in any way known in the art, such as, for example, spraying, rolling, pouring, spreading, brushing, or any combination of techniques.
  • the elastomer may be poured on to the compound fabric and the spread using a squeegee-type device. Such techniques may also cause the elastomer material to impregnate the fabric.
  • the method 100 comprises the step of curing 106 the elastomer coating.
  • Curing 106 may be accomplished by, for example, simply allowing time for the elastomer material to cure (e.g., cross-link). Curing 106 may be accomplished using other common techniques, including, for example, heating the elastomer. In this way, curing 106 the elastomer coating may be accomplished by passing the composite material (with elastomer in an uncured state), through a heater, such as an oven.
  • the method 100 may comprise the step of applying 109 an elastomer coating to the second side of the compound fabric. This step of applying 109 to the second side may be accomplished before or after curing 106 the elastomer coating of the first side.
  • an elastomer may be provided in sheet form (such as on a roll).
  • manufacturing a composite material comprises bonding a sheet of elastomer material to a compound fabric. Bonding may be accomplished using an interface, such as an adhesive, by heating the elastomer sheet, or by other techniques known in the art.
  • the present invention may also be embodied as a method 200 of manufacturing a multi-layer ballistic fabric.
  • the method comprises the step of weaving 202 a first ballistic woven layer having a first weave pattern and a second ballistic woven layer having a second weave pattern.
  • the first woven layer can be a plain weave
  • the second layer can be a sateen, such as a crowfoot weave.
  • the weave pattern of the second layer may be selected with a weave having good ballistic performance characteristics but may have less desirable physical characteristics. For example, sateens with high ratios of floats may lack integrity such that the yarns may spread easily and come apart at the edges of fabrics.
  • the first ballistic layer and second ballistic layer may be woven 202 such that the first layer stabilizes the second layer, thereby holding the second layer together.
  • the first layer and second layer may be tacked together by one or more weft yarns of the first layer with a pick of the second layer and/or one or more weft yarns of the second layer with a pick of the first layer.
  • a sateen layer e.g., the layer becoming unstable, losing its shape, and/or becoming unworkable
  • weaving a sateen ballistic layer to a plain weave ballistic layer can produce synergistic results.
  • a plain weave may “open up” (spread apart upon impact of a projectile) in a characteristic way (along force vectors) which is different from the way in which a twill weave opens up.
  • the method 200 may also include the step of applying 204 an elastomer coating to a first side of the woven multi-layer fabric.
  • the step of applying an elastomer layer can be omitted, and the multi-layer fabric may be manufactured 206 into a garment.

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Laminated Bodies (AREA)

