WO1991007632A1 - Ballistic resistant composite armor - Google Patents

Ballistic resistant composite armor Download PDF

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Publication number
WO1991007632A1
WO1991007632A1 PCT/US1990/006453 US9006453W WO9107632A1 WO 1991007632 A1 WO1991007632 A1 WO 1991007632A1 US 9006453 W US9006453 W US 9006453W WO 9107632 A1 WO9107632 A1 WO 9107632A1
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WO
WIPO (PCT)
Prior art keywords
layer
ceramic
poly
efficiency
bodies
Prior art date
Application number
PCT/US1990/006453
Other languages
English (en)
French (fr)
Inventor
Kwok W. Lem
Hong B. Chin
Young D. Kwon
Dusan C. Prevorsek
Original Assignee
Allied-Signal Inc.
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
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Application filed by Allied-Signal Inc. filed Critical Allied-Signal Inc.
Publication of WO1991007632A1 publication Critical patent/WO1991007632A1/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/18—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by an internal layer formed of separate pieces of material which are juxtaposed side-by-side
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B18/00—Layered products essentially comprising ceramics, e.g. refractory products
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00—Armour; Armour plates
    • F41H5/02—Plate construction
    • F41H5/04—Plate construction composed of more than one layer
    • F41H5/0414—Layered armour containing ceramic material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/54—Yield strength; Tensile strength
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/56—Damping, energy absorption
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2571/00—Protective equipment
    • B32B2571/02—Protective equipment defensive, e.g. armour plates or anti-ballistic clothing

Definitions

  • This invention relates to ballistic resistant composite articles. More particularly, this invention relates to such articles having improved ballistic protection and having improved multiple-hit capability.
  • Fibers conventionally used include aramid fibers such as poly (phenylenediamine terephthalamide) , graphite fibers, nylon fibers, ceramic fibers, glass fibers and the like.
  • aramid fibers such as poly (phenylenediamine terephthalamide)
  • graphite fibers such as poly (phenylenediamine terephthalamide)
  • nylon fibers such as poly (phenylenediamine terephthalamide)
  • ceramic fibers such as Kevity fibers
  • glass fibers and the like such as Kevity fibers
  • the fibers are used in a woven or knitted fabric.
  • the fibers are encapsulated or embedded in a matrix material.
  • US Patent Nos. 4,623,574 and 4,748,064 disclose a simple composite structure exhibits outstanding ballistic protection as compared to simple composites utilizing rigid matrices, the results of which are disclosed in the patents. Particularly effective are weight polyethylene and polypropylene such as disclosed in US Patent No. 4,413,110.
  • US Patent Nos. 4,737,402 and 4,613,535 disclose complex rigid composite articles having improved impact resistance which comprise a network of high strength fibers such as the ultra-high molecular weight polyethylene and polypropylene disclosed in US Patent No. 4,413,110 embedded in an elastomeric matrix material and at least one additional rigid layer on a major surface of the fibers in the matrix.
  • US Patent No. 4,836,084 discloses an armor plate composite composed of four main components, a ceramic impact layer for blunting the tip of a projectile, a sub-layer laminate of metal sheets alternating with fabrics impregnated with a viscoelastic synthetic material for absorbing the kinetic energy of the projectile by plastic deformation and a backing layer consisting of a pack of impregnated fabrics. It is disclosed that the optimum combination of the four main components gives " a high degree of protection at a limited weight per unit of surface area. Ballistic resistant armor made of ceramic tiles connected to a metal substrate exhibit certain properties which substantially reduces the multiple hit capability of the armor.
  • vibrational energy On impact of the projectile, substantial amounts of vibrational energy is produced in addition to the kinetic energy of the impact.
  • This vibrational energy can be transmitted as noise and shock, or can be transmitted to vibration sensitive areas of the armor such as to the ceramic impact layer resulting in a shattering and/or loosing of tiles.
  • This invention relates to a multilayer complex ballistic armor comprising: (a) a hard impact layer comprised of one or more ceramic bodies bound to a surface of a backing layer;
  • peripheral hard impact layer retaining means comprising an elastic material positioned about the outer periphery of said hard impact layer and in contact therewith;
  • peripheral ceramic body retaining means comprising an interconnected network comprising an elastic material positioned about the periphery of each of said ceramic bodies comprising said hard impact layer.
  • the concentrated impact energy of the projectile can be absorbed without fracture or loss of ceramic bodies surrounding the ceramic body at the point of impact and can be transmitted and distributed throughout the entire complex ballistic armor.
  • the performance of the tiles at the edges of the armor adjacent to peripheral impact layer retaining means and the performance of the portions of individual tiles adjacent to the peripheral ceramic retaining means which is relatively weak are as good as or substantially as good as the performance at the center of the armour and at the center of individual tiles.
  • FIG 1 is a view in cross-section and in side elevation of an armor plate according to this invention showing its essential elements of a ceramic impact layer, a peripheral hard impact layer retaining means, a peripheral ceramic body retaining means and a backing layer;
  • FIG 2 is a view in cross-section and side elevation of a modified embodiment of this invention depicted in Fig. 2 which includes a cover layer and a release layer.
  • FIG 3 is a view in cross-section and side elevation of a modified embodiment of this invention depicted in FIG 2 which includes vibration isolating layer.
  • the numeral 10 indicates a ballistic resistant article 10.
  • Article 10 as shown in FIG 1, comprises four main components; a ceramic impact layer 12, peripheral hard impact layer retaining means 14, peripheral ceramic body retaining means 16, and a backing layer 18.
  • a ceramic impact layer 12 is excellently suitable for blunting the tip of the projectile, particularly because the ceramic material forming layer 12 will retain its hardness and strength despite the high increase in temperature that will occur in the region struck by a projectile.
  • Ceramic impact layer 12 comprises one or more ceramic bodies 20.
  • layer 12 comprises a plurality of ceramic bodies 20, in the more preferred embodiments of the invention layer 12 comprises at least about four ceramic bodies 20 and in the most preferred embodiments , layer 12 comprises at least about nine ceramic bodies 20 with those embodiments in which the number of ceramic bodies 20 in layer 12 is at least about sixteen being the embodiment of choice.
  • Ceramic body 20 is formed of a ceramic material.
  • a "ceramic material” is an inorganic material having a hardness of at least about Brihell hardness of 25 or Mohs hardness of 2.
  • Useful ceramic materials may vary widely and include those materials normally used in the fabrication of ceramic armor which function to partially deform the initial impact surface of a projectile or cause the projectile to shatter. Illustrative of such metal and non-metal ceramic materials are those described in C.F. Liable, Ballistic Materials and Penetration Mechanics.
  • Al oxide Al oxide
  • BaO barium oxide
  • BeO beryllium oxide
  • CaO calcium oxide
  • CeO cerium oxides
  • Ce-O- and Ce0 2 chromium oxide
  • Dy_0_ dysprosium oxide
  • plutonium oxides PuO, Pu 2 0 3 and Pu0 2
  • praseodymium oxides Pr0 2 , Pr 6 0,. and Pr_0,
  • promethium oxide P ⁇ O-
  • samarium oxides SmO
  • Sm 2 0 3 scandium oxide
  • silicon dioxide Si0 2
  • strontium oxide SrO
  • tantalum oxide Ta 2 0 5
  • yerbium oxides Tb-,0 3 and Tb.O-,)
  • thorium oxide Th0 2
  • thulium oxide TiO, Ti 2 0 3 , Ti 3 0- and Ti0 2
  • uranium oxides Uo,, U g O g an ⁇ u ⁇ 3
  • vanadium oxides VO, V 2 0 3 , V0 2 and v 2 °5
  • Useful ceramic materials also include boron carbide, zirconium carbide, beryllium carbide, aluminum beride, aluminum carbide, boron carbide, barium titanate, silicon nitride, calcium titanate, tantalum carbide, graphites, tungsten; the ceramic alloys which include cordierite/MAS, lead zirconate titanate/PLZT, alumina-titanium carbide, alumina-zirconia, zirconia-cordierite/ZrMAS; the fiber reinforced ceramics and ceramic alloys; glassy ceramics; silicon carbide, aluminum carbide, titanium nitride, boron nitride, titanium carbide, titanium diboride, iron carbide, aluminum nitride, iron nitride, barium titanate, titanium niobate, boron carbide, silicon boride, as well as other useful materials.
  • Preferred materials for fabrication of ceramic body 16 in Fig. 2 are aluminum oxide, and metal and non metal nitrides
  • ceramic body 20 can vary widely depending on the use of the article.
  • ceramic body 20 can be a unitary structure composed of one ceramic material or of multilayer construction of the same material or of different ceramic materials.
  • ceramic body 20 is depicted as a cubular solid, the shape of ceramic body 20 can vary widely depending on the use of the article.
  • ceramic body 20 can be an irregularly or a regularly shaped body.
  • Illustrative of a useful ceramic body 20 are cubular, rectangular, cylindrical, and polygonal (such as triangular, pentagonal and hexagonal) shaped bodies.
  • ceramic body 20 is of cubular, rectangular or cylindrical cro ' ss- section.
  • the size (width and height) of ceramic bod -20 can also vary widely depending on the use of article 10. For example, in those instances where article 10 is intended for use in the fabrication of light ballistic resistant composites for use against light armaments, ceramic body 20 is generally smaller; conversely where article 10 is intended for use in the fabrication of heavy ballistic resistant composites for use against heavy armaments then ceramic body 20 is generally larger.
  • the embodiment 10 of FIG 1 includes peripheral ceramic body retaining means 20 between individual ceramic bodies 16 and a peripheral hard impact layer retaining means 14.
  • Peripheral ceramic body retaining means 16 and peripheral hard impact layer retaining means 14 minimizes or reduces the differeneces in ballistic resistant performance of ceramic impact layer 12 at the edges of ceramic layer 12 and ceramic bodies 20, and at the seams formed by adjacent ceramic bodies 20, which because of the segmented nature of ceramic layer 12 normally tends to be relatively weak areas, and at or about the center of ceramic bodies 20 and.ceramic layer 12 which tends to be relatively strong areas.
  • the relatively performance of the armor of this invention can be expressed as the efficiency of penetration resistance.
  • the specific energy absorption is employed to determine the difference in the penetration resistance performance (or the % efficiency of penetration resistance) at the weak areas (such as seams, edge, and corner) as compared to that for the cente of tile (strong area) .
  • the specific energy absorbed during a ballistic impact is calculated based on the areal density (AD) using the following equation:
  • V velocity of projectile which is statistically at the borderline of complete penetration (i.e. the projectile velocity which has a 50% probability of penetreating the target)
  • AD is the areal density and is the weight of armor per unit area kg/ 2.
  • the % efficiency can be calculated using the following equation:
  • SEAc is the specific energy absorption at about the center of ceramic body 20.
  • DSEA is the difference in specific energy absorption and is equal to SEA - specific energy absorption at the weak areas.
  • the % efficiency at about the seam between adjacent ceramic bodies 20 is at leaste about 80% of the % efficiency at or about the center of at least one of said adjacent ceramic bodies 20, the % efficiency at or about an edge of a ceramic body 20 is at least 70% of the % efficiency at or about the center of said ceramic body 20 and the % efficiency at or about a corner of a ceramic body 20 is at least about 60% of the % efficiency at or about the center of said ceramic body 20.
  • the % efficiency at or about a seam between adjacent ceramic bodies 20, at or about an edge of a ceramic body 20 and at or about a corner of a ceramic body 20 is at least about 95% of the % efficiency at or about the center of ceramic body 20, and in the most preferred embodiments of the invention, the % efficiency at or about a seam between adjacent ceramic bodies 20, at or about an edge of ceramic body 20 and at or about a corner of ceramic body 20 is at least about 99% of the 5 efficiency at or about the center of ceramic body 20.
  • Peripheral ceramic body retaining means 16 also allows the maximum loading of ceramic bodies 20 in segmented ceramic impact layer 12, provides optimized spacing between adjacent ceramic bodies 20; retains un-impacted ceramic bodies 20 in place upon severe impact deformation; and transmits and distributes the impact shock to the entire composite upon impact.
  • Peripheral ceramic body retaining means 16 and hard impact layer retaining means 14 are composed of an "elastic material", which may vary widely and may be metallic, semi- metallic material, an organic material and/or an inorganic material.
  • an "elastic material” is a material which is herently rigid, capable of free standing without collapsing.
  • Useful materials include high modulus thermoplastic polymeric materials such as polyamides as for example aramids, nylon 6 and nylon 66, and the like; polyesters such as poly(ethylene terephthalate) , poly(butylene terephthalate) , and the like; acetalo, polysulfones; polyethersulphones; polyacrylates, acylonitrile/butadine/ styrene copolymers, ⁇ oly(amideimide) , poly(etherethar ketones), polycarbonates; polyphenylenesulfides; polysulfides, vinylesters, polyurethanes, polyphenylene oxides; polyestercarbonates; polyesterimides and the like; ther osetting resins such as epoxy resins, phenolic resins, saturated polyesters, silicones, polyurethanes, alkyd resins, melamine and urea resins and the like; polymer alloys and blends of thermoplastics polymers and/or thermosetting resins described above
  • Useful preferred materials for fabrication of peripheral ceramic body retaining means 16 and peripheral hard impact layer retaining means 14 also include metals such as nickel, manganese, tungsten, magnesium, titanium, aluminum and steel.
  • Useful and preferred steels include carbon steels such as mild steels of grades AISI 1005 to AISI 1030, medium-carbon steels of grades AISI 1030 to AISI 1055, high-carbon steels of the grades AISI 1060 to AISI 1095, free-machining steels, low-temperature carbon steels, rail steel, and superplastic steels; high-speed steels such as tungsten steels, molybolenum steels, chromium steels, vanadium steels, and colbat steels; hot-die steels; low-alloy steels; low-expansion alloys; mold-steel; nitriding steels such as low-and medium-carbon steels with combinations of chromium and aluminum, or nickel, chromium, and aluminum; silicon steel such as transformer steel and silicon
  • Useful and preferred materials also include alloys such as manganese alloys, manganese aluminum alloy, manganese bronze alloy; nickel alloys, nickel bronze alloy, nickel cast iron alloy, nickel-chromium alloys, nickel-chromium steel alloy, nickel copper alloy, nickel-molyldenium iron alloy, nickel-molybdenum steel alloy, nickel-silver alloy, nickel-steel alloy; iron-chromium-molybdenum-cobalt steel alloy; magnesium alloys; aluminum alloys such as aluminum alloy 1000 series of commercially pure aluminum, aluminum-manganese alloys of aluminum alloy 300 series, aluminum-magnesium-manganese alloys, aluminum- magnesium alloys, aluminum-copper alloys, aluminum-silicon- magnesium alloys of 6000 series, aluminum-copper-chromium of 7000 series, aluminum casting alloys; aluminum brass alloy, and aluminum bronze.
  • alloys such as manganese alloys, manganese aluminum alloy, manganese bronze alloy; nickel alloys, nickel bronze alloy, nickel cast iron alloy, nickel-chro
  • the ceramic bodies 20 are attached to backing layer 18 which supports hard impact layer 12 peripheral hard impact layer retaining means 14 and peripheral ceramic body retaining means 16, and which provides additional ballistic protection.
  • the amount of a surface of backing layer 18 covered by ceramic bodies 20 may vary widely. In general, the greater the area percent of surface covered or surface loaded, the more effective the protection, and conversely, the lower the area percent of surface covered the less effective the protection. In the preferred embodiments of the invention, the area percent of the surface of backing layer 18 covered by ceramic bodies 20 is equal to or greater than about 95 area percent based on the total area of backing layer 18, and in the more preferred embodiments of the invention the area percent covered is equal to or greater than about 97 area percent on the aforementioned-basis. Amongst the more preferred embodiments of the invention, most preferred are those embodiments in which the area percent of the surface of backing layer 18 covered by ceramic bodies 20 is equal to or greater than about 98 or 99 area percent based on the total surface area of backing layer 18.
  • Means for attaching ceramic bodies 20 to backing layer 18 may vary widely and may include any means normally used on the art to provide this function.
  • attaching means is selected from the group consisting of flexible adhesive bonding agents.
  • flexible bonding agents provide several useful functions. For example, such agents enhance structural performance such that the compsite is capable of withstanding severe impact loads, and they enhance the retention of segmented tiles which are not at the point of impact and the retention of spall/particles created by the shattering of tiles on impact.
  • adhesive also enhance the conversion of absorbed energy into heat.
  • a "flexible adhesive” is a polymeric adhesive which exhibits a Shore A Hardness of from about 15 to 120.
  • the adhesive material is a low modulus, elastomeric material which has a tensile modulus, measured at about 23°C, of less than about 7,000 psi (41,300 kpa) .
  • the tensile modulus of the elastomeric material is less than about 5,000 psi (34,500 kpa), more preferably is less than 1,000 psi (5900 kpa) and most preferably is less than about 500 psi (3450 kpa) to provide even more improved performance.
  • the glass transition temperature (Tg) of the elastomeric material is less than about 0° C.
  • the Tg of the elastomeric material is less than about -40 °C, and more preferably is less than about -50°C.
  • the elastomeric material also has an elongation to break of at least about 5%.
  • the elongation to break of the elastomeric material is at least about 30%.
  • suitable elastomeric materials for use as a flexible adhesive are those wich have their structures, properties, and formulation together with cross-linking procedures summarized in the Encyclopedia of Polymer Science, Vol.
  • Preferred adhesives are polydienes such as polybutadiene, polychloroprene and polyisoprene; olefinic and co-polymers such as ethylene-propylene copolymers, ethylene-propylene-diene copolymers, isobutylene-isoprene copolymers, and chlorosulfonated polyethylene; natural rubber; polysulfides; polyurethane elastomers; polyacrylates; polyethers; fluoroelastomer; unsaturated polyesters; vinyl esters; alkyds; flexible epoxy; flexible polyamides; epichlorohydrin; poly vinyls; flexible, phenolics; silcone elastomers; thermoplastic elastomers; copolymers of ehtylene, polyvinyl formal, polyvinyl butyal; and poly(bis-maleimide) .
  • polydienes such as polybutadiene, polychloroprene and polyisoprene
  • Blends of any combination of one or more of the above-mentioned adhesive materials are polybutadiene, polyisoprene, natural rubber, ethylene-propylene copolymers, ethylene-propylene-diene terpolymers, polysulfides, polyurethane elastomers, chlorosulfonated polyethylene, polychloroprene, poly(isobutylene-co- isoprene) , polyacrylates, polyesters, polyethers, fluoroelastomers, unsaturated polyesters, vinyl esters, flexible epoxy, flexible nylon, silicone elastomers, copolymers of ethylene, polyvinyl formal, poly vinyl butryal. Blends of any combination of one or more of the above-mentioned adhesive materials.
  • Backing layer 18 is a rigid layer which functions to support hard ceramic impact layer 12.
  • the term "rigid" is used in the present specification and claims is intended to include structures which are free standing without collapsing which includes semi-flexible and semi-rigid structures.
  • the material employed in backing layer 18 may vary widely, and may be a metallic material, a semi-metallic material, an organic material and/or an inorganic material. Illustrative of such materials are those described in G.S. Brady and H.R. Clauser, Materials Handbook, 12th edition (1986).
  • Backing layer 18 is comprised of a ballistic resistant material which may vary widely depending on the uses of article 10, and offers additional ballistic protection.
  • Backing layer 18 can comprise a single layer or can comprise a plurality of layers of the same material or different materials. In the preferred embodiments of this invention, backing layer 18 comprises one or more rigid layers.
