EP1400775B1 - Ceramic bodies and ballistic armor incorporating the same - Google Patents
Ceramic bodies and ballistic armor incorporating the same Download PDFInfo
- Publication number
- EP1400775B1 EP1400775B1 EP20030255523 EP03255523A EP1400775B1 EP 1400775 B1 EP1400775 B1 EP 1400775B1 EP 20030255523 EP20030255523 EP 20030255523 EP 03255523 A EP03255523 A EP 03255523A EP 1400775 B1 EP1400775 B1 EP 1400775B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- bodies
- ceramic
- section
- panel
- head section
- 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.)
- Expired - Lifetime
Links
- 239000000919 ceramic Substances 0.000 title claims description 75
- 239000000463 material Substances 0.000 claims description 41
- 239000010410 layer Substances 0.000 claims description 37
- 239000002131 composite material Substances 0.000 claims description 21
- 229910010293 ceramic material Inorganic materials 0.000 claims description 13
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 11
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 9
- 239000000758 substrate Substances 0.000 claims description 8
- 239000000835 fiber Substances 0.000 claims description 6
- 239000002356 single layer Substances 0.000 claims description 6
- 229910052580 B4C Inorganic materials 0.000 claims description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 4
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 claims description 4
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 claims description 4
- 229910052749 magnesium Inorganic materials 0.000 claims description 4
- 239000011777 magnesium Substances 0.000 claims description 4
- 239000011159 matrix material Substances 0.000 claims description 4
- 150000001247 metal acetylides Chemical class 0.000 claims description 4
- 229910052750 molybdenum Inorganic materials 0.000 claims description 4
- 239000011733 molybdenum Substances 0.000 claims description 4
- 150000004767 nitrides Chemical class 0.000 claims description 4
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 4
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 4
- 239000000377 silicon dioxide Substances 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 4
- 229910052721 tungsten Inorganic materials 0.000 claims description 4
- 239000010937 tungsten Substances 0.000 claims description 4
- 229910052726 zirconium Inorganic materials 0.000 claims description 4
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 claims description 3
- 229910052582 BN Inorganic materials 0.000 claims description 3
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 claims description 3
- 229910052581 Si3N4 Inorganic materials 0.000 claims description 3
- 229910033181 TiB2 Inorganic materials 0.000 claims description 3
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 3
- 239000000395 magnesium oxide Substances 0.000 claims description 3
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims description 3
- 229910052814 silicon oxide Inorganic materials 0.000 claims description 3
- 239000008188 pellet Substances 0.000 description 70
- 229910052751 metal Inorganic materials 0.000 description 10
- 239000002184 metal Substances 0.000 description 10
- 230000005484 gravity Effects 0.000 description 8
- 239000012634 fragment Substances 0.000 description 7
- 229910000831 Steel Inorganic materials 0.000 description 6
- 230000000717 retained effect Effects 0.000 description 6
- 239000010959 steel Substances 0.000 description 6
- 229910052782 aluminium Inorganic materials 0.000 description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 5
- 230000003116 impacting effect Effects 0.000 description 5
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 5
- 239000011521 glass Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 239000011819 refractory material Substances 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- 241000264877 Hippospongia communis Species 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000013013 elastic material Substances 0.000 description 3
- 230000035515 penetration Effects 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- 239000004753 textile Substances 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 229910052593 corundum Inorganic materials 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- -1 e.g. Chemical compound 0.000 description 2
- 239000004417 polycarbonate Substances 0.000 description 2
- 229920000515 polycarbonate Polymers 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 229920001169 thermoplastic Polymers 0.000 description 2
- 229920001187 thermosetting polymer Polymers 0.000 description 2
- 229910001845 yogo sapphire Inorganic materials 0.000 description 2
- 229910000547 2024-T3 aluminium alloy Inorganic materials 0.000 description 1
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 241000531908 Aramides Species 0.000 description 1
- 241001606091 Neophasia menapia Species 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 230000001010 compromised effect Effects 0.000 description 1
- 230000003750 conditioning effect Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 229920001021 polysulfide Polymers 0.000 description 1
- 239000005077 polysulfide Substances 0.000 description 1
- 150000008117 polysulfides Polymers 0.000 description 1
- 238000010298 pulverizing process Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000002829 reductive effect Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- 239000012209 synthetic fiber Substances 0.000 description 1
Images
Classifications
-
- 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
-
- 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
- F41H5/023—Armour plate, or auxiliary armour plate mounted at a distance of the main armour plate, having cavities at its outer impact surface, or holes, for deflecting the projectile
-
- 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
- F41H5/0492—Layered armour containing hard elements, e.g. plates, spheres, rods, separated from each other, the elements being connected to a further flexible layer or being embedded in a plastics or an elastomer matrix
Definitions
- the present invention relates to a ceramic body for deployment in a composite armor panel, for absorbing and dissipating kinetic energy from projectiles and for ballistic armor panels incorporating the same. More particularly, the invention relates to improved ceramic bodies for use in structural armored plates for providing ballistic protection for light and heavy mobile equipment and for vehicles against high-velocity projectiles or fragments.
- the present invention is a modification of the inventions described in European patent application 96308166.6 ( EP-A-0843149 ), European patent application 98301769.0 , and International patent application PCT/GB97/02743 ( WO-A-98/15796 ), WO 99/60327 and WO99/53260 .
- EP-A-0843149 there is described a composite armor plate for absorbing and dissipating kinetic energy from high velocity, armor-piercing projectiles, said plate comprising a single internal layer of high density ceramic pellets which are directly bound and retained in plate form by a solidified material such that the pellets are bound in a plurality of superposed rows, characterized in that the pellets have an Al 2 O 3 content of at least 85%, preferably at least 93%, and a specific gravity of at least 2.5, the majority of the pellets each have at least one axis in the range of about 3-12 mm, and are bound by said solidified material in a single internal layer of superposed rows, wherein a majority of each of said pellets is in direct contact with at least 4 adjacent pellets, the total weight of said plate does not exceed 45 kg/m 2 and said solidified material and said plate are elastic.
- a composite armor plate for absorbing and dissipating kinetic energy from high velocity, armor-piercing projectiles, said plate comprising a single internal layer of high density ceramic pellets which are directly bound and retained in plate form by a solidified material such that the pellets are bound in a plurality of adjacent rows, characterized in that the pellets have an Al 2 O 3 content of at least 93% and a specific gravity of at least 2.5, the majority of the pellets each have at least one axis of at least 12 mm length and are bound by said solidified material in a single internal layer of adjacent rows, wherein a majority of each of said pellets is in direct contact with at least 4 adjacent pellets, and said solidified material and said plate are elastic.
- a ceramic body for deployment in a composite armor panel said body being substantially cylindrical in shape, with at least one convexly curved end face, wherein the ratio D/R between the diameter D of said cylindrical body and the radius R of curvature of said at least one convexly curved end face is at least 0.64:1.
- a composite armor plate for absorbing and dissipating kinetic energy from high velocity projectiles, said plate comprising a single internal layer of pellets which are directly bound and retained in plate form by a solidified material such that the pellets are bound in a plurality of adjacent rows, characterized in that the pellets have a specific gravity of at least 2 and are made of a material selected from the group consisting of glass, sintered refractory material, ceramic material which does not contain aluminum oxide and ceramic material having an aluminum oxide content of not more than 80%, the majority of the pellets each have at least one axis of at least 3 mm length and are bound by said solidified material in said single internal layer of adjacent rows such that each of a majority of said pellets is in direct contact with at least six adjacent pellets in the same layer to provide mutual lateral confinement therebetween, said pellets each have a substantially regular geometric form and said solidified material and said plate are elastic.