Abstract

A method of making a composite ballistic fabric of the present invention includes weaving a first ballistic woven layer having a first weave pattern and a second ballistic woven layer having a second weave pattern to form the composite ballistic fabric. The second weave pattern can have a different weave pattern than the first weave pattern. The present invention may also be embodied as a composite ballistic fabric including a first ballistic woven layer having a first weave pattern woven to a second ballistic woven layer having a second weave pattern. The second weave pattern can have a different weave pattern than the first weave pattern.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • The present application is a continuation-in-part of U.S. application Ser. No. 13/672,316 filed on Nov. 8, 2012, which in turn claims priority to U.S. Provisional Patent Application No. 61/557,006, filed on Nov. 8, 2011, and titled “Ballistic Composite Material and Method of Making. The disclosures of these applications are incorporated herein by reference in their entirety.
  • FIELD OF THE INVENTION
  • The present invention relates to the field of ballistic materials and methods for making same.
  • BACKGROUND OF THE INVENTION
  • Designers of bullet-resistant vests (“ballistic vests”) have long struggled with the conflicting priorities of increased bullet resistance and increased comfort and mobility of the wearer. Effective ballistic vests must be manufactured from a material that meets a minimum performance threshold for resistance to ballistic projectiles. Through the years, woven goods have not only provided the necessary ballistic protection, but also have encouraged users to wear the vests due to the relative comfort from the flexibility and reasonable weight. Recent changes in ballistic resistance standards, for example, National Institute of Justice (“NU”) Standard 0101.06, titled “Ballistic Resistance of Body Armor,” have created significant new limitations on vest performance. In particular, toughened standards on the “backface signature”—deformation of the wearer-side of a vest caused by the impact of a projectile—have caused vest designers to limit the quantity of woven fabrics formerly used in these garments. Stiffer materials, such as laminated, unidirectional, and/or non-woven materials have displaced up to 50% of the woven goods used in current vests. This changed has drastically reduced the comfort of the vests.
  • Para-aramid materials, such as Twaron® and Kevlar®, are currently the leading fibers due to their excellent mechanical performance and acceptable stability. Kevlar is spun into fibers, and weaving the fibers (or bundles of Kevlar fibers—“yarns”) causes an impacting bullet to stretch the fibers in order to penetrate. The bullet-stopping power is primarily due to the large amount of energy required to stretch a molecule of Kevlar. Therefore, a bullet's kinetic energy is absorbed in stretching (and breaking) the Kevlar fibers upon impact. Energy is also radially dissipated (radiating through the fabric layer from the point of impact) through the weave structure.
  • Composite materials using aramid fibers combined with vibration dampening substances are known in the art. U.S. Patent Application Publication 2009/0075026, to Vito et al., (the “'026 application”) discloses a composite material made by using an aramid fiber weave disposed between two elastomeric layers. Such technologies have been used successfully to reduce the effects of a non-ballistic impact of an object by absorbing mechanical vibrational energy in the first (outermost) elastomeric material, and redirecting vibrational energy and providing stiffness in the fibrous material layer. In ballistic resistant applications, however, an outer elastomer layer will have little effect in absorbing the kinetic energy of a bullet. The '026 application teaches the use of one or more generally rigid plates of rigid materials to distribute the impact force over an increased amount of the composite material. Such a composite with rigid plates is taught as useful in using the material in, for example, bulletproof vests. As such, designs of ballistic vests with composite materials include the use of stiffer, rigid materials in response to the backface signature standards of NIJ 0101.06. However, the usability and comfort of the wearer is affected by such composites due to the stiffness of the fibrous material layer and generally rigid plates.
  • Textiles used in ballistic resistant materials may be configured in weave patterns which have ballistic resistant qualities. Specifically, the weave pattern should be resistant to penetration of a ballistic projectile by causing the energy to be transformed into stretching and/or breaking fibers. This is best performed when the weave is capable of maintaining its configuration without, for example, spreading yarns apart to allow passage of the projectile without sufficient energy transferred into stretching fibers (or conversely being forced together by a passing projectile). A primary technique previously used to maintain the configuration of a weave is to create a textile with a tight weave (i.e., having low air permeability). However, such a tight weave typically increases the stiffness of the fabric—negatively impacting usability and comfort.
  • Accordingly, there is a need for an improved ballistic material which reduces rigidity while enhancing the ballistic resistance by, for example, reducing the backface signature of an impacting projectile.
  • BRIEF SUMMARY OF THE INVENTION
  • A composite material of the present invention is comprised of a textile layer of woven fabric and a first elastomer layer disposed on a first side of the textile layer. The textile layer may comprise a compound fabric such as a double-layer fabric. The double-layer fabric may have a first layer woven as a plain weave and a second layer woven as a crowfoot weave (3/1 twill weave). The composite material may further comprise a second elastomer layer disposed on the second side of the textile layer.
  • The present invention may be embodied as a method of manufacturing a composite material comprising the steps of coating a compound fabric with an elastomer material and allowing the elastomer material of the coating to cure.
  • The present invention may further be embodied as a method of making a composite ballistic fabric, including weaving a first ballistic woven layer having a first weave pattern with a second ballistic woven layer having a second weave pattern to form the composite ballistic fabric. The second weave pattern can have a different weave pattern than the first weave pattern.
  • Additionally, the present invention can be embodied as a composite ballistic fabric including a first ballistic woven layer having a first weave pattern woven to a second ballistic woven layer having a second weave pattern. The second weave pattern can have a different weave pattern than the first weave pattern.
  • DESCRIPTION OF THE DRAWINGS
  • For a fuller understanding of the nature and objects of the invention, reference should be made to the following detailed description taken in conjunction with the accompanying drawings, in which:
  • FIG. 1A depicts a cross-sectional diagram of a material having a double-layer compound fabric according to an embodiment of the present ;
  • FIG. 1B depicts a cross-sectional diagram of a material having a triple-layer compound fabric according to another embodiment of the present;
  • FIG. 2 depicts the weave structures of two fabrics, a plain weave and a crowfoot weave, suitable for use in embodiments of the present invention;
  • FIG. 3 is another view of the two fabrics of FIG. 2;
  • FIG. 4 depicts a double-layer fabric for use in an embodiment of the present invention;
  • FIG. 5 is another view of the double-layer fabric of FIG. 4;
  • FIG. 6 is another view of the double-layer fabric of FIGS. 4 and 5;
  • FIG. 7 depicts the structure of two fabrics, a plain weave and a crowfoot weave, suitable for use in embodiments of the present invention, wherein the yarns of the fabrics are thicker than those used in other embodiments;
  • FIG. 8 is another view of the two fabrics of FIG. 7;
  • FIG. 9 depicts a double-layer fabric for use in another embodiment of the present invention, wherein the yarns of the fabrics are thicker than those used in other embodiments;
  • FIG. 10 is another view of the double-layer fabric of FIG. 9;
  • FIG. 11 is another view of the double-layer fabric of FIGS. 9 and 10;
  • FIG. 12 is a flowchart showing a method according to another embodiment of the present invention; and
  • FIG. 13 is a flowchart showing a method according to another embodiment of the present invention.
  • DETAILED DESCRIPTION OF THE INVENTION
  • The present invention may be embodied as a composite material 10 comprising a woven fiber layer (“textile” layer). The textile layer may preferably be a compound fabric layer 11 woven from a plurality of warp and weft yarns. As used herein, a compound fabric is a fabric having more than one interlaced layer of woven fabric (further described below). FIGS. 1A and 1B depict exemplary embodiments of materials 10, 40 according to the present invention having a double-layer fabric 11 (FIG. 1A) and a triple-layer fabric 41 (FIG. 1B). The yarns of the fabric are assembled from a plurality of fibers—multifilament yarns. The fiber may be an aramid fiber. More specifically, the fiber may be a para-aramid, such as, for example, Kevlar® brand fiber. The yarns may be of any linear density, and preferably from approximately 200 denier to 3,000 denier.
  • The composite material 10 of the present invention further comprises a first elastomer layer 12 disposed on a first side of the compound fabric layer 11. As such the elastomer layer 12 may be described as a coating on the compound fabric layer 11. The elastomer layer 11 may be disposed on the compound fabric layer 11 such that a portion of the material forming the elastomer layer 11 impregnates at least a portion of the weave of the compound fabric layer 11. The elastomer layer 12 may function to hold the weave configuration of the compound fabric layer 11 together near the point of impact of a ballistic object (e.g., a bullet) and throughout a radial distance from the point of impact. The elastomer layer 12 may act as a shock absorber between yarns of the weave, absorbing the tendency to of the yarns to move relative to each other. In this way, the kinetic energy of the movement of yarns is transferred into heat energy by the elastic property of the elastomer used in the elastomer layer 12. Where the extent of the elasticity of the elastomer is reached, energy may be absorbed by the localized tearing (failure) of the elastomer.
  • The elastomer coating 12 may be formed from any elastomer. For example, the elastomer may be urethane rubber, silicone rubber, nitrile rubber, butyl rubber, acrylic rubber, natural rubber, styrene-butadiene rubber, and the like. In general, any elastomer material can be used to form the first elastomer layer without departing from the scope of the present invention. For example the elastomer layer may be a thermoset elastomer layer. Alternatively, the elastomer layer 12 can be a thermoplastic or any material suitable for thermoforming An interface layer may be used between the elastomer layer 12 and the compound fabric layer 11. Such an interface layer improves the bond between the chosen elastomer and the fibers of the fabric. The interface layer may be, for example, an adhesive or a primer. The elastomer used in the elastomer layer 12 may require a drying or curing operation step during manufacturing, depending on the chosen elastomer.
  • A second layer 18 of elastomer may be disposed on a second side of the compound fabric layer 11 (opposite the first side of the compound fabric layer 11). Similar to the first elastomer layer 12, described above, the second elastomer layer 18 may be constructed from any elastomer. The elastomer of the second elastomer layer 18 may be the same elastomer as that of the first elastomer layer 12. The elastomer of the second elastomer layer 18 may be different than that of the first elastomer layer 12.
  • An embodiment of a composite material 10 according to the present invention is depicted in FIG. 1A. The composite material 10 comprises a first elastomer layer 12 and a second elastomer layer 18. The compound fabric layer 11 of the depicted embodiment is a double-layer fabric comprising a first layer 14 and a second layer 16. The double-layer fabric may be a plain weave 22 fabric tied to a crowfoot weave 26 (3/1 twill weave) using a plurality of the yarns of one or both weaves 22, 26 to connect (tie) the weaves 22, 26 together into a single, compound (double-layer) fabric. FIGS. 4-6 depict an example of such a double-layer fabric 30. The double-layer fabric 30 may be constructed of the two layers of fabric 22, 26 tacked together by tack points 32 formed by picking certain warp yarns 34 of one layer with certain weft yarns 36 of the other layer.
  • The first and/or second elastomer layers 12, 18 may be made from elastomers which are foamed—e.g., elastomer materials incorporating a plurality of gas bubbles within the material. In some embodiments, the elastomer of the elastomer layers 12, 18 may comprise a chemical blowing agent which causes foaming upon certain conditions as is known in the art.
  • In testing, the performance of rubber (elastomer)-coated fabrics has been shown to be enhanced by use of a compound fabric layer 11, and further enhanced using certain weave patterns within the fabric. For example, a double-layer fabric (a fabric having a first layer and a second layer) may comprise two plain weave layers. In another embodiment, depicted in FIGS. 4-6, the double-layer fabric comprises a plain weave layer 22 and a twill weave layer, such as, for example, a crowfoot weave layer 26 (e.g., a 3/1 twill weave). In testing composite materials made according to the present invention, such crowfoot weaves 26 have been shown to perform better than other weaves. Compound fabric layers 11 made from double- and triple-layer fabrics according to the present disclosure have been shown to enhance the performance of rubber (elastomer)-coated fabrics. The weaves according to the present invention may also comprise additional layers (e.g., more than three).
  • In a multi-layer fabric, the structure of one woven layer is considered to enhance the integrity of another layer. As such, one layer may be thought of as holding the other layer together. This effect may be even more synergistic where the weave structures of the layers are not the same. For example, a plain weave may “open up” (spread apart upon impact of a projectile) in a characteristic way (along force vectors) which is different from the way in which a twill weave opens up. By combining, for example, two different weaves into a double-layer fabric, the integrity of the weave structure of each layer may be increased without adding a significant amount of rigidity.
  • FIGS. 7-8 depict two fabrics—plain weave 50 and crowfoot weave 55—which comprise yarns thicker than those used in the fabrics of FIGS. 2-3 (e.g., having a higher denier value). FIGS. 9-11 depict the formation of a double-layer fabric 60 used in another embodiment of a material according to the present invention using the thicker yarns. The number of tack points 62 is greater than the number used in embodiments using “thinner” yarns.
  • Composite materials of the present invention may be used to manufacture garments according to another embodiment of the present invention. The garments may be, for example, vests, jackets, pads, braces, etc. The materials may also be used to enhance objects such as cars, briefcases, backpacks, etc.
  • The present invention may be embodied as a method 100 of manufacturing a composite material such as those materials described above. The method 100 comprises the step of applying 103 an elastomer coating to a first side of a compound fabric. The elastomer coating may be applied 103 in any way known in the art, such as, for example, spraying, rolling, pouring, spreading, brushing, or any combination of techniques. For example, the elastomer may be poured on to the compound fabric and the spread using a squeegee-type device. Such techniques may also cause the elastomer material to impregnate the fabric.
  • The method 100 comprises the step of curing 106 the elastomer coating. Curing 106 may be accomplished by, for example, simply allowing time for the elastomer material to cure (e.g., cross-link). Curing 106 may be accomplished using other common techniques, including, for example, heating the elastomer. In this way, curing 106 the elastomer coating may be accomplished by passing the composite material (with elastomer in an uncured state), through a heater, such as an oven.
  • The method 100 may comprise the step of applying 109 an elastomer coating to the second side of the compound fabric. This step of applying 109 to the second side may be accomplished before or after curing 106 the elastomer coating of the first side.
  • In another embodiment of a method of manufacturing, an elastomer may be provided in sheet form (such as on a roll). In this way, manufacturing a composite material comprises bonding a sheet of elastomer material to a compound fabric. Bonding may be accomplished using an interface, such as an adhesive, by heating the elastomer sheet, or by other techniques known in the art.
  • The present invention may also be embodied as a method 200 of manufacturing a multi-layer ballistic fabric. The method comprises the step of weaving 202 a first ballistic woven layer having a first weave pattern and a second ballistic woven layer having a second weave pattern. For example, the first woven layer can be a plain weave, and the second layer can be a sateen, such as a crowfoot weave. The weave pattern of the second layer may be selected with a weave having good ballistic performance characteristics but may have less desirable physical characteristics. For example, sateens with high ratios of floats may lack integrity such that the yarns may spread easily and come apart at the edges of fabrics.
  • The first ballistic layer and second ballistic layer may be woven 202 such that the first layer stabilizes the second layer, thereby holding the second layer together. The first layer and second layer may be tacked together by one or more weft yarns of the first layer with a pick of the second layer and/or one or more weft yarns of the second layer with a pick of the first layer. In this manner, the negative effects of using a sateen layer (e.g., the layer becoming unstable, losing its shape, and/or becoming unworkable) are decreased. Consequently, weaving a sateen ballistic layer to a plain weave ballistic layer can produce synergistic results. Similarly, a plain weave may “open up” (spread apart upon impact of a projectile) in a characteristic way (along force vectors) which is different from the way in which a twill weave opens up. By combining, for example, two different weaves into a double-layer fabric, the integrity of the weave structure of each layer may be increased without adding a significant amount of rigidity.
  • The method 200 may also include the step of applying 204 an elastomer coating to a first side of the woven multi-layer fabric. Alternatively, the step of applying an elastomer layer can be omitted, and the multi-layer fabric may be manufactured 206 into a garment.
  • Although the present invention has been described with respect to one or more particular embodiments, it will be understood that these embodiments are intended to be exemplary and that other embodiments of the present invention may be made without departing from the spirit and scope of the present invention.

Claims (14)

We claim:
1. A method of making a composite ballistic fabric, comprising the steps of:
weaving a multi-layer fabric from a plurality of warp yarns and plurality of weft yarns, the double-layer fabric comprising a first layer having a first weave pattern and a second layer having a second weave pattern which is different than the first weave pattern, the first and second layers being joined to each other by picking one or more warp yarns of the second layer using a plurality of weft yarns from the first layer and/or picking one or more warp yarns of the first layer using a plurality of weft yarns from the second layer to form the composite ballistic fabric.
2. The method of claim 1, wherein the first layer is a plain weave pattern.
3. The method of claim 2, wherein the second layer is a sateen weave pattern.
4. The method of claim 3, wherein the sateen weave pattern is a crowfoot weave.
5. The method of claim 1, wherein the first weave pattern is configured to distribute the impact of a projectile along force vectors differently than the second weave pattern.
6. The method of claim 1, further comprising the step of applying an elastomer coating to a first side of the composite ballistic fabric.
7. The method of claim 1, further comprising the step of manufacturing the composite ballistic fabric into an article of clothing or a portion thereof without applying an elastomer coating to the composite ballistic fabric.
8. A composite ballistic fabric, comprising:
a first woven layer having a first weave pattern interconnected with a second woven layer having a second weave pattern;
wherein the second weave pattern is a different weave pattern than the first weave pattern.
9. The composite ballistic fabric of claim 8, wherein the first woven layer has a plain weave pattern.
10. The composite ballistic fabric of claim 9, wherein the second woven layer has a sateen weave pattern.
11. The composite ballistic fabric of claim 10, wherein the sateen weave pattern is a crowfoot weave.
12. The composite ballistic fabric of claim 8, wherein the first weave pattern is configured to distribute the impact of a projectile along force vectors differently than the second weave pattern.
13. The composite ballistic fabric of claim 8, further comprising an elastomer coating disposed on a first side of the composite ballistic fabric.
14. The composite ballistic fabric of claim 8, wherein the composite ballistic fabric does not include an elastomer coating.
US13/802,900 2011-11-08 2013-03-14 Ballistic Composite Materials, Ballistic Fabrics, and Methods of Making Abandoned US20140065907A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US13/802,900 US20140065907A1 (en) 2011-11-08 2013-03-14 Ballistic Composite Materials, Ballistic Fabrics, and Methods of Making

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201161557006P 2011-11-08 2011-11-08
US13/672,316 US20130111640A1 (en) 2011-11-08 2012-11-08 Ballistic Composite Materials and Methods of Making
US13/802,900 US20140065907A1 (en) 2011-11-08 2013-03-14 Ballistic Composite Materials, Ballistic Fabrics, and Methods of Making

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US13/672,316 Continuation-In-Part US20130111640A1 (en) 2011-11-08 2012-11-08 Ballistic Composite Materials and Methods of Making

Publications (1)

Publication Number Publication Date
US20140065907A1 true US20140065907A1 (en) 2014-03-06

Family

ID=50188171

Family Applications (1)

Application Number Title Priority Date Filing Date
US13/802,900 Abandoned US20140065907A1 (en) 2011-11-08 2013-03-14 Ballistic Composite Materials, Ballistic Fabrics, and Methods of Making

Country Status (1)

Country Link
US (1) US20140065907A1 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130111640A1 (en) * 2011-11-08 2013-05-09 Lincoln Fabrics Limited Ballistic Composite Materials and Methods of Making
WO2017116649A1 (en) 2015-12-31 2017-07-06 Tex Tech Industries, Inc. Ballistic materials incorporating spunlaced nonwovens
WO2019074651A1 (en) * 2017-10-11 2019-04-18 Vf Jeanswear, L.P. Multilayer and multifunctional woven fabrics and methods of making the same
US10302401B2 (en) 2013-03-15 2019-05-28 Scott R. Whitaker Ballistic shield
US10458756B2 (en) 2013-03-15 2019-10-29 Scott R. Whitaker Flexible adhesive ballistic shield
CN114717714A (en) * 2022-04-29 2022-07-08 河北普凡防护科技有限公司 Weaving method of bulletproof woven fabric
US11585639B1 (en) 2019-02-08 2023-02-21 The United States Of America, As Represented By The Secretary Of The Navy Personal armor resistant to sharp or pointed weaponry

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110162516A1 (en) * 2010-01-05 2011-07-07 Raytheon Company Method of Layering Composite Sheets to Improve Armor Capabilities
US20130090029A1 (en) * 2011-10-07 2013-04-11 Matscitechno Licensing Company Impact dissipating fabric
US20130111640A1 (en) * 2011-11-08 2013-05-09 Lincoln Fabrics Limited Ballistic Composite Materials and Methods of Making

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110162516A1 (en) * 2010-01-05 2011-07-07 Raytheon Company Method of Layering Composite Sheets to Improve Armor Capabilities
US20130090029A1 (en) * 2011-10-07 2013-04-11 Matscitechno Licensing Company Impact dissipating fabric
US20130111640A1 (en) * 2011-11-08 2013-05-09 Lincoln Fabrics Limited Ballistic Composite Materials and Methods of Making

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130111640A1 (en) * 2011-11-08 2013-05-09 Lincoln Fabrics Limited Ballistic Composite Materials and Methods of Making
US10302401B2 (en) 2013-03-15 2019-05-28 Scott R. Whitaker Ballistic shield
US10458756B2 (en) 2013-03-15 2019-10-29 Scott R. Whitaker Flexible adhesive ballistic shield
WO2017116649A1 (en) 2015-12-31 2017-07-06 Tex Tech Industries, Inc. Ballistic materials incorporating spunlaced nonwovens
EP3974174A1 (en) 2015-12-31 2022-03-30 DuPont Safety & Construction, Inc. Ballistic material incorporating spunlaced nonwovens
US11300386B2 (en) 2015-12-31 2022-04-12 Dupont Safety & Construction, Inc. Ballistic materials incorporating spunlaced nonwovens
WO2019074651A1 (en) * 2017-10-11 2019-04-18 Vf Jeanswear, L.P. Multilayer and multifunctional woven fabrics and methods of making the same
CN111542428A (en) * 2017-10-11 2020-08-14 Vf牛仔装公司 Multi-layer and multi-functional woven fabric and method of making same
US11585639B1 (en) 2019-02-08 2023-02-21 The United States Of America, As Represented By The Secretary Of The Navy Personal armor resistant to sharp or pointed weaponry
US11852444B1 (en) * 2019-02-08 2023-12-26 The United States Of America, As Represented By The Secretary Of The Navy Personal armor resistant to pointed or sharp weaponry
CN114717714A (en) * 2022-04-29 2022-07-08 河北普凡防护科技有限公司 Weaving method of bulletproof woven fabric

Similar Documents

Publication Publication Date Title
US20140065907A1 (en) Ballistic Composite Materials, Ballistic Fabrics, and Methods of Making
US20130111640A1 (en) Ballistic Composite Materials and Methods of Making
RU2668488C2 (en) Bulletproof material (options), which unites woven or non-woven composites
ES2529338T3 (en) Bulletproof fibrous composite material and method for its production
CN105452551B (en) Bullet resistant material
ES2709113T3 (en) Unidirectional hybrid fiber tape and composite laminates
JP4243559B2 (en) Bulletproof panel and bulletproof vest
DE60327760D1 (en) BALLISTIC TEXTILE COMPOSITE
US10081159B2 (en) Materials gradient within armor for balancing the ballistic performance
CA2710526A1 (en) Fabric architectures for improved ballistic impact performance
CN105555519A (en) Material for ballistic protection, method of preparation and use thereof
US20140137726A1 (en) Spall liners in combination with blast mitigation materials for vehicles
KR20120027250A (en) Improved ballistic composites having large denier per filament high performance yarns
WO2010042260A2 (en) Vacuum sealed protective cover for ballistic panel
JP2013538326A (en) Flexible body protection vest with chest plate
US20130071642A1 (en) Fabric assembly suitable for resisting ballistic objects and method of manufacture
JP4691159B2 (en) Fabric with increased bulletproof performance coated with polymer stripes
WO2016116774A1 (en) Ballistic resistant article and method of producing same
KR20140133522A (en) High density unidirectional fabric for soft ballistics applications
KR102181940B1 (en) Body armor using a hybrid laminated pattern of a bulletproof fabric sheet and a carbon nanotube sheet
US20150266266A1 (en) Composite fabrics and methods of making same
KR20120092933A (en) Fabric layer for bulletproof clothes
US20130068088A1 (en) Fabric assembly suitable for resisting ballistic objects and method of manufacture
KR101589786B1 (en) Bulletproof Material
KR102493274B1 (en) Ballistic laminates comprising textile elements in which ballistic threads intersect with non-ballistic threads.

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION