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US20160161223A1 - Impact protective multi-layered fabric - Google Patents

Impact protective multi-layered fabric Download PDF

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Publication number
US20160161223A1
US20160161223A1 US14/963,535 US201514963535A US2016161223A1 US 20160161223 A1 US20160161223 A1 US 20160161223A1 US 201514963535 A US201514963535 A US 201514963535A US 2016161223 A1 US2016161223 A1 US 2016161223A1
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US
United States
Prior art keywords
closed
layer
layers
fabric
folds
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
US14/963,535
Inventor
Javier Toral Vazques
Pablo GOYA ABAURREA
Esteban Martino Gonzalez
Diego Folch Cortes
Vasilis Votsios
Michel Fouinnetau
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SL
Airbus Operations SAS
Original Assignee
Airbus Operations SL
Airbus Operations SAS
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
Application filed by Airbus Operations SL, Airbus Operations SAS filed Critical Airbus Operations SL
Publication of US20160161223A1 publication Critical patent/US20160161223A1/en
Abandoned legal-status Critical Current

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    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00Woven fabrics designed to make specified articles
    • 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
    • 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
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D13/00Woven fabrics characterised by the special disposition of the warp or weft threads, e.g. with curved weft threads, with discontinuous warp threads, with diagonal warp or weft
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used