  • Preferred materials used in the fabrication of backing layer 18 are those materials preferred for use in the fabrication of peripheral hard impact layer retaining means 14 and peripheral ceramic body retaining means 16.
  • Such preferred materials include metals such as ni ' ckel, manganese, tungsten, magnesium, titanium, aluminum and steel and alloys such as manganese alloys, nickel alloys, and aluminum alloys which make optionally in fibrous reinforcement by inorganic fibers such as silicone carbide.
  • Such materials also include thermoplastic polymeric materials such as polycarbonates; polyether ether, polyamides, polyesters, ketones, polysulfides, polyethersulfones, polyacrylate, acrylonitrile/butadiene/ styrene copolymers, poly(amideimide) , polyphenylene- sulfides; polyurethanes, polyphenylene oxides, polyestercarbonates; polyesterimides, and the like; and thermoset resins such as epoxy resins, phenolic resins, vinyl ester resins, modified phenolic resins, unsaturated polyester, allylic resins, alkyd resins, urethanes and melamine and urea resins; polymer alloys and blends of thermoplastics and/or thermosetting resins; and interpenetrating polymer network such as those of polycyanatopolyol such as dicyanoester bisphenol A and a thermoplastic resin such as polysulfone.
  • thermoplastic polymeric materials such as polycarbonates;
  • backing layer 18 comprises one or more layers at least one of which comprises a network of high strength filaments having a tenacity of at least about 7 grams/denier, a tensile modulus of at least about 160 grams/denier and an energy-in-break of at least about 8 joules/gram in a matrix.
  • the fibers in the backing layer 18 may be arranged in networks having various configurations. For example, a plurality of filaments can be grouped together to form a twisted or untwisted yarn bundles in various alignment. In preferred embodiments of the invention, the filaments are aligned substantially parallel and unidirectionally to form a uniaxial layer in which a matrix material substantially coats the individual filaments. Two or more of these layers can be used to form a layer 18 with multiple layers of coated undirectional filaments in which each layer is rotated with respect to its adjacent layers. An example is a with the second, third, fourth and fifth layers rotate +45° ,
  • filaments used in the fabrication of layer 18 may vary widely and can be metallic filaments;, semi-metallic filaments, inorganic filaments and/or organic filaments.
  • Preferred filaments for use in the practice of this invention are those having a tenacity equal to or greater than about 10 g/d, a tensile modulus equal to or greater than about 150 g/d, and an energy-in-break equal to or greater than about 8 joules/grams.
  • Particularly preferred filaments are those having a tenacity equal to or greater than about 20 g/d, a tensile modulus equal to or greater than about 500 g/d and energy-to-break equal to or greater than about 30 joules/grams.
  • filaments of choice have a tenacity equal to or greater than about 30 g/d and the energy-to-break is equal to or greater than about 40 joules/gram.
  • useful organic filaments are those composed of aramids' (aromatic polyamides), such as poly(m-xylylene adipamide) , ⁇ oly( ⁇ -xylylene sebaca ide) , poly 2,2,2-trimethylhexamethylene terephthalamide) , poly (piperazine sebacamide), poly (metaphenylene isophthalamide) (Nomex) and poly (p-phenylene terephthalamide) (Kevlar) ; and aliphatic and cycloaliiphatic polyamides, such as the copolyamide of 30% hexamethylene diammonium isophthalate and 70% hexamethylene diammonium adipate, the copolya ide of up to 30% bis-(-amidocyclohexyl)methylene, terephthalic acid and caprolactam, polyhexamethylene adipamide (nylon 66), poly(butyrolactam) (nylon 4), poly (9-armids'
  • liquid crystalline polymers such as lyrotropic liquid crystalline polymers which include polypeptides such as poly ⁇ -benzyl L-glutamate, aromatic polyamides such as poly(l,4-benzamide), poly(chloro-l,4-phenylene terephthalamide), poly(l,4-phenylene fumaramide) , poly(chloro-l,4-phenylene fumaramide), poly(4,4'- benzanilide trans, trans-muconamide) , ⁇ oly(l,4-phenylene mesaconamide) , ⁇ oly(l,4-phenylene) (trans-1,4- cyclohexylene amide), poly(chloro-l,4-phenylene) (trans-l,4-cyclohexylene amide), poly(l,4-phenylene l,4-dimethyl-trans-l 4-cyclohexy
  • R. and R 2 are the same or different and are hydrogen,hydroxy, halogen, alkylcarbonyl, carboxy, alkoxycarbonyl, heterocycle or alkyl or aryl either unsubstituted or substituted with one or more substituents selected from the group consisting of alkoxy, cyano, hydroxy, alkyl and aryl.
  • polymers of L,B-unsaturated monomers are polymers including polystyrene, polyethylene, polypropylene, poly(l-octadence) , polyisobutylene, poly(l-pentene) , poly(2-methylstyrene) , poly(4-methylstyrene) , poly(l-hexene) , poly(l-pentene) , poly(4-methoxystrene) , poly(5-methyl-l-hexene) , poly(4-methylpentene) , poly (1-butene), polyvinyl chloride, polybutylene, polyacrylonitrile, poly(methyl pentene-1) , poly(vinyl alcohol), ⁇ oly(vinylacetate) , poly(vinyl butyral), poly(vinyl chloride), poly(vinylidene chloride), vinyl chloride-vinyl acetate chloride copolymer, ⁇ o
  • Illustrative of useful inorganic filament for use in the fabrication of backing layer 18 are those glass fibers which include quartz, magnesia alumosilicate, non-alkaline alumoborosilicate, soda borosilicate, soda silicate, soda lime-alumosilicate, lead silicate, non-alkaline lead boroalumina, non-alkaline barium boroalumina, non-alkaline zinc boroalumina, non-alkaline iron alumiosilicate, phosphate, borate, cadmium borate, alumina fibers which include "saffil" fiber n eta, delta, and theta phase form, asbestos, boron filaments, silicone carbide fibers, graphite and carbon fibers such as those derived from the carbonization of polyethylene fibers, polyvinylalcohol fibers, saras fibers, polyamide (Nomex) type fiber, nylon, polybenzi-midazole fiber, polyoxadiazole fiber, polyphene
  • backing layer 18 is fabricated from a filament network, which may include a high molecular weight polyethylene filament, a high molecular weight polypropylene filament, an aramid filament, a high molecular weight polyvinyl alcohol filament, a'high molecular weight poly ⁇ acrylonitrile filament or mixtures thereof.
  • Highly oriented polypropylene and polyethylene filaments of molecular weight at least 200,000, preferably at least one million and more preferably at least two million may be used in the fabrication of backing layer 18.
  • Such high molecular weight polyethylene and polypropylene may be formed into reasonably well oriented filaments by the techniques prescribed in the various references referred to above, and especially by the technique of US Patent Nos.
  • polypropylene is a much less crystalline material than polyethylene and contains pendant methyl groups
  • tenacity values achievable with polypropylene are generally substantially lower than the corresponding values for polyethylene. Accordingly, a suitable tenacity is at least about 8 grams/denier,with a preferred tenacity being at least about 11 grams/denier.
  • the tensile modulus for polypropylene is at least about 160 grams/denier, preferably at least about 200 grams/denier.
  • PV-OH filaments having high tensile modulus preferred for use in the fabrication of backing layer 18 are described in USP 4,440,711 to Y. Kwon et al., which is hereby incorporated by reference to the extent it is not inconsistent herewith.
  • PV-OH filament of molecular weight of at least about 200,000.
  • Particularly useful PV-OH filament should have a modulus of at least about 300 g/denier, a tenacity of at least about 7 g/denier (preferably at least about 10 g/denier, more preferably at about 14 g/denier, and most preferably at least about 17 g/denier), and an energy to break of at least about 8 joules/g.
  • PV-OH filaments having a weight average molecular weight of at least about 200,000, a tenacity of at least about 10 g/denier, a modulus of at least about 300 g/denier, and an energy to break of about 8 joules/g are more useful in producing a ballistic resistant article. PV-OH filament having such properties can be produced, for example, by the process disclosed in US Patent No. 4,599,267.
  • PAN filament for use in the fabrication of layer 18 are of molecular weight of at least about 4000,000. Particularly useful PAN filament should have a tenacity of at least about 10 g/denier and an energy-to-break of at least about 8 joule/g. PAN filament having a molecular weight of at least about 4000,000, a tenacity of at least about 15 to about 20 g/denier and an energy-to-break of at least about 8 joule/g is most useful in producing ballistics resistant articles; and such filaments are disclosed, for example, in US 4,535,027.
  • suitable aramid filaments for use in the fabrication of girdle 14 are those formed principally from aromatic polyamide are described in US Patent No. 3,671,542, which is hereby ' incorporated by reference.
  • Preferred aramid filament will have a tenacity of at least about 20 g/d, a tensile modulus of at least about 400 g/d and an energy-to-break at least about 8 joules/gram, and particularly preferred aramid filaments will have a tenacity of at least about 20 g/d, a modulus of at least about 480 g/d and an energy to break of at least about 20 joules/gram.
  • aramid filaments will have a tenacity of at least about 20 g/denier, a modulus of at least about 900 g/denier and an energy-to-break of at least about 30 joules/gram.
  • poly(phenylenediamine terephalamide) filaments produced commercially by Dupont Corporation under the
  • backing layer 18 is formed of filaments arranged in a network which can have various configurations. For example, a plurality of filaments can be grouped together to form a twisted or -untwisted yarn.
  • the filaments or yarn may be formed as a flet knitted or woven (plain, basked, sating and crow feet weaves, etc.) into a network, or formed into a network by any of a variety of conventional techniques.
  • the filaments are untwisted mono-filament yarn wherein the filaments are parallel, unidirectionally aligned.
  • the filaments may also be formed into nonwoven cloth layers by convention techniques. Wetting and adhesion of fiber to the polymer matrices, such as epoxy resins is enhanced by prior treatment of the surface of the yarn.
  • the method of surface treatment may be chemical, physical or a combination of chemical and physical actions. Examples of purely chemical treatments are used of S0 3 or chlorosulfonic acid. Examples of combined chemical and physical treatments are corona discharge treatment br ' plasma treatment using one of several commonly available machines.
  • backing layer 18 is composed by one or more layers of continuous fibers embedded in a continuous phase of matrix material which preferably substantially coats each filament contained in the bundle of filaments.
  • the manner in which the filaments are dispersed may vary widely.
  • the filaments may be aligned in a substantially parallel, unidirectional fashion, or filaments may be aligned in a multidirectional fashion, or filaments may be aligned in a multidirectional fashion with filaments at varying angles with each other.
  • filaments in each layer forming backing layer 18 are aligned in a substantially parallel, unidirectional fashion such as in a prepreg, pultruded sheet and the like.
  • the matrix material used in the formation of backing layer 18 may vary widely.
  • thermoplastic polymers such as polyesters, polyamides, polyurethanes, polyolefins, polycarbonates, polyamides, polyphenyloxides, polyurethane elastomers, polyestermides, polylactones, polyestercarbonates, polyphenylene sulfides and the like; and thermosetting resins such as epoxy resins; phenolic resins, vinyl ester resins, modified phenolic resins, unsaturated polyester, allylic resins, alkyd resins, urethanes and mela ine urea resins and the like.
  • a single material may be used as the matrix or blends can be used.
  • the matrix material is a mixture of a thermoplastic resins and a thermosetting resin.
  • the preferred thermosetting material is a vinyl ester resin and the preferred thermoplastic resin is a polyurethane.
  • the proportions of matrix to filament in backing layer 18 is not critical and may vary widely depending on a number of factors including, whether the matrix material has any ballistic-resistant properties of its own (which is generally not the case) and upon the rigidity, shape, heat resistance, wear resistance, flammability resistance and other properties desired for backing layer 18. .
  • the proportion of matrix to filament in backing layer 18 may vary from relatively small amounts where the amount of matrix is about 10% by volume of the filaments to relatively large amount where the amount of matrix is up to about 90% by volume of the filaments.
  • matrix amounts of from about 15 to about 80% by volume are employed. All volume percents are based on the total volume of backing layer 18.
  • layer 18 contains a relatively minor proportion of the matrix (e.g., about 10 to about 30% by volume of composite) , since the ballistic-resistant properties are almost entirely attributable to the filaments, and in the particularly preferred embodiments of the invention, the proportion of the matrix in backing layer 18 is from about 10 to about 30% by weight of filaments.
  • a relatively minor proportion of the matrix e.g., about 10 to about 30% by volume of composite
  • Backing layer 18 can be fabricated using conventional procedures. For example, in those embodiments of the invention where backing layer 18 is a metal, alloy or an alloy or metal containing inorganic fibrous reinforced layer 18 can be formed by conventional metal working techniques. In the most preferred embodiments of the invention in which backing layer 18 is a woven fabric composed of a polymeric material, backing layer 18 can be fabricated using conventional fabric weaving techniques of the type commonly employed for ballistic purposes such as a plain weave or a Panama weave. In those preferred embodiments of the invention in which backing layer 18 is a network of polymeric fibers in a matrix, backing layer 18 is formed by molding the combination of fibers and matrix material in the desired configurations and amounts, and then subjecting the combination to heat and pressure.
  • molding temperatures range from about 20 to about 150°C, preferably from about 80 to about 145 °C, more preferably from about 100 to about 135° C, and more preferably from about 110 to about 130°C.
  • the pressure may range from about 10 psi (69 kpa to about
  • the upper limitation of the temperature range would be about 10 to about 20 °C higher than for ECPE filament.
  • the polymeric filaments are pre-coated with the desired matrix material prior to being arranged in a network and molded into backing layer 18 as described above.
  • the coating may be applied to the filaments in a variety of ways and any method known to those of skill in the art for coating filaments may be used.
  • one method is to apply the matrix material to the stretched high modulus filaments either as a liquid, a sticky solid or particles in suspension, or as fluidized bed.
  • the matrix material may be applied as a solution or emulsion in a suitable solvent which does not adversely affect the properties of the filament at the temperature of application.
  • any liquid may be used.
  • preferred groups of solvents include water, paraffin oils, ketones, alcohols, aromatic solvents or hydrocarbon solvents or mixtures thereof, with illustrative specific solvents including paraffin oil, xylene, toluene and octane.
  • the techniques used to dissolve or disperse the matrix in the solvents will be those conventionally used for the coating of similar elastomeric materials on a variety of substrates.
  • Other techniques for applying the coating to the filaments may be used, including coating of the high modulus precursor (gel filament) before the high temperature stretching operation, either before or after removal of the solvent from the filament. The filament may then be stretched at elevated temperatures to produce the coated filaments.
  • the gel filament may be passed through a solution of the appropriate matrix material, as for example an elastomeric material dissolved in paraffin oil, or an aromatic oraliphatic solvent, under conditions to attain the desired coating. Crystallization of the polymer in the gel filament may or may not have taken place before the filament passes into the cooling solution. Alternatively, the filament may be extruded into a fluidized bed of the appropriate matrix material in powder form.
  • the proportion of coating on the coated filaments or fabrics in backing layer 18 may vary from relatively small amounts of (e.g. 1% by weight of filaments) to relatively large amounts (e.g.
  • backing layer 18 containing coated filaments should have a relatively minor proportion of coating (e.g. about 10 to about 30 percent by volume of filaments), since the ballistic-resistant properties of girdle 14 are almost entirely attributable to the filament. Nevertheless, coated filaments with higher coating contents may be employed. Generally, however, when the coating constitutes greater than about 60% (by volume of filament), the coated filament is consolidated with similar coated filaments to forma fiber layer without the use of additional matrix material.
  • the coating may be applied to a precursor material of the final filament.
  • the desired and preferred tenacity, modulus and other properties of the filament should be judged by continuing the manipulative process on the filament precursor in a manner corresponding to that employed on the coated filament precursor.
  • the coating is applied to the exerogel filament described in US Application Serial No. 572,607 of Kavesh et al.. and the coated xerogel filament is then stretched under defined temperature and stretch ratio conditions, then the filament tenacity and filament modulus values would be measured on uncoated xerogel filament which is similarly stretched.
  • each filament be substantially coated with the matrix material for the production of backing layer 18.
  • a filament is substantially coated by using any of the coating processes described above or can be substantially coated by employing any other process capable of producing a filament coated essentially to the same degree as a filament coated by the processes described heretofore (e.g., by employing known high pressure molding techniques) .
  • the filaments and networks produced therefrom are formed into “simple composites" as the precursor to preparing a more complex backing layer 18.
  • the term, "simple composite”, as used herein is intended to mean composites made up of one or more layers, each of the layers containing filaments as described above with a single major matrix material, which material may include minor proportions of other materials such as fillers, lubricants or the like as noted heretofore.
  • the proportion of matrix material to filament is variable for the simple composites, with matrix material amounts of from about 5% to about 150 vol %, by volume of the filament, representing the broad general range.
  • the filament network occupies different proportions of the total volume of the simple composite.
  • the filament network comprises at least about 30 volume percent of the simple composite.
  • the filament network comprises at least about 50 volume percent, more preferably about 70 volume percent, and most preferably at least about 75 volume percent, with the matrix occupying the remaining volume.
  • a particularly effective technique for preparing a preferred composite of this invention comprised of substantially parallel, undirectionally aligned filaments includes the steps of pulling a filament or bundles of filaments through a bath containing a solution of a matrix material preferably, an matrix material, and circumferentially winding this filament into a single sheet-like layer around and along a bundle of filaments the length of a suitable form, such as a cylinder. The solvent is then evaporated leaving a sheet-like layer of filaments embedded in a matrix that can be removed from the cylindrical form.
  • a plurality of filaments or bundles of filaments can be simultaneously pulled through the bath containing a solution or dispersion of a matrix material and laid down in closely positioned, substantially parallel relation to one another ron a suitable surface. Evaporation of the solvent leaves a sheet-like layer comprised of filaments which are coated with the matrix material and which are substantially parallel and aligned along a common filament direction.
  • the sheet is suitable for subsequent processing such as laminating to another sheet to form composites containing more than one layer.
  • a yarn-type simple composite can be produced by pulling a group of filament bundles through a dispersion or solution of the matrix material to substantially coat each of the individual filaments, and then evaporating the solvent to form the coated yarn.
  • the yarn can then, for example, be employed to form fabrics, which in turn, can be used to form more complex composite structures.
  • the coated yarn can also be processed into a simple composite by employing conventional filament winding techniques; for example, the simple composite can have coated yarn formed into overlapping filament layers.
  • the number of layers of fibers included in backing layer 18 may vary widely. In general, the greater the number of layers the greater the degree of ballistic protection provided and conversely, the lesser the number of layers the lessor the degree of ballistic protection provided.
  • backing layer 18 is a laminate in which one or more layers of filaments coated with matrix material (pre-molded if desired) are arranged in a sheet-like array and aligned parallel to one another along a common filament direction. Successive layers of such coated unidirectional filaments can be rotated with respect to the previous layer after which the laminate can be molded under heat and pressure to form the laminate.
  • a layered vibration isolating layer is the layered structure in which the second, third, fourth and fifth layer are rotated 45°, 45°, 90° and 0° with respect to the first layer, but not necessarily in that o.rder.
  • another example of such a layered layer 12 is a layered structure in which the various unidirectional layers forming girdle are aligned such that the common filament axis is adjacent layers is 0 °, 90° .
  • FIG 2 shows a variant of the embodiment of FIG 1 which is indicated at 22.
  • cover layer 24 which functions as an anti-spall layer to retain spall or particles resulting from the shattering of ceramic bodies 20 by a striking projectile and to maintain ceramic bodies 20 in position.
  • cover layer 24 consists of top cover 26 and release layer 28.
  • Top cover 26 is formed from a rigid material, as for example, the materials useful in the construction of backing layer 18.
  • metals such as steel, titanium and aluminum alloys, or of a rigid high strength polymeric composite such as a thermoplastic resin such as a polyurethane, a polyester or a polyamide, a thermo ⁇ setting resin such as epoxy, phenolic or vinyl ester resin reinforced with polymeric filaments such as aramid or extended chain polyethylene or inorganic filaments such as S-glass fibers, silicon carbide fibers, E-glass fibers, carbon fibers, boron fibers and the like.
  • Release layer 28 is formed from materials used in the fabrication of backing layer 34 which are fibrous composites comprised of a fiber network which optionally may be in a matrix in a matrix.
  • Release layer 32 functions to eliminate or to substantially reduce the strain on unhit ceramic bodies 20 in the deformation of the composites from impact by the projectile.
  • the construction of ceramic impact layer 12, peripheral hard impact layer retaining means 14 and peripheral ceramic body retaining means 16, and their materials of construction are the same as in article 10 of FIG 1.
  • FIG 3 depicts an armor plate composite 30 which differs from the armor plate 22 of FIG 2 by the inclusion of a vibration isolating layer 32, corresponding parts being referred to by like numerals.
  • Vibration isolating layer 32 minimizes the shock and vibration resulting from the impact of the projectiles which inhibits the transmission of shock and vibration to portions of ceramic impact layer 12 away from the point of impact which substantially increases the multiple hit capability of the armor.
  • vibration isolating layer 32 is composed of three superimposed constituent, essential layer 34 and two optional layers 36 and 38.
  • Optional layers 34 and 38 are thin layers of a metal or non-metal rigid material such as the materials used in the fabrication of backing layer 18 and layer 34 is one or more layers comprising a network of polymeric fibers (such as the extended chain polyethylene fibers) used in the fabrication of backing layer 18, which may be optionally and preferably in a matrix.
  • Rigid layers 42 and 44 function to improve the overall performance of vibration isolation layer 32, to improve the surface characteristics of vibration isolation layer 32, to provide a surface on which ceramic bodies 20 can be attached; and to retain dimensional stability (i.e. flatness and straightness) of the surface subject severe impact deformation.
  • constituent layer 34, 36 and 38 are bonded together with a suitable agent such as an adhesive as for example, the flexible adhesives described above for use to bond ceramic bodies 20 to backing layer 18 such as a polysulfide or an epoxy.
  • backing layer 18 is of double layer construction and includes rigid layer 40 which is formed of a metal or rigid polymeric material such as glass filled epoxy resin and ballistic resistant composite layer 42 and preferably formed from
  • cover layer 30, ceramic impact layer 12, peripheral hard impact layer retaining means 14 and peripheral ceramic body retaining means 16 and their material's of construction are the same as in composite 10 of FIG 1.
  • Complex ballistic articles of this invention have many uses.
  • such composites may be incorporated into more complex composites to provide a rigid complex composite article suitable, for example; as structural ballistic-resistant components, such as helmets, structural members of aircraft, and vehicle panels.
  • a panel consisting of a 4 by 4 checker board with square cell of dimensions of 4" (10.2 cm) by 4" (10.2 cm) by 1/2" (1.3 cm) depth was constructed.
  • the cells of the panel were divided with a 0.06" (0.15 cm) thick aluminum barrier wall. Each cell was filled with one alumina
  • the panel was constructed with Spectra composite as backing material to prevent damages of the tiles from shocks and vibrations induced by the ammunition hits.
  • the checker board was placed into a 16.25" (41.3 cm) by 16.25"
  • the multiple-hit capability of the article of EXAMPLE I was evaluated.
  • the tiles were shot by a projectile traveling at a speed around 3100 ft/sec. (945 m/sec) .
  • the remaining four (4) unhit tiles remained undamaged.
  • the location and distribution of cracks were confined in the panel composed of brittle solids at the point of impact.
  • the cracks and flaws initiated around the indentation were localized only at the point of contact loading for the tile which was hit and did not propagate in the entire panel. Spalls/particles created by the shattering of tile upon impact are retained locally around the point of impact. Visual inspection of neighboring tiles found that they were not damaged by spalls/particles created by comminution of the tiles on impact.
  • Example II was- repeated with the exception that marble tiles were used and the flexible bonding agent was replaced by inflexible vinyl ester resin.
  • One Thousand grams of a mixture of a vinyl ester resin (VE 8520 sold by Interplastics) and peroxide (Benzoate peroxide sold by Lucidol under the trade name Luperco AFR-400) and a promoter (N, N, dimetyl anilane) was poured in the mold until the article was completely covered.
  • the composition of the vinyl ester resin/peroxide/pro otor is 10/0.1/0.006. The material was cured for two hours at room temperature under pressure. The article was evaluated as in EXAMPLE II, and it exhibited multiple hit capability.
  • Example II A panel was constructed as described in Example II with the exception that no Spectra ® composite vibration and shock isolation material was used. The panel was tested following the conditions described in Example II. While the panel exhibited multiple hit capability at was not as effective as the panel of Example I. Cracks were found around the neighboring unhit tiles after the impact.
  • a panel was constructed following the procedure described in Example II with the exception that no elastic barrier wall was used. The panel was tested following the conditions described in Example II. While the panel exhibited multiple hit capability, it was not as effective as the panel of Example I. Cracks were found around the neighboring unhit tiles after the impact. Therefore, the performance at the center of tile and at the seams between adjacent tiles for another hit was not as good as in the panel of Example I.
  • a panel was constructed following the procedure described in Example I with the exception that a rigid bonding agent (thermosetting polyester resin) was used to bond the ceramic bodies to the backing layer.
  • the panel was tested following the conditions described in Example I. While the panel exhibited multiple hit capability, it was not as effective as the panel of Example I. Cracks were found around the neighboring unhit tiles after the impact. Also, some of the neighboring tiles were delaminated from the substrata. Therefore, the performance at the center of tile and at the seams ' between adjacent tiles for another hit was not as good as in the panel of Example I.
  • a panel was constructed following the procedure described in Example I with the exception that no-release material was used. The panel was tested following the conditions described in Example II. While the panel exhibited multiple hit capability, it was not as effective as the panel of Example I. Cracks were found around the neighboring unhit tiles after the impact.
  • Example II The efficiency of the penetration resistance of Example I was evaluated at the center of tile, seam, edge, and corner, following the experimental procedure described in Example II. It was found that, compared to the center of tile, he efficiency was at least 99% for the seam, adge, and corner.
  • a panel was constructed following the procedure described in Example I with the exception that no peripheral frame was used to surround the edges of the segmented layer of tiles.
  • the panel was tested following the conditions described in Examples II. The performance of the edges reduced drastically, down to about 20% of the performance at the center of the tiles. Cracks were found around the neighboring unhit tiles after the impact. Also, some of the neighboring tiles were delaminated from the substrata. Therefore, the performance at the neighboring areas of the hit for another hit was poor, and the panel did not exhibit acceptable multiple hit capability.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Laminated Bodies (AREA)
  • Numerical Control (AREA)
  • Laser Beam Processing (AREA)
PCT/US1990/006453 1989-11-13 1990-11-07 Ballistic resistant composite armor WO1991007632A1 (en)

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US43592289A 1989-11-13 1989-11-13
US435,922 1989-11-13

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WO1992020519A1 (en) * 1991-05-24 1992-11-26 Allied-Signal Inc. Flexible composites having flexing rigid panels and articles fabricated from same
US5435226A (en) * 1993-11-22 1995-07-25 Rockwell International Corp. Light armor improvement
GB2306630A (en) * 1995-10-25 1997-05-07 Denel Armouring
WO1999011997A1 (de) 1997-09-04 1999-03-11 Akzo Nobel Nv Verbundsystem für kugel- und splitterschutz
EP1128154A3 (en) * 2000-02-21 2001-11-14 Rafael Armament Development Authority Ltd. Ballistic armor panel
WO2004109216A2 (en) * 2002-10-28 2004-12-16 The Boeing Company Ballistic-resistant multilayered armor including a stitched composite reinforcement layer and method of making the same
EP1536199A1 (de) * 2003-11-25 2005-06-01 Sgl Carbon Ag Keramische ballistische Schutzschicht
WO2011101872A1 (en) 2010-02-16 2011-08-25 Tecno Drive S.R.L. Lifting device, particularly for lifting wheelchairs
WO2012063271A2 (en) 2010-11-10 2012-05-18 Petroceramics S.P.A. Antiballistic element
US8215223B2 (en) 2001-07-25 2012-07-10 Aceram Materials And Technologies Inc. Ceramic components, ceramic component systems, and ceramic armour systems
US8267001B2 (en) 2006-12-04 2012-09-18 Battelle Memorial Institute Composite armor and method for making composite armor
RU2476809C1 (ru) * 2011-08-02 2013-02-27 Закрытое акционерное общество "Научно-производственное объединение специальных материалов" Объемно-комбинированная броня
RU2517547C1 (ru) * 2013-05-24 2014-05-27 Закрытое акционерное общество "Научно-производственное объединение специальных материалов" Объемно-комбинированная броня
US8906484B1 (en) 2012-05-02 2014-12-09 The Boeing Company System of composite armor including release layers
WO2015071866A1 (en) 2013-11-14 2015-05-21 Petroceramics S.P.A. Antiballistic garment
WO2015071916A1 (en) 2013-11-14 2015-05-21 Petroceramics S.P.A. Antiballistic element
CN112729014A (zh) * 2020-12-09 2021-04-30 浙江立泰复合材料股份有限公司 一种抗多发弹密集打击复合装甲制备方法
CN114940016A (zh) * 2022-06-22 2022-08-26 中国兵器装备集团西南技术工程研究所 一种预应力三维约束防弹装甲板的制备方法

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JP5508743B2 (ja) * 2009-03-12 2014-06-04 美濃窯業株式会社 衝撃吸収部材

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FR2637063A1 (fr) * 1973-11-27 1990-03-30 Cem Comp Electro Mec Procede de realisation de plaques de blindage en ceramique et plaques obtenues par ledit procede
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WO1992020519A1 (en) * 1991-05-24 1992-11-26 Allied-Signal Inc. Flexible composites having flexing rigid panels and articles fabricated from same
US5316820A (en) * 1991-05-24 1994-05-31 Alliedsignal Inc. Flexible composites having flexing rigid panels and articles fabricated from same
US5435226A (en) * 1993-11-22 1995-07-25 Rockwell International Corp. Light armor improvement
GB2306630B (en) * 1995-10-25 2000-03-22 Denel Armour
US5905225A (en) * 1995-10-25 1999-05-18 Denel (Proprietary) Ltd. Armouring
GB2306630A (en) * 1995-10-25 1997-05-07 Denel Armouring
WO1999011997A1 (de) 1997-09-04 1999-03-11 Akzo Nobel Nv Verbundsystem für kugel- und splitterschutz
EP1128154A3 (en) * 2000-02-21 2001-11-14 Rafael Armament Development Authority Ltd. Ballistic armor panel
US6892623B2 (en) 2000-02-21 2005-05-17 The State Of Israel, Ministry Of Defense, Armament Development Authority Ballistic armor panel
US8215223B2 (en) 2001-07-25 2012-07-10 Aceram Materials And Technologies Inc. Ceramic components, ceramic component systems, and ceramic armour systems
WO2004109216A2 (en) * 2002-10-28 2004-12-16 The Boeing Company Ballistic-resistant multilayered armor including a stitched composite reinforcement layer and method of making the same
WO2004109216A3 (en) * 2002-10-28 2005-02-03 Boeing Co Ballistic-resistant multilayered armor including a stitched composite reinforcement layer and method of making the same
EP1536199A1 (de) * 2003-11-25 2005-06-01 Sgl Carbon Ag Keramische ballistische Schutzschicht
US8267001B2 (en) 2006-12-04 2012-09-18 Battelle Memorial Institute Composite armor and method for making composite armor
WO2011101872A1 (en) 2010-02-16 2011-08-25 Tecno Drive S.R.L. Lifting device, particularly for lifting wheelchairs
WO2012063271A2 (en) 2010-11-10 2012-05-18 Petroceramics S.P.A. Antiballistic element
RU2476809C1 (ru) * 2011-08-02 2013-02-27 Закрытое акционерное общество "Научно-производственное объединение специальных материалов" Объемно-комбинированная броня
US8906484B1 (en) 2012-05-02 2014-12-09 The Boeing Company System of composite armor including release layers
RU2517547C1 (ru) * 2013-05-24 2014-05-27 Закрытое акционерное общество "Научно-производственное объединение специальных материалов" Объемно-комбинированная броня
WO2015071866A1 (en) 2013-11-14 2015-05-21 Petroceramics S.P.A. Antiballistic garment
WO2015071916A1 (en) 2013-11-14 2015-05-21 Petroceramics S.P.A. Antiballistic element
CN112729014A (zh) * 2020-12-09 2021-04-30 浙江立泰复合材料股份有限公司 一种抗多发弹密集打击复合装甲制备方法
CN112729014B (zh) * 2020-12-09 2022-08-12 浙江立泰复合材料股份有限公司 一种抗多发弹密集打击复合装甲制备方法
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