EP3055639A1 - Élément de protection équipé d'une couche de découplage - Google Patents
Élément de protection équipé d'une couche de découplageInfo
- Publication number
- EP3055639A1 EP3055639A1 EP14801916.9A EP14801916A EP3055639A1 EP 3055639 A1 EP3055639 A1 EP 3055639A1 EP 14801916 A EP14801916 A EP 14801916A EP 3055639 A1 EP3055639 A1 EP 3055639A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- protective element
- armor plate
- armor
- layer
- decoupling layer
- 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.)
- Granted
Links
- 230000001681 protective effect Effects 0.000 claims description 114
- 239000010410 layer Substances 0.000 claims description 105
- 239000000463 material Substances 0.000 claims description 27
- 239000011241 protective layer Substances 0.000 claims description 25
- 229910000831 Steel Inorganic materials 0.000 claims description 19
- 239000010959 steel Substances 0.000 claims description 19
- 229920001971 elastomer Polymers 0.000 claims description 11
- 239000000919 ceramic Substances 0.000 claims description 10
- 229920003023 plastic Polymers 0.000 claims description 10
- 239000004033 plastic Substances 0.000 claims description 10
- 239000005060 rubber Substances 0.000 claims description 8
- 230000007613 environmental effect Effects 0.000 claims description 5
- 206010041662 Splinter Diseases 0.000 description 16
- 230000035939 shock Effects 0.000 description 11
- 238000002360 preparation method Methods 0.000 description 6
- 239000002131 composite material Substances 0.000 description 5
- 235000019589 hardness Nutrition 0.000 description 5
- 238000004080 punching Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 238000005452 bending Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000013016 damping Methods 0.000 description 3
- 239000000806 elastomer Substances 0.000 description 3
- 230000002349 favourable effect Effects 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 230000000149 penetrating effect Effects 0.000 description 3
- 238000005299 abrasion Methods 0.000 description 2
- 239000000654 additive Substances 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 239000003365 glass fiber Substances 0.000 description 2
- 230000003116 impacting effect Effects 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229920003052 natural elastomer Polymers 0.000 description 2
- 229920001194 natural rubber Polymers 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 229920002635 polyurethane Polymers 0.000 description 2
- 239000004814 polyurethane Substances 0.000 description 2
- 239000004576 sand Substances 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 229920003051 synthetic elastomer Polymers 0.000 description 2
- 239000005061 synthetic rubber Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 description 1
- 229910052580 B4C Inorganic materials 0.000 description 1
- 241000273930 Brevoortia tyrannus Species 0.000 description 1
- 244000043261 Hevea brasiliensis Species 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 229910033181 TiB2 Inorganic materials 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000004040 coloring Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- -1 polyethylene Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 238000004382 potting Methods 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 230000002123 temporal effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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
-
- 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
- F41H5/0428—Ceramic layers in combination with additional layers made of fibres, fabrics or plastics
-
- 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
- F41H5/0442—Layered armour containing metal
- F41H5/0457—Metal layers in combination with additional layers made of fibres, fabrics or plastics
Definitions
- the invention relates to a protective element for protecting an object from military threats with an armor plate, which has a threat side pointing in the direction of a threat and an object side pointing in the direction of the object to be protected. Further objects of the invention form a protective element arrangement and a vehicle body with such a protective element.
- Protective elements for the protection of objects, such as vehicles, bunkers, containers, etc. against military threats, such as more punctual impinging armor-piercing ammunition bodies or rather surface-impacting splinters, which arise, for example, during the detonation of a mine, are known from the prior art in various designs.
- protective elements made of a particularly hard material are mostly used, by means of which good protection against these rather punctiform ammunition bodies can be achieved.
- the use of ceramics or ultrahard armor steels has proven particularly useful in recent years.
- Such a protective element is known, for example, from EP 0 251 395 A1.
- the protective element On the threat side, the protective element has a harder but brittle ceramic layer for protection against armor-piercing ammunition and, on its object side facing the object to be protected, several layers of an aluminum alloy for protection against splinters.
- an aluminum alloy for protection against splinters.
- the invention is therefore based on the invention to provide a simple in construction, effective against armor-piercing ammunition as well as against splinters protective element.
- this object is achieved by a decoupling layer arranged on the threat side. Due to the arrangement of a decoupling layer on the threat side of the armor plate, an armor-piercing ammunition as well as a splinter initially strikes the decoupling layer. For an armor-piercing ammunition, the decoupling layer does not represent any appreciable resistance. The armor piercing ammunition striking the protective element penetrates the coupling layer largely undisturbed and is trapped on the underlying, much harder armor plate. When a rather flat meeting of a splitter on the decoupling layer results in a shock wave, which is initiated by the splitter on the decoupling layer in the armor plate.
- the shockwave propagates faster within the decoupling layer than the splitter penetrates into the decoupling layer, the shockwave runs in front of the penetrating splitter in the direction of the armor plate located behind it.
- the resistance of the protective element is thus increased by simple means such that both armor piercing ammunition and splinters are held in a simple manner.
- the armor plate is designed as a tank steel plate or as a ceramic armor plate.
- the armor steel plate can consist of ultra-hard steel armor.
- a ceramic armor plate this can be formed by a flat ceramic plate or several smaller ceramic elements, which are encapsulated by means of a potting compound to a composite armor plate.
- aluminum oxide, aluminum nitride, silicon carbide, boron carbide and titanium diboride may be considered as ceramic materials.
- the decoupling layer is arranged directly on the armor plate.
- a direct arrangement a defined transmission of the shock wave is achieved when a splitter hits the decoupling layer on the armor plate.
- the decoupling layer is glued to the armor plate, screwed or clamped.
- the decoupling layer is applied directly to the armor plate. For example, it can be sprayed on, painted on or be infused. It is particularly advantageous if the decoupling layer is attached over the entire surface of the armor plate.
- the thickness of the decoupling layer can be between 0.5 mm and 50 mm, preferably between 0.5 mm and 10 mm and even more preferably between 2 mm and 6 mm.
- the decoupling layer consists of a plastic or rubber material. Such materials have a much higher modulus of elasticity than the armor plate. As a result, a kind of damping effect is achieved.
- the decoupling layer comprises rubber, polymers, elastomers, natural and / or synthetic rubber, wherein a decoupling layer of an elastomer material is also distinguished over relatively long temperature ranges by good decoupling properties.
- the decoupling layer may consist of non-foamed polyurethane.
- the plastic or rubber material of the decoupling layer is formed fiber-free.
- the plastic or rubber has a homogeneous composition.
- the plastic or the rubber additives to increase the fire resistance, fire resistance, scratch resistance, abrasion resistance and / or coloration are examples of the plastic or the rubber additives to increase the fire resistance, fire resistance, scratch resistance, abrasion resistance and / or coloration.
- a reliable decoupling is achieved if the material of the decoupling layer has a Shore hardness of 70 to 95, in particular of 90. It is also advantageous for the decoupling properties if the material of the decoupling layer has a rebound resilience of 30% to 50%.
- the material of the decoupling layer has a bending coefficient of 2000 psi to 7000 psi.
- the material of the decoupling layer has a basis weight of 0.8 to 1, 5 kg / m 2 per mm thickness, in particular from 1, 0 to 1, 2 kg / m 2 per mm thickness.
- the decoupling layer is preferably arranged over the entire surface of the armor plate.
- a further development of the invention provides, in the case of an armor plate consisting of armor steel, that the armor plate has a hardness of at least 380 Brinell, preferably at least 500 Brinell and more preferably at least 600 Brinell.
- the armor plate has a hardness of at least 380 Brinell, preferably at least 500 Brinell and more preferably at least 600 Brinell.
- the thickness of the armor plate is preferably between 2 mm and 20 mm. It is preferably between 2 mm and 12 mm and more preferably between 4 mm and 10 mm. These thicknesses have proven especially in trained as armor steel plates armor plates.
- An embodiment which is advantageous in terms of a compact design provides that the protective element has a multilayer structure in which chem the armor plate forms the thickest single layer.
- the thickness of the armor plate may amount to at least 15%, preferably at least 50% and more preferably at least 75% of the thickness of the protective element.
- the ratio of the thickness of the armor plate to the thickness of the decoupling layer is at least 1 and / or at most 10, more preferably at least 2 and at most 5.
- the protective element has a protective layer covering the decoupling layer for protection against fire and / or environmental influences.
- the resistance of the protective element against environmental influences and fire can be increased. Also results in an extension of the lifetime of the protective element. Maintenance intervals are shortened.
- the damping effect of the decoupling layer can be improved by the protective layer, since the impact of a splitter is transferred from the protective layer to a larger surface of the decoupling layer than would be the case with a direct impact on the decoupling layer.
- the thickness of the protective layer is preferably 0.05 to 5 mm, more preferably 0.1 to 1 mm. In this thickness range, a good protective effect for the protective element against environmental influences sets in and the weight of the protective element is not unnecessarily increased.
- the protective layer is made of fiber composite material, metal or sand.
- fiber composite material metal or sand.
- Particularly advantageous are glass fiber composite material, Aluminum and steel proven, the steel is preferably thinner and softer than the armor plate.
- the armor plate is harder than the protective layer and the protective layer is harder than the decoupling layer.
- the protective layer is harder than the decoupling layer.
- the armor plate forms the hardest layer of the protective element.
- the protective layer advantageously forms on the threat side, the outermost layer of the protective element, so that the underlying layers are protected by the protective layer.
- the protective layer is preferably arranged directly on the decoupling layer. It can be glued to the decoupling layer, screwed, clamped or applied directly, in particular sprayed on, brushed or poured.
- the armor plate, the decoupling layer and / or the protective layer are preferably formed recess-free and / or free of cavities.
- the protective element is designed as a protection module.
- the protective element as
- the protective element can be mounted as a unit to an object and dismantled. In this respect, the assembly and the replacement of damaged protective elements is particularly simplified. In addition, to solve the above problem in a protective element arrangement of the type mentioned above, it is proposed that this has a protective element with one or more of the features described above.
- the protective element arrangement has a second armor plate, which is arranged on the object side of the protective element. Over the second armor plate a certain redundancy is achieved, so that even in the event of a breach of the outer protective element or its first armor plate protection is still given.
- the second armor plate is arranged at a distance from the armor plate of the protective element. By the distance, the protective effect of the protective element arrangement can be further increased.
- the disputed arrangement of the two pan plates results in a clearance space.
- the distance space between the armor plate of the protective element and the second armor plate may be filled with air and allow bending of the protective element, without this strikes directly on the underlying armor plate.
- the distance between the armor plate of the protective element and the second armor plate is preferably 2 mm to 50 mm, particularly preferably 4 mm to 15 mm.
- the second armor plate may be formed material identical to the armor plate of the protective element.
- the thicknesses of the two armor plates may be substantially the same.
- a decoupling layer is arranged on the threat side of the second armor plate. The decoupling layer may be formed analogously to the decoupling layer of the protective element, whereby the already described advantages result here as well.
- a third armor plate is disposed between the armor plate of the protective element and the second armor plate.
- the protective effect of the protective element arrangement can be further increased.
- the third armor plate is formed material identical to the first and / or second armor plate.
- the armor plate of the protective element, the second armor plate and the third armor plate are spaced from each other.
- the protective effect can be further increased.
- the distances of air gaps are formed.
- the distance between the second armor plate and the third armor plate is greater than the distance between the third armor plate and the armor plate of the protective element.
- the distance between the second armor plate and the third armor plate is 2 to 3 times greater than the distance between the third armor plate and the armor plate of the protective element.
- All armor plates may be formed identical material or made of different materials.
- the armor plates can be designed as armor steel plates and / or ceramic armor plates.
- one of the armor plates is formed as part of a vehicle body, whereby a particularly compact vehicle body or a particularly compact vehicle can be realized.
- This embodiment is particularly suitable for existing from a steel armor body parts, such as in particular the vehicle trays commonly used in military vehicles.
- the innermost armor plate is formed as part of the vehicle body, in particular as part of a vehicle pan receiving the vehicle crew.
- FIG. 1 is a schematic sectional view of a protective element according to the invention, a schematic sectional view of a protective element arrangement according to a first embodiment, Fig. 3 is a schematic sectional view of a protective element arrangement according to a second embodiment and
- Fig. 1 shows a schematic view of a protective element 1 for the protection of objects against military threats.
- the protective element 1 is a protective module which can be attached as a structural unit to an object to be protected, such as a military vehicle, for its protection against armor-piercing ammunition as well as for protection against splinters.
- the protective element 1 has an armor plate 2 consisting of a high-hardness material with a threat side 3 pointing in the direction of the military threat and an object side 4 pointing in the direction of the object to be protected.
- the armor plate 2 forms the innermost layer of the protective element 1 and serves mainly to protect against armor-piercing ammunition body, which penetrate the outer layers largely undisturbed and are not significantly affected until they reach the armor plate 2.
- the armor plate 2 is according to the embodiment, a high-strength armor steel plate with a hardness of more than 380 Brinell.
- the armor plate 2 not only forms the innermost layer of the protective element 1, but at the same time also its hardest layer in order to act against armor-piercing ammunition.
- the armor plate 2 has in the embodiment has a thickness of 10 mm.
- ceramic armor plates 2 have proven themselves under weight aspects.
- armor plates 2 of a high-hardness material act reliably against bombardment by armor-piercing ammunition which hits almost punctually, however, they have weaknesses in the case of splinters which act more extensively, armor plate 2 is preceded by a decoupling layer 5 at its threat side.
- the decoupling layer 5 can not provide any appreciable protection, since this consists of a softer material that is comparatively easy to penetrate from such a projectile.
- the decoupling layer 5 serves to protect against splinters, which rather impinge on the protective element 1 over a large area and, if they hit the brittle armor plate 2 directly, would, under certain circumstances, puncture them.
- the decoupling layer 5 serves in the manner of a damping layer, to prepare the splitter on the later impact on the armor plate 2 so that it will not penetrate.
- an elastic shock wave is introduced into the armor plate 2 via the decoupling layer 5.
- the shock wave is formed upon impact of the splitter on the decoupling layer 5 and propagates through it in the direction of the underlying armor plate 2 continued. Since the shock wave within the decoupling layer 5 moves faster than the splitter penetrates into the layer, the shockwave and the splitter uncouple from each other on the armor plate 2. This decoupling the impact of the splitter on the armor plate in time, space and geometric so prepared that the existing of a brittle material armor plate 2 is not punched.
- the decoupling layer 5 is located directly on the threat side of the armor plate 2 and is connected to this area by gluing. Alternatively, the decoupling layer 5 can also be bolted to the armor plate 2, clamped, sprayed on, painted or poured.
- the thickness of the decoupling layer is 4 mm.
- a thickness of the decoupling layer between 0.5 mm and 50 mm has proven to be advantageous. Particularly good results were found in a thickness range of 2 mm to 6 mm.
- the modulus of elasticity of the decoupling layer 5 is considerably lower than that of the armor plate 2.
- the decoupling layer 5 consists of non-foamed polyurethane. In principle, however, other materials are suitable as decoupling layer 5.
- the material of the decoupling layer 5 is comparatively soft. Plastics and rubber materials have proven to be particularly suitable.
- the Decoupling layer 5 of rubber, polymer, elastomer, natural rubber and / or synthetic rubber.
- the decoupling layer 5 can also be constructed of plastic mixtures.
- the plastic is formed without reinforcing fibers, so fiber-free.
- the plastic preferably has a homogeneous structure. However, additives for increasing the fire resistance, fire resistance, scratch resistance, abrasion resistance and / or coloring can be added to the plastic of the decoupling layer 5.
- Particularly suitable materials for the decoupling layer 5 have a rebound resilience of 30% to 50, a Shore hardness of 70 to 75 and / or a bending coefficient of 2000 psi to 7000 psi.
- the basis weight of the decoupling layer 5, in the embodiment 1, 1 kg per square meter per millimeter thickness.
- a protective layer 6 is provided for protection against external influences such as environmental influences or even fire or similar influences. By the protective layer 6 can be prevented, for example, that thrown on the vehicle Molotov cocktails damage the decoupling layer 5 in the way that it loses its effect.
- the protective layer 6 has a smaller thickness than the decoupling layer 5.
- the protective layer 6 forms the outermost layer of the protective element 1, is harder than the decoupling layer 5 and softer than the armor plate 2.
- the protective layer 6 consists of a fiber composite material, a metal such as steel or aluminum and / or sand.
- the protective layer 6 is made of a glass fiber composite material.
- the protective layer 6 is arranged directly on the decoupling layer 5 and bonded to the decoupling layer 5.
- the protective layer 6 can also be dersartig be connected to the decoupling layer 5, for example by coating or releasable connection, for example by jamming.
- FIG. 2 initially shows a protective element arrangement 10 with a protective element 1, in which further elements 7, 8 are arranged on the object side to improve the protective effect in a type of redundant arrangement.
- a second armor plate 7 is arranged, which is formed substantially identical to the armor plate 2 of the protective element 1.
- the second armor plate 7 also has a decoupling layer 8 on its threat side 11. However, this can also be omitted according to further, not shown embodiments.
- the armor plate 7 has a distance a relative to the armor plate 2 of the protective element 1, so that a clearance space is created between the protective element 1 and the armor plate 7 or the decoupling layer 8.
- the spacer space 13 is filled with air, which is why the protective element 1 can deform in the direction of the armor plate 7 or the decoupling layer 8 located behind it without colliding with it.
- FIG. 3 shows a further embodiment of a protective element arrangement 10.
- This protective element arrangement 10 essentially corresponds to the protective element arrangement according to FIG. 2, but has a third armor plate 9 which divides the spacer space 13 into two spacing spaces 14 and 15.
- the armor plate 2 of the protective element 1 has a distance b from the third armor plate 9 and the third armor plate 9 has a distance c from the second armor plate 7.
- the armor plates 2, 7, 9 are each formed as separate plate parts according to the illustrations in the figures, it is also conceivable that at least one of the armor plates 2, 7, 9 is formed by an armored vehicle trough.
- the left FSP 20 was fired on an armor plate 2 without a decoupling layer and penetrated it.
- the armor plate 2 behaves with the decoupling layer 5 against the impacting splitter tougher and punching are avoided.
- the arrangement of a decoupling layer 5 on the threat side 3 of an armor plate 2 a significantly higher level of protection is achieved and effective in a structurally simple structure punching through the armor plate 2 prevented. Overall, a significantly improved protection against armor-piercing ammunition as well as against splinters is achieved with simple means even with only a slight increase in weight compared to a simple armor plate 2.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102013111137.8A DE102013111137A1 (de) | 2013-10-08 | 2013-10-08 | Schutzelement mit Entkopplungsschicht |
PCT/DE2014/100351 WO2015051783A1 (fr) | 2013-10-08 | 2014-10-07 | Élément de protection équipé d'une couche de découplage |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3055639A1 true EP3055639A1 (fr) | 2016-08-17 |
EP3055639B1 EP3055639B1 (fr) | 2019-12-11 |
Family
ID=51945659
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14801916.9A Active EP3055639B1 (fr) | 2013-10-08 | 2014-10-07 | Élément de protection équipé d'une couche de découplage |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP3055639B1 (fr) |
DE (1) | DE102013111137A1 (fr) |
WO (1) | WO2015051783A1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102015116879B4 (de) | 2015-10-05 | 2019-10-31 | BENTELER Lightweight Protection GmbH & Co. KG | Fahrzeug-Panzerungsbauteil |
DE102015116884A1 (de) * | 2015-10-05 | 2017-04-06 | Benteler Defense Gmbh & Co. Kg | Fahrzeug-Panzerungsbauteil |
DE102019116363A1 (de) | 2019-06-17 | 2020-12-17 | Benteler Automobiltechnik Gmbh | Verfahren zur Herstellung eines Panzerungsbauteils für Kraftfahrzeuge |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4545286A (en) * | 1984-06-14 | 1985-10-08 | Victor Fedij | Active armor |
NL8601650A (nl) | 1986-06-24 | 1988-01-18 | Fokker Special Products | Pantserplaat. |
DE3741090A1 (de) * | 1987-12-04 | 1989-06-22 | Mak Maschinenbau Krupp | Flaechendaempfer fuer panzerfahrzeuge |
GB8918252D0 (en) * | 1988-12-10 | 1998-11-18 | Diehl Gmbh & Co | Armour |
DE10007186A1 (de) * | 2000-02-17 | 2001-10-11 | Verseidag Indutex Gmbh | Schutzvorrichtung |
US6532857B1 (en) * | 2000-05-12 | 2003-03-18 | Ceradyne, Inc. | Ceramic array armor |
DE10200472A1 (de) * | 2002-01-09 | 2003-07-10 | Contitech Vibration Control | Minenschutz für gepanzerte Fahrzeuge gegen Anti-Tank-Minen |
WO2005103363A2 (fr) * | 2004-04-23 | 2005-11-03 | The United States Of America, As Represented By The Secretary Of The Navy | Armature comprenant un elastomere durcissant sous sollicitations |
ATE449948T1 (de) * | 2003-12-29 | 2009-12-15 | Ruag Land Systems | Schutz-schicht gegen geformte ladungen |
-
2013
- 2013-10-08 DE DE102013111137.8A patent/DE102013111137A1/de not_active Withdrawn
-
2014
- 2014-10-07 WO PCT/DE2014/100351 patent/WO2015051783A1/fr active Application Filing
- 2014-10-07 EP EP14801916.9A patent/EP3055639B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
EP3055639B1 (fr) | 2019-12-11 |
WO2015051783A1 (fr) | 2015-04-16 |
DE102013111137A1 (de) | 2015-04-09 |
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