EP1078215B1 - Use of metal foams in armor systems - Google Patents

Use of metal foams in armor systems Download PDF

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Publication number
EP1078215B1
EP1078215B1 EP00937503A EP00937503A EP1078215B1 EP 1078215 B1 EP1078215 B1 EP 1078215B1 EP 00937503 A EP00937503 A EP 00937503A EP 00937503 A EP00937503 A EP 00937503A EP 1078215 B1 EP1078215 B1 EP 1078215B1
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Prior art keywords
metal
foam
deformation
layered
absorbing element
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EP00937503A
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German (de)
French (fr)
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EP1078215A1 (en
Inventor
Chin-Jye Yu
Terry Dennis Claar
Harald Heinrich Eifert
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Fraunhofer Gesellschaft zur Forderung der Angewandten Forschung eV
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Fraunhofer Gesellschaft zur Forderung der Angewandten Forschung eV
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/02Plate construction
    • F41H5/04Plate construction composed of more than one layer
    • F41H5/0442Layered armour containing metal

Definitions

  • This invention relates generally to armor systems for structural protection against ballistic impact or explosive blast, and more particularly to the use of a metallic foam as the shock energy-absorbing element in a multi-layer armor system.
  • a typical configuration for the armor system in medium weight military vehicles for example, consists of a high strength strike face (either a metal or a ceramic plate), bonded to a ceramic tile, which is subsequently bonded to a metallic backing plate.
  • the ceramic tile breaks-up or deforms an incoming projectile, and the metallic backing "catches" the extant penetrator and ceramic fragments.
  • the high strength strike plate aids the ceramic tile by providing front face confinement, and may, in some cases, protect the ceramic tile from field damage.
  • the three layer system includes a strike plate, a backing plate and an intermediate layer to reduce the risk of failure of the strike plate in order to limit backface deformation.
  • provision of the intermediate layer is of only limited benefit and there is therefore a need for an armour system to be provided having an improved shock absorbing element, and more particularly a shock absorbing element that gives more control of behind the target effects, such as backface deformation and spalling.
  • Metallic foams with a high fraction of porosity are a new class of materials which have attributes that lend themselves to various engineering applications, including sound and heat isolation, lightweight construction, and energy absorption.
  • the unique characteristics of a metallic cellular material include its comparatively high specific strength and its characteristic non-linear deformation behaviour.
  • An example of the use of metallic foams in an armour system is disclosed in DE2039343 which discloses an armour wall for a vehicle comprising two layers, one of which is a metal foam layer.
  • Such a two-layer armour system suffers from the same problem as mentioned above of a high failure rate and little or no control of behind the targets effects, such as backface deformation and spalling.
  • metal foams are effective in containing rearward deformation of a target under high-speed impact, and therefore are useful in controlling backface deformation and spalling. Moreover, metal foams are capable of mitigating impact-induced stress waves thereby delaying damage to ceramic layers in armour systems employing same.
  • an object of the invention to provide an armour system incorporating metal foam as a shock energy-absorbing element to improve protection of equipment and personnel behind the target.
  • this invention provides a multilayered armour system comprising a strike plate, a deformable back plate and one or more intermediate layers there-between, characterised in that the one or more intermediate layers include a shock absorbing element comprising a metallic foam having cells distributed therethrough and, on application of a force on said strike plate, the shock absorbing element is urged to undergo progressive modes of deformation corresponding to a substantially linear elastic deformation, a cellular collapse deformation and a densification deformation, in response to the magnitude of the force applied to the strike plate.
  • a shock absorbing element comprising a metallic foam having cells distributed therethrough and, on application of a force on said strike plate, the shock absorbing element is urged to undergo progressive modes of deformation corresponding to a substantially linear elastic deformation, a cellular collapse deformation and a densification deformation, in response to the magnitude of the force applied to the strike plate.
  • the metallic foam has a closed-cell pore structure and a high fraction of porosity, preferably ranging from about 50-98 percent by volume.
  • Metallic foams useful in the practice of the present invention may be, but are not limited to, metal foams of aluminum, steel, lead, zinc, titanium, nickel and alloys or metal matrix composites thereof.
  • Metal foams can be fabricated by various processes that are known for the manufacture of metal foams, including casting, powder metallurgy, metallic deposition, and sputter deposition. Exemplary processes for making metal foams are set forth in U.S. Patent Nos. 5,151,246; 4,973,358; and 5,181,549, the text of which is incorporated herein by reference.
  • the foamable material is heated to temperatures near the melting point of the matrix metal(s). During heating, the foaming agent decomposes, and the released gas forces the densified material to expand into a highly porous structure.
  • the density of the metal foams can be controlled by adjusting the content of the foaming agent and several other foaming parameters, such as temperature and heating rate.
  • the density of aluminum foams typically ranges from about 0.5 to 1 g/cm 3 .
  • Strength, and other properties of foamed metals can be tailored by adjusting the specific weight (or porosity), alloy composition, heat treatment history, and pore morphology as is known to those of skill in the art.
  • the metallic foam will have high mechanical strength.
  • Metal foams are easily processed into any desired shape or configuration by conventional techniques, such as sawing drilling, milling, and the like. Moreover, metal foams can be joined by known techniques, such as adhesive bonding, soldering, and welding.
  • the shock-absorbing element is closed-cell aluminum foam, and in a specific illustrative embodiment, the shock-absorbing element is closed-cell aluminum foam with a porosity of 80 percent by volume.
  • a multi-layered armor system suitable for structural protection against ballistic impact or explosive blast, such as armor systems used in connection with military armored vehicles, includes one or more layers of a metal foam as a shock energy-absorbing element.
  • multi-layer armor system means at least two plates of metal, metal foam, ceramic, plastic, and the like, known or developed, for defense or protection systems.
  • the multi-layer armor system includes at least a strike plate, or buffer plate, bonded or otherwise held in communication with, a shock-absorbing element that is a layer of metallic foam.
  • the metallic foam preferably has a closed-cell pore structure and a high fraction of porosity.
  • the metallic foam may be aluminum, steel, lead, zinc, titanium, nickel and alloys or metal matrix composites thereof, with porosity ranging from about 50-98 percent by volume.
  • the metallic foam is a closed-cell aluminum foam having a porosity of 80 percent by volume.
  • the term "strike plate” refers to a high strength metal or ceramic plate that has a front face surface that would receive the initial impact of a projectile or blast.
  • the back surface of the strike plate is adjacent to a first surface of the shock-absorbing element that, in the present invention, is a sheet or layer of metallic foam.
  • the term “strike plate,” as used herein, refers to any buffer plate of a high strength material that receives impact or impact-induced stress waves prior to a shock-absorbing element.
  • the strike plate may be a flat sheet of a high strength metal, ceramic or polymer-based composite, such as a fiber-reinforced polymer composite.
  • the multi-layer armor system of the present invention further includes a deformable backing plate bonded to, or otherwise held in communication with, a face surface of the metallic foam sheet or layer opposite, or distal, to the surface contiguous to the strike plate.
  • the backing plate illustratively is a sheet of a deformable metal, such as titanium, aluminum, or steel.
  • a shock-absorbing layer of metallic foam is sandwiched between a high strength strike plate and a deformable backing plate.
  • the multi-layered armor system may comprise additional elements, in any sequence, and the embodiments presented herein are solely for the purposes of illustrating the principles of the invention.
  • Fig. 1 is an illustrative schematic representation of an improved armor system 10 of the type having a high strength strike plate 11, at least one shock energy-absorbing element 12, and a backing plate 13.
  • a closed-cell metal foam is used as shock energy-absorbing element 12.
  • High strength strike plate 11 may be ceramic or metal.
  • Backing plate 13 is typically a highly deforming metal, such as titanium, aluminum, or steel. However, backing plate 13 may comprise one or more layers of metal and/or ceramic, as well as polymer-based composites.
  • the closed-cell metal foam is effective in containing rearward deformation of the strike plate 11 in a ballistic target structure.
  • the metal foam has the ability to control backface deformation, without sacrificing ballistic efficiency behind targets with highly deforming back plates, via a mechanism that will be discussed more completely hereinbelow.
  • the shock energy-absorbing element 12 preferably comprises a closed-cell metallic foam which, illustratively, may be aluminum, steel, lead, zinc, titanium, nickel, and alloys or metal matrix composites thereof.
  • Preferred metal foams have a high fraction of porosity, typically ranging from about 50-98 by volume percent.
  • shock energy-absorbing element 12 is a closed-cell aluminum foam having a porosity of 80 by volume.
  • Fig. 2 shows the microstructure ( i.e. , the pore structure) of this particular aluminum foam material.
  • This type of pore structure provides a substantial increase in the stiffness/weight ratio (SWR) of the material with a low fractional density. Under deformation, this microstructure features localized cell collapse and rapid compaction energy dissipation, which leads to unique deformation behaviors and material properties including high SWR and energy absorption in the material.
  • SWR stiffness/weight ratio
  • Fig. 3 is a graphical representation of the behavior of the metal foam of Fig. 2 under uniaxial load referred to as a "loading curve.”
  • the vertical axis of Fig. 3 represents stress and the horizontal axis represents strain.
  • the loading curve of Fig. 3 is divided into three regions: linear elastic region 31, collapse region 32 (where plateau stress remains relatively constant) and densification region 33. In linear elastic region 31, the elastic portion of the stress-strain curve is only partially reversible.
  • small-scale localized plastic deformation has already taken place within the sample.
  • Metal foams can be fabricated to maximize the energy absorption capability by adjusting foam parameters including alloying elements, density level, cell size, wall thickness, and uniformity. Improvements in modulus and plateau stress via heat treatment of the metal foam, or via addition of particulate or whisker reinforcements to the metal foam, are additional techniques known to increase the energy absorption capability.
  • Metal foams are capable of mitigating the impact-induced stress waves from the strike plate, thereby delaying or eliminating damage to underlying layers, which in some embodiments might be a ceramic tile, and improving protection of the personnel and equipment behind the target.
  • the deformation energy due to shock impact first densifies the front portion (in the loading direction) of the metal foam layer that forms the shock energy-absorbing element. Subsequent deformation introduces tearing and shearing of the cell walls, an effect of core shearing deformation for energy dissipation in the cellular structure. Thus, the deformation energy is redirected and dissipated sideways. This is best illustrated in Fig. 4 which is a cross-sectional view of the microstructure of the aluminum foam of Fig. 2 showing deformation following high energy impact.
  • This type of deformation mechanism reduces the transmitted deformation energy behind the target in the loading direction.
  • the energy of the impact-induced stress waves is also dissipated efficiently within the cellular network.
  • the high degree of porosity in metal foam is beneficial for the absorption of the wave energy, and the cellular network generates the cavity effect for scattering the wave energy within the network.
  • the armor systems of the present invention would be useful as protection systems for ballistic impact and for blast.
  • the illustrative embodiment presented herein is directed to a three element system, it is to be understood that invention contemplates the use of closed-cell, high strength metal foams having a high fraction of porosity, as a shock energy-absorbing element in any other configuration developed, or to be developed, wherein its ability to contain rearward deformation under high-speed impact, would be useful.

Abstract

In a multi-layer armor system (10), useful for military vehicles, a metallic foam is provided as the shock energy-absoring element. In a typical arrangement, the metallic foam shock-absorbing element (12) is sandwiched between a high strength strike plate (11) and a backing plate (13). Typically, the backing plate is a highly deforming metal, such a titanium, aluminum, or steel. Howevere, the backing plate may comprise one or more layers of metal, ceramic or polymer-based composites. The high strength strike plate may be ceramic or metal. The shock-absorbing element is preferably a closed-cell metal foam with a high porosity that is effective in containing rearward deformation of the strike plate from a projectile strike. In preferred embodiment, the shock-absorbing element is an aluminum foam with a porosity of 80 percent by volume.

Description

BACKGROUND OF THE INVENTION FIELD OF THE INVENTION
This invention relates generally to armor systems for structural protection against ballistic impact or explosive blast, and more particularly to the use of a metallic foam as the shock energy-absorbing element in a multi-layer armor system.
DESCRIPTION OF THE RELATED ART
With increasing terroristic violence and military action, there is a need for improved structural protection against ballistic impact from projectiles or blast protection from explosives. Such structural protection can be built into the infrastructure of a building to reinforce the building, or certain rooms within a building, against attack. Structural protection is also useful in vehicles, illustratively military vehicles, such as tanks, or civilian VIP vehicles. Presently, a multi-layer armor system is employed in known vehicular applications.
A typical configuration for the armor system in medium weight military vehicles, for example, consists of a high strength strike face (either a metal or a ceramic plate), bonded to a ceramic tile, which is subsequently bonded to a metallic backing plate. In this configuration, the ceramic tile breaks-up or deforms an incoming projectile, and the metallic backing "catches" the extant penetrator and ceramic fragments. The high strength strike plate aids the ceramic tile by providing front face confinement, and may, in some cases, protect the ceramic tile from field damage.
Upon projectile impact at typical ordnance velocities, a stress wave is generated and propagates through the ceramic tile. Reflections from boundaries and subsequent stress wave interactions result in tensile stress states and attendant microcracking. Microcracking due to these impact-induced stress waves weakens the ceramic tile, allowing a projectile to penetrate more easily. In armor system designs utilizing a metal strike plate over ceramic tile, stress waves from a projectile impact on the metal strike plate can run ahead into the ceramic, and failure may initiate prior to contact of the projectile with the ceramic tile. In an attempt to overcome the abovementioned problem, a three layer system has been proposed and is disclosed in DE9007336U. The three layer system includes a strike plate, a backing plate and an intermediate layer to reduce the risk of failure of the strike plate in order to limit backface deformation. However, provision of the intermediate layer is of only limited benefit and there is therefore a need for an armour system to be provided having an improved shock absorbing element, and more particularly a shock absorbing element that gives more control of behind the target effects, such as backface deformation and spalling.
Metallic foams with a high fraction of porosity are a new class of materials which have attributes that lend themselves to various engineering applications, including sound and heat isolation, lightweight construction, and energy absorption. In particular, the unique characteristics of a metallic cellular material include its comparatively high specific strength and its characteristic non-linear deformation behaviour. An example of the use of metallic foams in an armour system is disclosed in DE2039343 which discloses an armour wall for a vehicle comprising two layers, one of which is a metal foam layer. However, such a two-layer armour system suffers from the same problem as mentioned above of a high failure rate and little or no control of behind the targets effects, such as backface deformation and spalling.
As will be described more completely hereinbelow, certain metal foams are effective in containing rearward deformation of a target under high-speed impact, and therefore are useful in controlling backface deformation and spalling. Moreover, metal foams are capable of mitigating impact-induced stress waves thereby delaying damage to ceramic layers in armour systems employing same.
It is, therefore, an object of the invention to provide an armour system incorporating metal foam as a shock energy-absorbing element to improve protection of equipment and personnel behind the target.
It is a further object of the invention to provide an armour system incorporating metal foam as a shock energy-absorbing element to control behind-the-target effects as a result of backface deformation caused by the high energy impact of a projectile.
Summary of the Invention
The foregoing and other objects, features and advantages are achieved by this invention which provides a multilayered armour system comprising a strike plate, a deformable back plate and one or more intermediate layers there-between, characterised in that the one or more intermediate layers include a shock absorbing element comprising a metallic foam having cells distributed therethrough and, on application of a force on said strike plate, the shock absorbing element is urged to undergo progressive modes of deformation corresponding to a substantially linear elastic deformation, a cellular collapse deformation and a densification deformation, in response to the magnitude of the force applied to the strike plate.
In preferred embodiments, the metallic foam has a closed-cell pore structure and a high fraction of porosity, preferably ranging from about 50-98 percent by volume.
Metallic foams useful in the practice of the present invention may be, but are not limited to, metal foams of aluminum, steel, lead, zinc, titanium, nickel and alloys or metal matrix composites thereof. Metal foams can be fabricated by various processes that are known for the manufacture of metal foams, including casting, powder metallurgy, metallic deposition, and sputter deposition. Exemplary processes for making metal foams are set forth in U.S. Patent Nos. 5,151,246; 4,973,358; and 5,181,549, the text of which is incorporated herein by reference.
U.S. Patent 5,151,246, for example, describes a powder metallurgy process for making foamable materials using metallic powders and small amounts of propellants. The process starts by mixing commercially available metal powder(s) with a small amount of foaming agent. After the foaming agent is uniformly distributed within the matrix material, the mixture is compacted to yield a dense, semifinished product without any residual open porosity. Further shaping of the foamable material can be achieved through subsequent metalworking processes such as rolling, swaging or extrusion.
Following the metalworking steps, the foamable material is heated to temperatures near the melting point of the matrix metal(s). During heating, the foaming agent decomposes, and the released gas forces the densified material to expand into a highly porous structure. The density of the metal foams can be controlled by adjusting the content of the foaming agent and several other foaming parameters, such as temperature and heating rate. The density of aluminum foams, for example, typically ranges from about 0.5 to 1 g/cm3.
Strength, and other properties of foamed metals can be tailored by adjusting the specific weight (or porosity), alloy composition, heat treatment history, and pore morphology as is known to those of skill in the art. In advantageous embodiments, the metallic foam will have high mechanical strength.
Metal foams are easily processed into any desired shape or configuration by conventional techniques, such as sawing drilling, milling, and the like. Moreover, metal foams can be joined by known techniques, such as adhesive bonding, soldering, and welding.
In certain preferred embodiments of the invention, the shock-absorbing element is closed-cell aluminum foam, and in a specific illustrative embodiment, the shock-absorbing element is closed-cell aluminum foam with a porosity of 80 percent by volume.
In device embodiments of the present invention, a multi-layered armor system, suitable for structural protection against ballistic impact or explosive blast, such as armor systems used in connection with military armored vehicles, includes one or more layers of a metal foam as a shock energy-absorbing element.
As used herein, the term "multi-layer armor system" means at least two plates of metal, metal foam, ceramic, plastic, and the like, known or developed, for defense or protection systems. In the present invention, the multi-layer armor system includes at least a strike plate, or buffer plate, bonded or otherwise held in communication with, a shock-absorbing element that is a layer of metallic foam.
As described hereinabove, the metallic foam preferably has a closed-cell pore structure and a high fraction of porosity. Illustratively, the metallic foam may be aluminum, steel, lead, zinc, titanium, nickel and alloys or metal matrix composites thereof, with porosity ranging from about 50-98 percent by volume. In a particularly preferred embodiment of the invention, the metallic foam is a closed-cell aluminum foam having a porosity of 80 percent by volume.
The term "strike plate" refers to a high strength metal or ceramic plate that has a front face surface that would receive the initial impact of a projectile or blast. The back surface of the strike plate is adjacent to a first surface of the shock-absorbing element that, in the present invention, is a sheet or layer of metallic foam. It is to be understood that the term "strike plate," as used herein, refers to any buffer plate of a high strength material that receives impact or impact-induced stress waves prior to a shock-absorbing element.
The strike plate may be a flat sheet of a high strength metal, ceramic or polymer-based composite, such as a fiber-reinforced polymer composite.
In a preferred embodiment, the multi-layer armor system of the present invention further includes a deformable backing plate bonded to, or otherwise held in communication with, a face surface of the metallic foam sheet or layer opposite, or distal, to the surface contiguous to the strike plate. The backing plate illustratively is a sheet of a deformable metal, such as titanium, aluminum, or steel.
In a specific illustrative embodiment of a multi-layer armor system in accordance with the invention, a shock-absorbing layer of metallic foam is sandwiched between a high strength strike plate and a deformable backing plate. Of course, the multi-layered armor system may comprise additional elements, in any sequence, and the embodiments presented herein are solely for the purposes of illustrating the principles of the invention.
BRIEF DESCRIPTION OF THE DRAWING
Comprehension of the invention is facilitated by reading the following detailed description, in conjunction with the annexed drawing, in which:
  • Fig. 1 is a schematic representation of an illustrative armor system incorporating metallic foam as a shock energy-absorbing element in accordance with the principles of the present invention;
  • Fig. 2 is a photomicrograph of a high porosity, closed-cell aluminum foam showing the typical microstructure in cross-section;
  • Fig. 3 is a graphical representation of the typical behavior of a metal foam, of the type shown in Fig. 2, under a uniaxial load; and
  • Fig. 4 is photomicrograph of the aluminum foam of Fig. 2 showing a cross-sectional view of the microstructure following deformation by high energy impact.
  • DETAILED DESCRIPTION OF THE INVENTION
    Fig. 1 is an illustrative schematic representation of an improved armor system 10 of the type having a high strength strike plate 11, at least one shock energy-absorbing element 12, and a backing plate 13. In the embodiment of Fig. 1, a closed-cell metal foam is used as shock energy-absorbing element 12. High strength strike plate 11 may be ceramic or metal. Backing plate 13 is typically a highly deforming metal, such as titanium, aluminum, or steel. However, backing plate 13 may comprise one or more layers of metal and/or ceramic, as well as polymer-based composites. In armor system 10, the closed-cell metal foam is effective in containing rearward deformation of the strike plate 11 in a ballistic target structure. The metal foam has the ability to control backface deformation, without sacrificing ballistic efficiency behind targets with highly deforming back plates, via a mechanism that will be discussed more completely hereinbelow.
    The shock energy-absorbing element 12 preferably comprises a closed-cell metallic foam which, illustratively, may be aluminum, steel, lead, zinc, titanium, nickel, and alloys or metal matrix composites thereof. Preferred metal foams have a high fraction of porosity, typically ranging from about 50-98 by volume percent. In a specific preferred embodiment, shock energy-absorbing element 12 is a closed-cell aluminum foam having a porosity of 80 by volume. Fig. 2 shows the microstructure (i.e., the pore structure) of this particular aluminum foam material.
    This type of pore structure provides a substantial increase in the stiffness/weight ratio (SWR) of the material with a low fractional density. Under deformation, this microstructure features localized cell collapse and rapid compaction energy dissipation, which leads to unique deformation behaviors and material properties including high SWR and energy absorption in the material.
    During deformation, metal foams of the type shown in Fig. 2, exhibit the universal deformation behavior shown in Figure 3 as they move from the quasi-elastic regime to the plastic regime. Fig. 3 is a graphical representation of the behavior of the metal foam of Fig. 2 under uniaxial load referred to as a "loading curve." The vertical axis of Fig. 3 represents stress and the horizontal axis represents strain. The loading curve of Fig. 3 is divided into three regions: linear elastic region 31, collapse region 32 (where plateau stress remains relatively constant) and densification region 33. In linear elastic region 31, the elastic portion of the stress-strain curve is only partially reversible. During loading, small-scale localized plastic deformation has already taken place within the sample. These small-scale plastic deformations also contribute to the mechanical damping of metal foams. In collapse region 32, the cell wall-buckling event occurs and the foam progressively collapses until densification region 33. The deformation in densification region 33 is highly localized and is preceded by the advance of a densification front from deformed to undeformed regions of the sample. For strain rate insensitive materials such as aluminum, the deformation behavior at the high strain rates remain the same. The area under the loading curve represents the deformation energy absorbed by the metal foam.
    Metal foams can be fabricated to maximize the energy absorption capability by adjusting foam parameters including alloying elements, density level, cell size, wall thickness, and uniformity. Improvements in modulus and plateau stress via heat treatment of the metal foam, or via addition of particulate or whisker reinforcements to the metal foam, are additional techniques known to increase the energy absorption capability.
    Metal foams are capable of mitigating the impact-induced stress waves from the strike plate, thereby delaying or eliminating damage to underlying layers, which in some embodiments might be a ceramic tile, and improving protection of the personnel and equipment behind the target. The deformation energy due to shock impact first densifies the front portion (in the loading direction) of the metal foam layer that forms the shock energy-absorbing element. Subsequent deformation introduces tearing and shearing of the cell walls, an effect of core shearing deformation for energy dissipation in the cellular structure. Thus, the deformation energy is redirected and dissipated sideways. This is best illustrated in Fig. 4 which is a cross-sectional view of the microstructure of the aluminum foam of Fig. 2 showing deformation following high energy impact. This type of deformation mechanism reduces the transmitted deformation energy behind the target in the loading direction. The energy of the impact-induced stress waves is also dissipated efficiently within the cellular network. The high degree of porosity in metal foam is beneficial for the absorption of the wave energy, and the cellular network generates the cavity effect for scattering the wave energy within the network.
    The armor systems of the present invention would be useful as protection systems for ballistic impact and for blast. Moreover, while the illustrative embodiment presented herein is directed to a three element system, it is to be understood that invention contemplates the use of closed-cell, high strength metal foams having a high fraction of porosity, as a shock energy-absorbing element in any other configuration developed, or to be developed, wherein its ability to contain rearward deformation under high-speed impact, would be useful.
    Although the invention has been described in terms of specific embodiments and applications, persons skilled in the art can, in light of this teaching, generate additional embodiments without exceeding the scope of the invention as defined by the following claims. Accordingly, it is to be understood that the drawing and description in this disclosure are proffered to facilitate comprehension of the invention, and should not be construed to limit the scope thereof.

    Claims (7)

    1. A multi-layered armour system comprising a strike plate, a deformable back plate and one or more intermediate layers there between, characterised in that the one or more intermediate layers include a shock absorbing element comprising a metallic foam having cells distributed therethrough and, on application of a force on said strike plate, the shock absorbing element is urged to undergo progressive modes of deformation corresponding to a substantially linear elastic deformation, a cellular collapse deformation and a densification deformation, in response to the magnitude of the force applied to the strike plate.
    2. A multi-layered armour system according to claim 1 characterised in that the strike plate is selected from the group consisting of high strength metals, ceramics and polymer based composites.
    3. A multi-layered armour system according to claim 1 characterised in that the metallic foam is a closed cell metallic foam.
    4. A multi-layered armour system according to claim 3 characterised in that the closed cell metallic foam is selected from the group consisting of aluminium, steel, lead, zinc, titanium, nickel and alloys, or metal matrix composites thereof.
    5. A multi-layered armour system according to claim 3 characterised in that the closed cell metallic foam has a porosity that ranges from about 50-98 percent by volume.
    6. A multi-layered armour system according to claim 1 characterised in the deformable backing plate comprises a metal selected from the group consisting of titanium, aluminium or steel.
    7. A multi-layered armour system according to claim 3 characterised in that the closed cell metallic foam is formed from aluminium and has a porosity of 80 percent by volume.
    EP00937503A 1999-03-10 2000-03-10 Use of metal foams in armor systems Expired - Lifetime EP1078215B1 (en)

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    US12356999P 1999-03-10 1999-03-10
    US123569P 1999-03-10
    PCT/US2000/006220 WO2000055567A1 (en) 1999-03-10 2000-03-10 Use of metal foams in armor systems

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    Families Citing this family (14)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    DE10257942A1 (en) * 2002-12-12 2004-06-24 Krauss-Maffei Wegmann Gmbh & Co. Kg Protection module for protection against hollow charges includes layer sequence of three-dimensional metal grid structure or open-pore metal foam and air layers
    DE502004005697D1 (en) 2004-02-16 2008-01-24 Kovari Kalman Method and device for stabilizing a cavity excavated in underground mining
    DE102004012990A1 (en) * 2004-04-30 2005-11-24 Girlich, Dieter, Dr. Composite material e.g. for producing ceramic-metallic, made from open-porous metal foam with its pores completely or partly filled out with material and pores of open-porous metal foam are filled of different ceramic materials
    DE102004030780A1 (en) * 2004-06-25 2006-01-19 Audi Ag Composite material used in chassis production comprises cast metallic hollow balls and/or cast metal foams made from steel and cast from the same or similar cast material
    US7465500B2 (en) * 2004-10-28 2008-12-16 The Boeing Company Lightweight protector against micrometeoroids and orbital debris (MMOD) impact using foam substances
    DE102013113970A1 (en) * 2013-12-12 2015-06-18 Benteler Defense Gmbh & Co. Kg Layer composite armor
    CN104142096A (en) * 2014-07-17 2014-11-12 辽宁融达新材料科技有限公司 Anti-violence protecting panel and container manufactured by using the same
    WO2016118179A1 (en) * 2015-01-23 2016-07-28 Halliburton Energy Services, Inc. Perforating guns that include metallic cellular material
    DE102015119351B4 (en) 2015-11-10 2022-12-29 Proreta Tactical GmbH Ballistic protection device
    GB2550252B (en) * 2016-04-12 2019-07-03 Advanced Blast Prot Systems Llc Systems and methods for blast impulse reduction
    DE102016013673A1 (en) * 2016-11-14 2018-05-17 IfL Ingenieurbüro für Leichtbau GmbH & Co. KG Temporary mobile protection against ballistic and explosive outdoor use
    DE202020100838U1 (en) 2020-02-17 2020-03-24 Proreta Tactical GmbH Ballistic protection device
    US11378359B2 (en) 2020-05-28 2022-07-05 Tencate Advanced Armor Usa, Inc. Armor systems with pressure wave redirection technology
    WO2021242248A1 (en) * 2020-05-28 2021-12-02 Tencate Advanced Armor Usa, Inc. Armor systems with pressure wave redirection technology

    Family Cites Families (6)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US3604374A (en) * 1969-08-18 1971-09-14 United States Steel Corp Composite blast-absorbing structure
    DE2039343A1 (en) * 1970-08-07 1972-02-10 Dornier System Gmbh Armor
    US4973358A (en) 1989-09-06 1990-11-27 Alcan International Limited Method of producing lightweight foamed metal
    DE9007336U1 (en) * 1990-01-24 1991-07-04 Neuero Stahlbau Gmbh & Co, 4459 Emlichheim, De
    DE4101630A1 (en) 1990-06-08 1991-12-12 Fraunhofer Ges Forschung METHOD FOR PRODUCING FOAMABLE METAL BODIES AND USE THEREOF
    US5181549A (en) 1991-04-29 1993-01-26 Dmk Tek, Inc. Method for manufacturing porous articles

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    DE60007237D1 (en) 2004-01-29
    DE60007237T2 (en) 2004-05-27
    ATE256853T1 (en) 2004-01-15
    ES2213021T3 (en) 2004-08-16
    WO2000055567A1 (en) 2000-09-21

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