- a composite armor plate for absorbing and dissipating kinetic energy from high velocity, armor-piercing projectiles, as well as from soft-nosed projectiles, said plate comprising a single internal layer of high density ceramic pellets, characterized in that said pellets are arranged in a single layer of adjacent rows and columns, wherein a majority of each of said pellets is in direct contact with at least four adjacent pellets and each of said pellets are substantially cylindrical in shape with at least one convexly-curved end face, further characterized in that spaces formed between said adjacent cylindrical pellets are filled with a material for preventing the flow of soft metal from impacting projectiles through said spaces, said material being in the form of a triangular insert having concave sides complimentary to the convex curvature of the sides of three adjacent cylindrical pellets, or being integrally formed as part of a special interstices-filling pellet, said pellet being in the form of a six sided star with concave sides complimentary to the convex cur
- the first consideration is weight.
- Protective armor for heavy but mobile military equipment such as tanks and large ships, is known.
- Such armor usually comprises a thick layer of alloy steel, which is intended to provide protection against heavy and explosive projectiles.
- reduction of weight of armor, even in heavy equipment is an advantage since it reduces the strain on all the components of the vehicle.
- such armor is quite unsuitable for light vehicles such as automobiles, jeeps, light boats, or aircraft, whose performance is compromised by steel panels having a thickness of more than a few millimeters, since each millimeter of steel adds a weight factor of 7.8 kg/m 2 .
- Armor for light vehicles is expected to prevent penetration of bullets of any type, even when impacting at a speed in the range of 700 to 1000 meters per second.
- Due to weight constraints it is difficult to protect light vehicles from high caliber armor-piercing projectiles, e.g. of 12.7 and 14.5 mm, since the weight of standard armor to withstand such projectile is such as to impede the mobility and performance of such vehicles.
- a second consideration is cost. Overly complex armor arrangements, particularly those depending entirely on synthetic fibers, can be responsible for a notable proportion of the total vehicle cost, and can make its manufacture non-profitable.
- a third consideration in armor design is compactness.
- a thick armor panel including air spaces between its various layers, increases the target profile of the vehicle.
- a fourth consideration relates to ceramic plates used for personal and light vehicle armor, which plates have been found to be vulnerable to damage from mechanical impacts caused by rocks, falls, etc.
- said stem section has a regular geometric cross-section and especially preferred is a stem section with a circular cross-section or a regular polygonal cross-section such as a hexagonal cross-section.
- said head section also has a regular geometric cross-section and especially preferred is a stem section with a circular cross-section or a regular polygonal cross-section such as a hexagonal cross-section.
- head and stem sections can have the same, but differently sized, cross-section, this is not necessarily the case and, e.g., a body with a stem of circular cross-section and a head of hexagonal cross-section can also be molded for use in the present invention.
- a ballistic armor panel for absorbing and dissipating kinetic energy from high velocity projectiles, said panel comprising:
- a ballistic armor panel for absorbing and dissipating kinetic energy from high velocity projectiles, said panel comprising:
- the armor plates described in EP-A-0843149 and European patent application 98301769.0 are made using ceramic pellets made substantially entirely of aluminum oxide.
- the ceramic bodies are of substantially cylindrical shape having at least one convexly-curved end-face, and are preferably made of aluminum oxide.
- the improved properties of the plates described in the earlier patent applications of this series is as much a function of the configuration of the pellets, which are of regular geometric form with at least one convexly-curved end face (for example, the pellets may be spherical or ovoidal, or of regular geometric cross-section, such as hexagonal, with at least one convexly-curved end face), said panels and their arrangement as a single internal layer of pellets bound by an elastic solidified material, wherein each of a majority of said pellets is in direct contact with at least four adjacent pellets and said curved end face of each pellet is oriented to substantially face in the direction of an outer impact-receiving major surface of the plate.
- composite armor plates superior to those available in the prior art can be manufactured using pellets made of sintered refractory materials or ceramic materials having a specific gravity below that of aluminum oxide, e.g., boron carbide with a specific gravity of 2.45, silicon carbide with a specific gravity of 3.2 and silicon aluminum oxynitride with a specific gravity of about 3.2.
- sintered oxides; nitrides, carbides and borides of magnesium, zirconium, tungsten, molybdenum, titanium and silica can be used and especially preferred for use in said publication and also in the present invention the ceramic bodies utilized herein are formed of a ceramic material selected from the group consisting of sintered oxide, nitrides, carbides and borides of alumina, magnesium, zirconium, tungsten, molybdenum, titanium and silica.
- the present invention relates to a ceramic body as defined for absorbing and dissipating kinetic energy from high velocity armor piercing projectiles, wherein said body is made of a material selected from the group consisting of alumina, boron carbide, boron nitride, titanium diboride, silicon carbide, silicon oxide, silicon nitride, magnesium oxide, silicon aluminum oxynitride and mixtures thereof.
- a composite armor plate for absorbing and dissipating kinetic energy from high velocity projectiles, said plate comprising a single internal layer of pellets which are directly bound and retained in plate form by a solidified material such that the pellets are bound in a plurality of adjacent rows, said pellets having a specific gravity of at least 2 and being made of a material selected from the group consisting of glass, sintered refractory material and ceramic material, the majority of the pellets each having at least one axis of at least 3 mm length and being bound by said solidified material in said single internal layer of adjacent rows such that each of a majority of said pellets is in direct contact with six adjacent pellets in the same layer to provide mutual lateral confinement therebetween, said pellets each having a substantially regular geometric form, wherein said solidified material and said plate are elastic, characterized in that a channel is provided in each of a plurality of said pellets, substantially opposite to an outer impact-receiving major surface of said plate, thereby
- each of said channels occupies a volume of up to 25% within its respective pellet
- Said channels can be bored into preformed pellets or the pellets themselves can be pressed with said channel already incorporated therein.
- a channel is provided in said body to reduce the weight per area thereof and preferably said channel occupies a volume of up to 25% of said body.
- said channels are preferably of a shape selected from the group consisting of cylindrical, pyramidal, hemispherical and quadratic, hexagonal prism and combinations thereof.
- said pellets each have a major axis and said pellets are arranged with their major axes substantially parallel to each other and oriented substantially perpendicularly relative to said outer impact-receiving major surface of said panel.
- the present invention also provides an armored vehicle having ballistic armor panels according to the present invention incorporated therein.
- the ceramic bodies of the present invention are constructed of transparent ceramic material.
- the plate member utilized in the ballistic armor panel is formed from a plurality of interconnected rings which optionally are further bound together by a solidified material.
- the solidified material can be any suitable material, such as aluminum, a thermoplastic polymer such as polycarbonate, or a thermoset plastic such as epoxy.
- a multi-layered armor panel comprising an outer, impact-receiving layer formed by a composite armor plate as hereinbefore defined for deforming and shattering an impacting high velocity projectile; and an inner layer adjacent to said outer layer and, comprising an elastic material' for absorbing the remaining kinetic energy from said fragments.
- Said elastic material will be chosen according to cost and weight considerations and can be made of any suitable material, such as aluminum or woven or non-woven textile material.
- the inner layer adjacent to said outer layer comprises a tough woven textile material for causing an asymmetric deformation of the remaining fragments of said projectile and for absorbing the remaining kinetic energy from said fragments, said multi-layered panel being capable of stopping three projectiles fired sequentially at a triangular area of said multi-layered panel, wherein the height of said triangle is substantially equal to three times the length of the axis of said pellets.
- composite armor plate comprising a mass of spherical ceramic balls distributed in an aluminum alloy matrix is known in the prior art.
- such prior art composite armor plate suffers from one or more serious disadvantages, making it difficult to manufacture and less than entirely suitable for the purpose of defeating metal projectiles.
- the ceramic balls are coated with a binder material containing ceramic particles, the coating having a thickness of between 0.76 and 1.5 and being provided to help protect the ceramic cores from damage due to thermal shock when pouring the molten matrix material during manufacture of the plate.
- the coating serves to separate the harder ceramic cores of the balls from each other, and will act to dampen the moment of energy which is transferred and hence shared between the balls in response to an impact from a bullet or other projectile. Because of this and also because the material of the coating is inherently less hard than that of the ceramic cores, the stopping power of a plate constructed as described in said patent is not as good, weight for weight, as that of a plate in accordance with the present invention, in which the head of each of the bodies is in direct contact with six adjacent bodies.
- U.S. Patent 3,705,558 discloses a lightweight armor plate comprising a layer of ceramic balls.
- the ceramic balls are in contact with each other and leave small gaps for entry of molten metal.
- the ceramic balls are encased in a stainless steel wire screen; and in another embodiment, the composite armor is manufactured by adhering nickel-coated alumina spheres to an aluminum alloy plate by means of a polysulfide adhesive.
- a composite armor plate as described in this patent is difficult to manufacture because the ceramic spheres may be damaged by thermal shock arising from molten metal contact. The ceramic spheres are also sometimes displaced during casting of molten metal into interstices between the spheres
- U.S. Patents 4,534,266 and 4,945,814 propose a network of interlinked metal shells to encase ceramic inserts during casting of molten metal. After the metal solidifies, the metal shells are incorporated into the composite armor. It has been determined, however, that such a network of interlinked metal shells substantially increases the overall weight of the armored panel and decreases the stopping power thereof.
- U.S. Patent 3,705,558 suggests and teaches an array of ceramic balls disposed in contacting pyramidal relationship, which arrangement also substantially increases the overall weight of the armored panel and decreases the stopping power thereof, due to a billiard-like effect upon impact
- U.S. Patent 5,134,725 there are described armored panels incorporating ceramic and glass balls. It will be noted that the teachings of U.S. Patent 5,134,725 is limited to an armor plate having a plurality of constituent bodies of glass or ceramic material which are arranged in at least two superimposed layers, which arrangement is similar to that seen in US Patent 3,705,558 .
- reference to Figures 3 and 4 of said patent show that pellets of a first layer do not contact pellets of the same layer and are only in contact with pellets of an adjacent layer and therefore do not benefit from the support of adjacent pellets in the same layer to provide mutual lateral confinement of the pellets, as taught in the present invention.
- a structural, load-bearing ballistic armor wherein the plate member having a plurality of openings provides the structural framework while the peg-like configuration of the ceramic bodies of the present invention assure that the bodies are still in direct contact with each other via their head sections thereby providing mutual lateral confinement and reinforcement not available in armor wherein the pellets are separated by a rigid honey-comb array.
- novel armor of the present invention traps incoming projectiles between several pellets which are held with their head sections in a single layer in rigid mutual abutting and laterally-confining relationship.
- An incoming projectile may contact the pellet array in one of three ways:
- FIG. 1 a ceramic body 10 intended for deployment in a composite armor panel. Examples of several such panels will be shown starting with FIG. 6a .
- the panel is designed for absorbing and dissipating kinetic energy from high velocity projectiles, such as rifle fire and small shell fragments.
- the body 10 has a peg-like configuration consisting of a stem section 12 and a head section 14. As can be seen, a cross-sectional area across the stem section 12 is less than a cross-sectional area across the head section 14. in the preferred embodiment seen in the figure, the stem section 12 has a regular geometric cross-section, which in this case is circular. In the present embodiment the head section also has a circular cross-section, and a flat top face 16.
- the body 10 is formed of a ceramic material.
- Preferred ceramics are sintered oxide, nitrides, carbides and borides of alumina, magnesium, zirconium, tungsten, molybdenum, titanium and silica. Where the pellet is intended to be used for absorbing and dissipating kinetic energy from armor piercing projectiles, other materials are preferred. These materials are typically alumina, boron carbide, boron nitride, titanium diboride, silicon carbide, silicon oxide, silicon nitride, magnesium oxide, silicon aluminum oxynitride and mixtures thereof.
- FIG. 2 illustrates a ceramic body 18 wherein the head section 20 is provided with a convex head face 22 and a convex end face 24.
- the convex head shape 22 encourages sideways deflection of bullets impacting the pellet head. Thus the projectile is stopped as explained above regarding "Flank Contact”.
- the convex end face 24 facilitates assembly of the body 18 into an armor panel, which will be seen in FIG. 7 .
- FIG. 3 there is depicted a ceramic body 26 wherein the head section 28 has a regular geometric cross-section; in the present embodiment the head section is hexagonal.
- the armor panel resulting from use of this arrangement will be described with reference to FIG. 6b .
- FIG. 4 illustrates a further embodiment of a ceramic body 30 wherein also the stem section 32 has a regular polygonal cross-section. Such configuration is useful in applications where it is advantageous to prevent the rotation of the body if the head section 34 is impacted by a high-velocity fragment.
- Seen in FIG. 5 is a ceramic body 36 wherein the head section 38 has a regular polygonal cross-section, in the present embodiment this being square.
- the body has a peg-like configuration consisting of a stem section 40 and a head section 38.
- the cross-sectional area across the stem section 40 is less than the cross-sectional area across the head section 38.
- FIGS. 6a and 6b there is depicted a ballistic armor panel 42 for absorbing and dissipating kinetic energy from high velocity projectiles.
- the outer face 44 of the panel 42 comprises a large number of ceramic bodies 26, as described with reference to FIG. 3 .
- the ceramic bodies 26 are inserted and held in a close-packed, single layer array 46. Excepting the ceramic bodies 26' around the outer borders of the panel, each body 26 is positioned with its head section 28 in direct contact with the head section 28 of six adjacent bodies 26. Thus the ceramic bodies provide mutual lateral confinement and reinforcement, which is important for retaining stopping power after a first projectile has impacted the panel 42 resulting in some damage to the ceramic body 26 which was hit.
- the stems 12 of the bodies 26 are supported and held by the substrate 50.
- FIG. 7 shows a further ballistic armor panel 52 for absorbing and dissipating kinetic energy from high velocity projectiles.
- a plurality of ceramic bodies 18 are seen, as described with reference to FIG. 2 .
- the bodies 18 are retained in a plate member 54 having many openings 56, each opening being sized to receive the stem section 58 of one of the ceramic bodies.
- the underside 60 of the head section 20 of the body 18 overrides the periphery of the opening 56. Except for the outer edges 62 of the armor panel 52, each body is positioned with its head section 20 in direct contact with six adjacent bodies 18 inserted in the plate member 54.
- FIG. 8 there is seen a ballistic armor panel faced with ceramic bodies 68.
- the body 68 is similar to the body 26 seen in FIG. 3 , except that the head of the body 68 is convex.
- the plate member 70 is formed from a plurality of interconnected rings 72.
- the rings 72 can be mass produced using dedicated tooling therefor.
- the rings 72 are further bound together by a solidified material 74, for example aluminum, or a thermoplastic polymer such as polycarbonate, or a thermoset plastic such as epoxy.
- FIG 9 shows a further embodiment of a ceramic body 76.
- the body 76 is similar to the body 18 seen in FIG. 2 .
- An important feature of body 76 is a channel 78 provided in the body to reduce the weight per area thereof.
- the channel 78 occupies a volume of up to 25% of the body 76.
- the body 76 is particularly useful for airborne use and for personal applications.
- the panel 80 has an inner 82 and an outer 84 surface, the outer surface 84 facing the impact side. Ceramic bodies 36 are arranged in a plurality of adjacent rows. The axes of the stems sections 40 of the bodies 36 are substantially parallel with each other and perpendicular to the surfaces of the panels 82, 84.
- the inner layer 82 is formed from a plurality of adjacent layers 82', 82", each layer comprising a plurality of unidirectional coplanar anti-ballistic fibers embedded in a polymeric matrix.
- the fibers of adjacent layers 82', 82" are oriented at an angle of between about 45° to 90° to each other.
- the outer, impact-receiving layer deforms and shatters an impacting high velocity projectile.
- the inner layer being elastic, is then able to absorb the remaining kinetic energy from the projectile fragments.
- the elastic material is chosen according to cost and weight considerations applicable to the designated application. Although any suitable material can be used, such as aluminum or woven or non-woven textile material, the preference is for at least 90% Aramide fiber, fiber orientation being as described. The final material selection is based on meeting weight and volume restraints at lowest cost.
- FIGS. 11 and 11 a there is seen an armored vehicle 86 wherein a panel 88 of the present invention has been provided in an opening (not shown) of said vehicle, the panel 88, in the embodiment shown, incorporating ceramic bodies 90 having cylindrical heads and cylindrical stems, said panel being shown in an enlarged detail view in FIG. 11a .
- the panels of the present invention are lighter in weight then steel panels of comparable size and provide even better protection it is advantageous to incorporate several panels according to the present invention in such vehicles in place of standard steel armor in order to reduce the overall weight of the vehicle.
- transparent ceramic material is available as described e.g., in H1567 and H1519 and such material could be used in the panels of the present invention.
- a panel was prepared with the size of 10 X 12 in and ceramic bodies having a cylindrical stem and hexagonal head section with a convexly curved end face as illustrated in FIG. 8 was prepared and sent to the H.P. White Laboratory, Inc. in Maryland for ballistic resistance testing.
- said panel having a weight of only 7.2 pounds provided exceptional multi-impact performance wherein none of the 7.62 X 51 mm, 150 grain, armor piercing, M61 projectiles fired at a distance of 45 feet from the target penetrated said panel.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Laminated Bodies (AREA)
Description
- The present invention relates to a ceramic body for deployment in a composite armor panel, for absorbing and dissipating kinetic energy from projectiles and for ballistic armor panels incorporating the same. More particularly, the invention relates to improved ceramic bodies for use in structural armored plates for providing ballistic protection for light and heavy mobile equipment and for vehicles against high-velocity projectiles or fragments.
- The present invention is a modification of the inventions described in European patent application
96308166.6 EP-A-0843149 ), European patent application98301769.0 PCT/GB97/02743 WO-A-98/15796 WO 99/60327 WO99/53260 - In
EP-A-0843149 there is described a composite armor plate for absorbing and dissipating kinetic energy from high velocity, armor-piercing projectiles, said plate comprising a single internal layer of high density ceramic pellets which are directly bound and retained in plate form by a solidified material such that the pellets are bound in a plurality of superposed rows, characterized in that the pellets have an Al2O3 content of at least 85%, preferably at least 93%, and a specific gravity of at least 2.5, the majority of the pellets each have at least one axis in the range of about 3-12 mm, and are bound by said solidified material in a single internal layer of superposed rows, wherein a majority of each of said pellets is in direct contact with at least 4 adjacent pellets, the total weight of said plate does not exceed 45 kg/m2 and said solidified material and said plate are elastic. - In European patent application
98301769.0 - In
WO-A-9815796 - In
WO 99/60327 - In
WO 99/53260 - There are four main considerations concerning protective armor panels. The first consideration is weight. Protective armor for heavy but mobile military equipment, such as tanks and large ships, is known. Such armor usually comprises a thick layer of alloy steel, which is intended to provide protection against heavy and explosive projectiles. However, reduction of weight of armor, even in heavy equipment, is an advantage since it reduces the strain on all the components of the vehicle. Furthermore, such armor is quite unsuitable for light vehicles such as automobiles, jeeps, light boats, or aircraft, whose performance is compromised by steel panels having a thickness of more than a few millimeters, since each millimeter of steel adds a weight factor of 7.8 kg/m2.
- Armor for light vehicles is expected to prevent penetration of bullets of any type, even when impacting at a speed in the range of 700 to 1000 meters per second. However, due to weight constraints it is difficult to protect light vehicles from high caliber armor-piercing projectiles, e.g. of 12.7 and 14.5 mm, since the weight of standard armor to withstand such projectile is such as to impede the mobility and performance of such vehicles.
- A second consideration is cost. Overly complex armor arrangements, particularly those depending entirely on synthetic fibers, can be responsible for a notable proportion of the total vehicle cost, and can make its manufacture non-profitable.
- A third consideration in armor design is compactness. A thick armor panel, including air spaces between its various layers, increases the target profile of the vehicle. In the case of civilian retrofitted armored automobiles which are outfitted with internal armor, there is simply no room for a thick panel in most of the areas requiring protection.
- A fourth consideration relates to ceramic plates used for personal and light vehicle armor, which plates have been found to be vulnerable to damage from mechanical impacts caused by rocks, falls, etc.
- Fairly recent examples of armor systems are described in
U.S. Patent No. 4,836,084 , disclosing an armor plate composite including a supporting plate consisting of an open honeycomb structure of aluminum; andU.S. Patent No. 4,868,040 , disclosing an antiballistic composite armor including a shock-absorbing layer. Also of interest isU.S. Patent 4,529,640 , disclosing spaced armor including a hexagonal honeycomb core member. - Other armor plate panels are disclosed in British Patents
1,081,464 1, 352, 418 2,272,272 U.S. Patent 4,061,815 wherein the use of sintered refractory material, as well as the use of ceramic materials, are described.
According to the present invention there is now provided a ceramic body for deployment in a composite armor panel, for absorbing and dissipating kinetic energy from high velocity projectiles, said body having a peg-like configuration consisting of a stem section and a head section wherein a cross-sectional area across said stem is less than a cross-sectional area across said head section. - In preferred embodiments of the present invention, said stem section has a regular geometric cross-section and especially preferred is a stem section with a circular cross-section or a regular polygonal cross-section such as a hexagonal cross-section.
- In further preferred embodiments of the present invention, said head section also has a regular geometric cross-section and especially preferred is a stem section with a circular cross-section or a regular polygonal cross-section such as a hexagonal cross-section.
- While the head and stem sections can have the same, but differently sized, cross-section, this is not necessarily the case and, e.g., a body with a stem of circular cross-section and a head of hexagonal cross-section can also be molded for use in the present invention.
- In a further aspect of the present invention, there is provided a ballistic armor panel for absorbing and dissipating kinetic energy from high velocity projectiles, said panel comprising:
- a plurality of ceramic bodies, each of said bodies having a peg-like configuration consisting of a stem section and a head section wherein a cross-sectional area across said stem is less than a cross-sectional area across said head section; and a substrate for assembling said bodies in a close-packed, single layer array, such that each of a majority of said bodies is positioned with its head section in direct contact with the head section of at least four and preferably six adjacent bodies and the stems of said bodies are supported and held by said substrate.
- In especially preferred embodiments of the present invention there is provided a ballistic armor panel for absorbing and dissipating kinetic energy from high velocity projectiles, said panel comprising:
- a plurality of ceramic bodies, each of said bodies having a peg-like configuration consisting of a stem section and a head section wherein a cross-sectional area across said stem is less than a cross-sectional area across said head section; and
- a plate member having a plurality of openings, each of said opening sized to receive a stem section of a body with the underside of the head section of said body overriding the periphery of said opening, such that each of a majority of said bodies is positioned with its head section in direct contact with the head section of at least four and preferably six adjacent bodies inserted in said plate.
- The armor plates described in
EP-A-0843149 and European patent application98301769.0 WO-A-9815796 - In
WO 99/60327 - Thus, it was described in said publication that sintered oxides; nitrides, carbides and borides of magnesium, zirconium, tungsten, molybdenum, titanium and silica can be used and especially preferred for use in said publication and also in the present invention the ceramic bodies utilized herein are formed of a ceramic material selected from the group consisting of sintered oxide, nitrides, carbides and borides of alumina, magnesium, zirconium, tungsten, molybdenum, titanium and silica.
- More particularly, the present invention relates to a ceramic body as defined for absorbing and dissipating kinetic energy from high velocity armor piercing projectiles, wherein said body is made of a material selected from the group consisting of alumina, boron carbide, boron nitride, titanium diboride, silicon carbide, silicon oxide, silicon nitride, magnesium oxide, silicon aluminum oxynitride and mixtures thereof.
- In
USSN 09/924745 - In preferred embodiments described therein each of said channels occupies a volume of up to 25% within its respective pellet
- Said channels can be bored into preformed pellets or the pellets themselves can be pressed with said channel already incorporated therein.
- Thus, in preferred embodiments of the present invention a channel is provided in said body to reduce the weight per area thereof and preferably said channel occupies a volume of up to 25% of said body.
- In accordance with the present invention said channels are preferably of a shape selected from the group consisting of cylindrical, pyramidal, hemispherical and quadratic, hexagonal prism and combinations thereof.
- As is known, there exists a ballistic effect known in the art in which a projectile striking a cylinder at an angle has a tendency to move this cylinder out of alignment causing a theoretical possibility that a second shot would have more penetration effect on a panel.
- As will be realized, since material is removed from the pellets of the present invention their weight is decreased, as is the overall weight of the entire composite armor plate from which they are formed, thereby providing the unexpected improvement of reduced weight of protective armor panels without loss of stopping power, as shown in the examples hereinafter.
- In preferred embodiments of the present invention said pellets each have a major axis and said pellets are arranged with their major axes substantially parallel to each other and oriented substantially perpendicularly relative to said outer impact-receiving major surface of said panel.
- In a most preferred embodiment of the present invention a ballistic armor panel as defined herein is provided for incorporation in an opening provided in an armored vehicle
- Thus the present invention also provides an armored vehicle having ballistic armor panels according to the present invention incorporated therein.
- In further embodiments of the present invention the ceramic bodies of the present invention are constructed of transparent ceramic material.
- In especially preferred embodiments of the present invention the plate member utilized in the ballistic armor panel is formed from a plurality of interconnected rings which optionally are further bound together by a solidified material.
- The solidified material can be any suitable material, such as aluminum, a thermoplastic polymer such as polycarbonate, or a thermoset plastic such as epoxy.
- In French Patent
2,711,782 - According to a further aspect of the invention, there is provided a multi-layered armor panel, comprising an outer, impact-receiving layer formed by a composite armor plate as hereinbefore defined for deforming and shattering an impacting high velocity projectile; and an inner layer adjacent to said outer layer and, comprising an elastic material' for absorbing the remaining kinetic energy from said fragments. Said elastic material will be chosen according to cost and weight considerations and can be made of any suitable material, such as aluminum or woven or non-woven textile material.
- In especially preferred embodiments of the multi-layered armor panel, the inner layer adjacent to said outer layer comprises a tough woven textile material for causing an asymmetric deformation of the remaining fragments of said projectile and for absorbing the remaining kinetic energy from said fragments, said multi-layered panel being capable of stopping three projectiles fired sequentially at a triangular area of said multi-layered panel, wherein the height of said triangle is substantially equal to three times the length of the axis of said pellets.
- As described, e.g., in
U.S. Patent 5,361,678 , composite armor plate comprising a mass of spherical ceramic balls distributed in an aluminum alloy matrix is known in the prior art. However, such prior art composite armor plate suffers from one or more serious disadvantages, making it difficult to manufacture and less than entirely suitable for the purpose of defeating metal projectiles. More particularly, in the armor plate described in said patent, the ceramic balls are coated with a binder material containing ceramic particles, the coating having a thickness of between 0.76 and 1.5 and being provided to help protect the ceramic cores from damage due to thermal shock when pouring the molten matrix material during manufacture of the plate. However, the coating serves to separate the harder ceramic cores of the balls from each other, and will act to dampen the moment of energy which is transferred and hence shared between the balls in response to an impact from a bullet or other projectile. Because of this and also because the material of the coating is inherently less hard than that of the ceramic cores, the stopping power of a plate constructed as described in said patent is not as good, weight for weight, as that of a plate in accordance with the present invention, in which the head of each of the bodies is in direct contact with six adjacent bodies. -
U.S. Patent 3,705,558 discloses a lightweight armor plate comprising a layer of ceramic balls. The ceramic balls are in contact with each other and leave small gaps for entry of molten metal. In one embodiment, the ceramic balls are encased in a stainless steel wire screen; and in another embodiment, the composite armor is manufactured by adhering nickel-coated alumina spheres to an aluminum alloy plate by means of a polysulfide adhesive. A composite armor plate as described in this patent is difficult to manufacture because the ceramic spheres may be damaged by thermal shock arising from molten metal contact. The ceramic spheres are also sometimes displaced during casting of molten metal into interstices between the spheres - In order to minimize such displacement,
U.S. Patents 4,534,266 and4,945,814 propose a network of interlinked metal shells to encase ceramic inserts during casting of molten metal. After the metal solidifies, the metal shells are incorporated into the composite armor. It has been determined, however, that such a network of interlinked metal shells substantially increases the overall weight of the armored panel and decreases the stopping power thereof. - It is further to be noted that
U.S. Patent 3,705,558 suggests and teaches an array of ceramic balls disposed in contacting pyramidal relationship, which arrangement also substantially increases the overall weight of the armored panel and decreases the stopping power thereof, due to a billiard-like effect upon impact - In
U.S. Patent 5,134,725 there are described armored panels incorporating ceramic and glass balls. It will be noted that the teachings ofU.S. Patent 5,134,725 is limited to an armor plate having a plurality of constituent bodies of glass or ceramic material which are arranged in at least two superimposed layers, which arrangement is similar to that seen inUS Patent 3,705,558 . In addition, reference toFigures 3 and 4 of said patent show that pellets of a first layer do not contact pellets of the same layer and are only in contact with pellets of an adjacent layer and therefore do not benefit from the support of adjacent pellets in the same layer to provide mutual lateral confinement of the pellets, as taught in the present invention. - As will be realized in the preferred embodies of the present invention there is provided a structural, load-bearing ballistic armor wherein the plate member having a plurality of openings provides the structural framework while the peg-like configuration of the ceramic bodies of the present invention assure that the bodies are still in direct contact with each other via their head sections thereby providing mutual lateral confinement and reinforcement not available in armor wherein the pellets are separated by a rigid honey-comb array.
- Thus, it has been found that the novel armor of the present invention traps incoming projectiles between several pellets which are held with their head sections in a single layer in rigid mutual abutting and laterally-confining relationship.
- An incoming projectile may contact the pellet array in one of three ways:
- 1. Center contact. The impact allows the full volume of the pellet to participate in stopping the projectile, which cannot penetrate without pulverizing the whole pellet, an energy-intensive task. The pellets used are preferably of circular or hexagonal cross-section or other regular geometric shapes having at least one convexly-curved end face, said end face being oriented to substantially face in the direction of an outer impact receiving major surface of said plate.
- 2. Flank contact. The impact causes projectile yaw, thus making projectile arrest easier, as a larger frontal area is contacted, and not only the sharp nose of the projectile. The projectile is deflected sideways and needs to form for itself a large aperture to penetrate, thus allowing the armor to absorb the projectile energy.
- 3. Valley contact. The projectile is jammed, usually between the flanks of three pellets, all of which participate in projectile arrest. The high side forces applied to the pellets are resisted by the pellets adjacent thereto as held by the substrate or plate, and penetration is prevented.
- The invention will now be described in connection with certain preferred embodiments with reference to the following illustrative figures so that it may be more fully understood.
- With reference now to the figures in detail, it is stressed that the particulars shown are by way of example and for purposes of illustrative discussion of the preferred embodiments of the present invention only, and are presented in the cause of providing what is believed to be the most useful and readily understood description of the principles and conceptual aspects of the invention. In this regard, no attempt is made to show structural details of the invention in more detail than is necessary for a fundamental understanding of the invention, the description taken with the drawings making apparent to those skilled in the art how the several forms of the invention may be embodied in practice.
In the drawings: -
FIG. 1 is a perspective view of a preferred embodiment of the ceramic body according to the invention; -
FIG. 2 is an elevational view of a similar ceramic body provided with convex ends; -
FIG. 3 is a perspective view of an embodiment provided with a hexagonal head; -
FIG. 4 is a perspective view of an embodiment provided with a prismatic stem section; -
FIG. 5 is a perspective view of a ceramic body having a square head; -
FIG. 6a is a perspective view of a ballistic armor panel constructed using the ceramic body seen inFIG. 3 ; -
FIG. 6b is an elevational view of the panel seen inFIG. 6a ; -
FIG. 7 is a perspective view of a panel built using the ceramic body seen inFIG. 2 ; -
FIG. 8 is a perspective view of an armor panel built using a ceramic body similar to that shown inFIG. 3 , the head section end being convex; -
FIG. 9 is a partially-sectioned elevational view of a ceramic body having a weight-deducing slot; -
FIG. 10 is a fragmented perspective view of a further embodiment of a ballistic armor panel; and -
FIGS. 11 and 11a are schematic illustrations of an armored vehicle incorporating a panel of the present invention. - There is seen in
FIG. 1 aceramic body 10 intended for deployment in a composite armor panel. Examples of several such panels will be shown starting withFIG. 6a . The panel is designed for absorbing and dissipating kinetic energy from high velocity projectiles, such as rifle fire and small shell fragments.
Thebody 10 has a peg-like configuration consisting of astem section 12 and ahead section 14. As can be seen, a cross-sectional area across thestem section 12 is less than a cross-sectional area across thehead section 14.
in the preferred embodiment seen in the figure, thestem section 12 has a regular geometric cross-section, which in this case is circular. In the present embodiment the head section also has a circular cross-section, and a flattop face 16.
Thebody 10 is formed of a ceramic material. Preferred ceramics are sintered oxide, nitrides, carbides and borides of alumina, magnesium, zirconium, tungsten, molybdenum, titanium and silica.
Where the pellet is intended to be used for absorbing and dissipating kinetic energy from armor piercing projectiles, other materials are preferred. These materials are typically alumina, boron carbide, boron nitride, titanium diboride, silicon carbide, silicon oxide, silicon nitride, magnesium oxide, silicon aluminum oxynitride and mixtures thereof. -
FIG. 2 illustrates aceramic body 18 wherein thehead section 20 is provided with aconvex head face 22 and aconvex end face 24. Theconvex head shape 22 encourages sideways deflection of bullets impacting the pellet head. Thus the projectile is stopped as explained above regarding "Flank Contact".
Theconvex end face 24 facilitates assembly of thebody 18 into an armor panel, which will be seen inFIG. 7 . - Referring now to
FIG. 3 , there is depicted aceramic body 26 wherein thehead section 28 has a regular geometric cross-section; in the present embodiment the head section is hexagonal.
The armor panel resulting from use of this arrangement will be described with reference toFIG. 6b . -
FIG. 4 illustrates a further embodiment of aceramic body 30 wherein also thestem section 32 has a regular polygonal cross-section. Such configuration is useful in applications where it is advantageous to prevent the rotation of the body if thehead section 34 is impacted by a high-velocity fragment. - Seen in
FIG. 5 is aceramic body 36 wherein thehead section 38 has a regular polygonal cross-section, in the present embodiment this being square. As in previous embodiments the body has a peg-like configuration consisting of astem section 40 and ahead section 38. The cross-sectional area across thestem section 40 is less than the cross-sectional area across thehead section 38. - Referring now to
FIGS. 6a and 6b , there is depicted aballistic armor panel 42 for absorbing and dissipating kinetic energy from high velocity projectiles. Theouter face 44 of thepanel 42 comprises a large number ofceramic bodies 26, as described with reference toFIG. 3 . - The
ceramic bodies 26 are inserted and held in a close-packed,single layer array 46. Excepting the ceramic bodies 26' around the outer borders of the panel, eachbody 26 is positioned with itshead section 28 in direct contact with thehead section 28 of sixadjacent bodies 26. Thus the ceramic bodies provide mutual lateral confinement and reinforcement, which is important for retaining stopping power after a first projectile has impacted thepanel 42 resulting in some damage to theceramic body 26 which was hit.
The stems 12 of thebodies 26 are supported and held by thesubstrate 50. -
FIG. 7 shows a furtherballistic armor panel 52 for absorbing and dissipating kinetic energy from high velocity projectiles.
A plurality ofceramic bodies 18 are seen, as described with reference toFIG. 2 .
Thebodies 18 are retained in aplate member 54 havingmany openings 56, each opening being sized to receive thestem section 58 of one of the ceramic bodies. Theunderside 60 of thehead section 20 of thebody 18 overrides the periphery of theopening 56.
Except for theouter edges 62 of thearmor panel 52, each body is positioned with itshead section 20 in direct contact with sixadjacent bodies 18 inserted in theplate member 54. - Turning now to
FIG. 8 , there is seen a ballistic armor panel faced withceramic bodies 68. Thebody 68 is similar to thebody 26 seen inFIG. 3 , except that the head of thebody 68 is convex.
Theplate member 70 is formed from a plurality of interconnected rings 72. Therings 72 can be mass produced using dedicated tooling therefor. Advantageously therings 72 are further bound together by a solidifiedmaterial 74, for example aluminum, or a thermoplastic polymer such as polycarbonate, or a thermoset plastic such as epoxy. -
FIG 9 shows a further embodiment of aceramic body 76. Thebody 76 is similar to thebody 18 seen inFIG. 2 . An important feature ofbody 76 is achannel 78 provided in the body to reduce the weight per area thereof. Suitably, thechannel 78 occupies a volume of up to 25% of thebody 76.
Thebody 76 is particularly useful for airborne use and for personal applications. - Referring now to
FIG.10 , there is seen a further embodiment of aballistic armor panel 80. Thepanel 80 has an inner 82 and an outer 84 surface, theouter surface 84 facing the impact side.Ceramic bodies 36 are arranged in a plurality of adjacent rows. The axes of thestems sections 40 of thebodies 36 are substantially parallel with each other and perpendicular to the surfaces of thepanels
Preferably theinner layer 82 is formed from a plurality ofadjacent layers 82', 82", each layer comprising a plurality of unidirectional coplanar anti-ballistic fibers embedded in a polymeric matrix. Advantageously, the fibers ofadjacent layers 82', 82", are oriented at an angle of between about 45° to 90° to each other.
In operation the outer, impact-receiving layer deforms and shatters an impacting high velocity projectile. The inner layer, being elastic, is then able to absorb the remaining kinetic energy from the projectile fragments. The elastic material is chosen according to cost and weight considerations applicable to the designated application. Although any suitable material can be used, such as aluminum or woven or non-woven textile material, the preference is for at least 90% Aramide fiber, fiber orientation being as described. The final material selection is based on meeting weight and volume restraints at lowest cost. - Referring now to
FIGS. 11 and 11 a there is seen anarmored vehicle 86 wherein apanel 88 of the present invention has been provided in an opening (not shown) of said vehicle, thepanel 88, in the embodiment shown, incorporating ceramic bodies 90 having cylindrical heads and cylindrical stems, said panel being shown in an enlarged detail view inFIG. 11a . - As will be realized since the panels of the present invention are lighter in weight then steel panels of comparable size and provide even better protection it is advantageous to incorporate several panels according to the present invention in such vehicles in place of standard steel armor in order to reduce the overall weight of the vehicle.
- As is known transparent ceramic material is available as described e.g., in H1567 and H1519 and such material could be used in the panels of the present invention.
- In order to establish the effectiveness of the ceramic bodies of the present invention and composite armor panels incorporating the same a panel was prepared with the size of 10
X 12 in and ceramic bodies having a cylindrical stem and hexagonal head section with a convexly curved end face as illustrated inFIG. 8 was prepared and sent to the H.P. White Laboratory, Inc. in Maryland for ballistic resistance testing. - The description of the test and the results are set forth hereinafter.
TEST PANEL Manufacturor : MOFET ETZION Sample No. : LI8A A Size: 10x12 In. Weight: 7.20 lbs. Dals Rec'd. : 09/04/05 Thioxnoese : 0,919, 0.920, 0.913, 0.909 in. Heronoss: NA Va: HAND CARRIED Aug. Thicx. : 0.915 in. Plies/Laminates : NA Rohrned : FedEx Description : PROPRIETARY SET-UP Primary Vel. Screen = : 15.0 ft., 35.0 ft. Range No. : 3 Shot Spacing : PER CUSTOMER REQUEST Primary Val. Location : 25.0 ft. From Muzzle Temp.: 73 F Wirnoss Ponal : 0.020, 2024T3 ALUMINIUM Residual Vel. Screen : NA BP : 30.17 in. Hg Obliquity: 0 deg. Residual Val. Location: NA RH: 62% booking Material : NA Range la Target : 45.0 ft. Barrel No/Gun : TEST BARREL Conditioning : AMBIENT Target lo Wit. : 6.0 in. Gumnar: FULK Recorder: POOLE AMMUNITION (1): 7.62mm AP. M51, 150 gr. Lot No.: 01FNS88 (2) Lot No.: (3) : Lot No.: (4) : Lot No.: -
- (1) : PER CUSTOMER REQUEST
- (2) :
- (3) :
- As will be noted said panel having a weight of only 7.2 pounds provided exceptional multi-impact performance wherein none of the 7.62 X 51 mm, 150 grain, armor piercing, M61 projectiles fired at a distance of 45 feet from the target penetrated said panel.
- It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments and that the present invention may be embodied in other specific forms. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims.
Short | Ammo. | Time 1 | Velocity 1 | Time 2 | Velocity 2 | Avg. Vel, | Vcl. L.ces | Strico Vel | Punctration | Fouenatic |
No. | (usec) | (ft/s) | (usec) | (ft/a) | (ft=) | (ft/s) | (ft/s) | |||
1 | 1 | 7087 | 2822 | 7091 | 2820 | 2921 | 16 | 2806 | None | |
2 | 1 | 7115 | 2311 | 7118 | 2810 | 2810 | 16 | 2795 | None | |
3 | 1 | 7092 | 2820 | 7093 | 2320 | 2820 | 16 | 2804 | None | |
4 | 1 | 7131 | 2805 | 7137 | 2802 | 2803 | 15 | 2788 | None | |
5 | 1 | 7079 | 2925 | 7082 | 2324 | 2825 | 16 | 2809 | None | |
6 | 1 | 7095 | 2819 | 7098 | 2818 | 2818 | 16 | 2303 | None |
Claims (22)
- A ceramic body for deployment in a composite armor panel, for absorbing and dissipating kinetic energy from high velocity projectiles, said body having a peg-like configuration consisting of a stem section and a head section wherein a cross-sectional area across said stem is less than a cross-sectional area across said head section:
- A ceramic body according to claim 1, wherein said stem section has a regular geometric cross-section.
- A ceramic body according to claim 2, wherein said stem section has a regular polygonal cross-section.
- A ceramic body according to claim 2, wherein said stem section has a circular cross-section.
- A ceramic body according to claim 1, wherein said head section has a regular geometric cross-section.
- A ceramic body according to claim 5, wherein said head section has a regular polygonal cross-section.
- A ceramic body according to claim 5, wherein said head section has a circular cross-section.
- A ceramic body according to claim 1, wherein said body is formed of a ceramic material selected from the group consisting of sintered oxide, nitrides, carbides and borides of alumina, magnesium, zirconium, tungsten, molybdenum, titanium and silica.
- A ceramic body as claimed in claim 1 for absorbing and dissipating kinetic energy from high velocity armor piercing projectiles, wherein said body is made of a material selected from the group consisting of alumina, boron carbide, boron nitride, titanium diboride, silicon carbide, silicon oxide, silicon nitride, magnesium oxide, silicon aluminum oxynitride and mixtures thereof.
- A ceramic body according to claim 1, wherein said head section is provided with a convexly curved end face.
- A ceramic body according to claim 1, characterized in that a channel is provided in said body to reduce the weight per area thereof.
- A ceramic body according to claim 11, wherein said channel occupies a volume of up to 25% of said body.
- A ballistic armor panel for absorbing and dissipating kinetic energy from high velocity projectiles, said panel comprising:a) a plurality of ceramic bodies, according to claim 1 ; andb) a substrate for assembling said bodies in a close-packed, single layer array, such that each of a majority of said bodies is positioned with its head section in direct contact with the head section of at least four adjacent bodies and the stems of said bodies are supported and held by said substrate.
- A ballistic armor panel for absorbing and dissipating kinetic energy from high velocity projectiles, said panel comprising:a) a plurality of ceramic bodies, according to claim 1 ; andb) a substrate for assembling said bodies in a close-packed, single layer array, such that each of a majority of said bodies is positioned with its head section in direct contact with the head section of six adjacent bodies and the stems of said bodies are supported and held by said substrate.
- A ballistic armor panel for absorbing and dissipating kinetic energy from high velocity projectiles, said panel comprising:a) a plurality of ceramic bodies, according to claim 1 ; andb) a plate member having a plurality of openings, each of said opening sized to receive a stem section of a body with the underside of the head section of said body overriding the periphery of said opening, such that each of a majority of said bodies is positioned with its head section in direct contact with the head section of at least four adjacent bodies inserted in said plate.
- A ballistic armor panel for absorbing and dissipating kinetic energy from high velocity projectiles, said panel comprising:a) 6 plurality of ceramic bodies, according to claim 1 ; andb) a plate member having a plurality of openings, each of said opening sized to receive a stem section of a body with the underside of the head section of said body overriding the periphery of said opening, such that each of a majority of said bodies is positioned with its head section in direct contact with the head section of six adjacent bodies inserted in said plate.
- A ballistic armor panel according to claim 16 wherein said plate member is formed from a plurality of interconnected rings.
- A ballistic armor panel according to claim 17 wherein said rings are further bound together by a solidified material.
- A ballistic armor according to claim 16, wherein said panel has an inner and an outer surface, said outer surface facing the impact side and said ceramic bodies are arranged in a plurality of adjacent rows, the axis of the stems of said bodies being substantially parallel with each other and perpendicular to the surfaces of the panels.
- A ballistic armor according to claim 17, further comprising an inner layer adjacent said inner surface of said panel, said inner layer being formed from a plurality of adjacent layers, each layer comprising a plurality of unidirectional coplanar anti-ballistic fibers embedded in a polymeric matrix, the fibers of adjacent layers being at an angle of between about 45° to 90° to each other.
- An armored vehicle comprising a ballistic armor panel according to claim 13.
- A ceramic body according to claim 1 wherein said body is formed of a transparent ceramic material.
Applications Claiming Priority (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL15183002 | 2002-09-19 | ||
IL15183002 | 2002-09-19 | ||
US25611202A | 2002-09-26 | 2002-09-26 | |
US256112 | 2002-09-26 | ||
US10/322,237 US6860186B2 (en) | 2002-09-19 | 2002-12-18 | Ceramic bodies and ballistic armor incorporating the same |
US322237 | 2002-12-18 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1400775A1 EP1400775A1 (en) | 2004-03-24 |
EP1400775B1 true EP1400775B1 (en) | 2008-12-17 |
Family
ID=31950344
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20030255523 Expired - Lifetime EP1400775B1 (en) | 2002-09-19 | 2003-09-04 | Ceramic bodies and ballistic armor incorporating the same |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1400775B1 (en) |
AU (1) | AU2003248118B2 (en) |
CA (1) | CA2439183C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2363682A2 (en) | 2010-03-05 | 2011-09-07 | Krauss-Maffei Wegmann GmbH & Co. KG | Method for repairing a compound armour element and repair set for performing the repairs |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IL158320A0 (en) † | 2003-10-09 | 2004-08-31 | Cohen Michael | A composite armor plate and ceramic bodies for use therein |
IL158045A (en) * | 2003-09-22 | 2010-04-15 | Cohen Michael | Modular armored vehicle system including a combat vehicle chassis with openings and armored plates for covering the same |
US20060213360A1 (en) | 2005-03-23 | 2006-09-28 | Mosche Ravid | Perforated armor plates |
DE102005013660A1 (en) * | 2005-03-24 | 2006-09-28 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Composite armor plate for protecting vehicles or buildings from armor-piercing projectiles with high kinetic energy |
US20090320675A1 (en) * | 2007-04-23 | 2009-12-31 | Landingham Richard L | Mosaic Transparent Armor |
DE102010000648B4 (en) * | 2010-03-05 | 2024-09-19 | Knds Deutschland Gmbh & Co. Kg | Composite armor element for protection against projectiles |
RU2478900C2 (en) * | 2010-12-13 | 2013-04-10 | Николай Алексеевич Кулаков | Composite higher-survivorship armor (versions) |
CN115682837B (en) * | 2022-11-02 | 2023-09-01 | 潍坊衡瑞硼业新材料科技有限公司 | Light bulletproof material and preparation method thereof |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2601562A1 (en) * | 1975-07-02 | 1977-01-13 | Pignal | ARMOR PLATE |
FR2419498A1 (en) * | 1978-03-08 | 1979-10-05 | Merlin Gerin | CAST COMPOSITE SHIELD |
FR2559254A1 (en) * | 1984-02-02 | 1985-08-09 | Picard | Armour resistant to piercing and process for producing it. |
FR2642419A1 (en) * | 1988-12-19 | 1990-08-03 | Europ Propulsion | PROTECTIVE MATERIAL WITH MULTI-LAYERED CERAMIC STRUCTURE |
US6203908B1 (en) * | 1996-08-26 | 2001-03-20 | Michael Cohen | Composite armor |
US6289781B1 (en) * | 1996-08-26 | 2001-09-18 | Michael Cohen | Composite armor plates and panel |
IL124085A (en) * | 1998-04-14 | 2001-06-14 | Cohen Michael | Composite armor panel |
US6200664B1 (en) * | 1999-11-01 | 2001-03-13 | Ward Figge | Explosion barrier |
IL138897A0 (en) * | 2000-10-05 | 2004-08-31 | Cohen Michael | Composite armor panel |
-
2003
- 2003-09-02 CA CA 2439183 patent/CA2439183C/en not_active Expired - Fee Related
- 2003-09-04 EP EP20030255523 patent/EP1400775B1/en not_active Expired - Lifetime
- 2003-09-18 AU AU2003248118A patent/AU2003248118B2/en not_active Ceased
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2363682A2 (en) | 2010-03-05 | 2011-09-07 | Krauss-Maffei Wegmann GmbH & Co. KG | Method for repairing a compound armour element and repair set for performing the repairs |
DE102010000649A1 (en) | 2010-03-05 | 2011-09-08 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method for repairing a composite armor element and repair set for carrying out the repair |
DE102010000649B4 (en) * | 2010-03-05 | 2013-04-25 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method for repairing a composite armor element and repair set for carrying out the repair |
EP2363682B1 (en) | 2010-03-05 | 2019-09-04 | Krauss-Maffei Wegmann GmbH & Co. KG | Method for repairing a compound armour element and repair set for performing the repairs |
Also Published As
Publication number | Publication date |
---|---|
AU2003248118A1 (en) | 2004-04-08 |
EP1400775A1 (en) | 2004-03-24 |
CA2439183A1 (en) | 2004-03-19 |
CA2439183C (en) | 2011-04-05 |
AU2003248118B2 (en) | 2009-01-22 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6860186B2 (en) | Ceramic bodies and ballistic armor incorporating the same | |
US7117780B2 (en) | Composite armor plate | |
CA2532305C (en) | Ceramic pellets and composite armor panel containing the same | |
US6575075B2 (en) | Composite armor panel | |
US6408734B1 (en) | Composite armor panel | |
US6289781B1 (en) | Composite armor plates and panel | |
US7603939B2 (en) | Ceramic bodies for armor panel | |
US8281700B2 (en) | Composite armor plate and ceramic bodies for use therein | |
US20070028757A1 (en) | Composite armor plate and ceramic bodies for use therein | |
EP1080337B2 (en) | Composite armor plate | |
EP1707913B1 (en) | Ceramic pellets and composite armor panel containing the same | |
EP1400775B1 (en) | Ceramic bodies and ballistic armor incorporating the same | |
IL168029A (en) | Ceramic pellets and composite armor panel containing the same |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL LT LV MK |
|
AKX | Designation fees paid | ||
17P | Request for examination filed |
Effective date: 20040807 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: 8566 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
REF | Corresponds to: |
Ref document number: 60325309 Country of ref document: DE Date of ref document: 20090129 Kind code of ref document: P |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 |
|
NLV1 | Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act | ||
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20090328 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20090317 Ref country code: BE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20090518 Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20090317 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 |
|
26N | No opposition filed |
Effective date: 20090918 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20090930 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20090904 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20090930 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20090930 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20090318 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20090904 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20090618 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20081217 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 14 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20160922 Year of fee payment: 14 Ref country code: GB Payment date: 20160928 Year of fee payment: 14 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20160921 Year of fee payment: 14 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20160923 Year of fee payment: 14 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 60325309 Country of ref document: DE |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20170904 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20180531 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180404 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170904 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171002 Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170904 |