Definitions

  • the present disclosure refers to impact absorbing woven fabrics for impact protection or ballistic applications.
  • An object of the present disclosure is to increase the impact energy absorption capability of a dry-fabric material, namely a textile material, without increasing the weight of the same.
  • two distinct groups of yarns are interwoven with each other, generally warp yarns run length-wise and weft yarns runs transversally to the warp yarns.
  • two or more layers of woven fabric are bonded together to produce a multi-layer structure, for example various layers may be layered up and then joined together by a resin.
  • multiple layers of woven fabric are stacked and then stitched together.
  • the layers can be stacked without any resin, and in the case of ballistic protection for vehicles (hard protection), the layers can be bonded together with a resin.
  • FIG. 1 The behaviour of dry-fabrics when impacted is shown in FIG. 1 .
  • the impact pushes the layer ( 1 ) out of plane ( FIG. 1A ) and they react as a membrane absorbing the impact load in tension.
  • the layer ( 1 ) breaks when the absorbed energy (Eabs 1 ) reaches the ultimate tensile strength absorbing energy (a max) and decelerating the impactor ( 2 ) ( FIG. 1B ).
  • the disclosure improves the energy absorption capability of dry fabrics, by folding a fabric layer to form one or more folds or loops (in a cross-sectional view), and by stitching the loops, such as, when the fabric layer receives an impact, the fold would open or deploy and the stitches would break sequentially, thereby absorbing impact energy.
  • One aspect of the disclosure refers to a fabric structure capable of providing protection against impacts, wherein the fabric structure is formed by a plurality of woven layers of a dry-fabric material, placed on top of each to form a pile or stack of layers.
  • the disclosure is characterized in that at least one of the layers of the pile of layers is conformed such as the layer forms at least one closed fold in the form of a pocket, which extends longitudinally across the layer, for example extending from one edge of the layer to the opposite edge.
  • a dry-fabric is a textile material without resin, that is, a material formed by fibers grouped to form strings, wherein these strings are interlaced.
  • the pocket-like fold of that layer has first and second walls placed one in front of the other, and these two walls are stitched to each other by means of at least one yarn or thread of a dry-fabric material. These two walls are stitched in the entire extension or at least a major part of the extension of the closed fold.
  • first and second walls of the closed fold are stitched to each other by means of several stitching lines, such as each stitching line extends along the closed fold, that is, each stitching line is placed according to the longitudinal direction of the closed fold.
  • the stitching lines within the same closed fold are arranged one above the other.
  • the plurality of layers forming the same would expand such as the fold would the forced to unfold or deploy, and the stitching lines would break sequentially, from the one closer to the entrance of the fold towards the one closer to the bottom of the same.
  • the fabric of the disclosure can be used for protecting a part of an aircraft against engine debris, from intermediate to high speed impacts, especially for protecting an aircraft fuselage in the case of an Open Rotor aircrafts, against accidental blade release threats.
  • the disclosure can also be applicable for engine debris protections of any type of engine (Turbofan, Turboprop, gas generator, etc.) and even other more classical (low speed) impact threats, even for ballistic protections for personal or material shielding.
  • FIGS 1A and 1B show the behavior of a conventional dry-fabric material during the impact of an object.
  • Figure lA shows the elastic deformation (represented by arrows) of a dry-fabric layer due to the impact
  • FIG. 1B is a graph representing the impact energy absorption dynamic, wherein a is the energy absorbed by the fabric layer shown in the figure.
  • FIGS. 2A and 2B show a similar representation than FIGS. 1A and 1B but corresponding to a fabric layer according to the disclosure.
  • FIGS. 3A and 3B show a schematic representation of a portion of a fabric layer according to the disclosure, wherein FIG. 3A is a perspective view of the portion, and FIG. 3B is a side elevational view.
  • FIGS. 4A and 4B show a schematic representation in a cross-sectional view, of two alternatives of a multi-layered fabric structure according to the disclosure.
  • FIG. 2A shows a dry-fabric layer ( 1 ) for impact protection conformed to have at least one closed fold ( 3 ), obtained by folding the layer ( 1 ) along a folding (straight) line ( 4 ) across the layer, such as the major part of the layer ( 1 ) remains substantially flat and at least one closed fold ( 3 ) in the form of a channel or pocket is formed in the layer, having first and second walls ( 5 , 6 ) substantially facing each other.
  • Each closed fold ( 3 ) extends across the layer ( 1 ) in a longitudinal direction from one edge to the other edge ( 1 ′, 1 ′′) of the layer. Furthermore, the first and second walls ( 5 , 6 ) of each closed fold ( 3 ), are stitched to each other by means of one or more yarns ( 7 ) made of a dry-fabric material, that is, a textile material . First and second walls ( 5 , 6 ) are in contact with each other due to the stitching, although in the Figures are shown spaced apart from each other for the sake of clarity of the illustration.
  • the stitching is designed in a way that the stitches would break sequentially, that is, one after the other, until the stress in the layer archives its maximum tensile strength.
  • the first and second walls ( 5 , 6 ) of the closed fold ( 3 ) are stitched to each other by means of two or more stitching lines ( 8 ), each stitching line extending along the closed fold and in major part of the length of the same, and wherein the stitching lines ( 8 ) are arranged one above the other.
  • each stitching line ( 8 ) is lying on an imaginary plane, and all the planes are parallel to each other.
  • the energy absorption capability of the layer of the disclosure (Eabs 2 ) is increased with respect to the prior art (Eabs 1 ), as it observed in the graph of FIG. 2B compared with the graph of FIG. 1B , such as (Eabs 2 )>>(Eabs 1 ).
  • the graph of FIG. 1B has a serrated shape, wherein each peak corresponds to the energy absorbed by one stitching line ( 8 ).
  • This configuration of the dry fabric layer according to the disclosure improve the protection performance of any dry fabric of the prior art in a very simple manner and more importantly, without increasing its weight.
  • a pile or stack of fabric layers ( 1 a , 1 b , 1 c ) are provided forming a multi-layered structure ( 9 ) as shown in FIGS. 4A and 4B , wherein all the layers ( 1 a , 1 b , 1 c ) of the structure or only some of them are provided with closed folds ( 3 ).
  • At least one of the layers ( 1 a , 1 b , 1 c ) comprises two or more closed folds ( 3 ), each closed fold extends longitudinally across the layer in which there are formed, and wherein the two or more closed folds are arranged substantially parallel to each other. All the folds of the multi-layered structure ( 9 ) are arranged in the same longitudinal direction.
  • any possible relative position between closed folds ( 3 ) of different layers is possible.
  • the closed folds ( 3 ) of different layers ( 1 a , 1 b , 1 c ) are arranged right one above the other and are aligned in groups defining a grid-like pattern.
  • the closed folds ( 3 ) of different layers ( 1 a , 1 b , 1 c ) are interleaved.
  • the closed folds ( 3 ) are bended such as the first and second walls ( 5 , 6 ) of each closed fold, are substantially parallel with the layer ( 1 a , 1 b , 1 c ) in which they are formed.
  • the first and second walls ( 5 , 6 ) the closed folds ( 3 ) are substantially perpendicular or straight to the layer ( 1 a , 1 b , 1 c ) in which they are formed.
  • the layers are in contact which each other, however, in other cases ( FIG. 4B ), there may be a gap or space between adjacent layers, such as adjacent layers are not in contact directly with each other, in order to allow the closed folds to deploy easily without adjacent layers rubbing with each other.
  • the layers of the pile of layers may be joined together by means of stitches provided a specific position of the pile, as to maintain the pile together, however, those stitches would not provide resistance to impacts.
  • Preferred materials for the woven fabric are:
  • Preferred materials for the stitching yarn are:

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Ceramic Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Professional, Industrial, Or Sporting Protective Garments (AREA)
  • Laminated Bodies (AREA)
  • Woven Fabrics (AREA)

Abstract

The disclosure refers to an impact protective multi-layered fabric comprising a pile of layers of a dry-fabric material, wherein at least one of the layers is conformed to have least one closed fold extending longitudinally across the layer, the closed fold having first and second walls substantially facing each other, and wherein the first and second walls are stitched to each other by means of at least one yarn of a dry-fabric material. According to an aspect, the first and second walls of the closed fold, are stitched to each other by means of two or more stitching lines are arranged one above the other within the closed fold, such as when an object impact on the fabric layer, the stitches of the stitching lines break sequentially one after the other, such the energy absorption capability of the layer is increased in a simple manner and without increasing its weight.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • The present application claims priority to European Application No. 14382500.8 filed on Dec. 9, 2014, which is hereby incorporated by reference, as though set forth fully herein.
  • FIELD OF DISCLOSURE
  • The present disclosure refers to impact absorbing woven fabrics for impact protection or ballistic applications.
  • An object of the present disclosure is to increase the impact energy absorption capability of a dry-fabric material, namely a textile material, without increasing the weight of the same.
  • BACKGROUND OF THE DISCLOSURE
  • To form woven fabrics, two distinct groups of yarns are interwoven with each other, generally warp yarns run length-wise and weft yarns runs transversally to the warp yarns. For some ballistic applications, two or more layers of woven fabric are bonded together to produce a multi-layer structure, for example various layers may be layered up and then joined together by a resin. In other types of fabrics, multiple layers of woven fabric are stacked and then stitched together.
  • In the case of a bullet-proof jackets (soft protection), the layers can be stacked without any resin, and in the case of ballistic protection for vehicles (hard protection), the layers can be bonded together with a resin.
  • The most widespread type of fabric used in the field of impact protections, in particular for intermediate and high speed impacts including ballistic protection, are dry-fabrics (Aramid i.e. Kevlar ®, Ultra High Molecular Weight Poly Ethylene, PBO, etc.). The architecture of these protections consists typically in a stack of layers, each of them being 2D woven layers.
  • The behaviour of dry-fabrics when impacted is shown in FIG. 1. The impact pushes the layer (1) out of plane (FIG. 1A) and they react as a membrane absorbing the impact load in tension. The layer (1) breaks when the absorbed energy (Eabs1) reaches the ultimate tensile strength absorbing energy (a max) and decelerating the impactor (2) (FIG. 1B).
  • It is always desirable to increase the capability of this type of fabrics to absorb impact energy, but without increasing the weight of the material.
  • SUMMARY OF THE DISCLOSURE
  • The disclosure improves the energy absorption capability of dry fabrics, by folding a fabric layer to form one or more folds or loops (in a cross-sectional view), and by stitching the loops, such as, when the fabric layer receives an impact, the fold would open or deploy and the stitches would break sequentially, thereby absorbing impact energy.
  • One aspect of the disclosure refers to a fabric structure capable of providing protection against impacts, wherein the fabric structure is formed by a plurality of woven layers of a dry-fabric material, placed on top of each to form a pile or stack of layers. The disclosure is characterized in that at least one of the layers of the pile of layers is conformed such as the layer forms at least one closed fold in the form of a pocket, which extends longitudinally across the layer, for example extending from one edge of the layer to the opposite edge.
  • A dry-fabric is a textile material without resin, that is, a material formed by fibers grouped to form strings, wherein these strings are interlaced.
  • The pocket-like fold of that layer, has first and second walls placed one in front of the other, and these two walls are stitched to each other by means of at least one yarn or thread of a dry-fabric material. These two walls are stitched in the entire extension or at least a major part of the extension of the closed fold.
  • According to an aspect, first and second walls of the closed fold, are stitched to each other by means of several stitching lines, such as each stitching line extends along the closed fold, that is, each stitching line is placed according to the longitudinal direction of the closed fold. The stitching lines within the same closed fold are arranged one above the other.
  • Due to the provision of the folds in the fabric layer, and the way the folds are stitched by means of several stitching lines one above the other, when an object impact on the fabric, the plurality of layers forming the same would expand such as the fold would the forced to unfold or deploy, and the stitching lines would break sequentially, from the one closer to the entrance of the fold towards the one closer to the bottom of the same.
  • In this way, the impact energy absorption capability of a conventional dry-fabric material is improved in a very simple manner, and without significantly increasing the weight of the same, since the only component added with respect to a prior art fabric, are the yarns for stitching the folds, but the weight of these yarns is not significant.
  • The fabric of the disclosure can be used for protecting a part of an aircraft against engine debris, from intermediate to high speed impacts, especially for protecting an aircraft fuselage in the case of an Open Rotor aircrafts, against accidental blade release threats.
  • The disclosure can also be applicable for engine debris protections of any type of engine (Turbofan, Turboprop, gas generator, etc.) and even other more classical (low speed) impact threats, even for ballistic protections for personal or material shielding.
  • BRIEF DESCRIPTION OF THE FIGURES
  • Aspects of the present disclosure are henceforth described with reference to the accompanying Figures, in which:
  • FIGS 1A and 1B show the behavior of a conventional dry-fabric material during the impact of an object. Figure lA shows the elastic deformation (represented by arrows) of a dry-fabric layer due to the impact, and FIG. 1B is a graph representing the impact energy absorption dynamic, wherein a is the energy absorbed by the fabric layer shown in the figure.
  • FIGS. 2A and 2B show a similar representation than FIGS. 1A and 1B but corresponding to a fabric layer according to the disclosure.
  • FIGS. 3A and 3B show a schematic representation of a portion of a fabric layer according to the disclosure, wherein FIG. 3A is a perspective view of the portion, and FIG. 3B is a side elevational view.
  • FIGS. 4A and 4B show a schematic representation in a cross-sectional view, of two alternatives of a multi-layered fabric structure according to the disclosure.
  • DETAILED DESCRIPTION OF THE PRESENT DISCLOSURE
  • FIG. 2A shows a dry-fabric layer (1) for impact protection conformed to have at least one closed fold (3), obtained by folding the layer (1) along a folding (straight) line (4) across the layer, such as the major part of the layer (1) remains substantially flat and at least one closed fold (3) in the form of a channel or pocket is formed in the layer, having first and second walls (5,6) substantially facing each other.
  • Each closed fold (3) extends across the layer (1) in a longitudinal direction from one edge to the other edge (1′, 1″) of the layer. Furthermore, the first and second walls (5,6) of each closed fold (3), are stitched to each other by means of one or more yarns (7) made of a dry-fabric material, that is, a textile material . First and second walls (5, 6) are in contact with each other due to the stitching, although in the Figures are shown spaced apart from each other for the sake of clarity of the illustration.
  • The stitching is designed in a way that the stitches would break sequentially, that is, one after the other, until the stress in the layer archives its maximum tensile strength. Preferably, as shown in FIGS. 3A and 3B, the first and second walls (5, 6) of the closed fold (3), are stitched to each other by means of two or more stitching lines (8), each stitching line extending along the closed fold and in major part of the length of the same, and wherein the stitching lines (8) are arranged one above the other.
  • This arrangement of the stitching lines (8) can be seen more clearly in FIG. 3B, wherein it can be seen that each stitching line (8) is lying on an imaginary plane, and all the planes are parallel to each other.
  • When an object (2) impact the layer (1), this is expanded by the impact energy as illustrated by arrows in FIG. 2A, such as the closed fold (3) opens and the stitches would break sequentially, that is, first the stitches of stitching line (8) closer to the major part of the layer (1) would break, then the stitches of the second stitching line (8), then thirds, and so on until the stitches of the stitching line (8) closer to the bottom of the closed fold (3) are broken. After all the stitches are broken, the layer (1) would absorb more energy conventionally as explained previously with respect to FIG. 1A.
  • In this way, the energy absorption capability of the layer of the disclosure (Eabs2) is increased with respect to the prior art (Eabs1), as it observed in the graph of FIG. 2B compared with the graph of FIG. 1B, such as (Eabs2)>>(Eabs1). The graph of FIG. 1B has a serrated shape, wherein each peak corresponds to the energy absorbed by one stitching line (8).
  • This configuration of the dry fabric layer according to the disclosure, improve the protection performance of any dry fabric of the prior art in a very simple manner and more importantly, without increasing its weight.
  • According to an aspect, a pile or stack of fabric layers (1 a, 1 b, 1 c) are provided forming a multi-layered structure (9) as shown in FIGS. 4A and 4B, wherein all the layers (1 a, 1 b, 1 c) of the structure or only some of them are provided with closed folds (3). At least one of the layers (1 a, 1 b, 1 c) comprises two or more closed folds (3), each closed fold extends longitudinally across the layer in which there are formed, and wherein the two or more closed folds are arranged substantially parallel to each other. All the folds of the multi-layered structure (9) are arranged in the same longitudinal direction.
  • Any possible relative position between closed folds (3) of different layers, is possible. In the embodiment of FIG. 4B, the closed folds (3) of different layers (1 a, 1 b, 1 c) are arranged right one above the other and are aligned in groups defining a grid-like pattern. In the embodiment of FIG. 4A, the closed folds (3) of different layers (1 a, 1 b, 1 c) are interleaved.
  • In some preferred embodiments, as the one shown in FIG. 4A, the closed folds (3) are bended such as the first and second walls (5, 6) of each closed fold, are substantially parallel with the layer (1 a, 1 b, 1 c) in which they are formed. Alternatively, as shown in FIG. 4B, the first and second walls (5, 6) the closed folds (3) are substantially perpendicular or straight to the layer (1 a, 1 b, 1 c) in which they are formed.
  • In some cases, as the one shown in FIG. 4A, the layers are in contact which each other, however, in other cases (FIG. 4B), there may be a gap or space between adjacent layers, such as adjacent layers are not in contact directly with each other, in order to allow the closed folds to deploy easily without adjacent layers rubbing with each other.
  • The layers of the pile of layers may be joined together by means of stitches provided a specific position of the pile, as to maintain the pile together, however, those stitches would not provide resistance to impacts.
  • Other preferred embodiments of the disclosure, include any combination of the above-mentioned features, namely bended and/or perpendicular closed folds, and/or interleaved or grip-like closed folds distribution.
  • Preferred materials for the woven fabric are:
      • Aramida, commercially available as: Kevlar®, Twaron®,
      • Ultra-High Molecular Weight Polyethylene, commercially available as: Dyneema®, Spectra®
      • glass fiber
      • P-phenylene-2, 6-benzobisoxazole, commercially available as: Zylon®.
  • Preferred materials for the stitching yarn are:
      • Aramida fiber
      • Glass fiber
      • Ultra-High Molecular Weight Polyethylene, commercially available as: Dyneema®, Spectra®.
  • Other preferred embodiments of the present disclosure are described in the appended dependent claims and the multiple combinations of these claims.

Claims (7)

What is claimed:
1. An impact protective multi-layered fabric, comprising:
a pile of layers of a textile material, wherein at least one of said layers is conformed to have at least one closed fold extending longitudinally across the layer, wherein said closed fold has a first wall and a second wall substantially facing each other, and wherein said first wall and said second wall are stitched to each other by means of at least one yarn of a textile material.
2. The impact protective multi-layered fabric of claim 1, wherein the first and second walls of the closed fold are stitched to each other by means of at least two stitching lines, wherein each stitching line extends along the closed fold and in major part of the length of the same, and wherein said stitching lines are arranged one above the other.
3. The impact protective multi-layered fabric of claim 1, wherein said at least one layer has at least two closed folds, wherein each closed fold extends longitudinally across the layer, and wherein the at least two closed folds are arranged substantially parallel to each other.
4. The impact protective multi-layered fabric of claim 1, further comprising:
at least two layers with at least two closed folds, and wherein the closed folds of different layers are arranged one above the other and are aligned.
5. The impact protective multi-layered fabric of claim 1, further comprising:
at least two layers with at least two closed folds, and wherein the closed folds of different layers are interleaved.
6. The impact protective multi-layered fabric of claim 4, wherein the at least two closed folds are bended such as the first and second walls of each closed fold, are substantially parallel with the layer in which they are formed.
7. The impact protective multi-layered fabric of claim 4, wherein the at least two closed folds are substantially perpendicular to the layer in which they are formed.
US14/963,535 2014-12-09 2015-12-09 Impact protective multi-layered fabric Abandoned US20160161223A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP14382500.8 2014-12-09
EP14382500.8A EP3032210B1 (en) 2014-12-09 2014-12-09 Impact protective multi-layered fabric

Publications (1)

Publication Number Publication Date
US20160161223A1 true US20160161223A1 (en) 2016-06-09

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EP (1) EP3032210B1 (en)
CN (1) CN105696144B (en)
ES (1) ES2650377T3 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3519529A (en) * 1967-02-13 1970-07-07 Goodyear Aerospace Corp Puncture resistant laminate with crinkled film layer
DE3150725A1 (en) * 1981-12-22 1983-06-30 Horst Schmolmann Bulletproof wrinkle construction
US5723201A (en) * 1996-05-22 1998-03-03 Czetto, Jr.; Paul Penetration resistant protective armor construction
DE60033424T2 (en) * 1999-11-03 2007-11-15 Oy Oms Optomedical Systems Ltd. ELASTIC COMPOSITE STRUCTURE
ATE335982T1 (en) * 2002-02-08 2006-09-15 Teijin Twaron Gmbh STAB-PROOF AND ANTI-BALLISTIC MATERIAL AND METHOD FOR PRODUCING THE SAME
US20100313321A1 (en) * 2009-06-11 2010-12-16 Carlson Richard A Pleated ballistic package for soft body armor

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Publication number Publication date
CN105696144A (en) 2016-06-22
ES2650377T3 (en) 2018-01-18
EP3032210B1 (en) 2017-07-19
EP3032210A1 (en) 2016-06-15
CN105696144B (en) 2019-06-04

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