US20120174750A1 - Armor materials, body armor articles and methods of manufacture - Google Patents

Armor materials, body armor articles and methods of manufacture Download PDF

Info

Publication number
US20120174750A1
US20120174750A1 US11/923,316 US92331607A US2012174750A1 US 20120174750 A1 US20120174750 A1 US 20120174750A1 US 92331607 A US92331607 A US 92331607A US 2012174750 A1 US2012174750 A1 US 2012174750A1
Authority
US
United States
Prior art keywords
cells
powder
armor
plate
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.)
Abandoned
Application number
US11/923,316
Inventor
Reza Oboodi
Derek Raybould
Thomas E. Strangman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honeywell International Inc filed Critical Honeywell International Inc
Priority to US11/923,316 priority Critical patent/US20120174750A1/en
Assigned to HONEYWELL INTERNATIONAL, INC. reassignment HONEYWELL INTERNATIONAL, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: OBOODI, REZA, RAYBOULD, DEREK, STRANGMAN, THOMAS E.
Publication of US20120174750A1 publication Critical patent/US20120174750A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • 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
    • 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
    • F41H5/0414Layered armour containing ceramic material
    • F41H5/0421Ceramic layers in combination with metal layers
    • 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
    • F41H5/0492Layered 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Laminated Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

An armor material, body armor articles, and methods of manufacturing the armor material are provided. In an embodiment, by way of example only, the armor material includes a first plate, a second plate, and a powder material. The first plate includes a layer comprising a metallic material. The second plate is spaced apart from the first plate and includes a layer comprising a ceramic material. The powder material is disposed between the first and the second plates, and comprises loose powder including at least one of a plurality of ceramic particles and a plurality of metallic particles.

Description

    TECHNICAL FIELD
  • The inventive subject matter generally relates to armor material, and more particularly relates to projectile-resistant armor material.
  • BACKGROUND
  • Protective armor is used for protecting a person, vehicle or device from penetrating threats that may originate from devices used for explosive or ballistic events. Conventionally, the protective armor may be made of sheets of ceramic, metal, or a combination of these materials. Although these materials generally provide excellent protection, they may be improved. Specifically, it is desirable to provide a protective armor that may be more lightweight than conventional protective armor. Additionally, it is desirable to have a protective armor that may protect against various forms of projectile threats, such as solid particles and liquid molten metals. Moreover, it is desirable to have a protective armor made from material that is relatively inexpensive and simple to manufacture. Furthermore, other desirable features and characteristics of the inventive subject matter will become apparent from the subsequent detailed description of the inventive subject matter and the appended claims, taken in conjunction with the accompanying drawings and this background of the inventive subject matter.
  • BRIEF SUMMARY
  • An armor material, a body armor article, and methods of manufacturing the armor material are provided.
  • In an embodiment, by way of example only, the armor material includes a first plate, a second plate, and a powder material. The first plate includes a layer comprising a metallic material. The second plate is spaced apart from the first plate and may include a layer comprising a ceramic material. The powder material is disposed between the first and the second plates, and comprises loose powder including at least one of a plurality of ceramic particles and a plurality of metallic particles.
  • In another embodiment, by way of example only, the body armor article includes a panel. The panel includes an armor material that has a first plate, a second plate, and a powder material. The first plate includes a layer comprising a metallic material. The second plate is spaced apart from the first plate and includes a layer comprising a ceramic material. The powder material is disposed between the first and the second plates, and comprises loose powder including at least one of a plurality of ceramic particles and a plurality of metallic particles.
  • In still another embodiment, by way of example only, the method includes placing and compacting loose powder material in selected cells of a plurality of cells between a first and a second plate.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The inventive subject matter will hereinafter be described in conjunction with the following drawing figures, wherein like numerals denote like elements, and
  • FIG. 1 is a cross-sectional view of an armor material, according to an embodiment;
  • FIG. 2 is a cross-sectional view of an armor material, according to another embodiment;
  • FIG. 3 is a side cross-sectional view of an armor material, according to still another embodiment;
  • FIG. 4 is a cross-sectional view of the armor material in FIG. 3 taken along line 4-4, according an embodiment;
  • FIG. 5 is a side cross-sectional view of an armor material, according to another embodiment;
  • FIG. 6 is a cross-sectional view of the armor material in FIG. 5 taken along line 6-6, according an embodiment;
  • FIG. 7 is a flow diagram of a method of manufacturing a armor material, according an embodiment; and
  • FIG. 8 is a perspective view of an article of body armor, according to an embodiment.
  • DETAILED DESCRIPTION
  • The following detailed description is merely exemplary in nature and is not intended to limit the inventive subject matter or the application and uses of the inventive subject matter. Furthermore, there is no intention to be bound by any theory presented in the preceding background or the following detailed description.
  • FIG. 1 is a cross-sectional view of an armor material 100, according to an embodiment. The armor material 100 may be used to protect a person, vehicle, or a device from projectiles that may originate from an explosive or a ballistic threat. For example, the armor material 100 may be used as body armor, or may be implemented into or used to cover a vehicle or a device.
  • In an embodiment, the armor material 100 is configured to dissipate and absorb kinetic energy of a projectile by maintaining the projectile intact and/or by adding material to the projectile as it travels through the armor material 100. Generally, the armor material 100 includes a first plate 102, a second plate 104, and a powder material 106, according to an embodiment. As shown in FIG. 1, the first plate 102 and the second plate 104 are spaced apart from each other, and the powder material 106 is disposed therebetween. In an embodiment, the first and second plates 102, 104 may be spaced between about 0.2 cm and about 10 cm apart. In another embodiment, a fiber-composite fabric 108 (shown in phantom) may be positioned adjacent to the second plate 104 and may be separate from or adhered thereto. Each of these components will now be described in more detail below.
  • The first plate 102 may be initially impacted by the projectile and thus, is configured to absorb at least a portion of the kinetic energy therefrom. In an embodiment, the first plate 102 may be made of a metallic material, such as aluminum, titanium or steel. In an embodiment, the first plate 102 may have a thickness of between about 0.2 and about cm. In another embodiment, the first plate 102 may be a laminate and may include a first layer 110 and a second layer 112. Each layer 110, 112 may have a thickness of between about 0.1 cm and about 5 cm. At least one of the layers 110, 112 may comprise a first metallic material, such as aluminum, while the other layer 110, 112 may comprise a second metallic material, such as steel, titanium, or aluminum. The second layer 112 or an additional layer may comprise a ceramic material. Suitable ceramic materials include, but are not limited to, alumina, aluminum nitride, aluminosilicate, boron carbide, boron nitride silica, silicon nitride, silicon carbide, and zirconia. In an embodiment, where the first layer 110 is a soft metal such as aluminum and the second layer 112 is made of a relatively hard metal or ceramic material, the first layer 110 may facilitate projectile deformation (pancaking) on an outer surface of the armor material 100 with minimal shear stress transmitted to the second layer 112. As a result, the second layer 112 may have an enhanced ability to resist projectile penetration.
  • The powder material 106 is configured to absorb another portion of kinetic energy from the moving projectile to further reduce the speed at which the projectile is traveling, in an event in which the projectile passes through the first plate 102. In this regard, the powder material 106 may be disposed between the first plate 102 and the second plate 104 as a loose powder or partially compacted powder. In this way, the powder material 106 becomes compacted when impacted by the projectile. The work required for compaction of the powder thereby absorbs another portion of the impacting projectile's kinetic energy. In an embodiment, the powder material 106 may be disposed between the plates 102, 104 such that it is a loose powder. Depending on powder particle size and shape, the loose powder may be pre-compacted to have a weight that is about 30% of the weight of the solid from which the powder material 106 is made. In another embodiment, the powder material 106 may be precompacted, and may have a weight that may be about 50% of the weight of its solid form. In still other embodiments, it may be desirable for the powder material 106 to have a compacted density that creates an even higher pressure when the projectile impacts the powder; for such embodiments, the powder material 106 may be pre-compacted to a form a preform having a predetermined density, which may also facilitate packaging of the powder. For example, the powder may be precompacted to about 70% of the weight of the solid form.
  • The second plate 104 may be configured to absorb at least a portion of the kinetic energy remaining in a projectile with which it comes into contact. For example, in an embodiment, the second plate 104 may be made of a ceramic material. Suitable ceramic materials include, but are not limited to, alumina, aluminum nitride, aluminosilicate, boron carbide, boron nitride, silica, silicon nitride, silicon carbide, zirconia, and sand (calcia-magnesia-alumina-silicate). In an embodiment, the second plate 104 may have a thickness of between about 0.1 and about 5 cm. In another embodiment, the second plate 104 may be a laminate and may include a first layer 116 and a second layer 118. The layers 116, 118 may or may not have substantially identical thicknesses and may have thicknesses between about 0.1 and about 5 cm. At least one of the layers 116, 118 may comprise a first metallic material, while the other of the layers 116, 118 may comprise a second metallic material. In another embodiment, the second layer 118 or an additional layer may comprise may be a metallic material, such as aluminum, titanium or steel. In an embodiment, the second plate 104 may make up a wall of a device or vehicle into which the armor material 100 is being incorporated.
  • A fiber-composite fabric 108 (shown in phantom) may be positioned adjacent to the second plate 104 and may be separate from or adhered thereto. The fiber-composite fabric 108 may serve to catch projectiles that still have kinetic energy and thereby block the projectile from completely traveling through the armor material 100. The fiber-composite fabric 108 may be made from aramids, high molecular weight polyethylene fiber, or glass fiber. In an embodiment, the fiber-composite fabric 108 may be Spectra® fiber available through Honeywell International, Inc., Specialty Materials Group, of Morristown, N.J.
  • As mentioned briefly above, the powder material 106 is disposed between the first plate 102 and the second plate 104 and comprises loose powder. The powder material 106 may include at least one of a plurality of ceramic particles and a plurality of metallic particles. Thus, in some embodiments, the powder material 106 may be a mixture of ceramic particles and metallic particles. In an embodiment, the powder material 106 occupies substantially all of a volume defined between the first and the second plates 102, 104. In another embodiment, the powder material 106 may be disposed in structures that are incorporated between the first and the second plates 102, 104. FIG. 2 is a cross-sectional view of an armor material 200 including such a structure, according to an embodiment. Here, the powder material 206 is contained in a plurality of cells 214 disposed between a first plate 202 and a second plate 204. Although shown as being disposed in all of the cells 214, a portion of the cells 214 may not include powder material 206, in other embodiments. In such case, spaces 217 may exist between the cells 214 that may not include the powder material 106 to thereby maintain portions of the powder material 206 separated from each other. In some embodiments, one or more different types of powder materials 206 may be used, and some cells 214 may be filled with a first type of material, while other cells 214 may be filled with a second type of material. The use of different types of powders may allow selected areas of the armor material 100 to compact at relatively different rates when impacted with a projectile, which may promote shear deformation (energy dissipation) to occur within a penetrating projectile.
  • The cells 214 may have any one of numerous configurations. In an embodiment, the cells 214 are capsules having a predetermined shape. The capsules may be made of a material capable of deforming when impacted by the projectile to allow the powder material 106 to be compacted. The capsules may be configured to plastically deform to thereby absorb at least a portion of the energy of the projectile. Suitable capsule materials include, but are not limited to glass, ceramic, plastic, aluminum, titanium, copper and steel. The predetermined shape of the capsules may be spherical, ovular, cubic, or hexagonal. In an embodiment, the capsules may have a diameter of between about 2 mm and about 50 mm. In another embodiment, the capsules may include a wall 220 having a thickness of between about 0.1 mm and about 10 mm.
  • FIG. 3 is a cross-sectional side view of an armor material 300 including cells 314 in another configuration, and FIG. 4 is a cross-sectional view of the material 300 shown in FIG. 3 taken along line 4-4, according to an embodiment. Here, the cells 314 may be defined by a lattice structure that is disposed between first and second plates 302, 304. The lattice structure forms a honeycomb pattern, where each cell 314 has a diameter and a volume. In an embodiment, the diameter of each cell 314 may be substantially identical to each other or may not be. In another embodiment, the cell diameters may be between about 2 mm and about 50 mm. Each cell 314 may also have a cell cross-sectional shape. Although the cell cross-sectional shape in this embodiment is shown as being hexagonal, it will be appreciated that round or any other cell cross-sectional shape may alternatively be employed.
  • The powder material 306 in this embodiment is disposed in at least a portion of the cells 314. In an embodiment, the powder material 306 is disposed in substantially all of the cells 314 and fills substantially an entire volume of each cell 314 occupied. In other embodiments, between about 5% and about 95% of the plurality of cells 314 is filled with the powder material 306. In another embodiment, the powder material 306 is disposed in about 50% of the plurality of cells 314, and occupies substantially an entire volume of each occupied cell 314. In any event, the occupied cells 314 may form a pattern. For example, one or more occupied cells 314 may be interposed between two or more empty cells.
  • The cells 314 shown in FIGS. 3 and 4 are positioned such that each has a wall 320 having a height that extends between the first and second plates 302, 304. In an embodiment, the walls 320 may have thickness of between about 0.2 mm and about 10 mm. Such positioning may allow areas of the armor material 300 to be impacted, while minimally affecting areas adjacent to the impacted areas.
  • FIG. 5 is a cross-sectional view of an armor material 500 including a plurality of cells 514 formed between a first plate 502 and a second plate 504, and FIG. 6 is a cross-sectional view of the material 500 shown in FIG. 5 taken along line 6-6, according to another embodiment. Here, the cells 514 have walls 520 and form a corrugated pattern and are stacked in layers 522, 524. In an embodiment, the walls 520 may be made of a metal alloy and may have thickness of between about 0.2 mm and about 10 mm and a height of between about 30% to about 80% of a total distance between the plates 502, 504. Although two layers 522, 524 are shown, fewer or more may alternatively be employed. The layers 522, 524 may each include a plurality of cells 514 that may or may not be substantially identically shaped and sized. In an embodiment, the layers 522, 524 may or may not be substantially identically sized.
  • In another embodiment, a first portion of the plurality of cells 514 in the first layer 522 includes powder material 506, while a second portion of the plurality of cells 514 in the first layer 522 is empty. In still another embodiment, the cells of the first layer 522 may have an opening that communicates with an opening formed in the cells of the second layer 524. The opening may have a width that is slightly smaller (e.g. about 10% smaller) than the size of a particle of the powder material 506 so that flow of the powder material 506 may occur by back extrusion after the powder is nearly fully compacted. The armor material 500 may be further configured such that a first portion of the plurality of cells 514 in the first layer 522 may include the powder material 506. In an embodiment, the plurality of cells 514 in the second layer 524 communicating with the first portion of the plurality of cells 514 in the first layer 522 may not initially include powder material 506. Thus, when the armor material 500 is subjected to projectile impact, the powder material 506 can flow from the first layer 522 to the second layer 524 to provide an improved ability to absorb the projectiles' energy and also to withstand repeated impacts. In another embodiment, those cells in the second layer 524, which may oppose the filled cells of the first layer 522 may be filled with powder material 506. The layers 522, 524, may have cells and cell walls made of material that has a melting point that is greater than a molten projectile and powder material 506 having a melting point that is greater than the molten projectile. As a result, the compacted powder-filled cells form a high-melting point barrier to molten projectiles. Additionally, energy from the impact of the molten projectile may dissipate due to the powder compaction, friction between sliding cells of the layers 522, 524, and buckling of the cell walls.
  • In any case, the powder material 106, 206, 306, 506 may be formed to reduce the kinetic energy of one or more different types of projectiles. In this regard, the powder material 106, 206, 306, 506 may have particular characteristics suitable for reducing kinetic energy when impacted by projectiles. For example, the powder material 106, 206, 306, 506 may include particles having predetermined shapes, such as spherical. The particles may or may not be uniform in shape. In another example, the powder material 106, 206, 306, 506 may have a particular granularity having an irregular atomized shape. The particles may also be relatively flat having a shape characteristic of powder made by mechanical alloying. For instance, in an embodiment, the particles of the powder material 106, 206, 306, 506 may be fine and may have each particle may have a diameter of between about 10 μm and about 300 μm. In another embodiment, the particles may be relatively coarse and have a diameter of between about 0.5 mm and about 5 mm.
  • The type of powder selected for use may depend on an ability of the powder to obtain maximum absorption of the projectile energy and on the probable type of projectile. In an embodiment, the powder material 106, 206, 306, 506 may be formulated to reduce the kinetic energy of a projectile that may be a solid particle, and the powder material 106, 206, 306, 506 may include a plurality of particles that may deform when impacted by the projectile to thereby weld thereto and increase the size thereof. Suitable particles include, but are not limited to, one or more types of metals or alloys thereof, such as aluminum, iron, steel or copper. In another example, the projectile may comprise liquid metal, and the powder material 106, 206, 306, 506 may include a plurality of particles having a melting point that may be greater than that of the material from which the fully or partially molten projectile may originate. These types of particles may be relatively difficult to compact and may absorb kinetic energy from the molten particle. Suitable particles may include metals such as steels or superalloys or ceramics particles, such as Al2O3, SiN4, SiC, SiO2, and the like. Other suitable particles may be those having a melting point that is greater than that of copper (e.g., 1085° C.). In cases in which the armor material 100, 200, 300, 500 may be subjected to multiple types of projectiles, the powder material 106 may be a mixture of metallic particles and ceramic particles. It will be appreciated that a ratio of metallic particles to ceramic particles may be selected based on a predicted likelihood of a particular threat that may be encountered.
  • To maintain the powder material 106, 206, 306, 506 in loose form, one or more additives may be included. For example, the powder material 106, 206, 306, 506 may include a small amount of an organic additive (e.g., less than about 5% by weight). The organic additive may serve as a contaminant that prevents or inhibits welding of the particles of the powder material 106, 206, 306, 506. Possible organic contaminates include, but are not limited to, carbon, epoxy, foam or glue. Epoxy or glue may be formulated to adhere to a portion of the particles of the powder material 106, 206, 306, 506 so that the particles remain separate from each other even when subjected to vibration.
  • In an embodiment, the organic additive, either the foam, glue, or another material, may be formulated to vaporize due to heat energy resulting from compaction of the powder material 106, 206, 306, 506 upon projectile impact. The resulting vapor may contaminate substantially all of the powder particles to thereby prevent the particles from welding together and to improve an ability of the armor material 100, 200, 300, 500 to withstand repeated impact to an area. In another example, the additives may include plastics having a melting point below a temperature of the heat energy resulting from compaction of the powder material 106 upon projectile impact. The plastics may further be formulated to vaporize due to the compaction of the powder material 106. Suitable low-melting plastics include, but are not limited to polyacrylonitrile butadiene styrene, nylon, nylon6, polypropylene, polystyrene, polytetra fluoro ethylene, polyfloride and polychloride.
  • The armor materials discussed above may be manufactured using any suitable method. One example of a suitable method 700 is provided in FIG. 7. First, the powder material is formulated, step 702. The powder material may be formulated according to any of the embodiments described previously, and the formulation may depend on the anticipated type of projectile threat that may be encountered. The powder material is placed between two plates, step 704. In an embodiment, the plates may be placed adjacent to and spaced apart from one another and may be attached to each other by one or more walls or other attachment means. The powder material in loose powder form may be disposed in selected one of a plurality of cells and compacted to a desired density. In another embodiment, a lattice structure defining a plurality of cells may be included, and the lattice structure is attached to one or both plates, either by brazing, welding, bolts, or other means. The powder material in loose powder form is then placed in selected ones of the cells of the lattice structure and compacted to a desired density. In an embodiment in which the lattice structure is attached only to one plate, another plate is attached to the lattice structure to maintain the powder material in the cells. In still another embodiment, the powder material is placed in a plurality of capsules, and the capsules are disposed between the two plates. Next, the fiber composite fabric is attached to one of the plates, step 706. In an embodiment, the fiber composite fabric is adhered to the plate using epoxy, or other type of adhesive.
  • After manufacture, the armor material may be incorporated into any article that may be worn on a person or may be incorporated into a vehicle. For example, FIG. 8 is a perspective view of a body armor article 800. The body armor article 800 may include the armor material 100, 200, 300, 500 described above. In an embodiment, the body armor article 800 may be made entirely of the material 100, 200, 300, 500. In another embodiment, the body armor article 800 is made of at least two sheets of fabric 802, 804 that are attached to each other to form a vest (as depicted in FIG. 8). The two sheets of fabric 802, 804 may form a pocket 806 therebetween within which one or more panels 808 is disposed. The panels 808 may be made of the material 100, 200, 300, 500.
  • Armor materials have now been provided that may be more lightweight than conventional armor materials. Additionally, the armor materials may be used as a shield against solid and/or molten and liquid projectile threats by providing a compactable, alloyable, and collapsible structure. The structure may be used to absorb kinetic energy of a projectile, while either adding material thereto. Moreover, the armor materials may be relatively simple and inexpensive to manufacture, compared to conventional materials.
  • While at least one exemplary embodiment has been presented in the foregoing detailed description of the inventive subject matter, it should be appreciated that a vast number of variations exist. It should also be appreciated that the exemplary embodiment or exemplary embodiments are only examples, and are not intended to limit the scope, applicability, or configuration of the inventive subject matter in any way. Rather, the foregoing detailed description will provide those skilled in the art with a convenient road map for implementing an exemplary embodiment of the inventive subject matter. It being understood that various changes may be made in the function and arrangement of elements described in an exemplary embodiment without departing from the scope of the inventive subject matter as set forth in the appended claims.

Claims (20)

1. An armor material, comprising:
a first plate including a layer comprising a metallic material;
a second plate spaced apart from the first plate, the second plate including a layer comprising a ceramic material; and
a powder material disposed between the first and the second plates, the powder material comprising loose powder including at least one of a plurality of ceramic particles and a plurality of metallic particles.
2. The armor material of claim 1, wherein the first plate further includes a ceramic layer.
3. The armor material of claim 1, wherein the second plate further includes a metal layer.
4. The armor material of claim 1, wherein the powder material is precompacted to a density of between about 30% and about 70% of a density of a solid form of the powder material.
5. The armor material of claim 1, wherein the powder material further contains one or more organic additives.
6. The armor material of claim 1, further comprising a plurality of cells disposed between the first plate and the second plate, wherein the powder material is disposed within at least a portion of the plurality of cells.
7. The armor material of claim 6, wherein the powder material is disposed in between about 5% and about 95% of the plurality of cells.
8. The armor material of claim 6, wherein each cell of the plurality of cells has a height extending between the first plate and the second plate, and each cell having the powder material disposed therein has a volume that is substantially occupied by the powder material.
9. The armor material of claim 6, wherein the plurality of cells are disposed in a plurality of layers, the plurality of layers including a first layer of cells and a second layer of cells disposed over the first layer of cells, the first and second layers of cells disposed between the first and second plates.
10. The armor material of claim 9, wherein each cell of the plurality of cells of the first layer of cells has an opening that communicates with an opening of a corresponding cell of a plurality of cells of the second layer of cells, and at least a portion of the plurality of cells of the first layer of cells includes loose powder.
11. The armor material of claim 10, wherein the plurality of cells of the second layer of cells communicating with the first layer of cells do not include the powder material.
12. The armor material of claim 6, wherein the plurality of cells comprises a plurality of capsules containing the powder material.
13. The armor material of claim 1, wherein the powder material comprises a first type of powder and a second type of powder, the first type of powder is disposed in a first portion of the plurality of cells, and the second type of powder is disposed in a second portion of the plurality of cells.
14. The armor material of claim 1, further comprising:
a fiber composite fabric disposed adjacent at least a portion of the second plate.
15. The armor material of claim 14, wherein the fiber composite fabric comprises a material selected from the group consisting of aramid, polyethylene fiber, and glass fiber.
16. A body armor article comprising:
a panel comprising an armor material including:
a first plate including a layer comprising a metallic material;
a second plate spaced apart from the first plate, the second plate including a layer comprising a ceramic material; and
a powder material disposed between the first and the second plates, the powder material comprising loose powder including at least one of a plurality of ceramic particles and a plurality of metallic particles.
17. The body armor article of claim 16, further comprising a plurality of panels attached together to form a vest.
18. The body armor article of claim 16, further comprising a plurality of cells disposed between the first plate and the second plate, wherein the powder material is disposed within at least a portion of the plurality of cells.
19. The body armor article of claim 16, further comprising a fiber composite fabric disposed adjacent at least a portion of the second plate.
20. The body armor article of claim 16, wherein the powder material comprises a first type of powder and a second type of powder, the first type of powder is disposed in a first portion of the plurality of cells, and the second type of powder is disposed in a second portion of the plurality of cells.
US11/923,316 2007-10-24 2007-10-24 Armor materials, body armor articles and methods of manufacture Abandoned US20120174750A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US11/923,316 US20120174750A1 (en) 2007-10-24 2007-10-24 Armor materials, body armor articles and methods of manufacture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/923,316 US20120174750A1 (en) 2007-10-24 2007-10-24 Armor materials, body armor articles and methods of manufacture

Publications (1)

Publication Number Publication Date
US20120174750A1 true US20120174750A1 (en) 2012-07-12

Family

ID=46454222

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/923,316 Abandoned US20120174750A1 (en) 2007-10-24 2007-10-24 Armor materials, body armor articles and methods of manufacture

Country Status (1)

Country Link
US (1) US20120174750A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8789454B1 (en) * 2010-04-12 2014-07-29 The United States Of America, As Represented By The Secretary Of The Navy Multi-ply heterogeneous armor with viscoelastic layers and cylindrical armor elements
US20170197873A1 (en) * 2014-06-06 2017-07-13 The Royal Institution For The Advancement Of Learning/Mcgill University Methods and systems relating to enhancing material toughness

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6042663A (en) * 1976-03-03 2000-03-28 Royal Ordnance Plc Propellant compositions with nitrocellulose and a polymer
US6537654B1 (en) * 1999-11-04 2003-03-25 Sgl Technik Gmbh Protection products and armored products made of fiber-reinforced composite material with ceramic matrix
US6895851B1 (en) * 2003-06-16 2005-05-24 Ceramics Process Systems Multi-structure metal matrix composite armor and method of making the same
US7104177B1 (en) * 2000-01-11 2006-09-12 Aghajanian Michael K Ceramic-rich composite armor, and methods for making same

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6042663A (en) * 1976-03-03 2000-03-28 Royal Ordnance Plc Propellant compositions with nitrocellulose and a polymer
US6537654B1 (en) * 1999-11-04 2003-03-25 Sgl Technik Gmbh Protection products and armored products made of fiber-reinforced composite material with ceramic matrix
US7104177B1 (en) * 2000-01-11 2006-09-12 Aghajanian Michael K Ceramic-rich composite armor, and methods for making same
US6895851B1 (en) * 2003-06-16 2005-05-24 Ceramics Process Systems Multi-structure metal matrix composite armor and method of making the same

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8789454B1 (en) * 2010-04-12 2014-07-29 The United States Of America, As Represented By The Secretary Of The Navy Multi-ply heterogeneous armor with viscoelastic layers and cylindrical armor elements
US20150061182A1 (en) * 2010-04-12 2015-03-05 The Government Of The Us, As Represented By The Secretary Of The Navy Method for forming cylindrical armor elements
US9297617B2 (en) * 2010-04-12 2016-03-29 The United States Of America, As Represented By The Secretary Of The Navy Method for forming cylindrical armor elements
US9400146B1 (en) 2010-04-12 2016-07-26 The United States Of America, As Represented By The Secretary Of The Navy Method for forming cylindrical armor elements
US20170197873A1 (en) * 2014-06-06 2017-07-13 The Royal Institution For The Advancement Of Learning/Mcgill University Methods and systems relating to enhancing material toughness

Similar Documents

Publication Publication Date Title
US10753418B2 (en) Energy absorbing truss structures for mitigation of injuries from blasts and impacts
US7866248B2 (en) Encapsulated ceramic composite armor
EP2496906B1 (en) Improvements relating to armour
AU2002223998B2 (en) Laminated armor
US20120024138A1 (en) Armor panels having strip-shaped protection elements
US20110259184A1 (en) Multi-structure metal matrix composite armor with integrally cast holes
CA2612935C (en) Protective composite structures and methods of making protective composite structures
US8528457B2 (en) Method of producing a hybrid tile metal matrix composite armor
US20080264244A1 (en) Armor
US9890827B2 (en) Energy absorbing truss structures for mitigation of injuries from blasts and impacts
CA2479242A1 (en) Structural composite armor and method of manufacturing it
US20160375648A1 (en) Structural panel insert having encapsulated filler materials
US20090145289A1 (en) Composite armor plate and method for using the same
US7543523B2 (en) Antiballistic armor
US8464626B2 (en) Multi-layer metal matrix composite armor with edge protection
CA2309053C (en) Composite armor panel
US20120174750A1 (en) Armor materials, body armor articles and methods of manufacture
US20120247312A1 (en) Structural panel insert with honeycomb core
JP2012117705A (en) Shock absorbing member, and armor glass
EP2776782B1 (en) Composite passive armor protection
WO2008097375A2 (en) Encapsulated ceramic composite armor
US20120291618A1 (en) Teardrop lattice structure for high specific strength materials
KR101315855B1 (en) Mixed multi-layer amorphous surface composite for armor
US10942010B1 (en) Architected armor
EP2776781B1 (en) Composite passive armor protection

Legal Events

Date Code Title Description
AS Assignment

Owner name: HONEYWELL INTERNATIONAL, INC., NEW JERSEY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:OBOODI, REZA;RAYBOULD, DEREK;STRANGMAN, THOMAS E.;SIGNING DATES FROM 20071019 TO 20071024;REEL/FRAME:020008/0407

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION