WO2012121818A2 - Transparent and opaque reactive armor - Google Patents

Transparent and opaque reactive armor Download PDF

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Publication number
WO2012121818A2
WO2012121818A2 PCT/US2012/023283 US2012023283W WO2012121818A2 WO 2012121818 A2 WO2012121818 A2 WO 2012121818A2 US 2012023283 W US2012023283 W US 2012023283W WO 2012121818 A2 WO2012121818 A2 WO 2012121818A2
Authority
WO
WIPO (PCT)
Prior art keywords
armor system
bag
armor
fill
projectile
Prior art date
Application number
PCT/US2012/023283
Other languages
French (fr)
Other versions
WO2012121818A3 (en
Inventor
Vernon P. Joynt
Gregory W. Engleman
Robert A. Cole
Thomas E BORDER'S
Keith T. Williams
Paul OSBUN
Original Assignee
Force Protection Technologies, 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
Priority claimed from US13/024,640 external-priority patent/US20120204711A1/en
Application filed by Force Protection Technologies, Inc. filed Critical Force Protection Technologies, Inc.
Publication of WO2012121818A2 publication Critical patent/WO2012121818A2/en
Publication of WO2012121818A3 publication Critical patent/WO2012121818A3/en

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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
    • F41H5/007Reactive armour; Dynamic armour
    • 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
    • F41H5/0407Transparent bullet-proof laminatesinformative reference: layered products essentially comprising glass in general B32B17/06, e.g. B32B17/10009; manufacture or composition of glass, e.g. joining glass to glass C03; permanent multiple-glazing windows, e.g. with spacing therebetween, E06B3/66
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H7/00Armoured or armed vehicles
    • F41H7/02Land vehicles with enclosing armour, e.g. tanks
    • F41H7/04Armour construction

Definitions

  • the present disclosure relates to an armor system that resists penetration by projectiles including, as examples, shaped charges, explosively formed penetrators, and other energetic or high-velocity projectiles.
  • Conventional armor systems may be applied to armored fighting vehicles to protect against a variety of anti-tank munitions.
  • An example of anti-tank munitions is the RPG-7, a Russian-origin rocket propelled grenade with a shaped- charge (or hollow-charge) warhead that may penetrate several inches of armored steel.
  • Conventional armor systems and similar systems such as passive armors, defensive aid systems, and reactive armors, may defeat the threat from such antitank munitions like the RPG-7.
  • Passive armor systems such as bar or slat armor and RPG nets, may offer a relatively simple and affordable solution for defending against RPGs, but typically offer a 60-70% success rate against preventing detonation of the RPG by shorting out the fusing mechanism.
  • these systems may add
  • Defensive aid systems may detect incoming threats and counter those threats to prevent the vehicle from being hit.
  • Typical defensive aid systems may include a detection unit, such as radar, countermeasures, such as missiles and blast modules, and a control system to process threat signature and activate the countermeasures.
  • detection unit such as radar
  • countermeasures such as missiles and blast modules
  • control system to process threat signature and activate the countermeasures.
  • Such defensive aid systems are generally complex and expensive.
  • Explosive reactive armor systems may be generally effective to protect the vehicle from shaped-charges.
  • Such systems typically may include an explosive sandwich having a front and a back plate (typically metallic) separated by a thin sheet of explosive material.
  • the plates Upon detonation of the explosive material triggered by an impinging shaped-charge jet, the plates may be driven apart. The movement of the plates may increase the dynamic thickness of the armor system and may cause disruption of the jet by feeding material (e.g., the plates and the exploded material) into the path of the jet stream.
  • the high-velocity jet particles may be knocked off-line and reduce the penetration of the jet into the armor and vehicle.
  • Passive armor systems such as non-explosive/energetic reactive armors and electromagnetic armors, may use passive materials or electromagnetic forces to cause a front and a back plate to be driven apart.
  • the plates may be projected outwards at high velocities and may pose a threat to those around the vehicle.
  • the energetic materials used in passive armor systems may be regulated under hazard classifications and may require special handling.
  • Armor solutions that offer a weight advantage against these types of weapons may be measured in how much weight of rolled-homogenous-armor (RHA) it saves when compared with the RHA needed to stop a particular weapon from penetrating.
  • RHA rolled-homogenous-armor
  • This advantage may be calculated as a protection ratio, the ratio being equal to the baseline RHA penetration of a warhead minus the residual penetration into RHA, all divided by the areal density of the armor.
  • Such weights may be calculated per unit frontal area presented in the direction of the anticipated trajectory of the weapon.
  • Such armor may be made of materials that can be readily fabricated and incorporated into a vehicle design at a reasonable cost, and may be added to existing vehicles.
  • the present disclosure is directed to overcoming shortcomings and/or other deficiencies in existing technology.
  • the present disclosure is directed toward an armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory.
  • the armor system may include a plurality of modules.
  • Each module may include a bag, wherein each bag shares at least one seal with an adjacent bag, and a material contained in the bag and capable of being detonated, wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory.
  • the present disclosure is directed toward an armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory.
  • the armor system may include a plurality of modules. Each module may include a bag, wherein each bag shares at least one seal with an adjacent bag, and a material contained in the bag and capable of being detonated, wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory.
  • the armor system may also include a vessel housing the plurality of modules, wherein the vessel is substantially transparent.
  • the present disclosure is directed toward an armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory.
  • the armor system may include a plurality of modules. Each module may include a bag, wherein each bag shares at least one seal with an adjacent bag, and a material contained in the bag and capable of being detonated, wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory.
  • the armor system may also include a vessel housing the plurality of modules, wherein the vessel includes a separation element configured to separate the plurality of modules along the seams of the bags.
  • the present disclosure is directed toward an armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory.
  • the armor system may include a first element, leading relative to the expected projectile trajectory, a second element disposed behind the first element, relative to the expected projectile trajectory, wherein the first element and the second element are spaced apart to form a cavity, and a fill capable of being detonated disposed in the cavity, wherein the fill may include one or more of a desensitizer and a sensitizer.
  • FIG. 1 is a perspective view of an exemplary disclosed armor system
  • FIG. 2 is a schematic, cross-sectional view of a first exemplary disclosed embodiment of the armor system of Fig. 1 ;
  • Fig. 2A is a schematic view of another armor system
  • Fig. 2B is a schematic view of another armor system
  • Fig. 2C is a schematic view of another armor system
  • Fig. 2D is a schematic view of another armor system
  • FIG. 3 is a schematic, cross-sectional view of a second exemplary disclosed embodiment of the armor system of Fig. 1 ;
  • FIG. 4 is a schematic, cross-sectional view of a third exemplary disclosed embodiment of the armor system of Fig. 1 ;
  • FIG. 5 is a schematic, plan view of a fourth exemplary disclosed embodiment of the armor system of Fig. 1 ;
  • FIG. 6 is a schematic, cross-sectional view of the fourth exemplary disclosed embodiment of Fig. 5;
  • FIG. 7 is a schematic, detailed view of a fifth exemplary disclosed embodiment of the armor system of Fig. 1 ;
  • Fig. 8 is a schematic, detailed view of the armor system of Fig. 5;
  • FIG. 9 is a schematic, cross-sectional view of a fifth exemplary disclosed embodiment of the armor system of Fig. 1 ;
  • Fig. 0 is a schematic, cross-sectional view of a sixth exemplary disclosed embodiment of the armor system of Fig. 1 ;
  • Fig. 1 1 is a schematic, cross-sectional view of a seventh exemplary disclosed embodiment of the armor system of Fig. 1 ;
  • Fig. 12 is a schematic, cross-sectional view of an eighth exemplary disclosed embodiment of the armor system of Fig. 1 ;
  • FIG. 13 is a schematic illustration of an exemplary disclosed armor subsystem of the armor system of Fig. 1 ;
  • Fig. 14 is a schematic, plan view of yet another exemplary disclosed embodiment of the armor system.
  • FIG. 15 is another view of the exemplary disclosed embodiment of Fig. 14.
  • Fig. 16 is a schematic, cross-sectional view of the exemplary disclosed embodiment of Fig. 14.
  • Fig. 1 illustrates an exemplary disclosed armor system 10 for protecting a vehicle 11 from a projectile 12 such as, for example, an HC jet, EFP, and Hybrid warhead.
  • projectile 2 has an expected trajectory 15 relative to vehicle 1 1.
  • Trajectory 15 establishes a direction for understanding certain terms used in the following discussion (e.g., "leading,” “rear,” “behind,” “front,” etc.), describing the components of armor system 10 that projectile 12 successively confronts as it approaches a vehicle hull 20.
  • Armor system 10 may include one or more armor subsystems such as armor subsystem 25 and a distribution subsystem 30 (shown dotted) that may be disposed within hull 20.
  • Distribution subsystem 30 may provide a fill including at least one of a liquid and a gas to armor subsystem 25 of vehicle 11.
  • Fig. 1 also depicts additional embodiments of armor subsystems in accordance with the present disclosure, which will be described below.
  • armor subsystem 25 may include a first layer 35, a second layer 40, and a plurality of spacing elements 45. First layer 35, second layer 40, and spacing elements 45 together may form a cavity 50 that holds a fill 55. Armor subsystem 25 may also include a mount assembly 65 for mounting armor subsystem 25 to vehicle 11.
  • First layer 35 may lead second layer 40 relative to trajectory 15.
  • First layer 35 and second layer 40 may include, for example, transparent materials.
  • First layer 35 and second layer 40 may also be, for example, sheet-like layers including material such as, for example, glass, transparent ceramics, acrylic, polycarbonate, aluminum, delrin, UHMW PP (ultra high molecular weight polypropylene), UHMW PE (ultra high molecular weight polyethylene), and/or borosilicate.
  • First layer 35 and second layer 40 may be of any suitable thickness for containing a liquid or a gas such as, for example, between about 1/2" thick and about 3" thick.
  • first layer 35 and second layer 40 may be layers having a thickness of about 1/2" and including substantially only borosilicate.
  • First layer 35 and/or second layer 40 may also include one or more apertures 67 for draining and filling cavity 50 with fill 55.
  • Aperture 67 may be in fluid communication with cavity 50 and may be configured to receive a removable stopper 68. It is also contemplated that aperture 67 and stopper 68 may be included on other portions of armor subsystem 25 such as, for example, spacing elements 45
  • Spacing elements 45 may be formed from a chemical resistant material and include any material suitable for spacing first layer 35 from second layer 40 such as, for example, delrin or UHMW PE.
  • spacing elements 45 may be delrin gaskets.
  • Spacing elements 45 may be hollow or solid elements, and may be sealed with first layer 35 and second layer 40 by a chemical resistant sealant such as, for example, butyl rubber.
  • Cavity 50 may be a hollow, sealed space formed by first layer 35, second layer 40, and spacing elements 45. Cavity 50 may be partially or substantially filled by fill 55. Spacing elements 45 may space first layer 35 and second layer 40 apart to provide cavity 50 with a suitable dimensional thickness 60, as discussed below.
  • the fill disclosed in the below embodiments and used herein may include a material that is sufficiently reactive to be capable of detonation when exposed to a severe shock such as, for example, an impact of an HC jet from projectile 12.
  • a severe shock such as, for example, an impact of an HC jet from projectile 12.
  • Fill 55 may include a reactive liquid such as, for example, a liquid explosive, catalyst, and/or accelerant.
  • fill 55 may include a fuel such as methanol, and/or a clear liquid explosive such as
  • Fill 55 may also be a reactive liquid such as, for example, isopropyl nitrate, nitrobenzene, nitrogen tetroxide, and/or a fuel-like toluene.
  • fill 55 may include nitrobenzene having a detonation velocity of about 7,300 m/s (at about 1 atm pressure).
  • fill 55 may include a mixture of about 82% nitrogen tetroxide and about 18% toluene, and may have a detonation velocity of about 8,100 m/s (at about 1 atm pressure).
  • Fill 55 may also be a liquid in a highly viscous form such as, for example, gel form.
  • Cavity 50 may provide fill 55 with a suitable dimensional thickness 60 such as, for example between about 1" and about 8", between about 1" and about 6", and between about 1 1/2" and about 4".
  • Thickness 60 may be any sufficient thickness to support a continuous detonation of fill 55 following an initial detonation of fill 55 by a tip and/or jet of projectile 12.
  • the sufficient dimensional thickness to support continuous detonation may be larger than the "Minimum Detonation Thickness" (MDT), which may vary from explosive to explosive based on a given explosive's sensitivity to Shockwaves.
  • Dimensional thickness 60 may be greater than an MDT of fill 55.
  • fill 55 may have a 1" dimensional thickness when fill 55 includes substantially only nitromethane, based on MDT.
  • Fill 55 may also include a nonreactive liquid such as, for example, water.
  • Fill 55 may additionally include a mixture of one or more reactive liquids and one or more nonreactive liquids such as, for example, a mixture of fuel and water.
  • fill 55 may be a mixture of about 50% methanol and about 50% water, which may be substantially resistant to freezing at cold temperatures in the field and may keep interior surfaces of layers 35 and 40 substantially clean.
  • fill 55 may include transparent liquids and may be substantially transparent.
  • Fill 55 may also include a reactive gas such as, for example, ether, ethylene, acetylene, and/or hydrogen. Fill 55 may include a reactive gaseous mixture having a lower detonation velocity relative to reactive liquid mixtures. Fill 55 may also include a fuel that is at a gaseous state at ambient temperatures, e.g., at room temperature. Fill 55 may also include a mixture of one or more reactive gases and one or more nonreactive gases.
  • a reactive gas such as, for example, ether, ethylene, acetylene, and/or hydrogen.
  • Fill 55 may include a reactive gaseous mixture having a lower detonation velocity relative to reactive liquid mixtures.
  • Fill 55 may also include a fuel that is at a gaseous state at ambient temperatures, e.g., at room temperature. Fill 55 may also include a mixture of one or more reactive gases and one or more nonreactive gases.
  • fill 55 may include a mixture of ether and oxygen having a detonation velocity of about 2,300 m/s (at about 1 atm pressure), a mixture of ethylene and oxygen having a detonation velocity of about 2,423 m/s (at about 1 atm pressure), a mixture of acetylene and oxygen having a detonation velocity of about 2,900 m/s (at about 1 atm pressure), and/or a mixture of hydrogen and oxygen having a detonation velocity of about 3,800 m/s (at about 1 atm pressure). It is contemplated that the detonation velocities of reactive gases in fill 55 may be increased by pressurizing cavity 50 above a pressure of 1 atm.
  • fill 55 may include a mixture of hydrogen and oxygen that is pressurized, for example, at between about 1.4 atm and about 2.7 atm (between about 20 psi and about 40 psi). Fill 55 including a pressurized mixture of hydrogen and oxygen may provide a detonation velocity of greater than about 3,800 m/s. Also, for example, fill 55 may include an ideal gas pressurized at about 30 psi, and containing about three times more mass and energy than the same ideal gas may contain when unpressurized. Also, fill 55 may include transparent gases and may be substantially transparent.
  • fill 55 may include a number of materials, components, and mixtures thereof to tailor or customize the explosive sensitivity of fill 55.
  • fill 55 may include any combination of one or more sensitizers, desensitizers, and reactive materials to control the detonation velocity and/or the detonation susceptibility of fill 55.
  • the ability to control the explosive sensitivity of fill 55 may prevent certain types of projectiles from detonating fill 55, while detonating fill 55 upon impact from other types of projectiles to protect vehicle 11.
  • fill 55 may be desensitized by, for example, the presence of desensitizers, which may prevent detonation of fill 55 from impact from small arms fire, such as bullets and the like.
  • desensitizing fill 55 may produce a slower detonation velocity relative to traditional reactive materials used in explosive reactive armors.
  • the slower detonation velocity may be 5,400 m/s (at about 1 atm pressure).
  • the slower detonation velocity of fill 55 may cause larger Shockwaves to collide into projectile 12.
  • first layer 35 and spacing elements 45 may be formed of a frangible material, such as glass, polycarbonate, or an acrylic, and upon detonation of fill 55, first layer 35 and spacing elements 45 may shatter into many relatively small, non-lethal fragments.
  • the larger Shockwaves, the many fragments created by the shattered first layer 35 and spacing elements 45, and the density of fill 55 may reduce the penetration ability of projectile 12 into vehicle 11.
  • the slower detonation velocity and density of fill 55 may allow the
  • fill 55 may include any combination of sensitizers, desensitizers, and reactive materials to vary the explosive sensitivity of fill 55.
  • the reactive materials may include liquid explosives, such as, for example, nitromethane, and/or reactive liquid such as, for example, isopropyl nitrate, nitrobenzene, nitrogen tetroxide, and/or a fuel like toluene.
  • Desensitizers may include less reactive liquids, such as methanol, fire retardants, and/or nonreactive liquids, such as water.
  • structures, such as plates and/or sheets, formed of low speed of sound materials, such as rubber or polymers, may be contained within fill 55 to act as a desensitizer.
  • the plates and/or sheets may include varying thicknesses ranging from 1 mm to 25 mm.
  • Sensitizers may also include structures, such as sheets, spheres and/or cylindrical rods, formed of high speed of sound materials, such as ceramics, glass, aluminum, and/or steel.
  • the cross-sectional diameters of the sheets, spheres and/or cylindrical rods may range from 10 m to 50 mm.
  • the MDT and detonation velocity of fill 55 may be varied by selecting a combination of sensitizers, desensitizers, and reactive materials.
  • fill 55 may be desirably desensitized by including a suitable amount of desensitizers and sensitizers, thus decreasing the detonation velocity and the MDT of fill 55.
  • a housing holding fill 55 may be made thinner, thus reducing the weight on vehicle 11 and material costs.
  • one or more of first layer 35, second layer 40, and spacing elements 45 may have a thickness substantially between 1 mm and 100 mm.
  • sheets, rods and/or spheres may be used as a sensitizer for fill 55, and plates and/or sheets may be used as a desensitizer for fill 55. It should also be appreciated that the rods, spheres, plates, and/or sheets may also be used to manipulate the direction of the Shockwaves induced from the detonation reaction of fill 55. For example, and as shown in Fig. 2A, upon impact of projectile 12 with armor subsystem 25, fill 55 may detonate and induce
  • Sheets, Spheres and/or rods 2010 may divert the direction of Shockwaves 2000, in for example, a radial direction relative to spheres and/or rods 2010. It should be appreciated that sheets, spheres and/or rods 2010 may be arranged in a symmetrical or random configuration within fill 55, and may vary in cross-sectional diameter. As shown in Fig. 2B, Shockwaves 2000 induced by the detonation of fill 55 may be diverted by sheets and/or plates 2020. For example, the direction of Shockwaves 2000 may be directed away from the surfaces of sheets and/or plates 2020.
  • sheets and/or plates 2020 may be arranged in any other suitable configuration within fill 55, such as, for example, diagonally stacked (Fig. 2C), or may be a single sheet and/or plate 2020 arranged diagonally across fill 55 (Fig. 2D). Moreover, sheets and/or plates 2020 may vary in cross-sectional diameter.
  • armor subsystem 25 may be mounted to vehicle 11 by a mounting apparatus such as, for example, mount assembly 65.
  • Mount assembly 65 may include a mount 75, a hinge 80, and a frame 85.
  • Mount 75 may be operably connected to hinge 80, which may be connected to armor subsystem 25 by any suitable means known in the art.
  • armor subsystem 25 may be framed by a structural frame 85 on which hinge 80 is rotatably mounted. Armor subsystem 25 may thus be rotated about hinge 80.
  • Mount 75 may also be raised or lowered about a pivot point 90. Therefore, armor subsystem 25 may be adjusted as a louver system in front of an exterior surface 70 of vehicle 11 , as depicted in Fig. 2.
  • Armor subsystem 25 may be adjusted by mount assembly 65 by any suitable means in the art.
  • mount assembly 65 may be manually adjusted by an operator, or may be mechanically adjusted by a motor 95.
  • Armor subsystem 25 may be configured to adjust to provide clearance for the various systems of vehicle 11 such as, for example, emergency egress windows and antennas.
  • Armor subsystem 25 may be used to provide additional protection at any suitable location of vehicle 11 such as, for example, additional protection for transparent armor of windows of vehicle 11 and additional perimeter protection for opaque armor on a side of vehicle 11.
  • armor subsystem 25 may be rotatably mounted via mount assembly 65 at an angle 00, relative to trajectory 15, where trajectory 15 may be substantially perpendicular to vehicle exterior surface 70. Armor subsystem 25 may be rotatably adjusted so that angle 100 is oriented, for example, at about 30°, 45°, 60°, or 90°
  • Figs. 1 and 3 depict a second embodiment, armor subsystem 125, of armor system 10.
  • armor subsystem 125 may include a first element 130, a second element 135, and a plurality of spacing elements 140.
  • First element 130, second element 135, and spacing elements 140 may form a cavity 145 that holds a fill 150.
  • Armor subsystem 125 may also include a mount assembly similar to mount assembly 65 of armor subsystem 25.
  • Spacing elements 140 may be similar to spacing elements 45 of armor subsystem 25, and cavity 145 may be similar to cavity 50 of armor subsystem 25.
  • First element 130 may lead second element 135 relative to trajectory 15.
  • First element 130 may include a plurality of layers 155 and an intermediate layer 160 that may be disposed between layers 155.
  • Layers 155 may be sheet-like layers including material such as, for example, glass, transparent ceramics, acrylic, polycarbonate, aluminum, delrin, UHMW PP, UHMW PE, and/or borosilicate.
  • Layers 155 may be suitable thin-walled layers for containing a liquid or a gas.
  • layers 155 may be glass sheets having a thickness of about 1/8".
  • Intermediate layer 160 may include a nonreactive liquid or gas.
  • intermediate layer 160 may include a nonreactive liquid such as, for example, water. It is also contemplated that intermediate layer 160 may include a reactive liquid or gas.
  • Intermediate layer 160 may have any suitable thickness for an armored layer such as, for example, between about 1/8" and about 6". For example, intermediate layer 160 may have a thickness of about 1/2".
  • Second element 135 may include a plurality of layers 165 and an intermediate layer 170 that may be disposed between layers 165. Layers 165 of second element 135 may be similar to layers 155 of first element 130, and intermediate layer 170 of second element 135 may be similar to intermediate layer 160 of first element 130, respectively.
  • armor subsystem 125 may be mounted at an exterior of vehicle 11 , as a louver as shown in Fig. 1 , and/or as a window module in a shaped aperture of vehicle 11 , as discussed henceforth in relation to armor subsystem 225.
  • first element 130 and/or second element 135 may also include one or more apertures 175, each configured to receive a removable stopper 180.
  • Aperture 175 and stopper 180 may be similar to aperture 67 and stopper 68, respectively, of armor subsystem 25. It is also contemplated that aperture 175 and stopper 180 may be included on other portions of armor subsystem 125 such as, for example, spacing elements 140.
  • Fill 150 may include a reactive and/or nonreactive liquid or gas, and may be similar to fill 55 of armor subsystem 25.
  • fill 150 may include a reactive liquid such as, for example, nitromethane and/or isopropyl nitrate.
  • Fill 150 may have a dimensional thickness 185 that is greater than an MDT of fill 150.
  • Figs. 1 and 4 depict a third embodiment, armor subsystem 225, of armor system 10.
  • armor subsystem 225 may include a layer 230, at least one transparent armor layer 235, at least one seal 240, and at least one frame element 245.
  • Layer 230, transparent armor layer 235, and seal 240 may be supported by frame element 245 and may form a cavity 250 that holds a fill 255.
  • Layer 230 may lead transparent armor layers 235 relative to trajectory 15, and layer 230 may be similar to first layer 35 and second layer 40 of armor subsystem 25. To facilitate use in a window of vehicle 11 , layer 230 may include a transparent material. Layer 230 may be spaced apart from the at least one transparent armor layer 235.
  • the one or more transparent armor layers 235 may include glass, transparent ceramics, acrylic, polycarbonate, and/or borosilicate.
  • Transparent armor layer 235 may be of any suitable thickness such as, for example, between about 1/8" and about 6" thick.
  • the one or more seals 240 may include materials similar to spacing elements 45 of armor subsystem 25.
  • the one or more seals 240 may include a single gasket or a plurality of seals.
  • the one or more seals 240 may form a seal between layer 230, transparent armor layers 235, and one or more frame elements 245 to seal fill 255 within cavity 250.
  • seal 240 may be a single rubber gasket that surrounds and seals layer 230 and transparent armor layers 235, and fits within frame element 245.
  • Frame element 245 may support armor subsystem 225 within a shaped aperture 260 of vehicle 1 1. Shaped aperture 260 may extend into an interior of vehicle 1 1.
  • armor subsystem 225 may provide a transparent armored window for vehicle 1 1 , as shown in Fig. 1 , but may also be used in a louver configuration as shown in armor subsystems 25 and 125.
  • Seal 240 and/or frame 245 may include one or more apertures 265 and stoppers 270, for draining and/or filling fill 255 in cavity 250.
  • Apertures 265 and stoppers 270 may be similar to aperture 67 and stopper 68 of armor subsystem 25.
  • Fill 255 may be similar to fill 55 of armor subsystem 25.
  • Fill 255 may include a reactive or nonreactive liquid or gas.
  • fill 255 may include substantially only nitromethane and may have a thickness such as, for example, 1 1/2".
  • fill 255 may include, for example, substantially only isopropyl nitrate.
  • Fill 255 may have a dimensional thickness 272 that is greater than an MDT of fill 255.
  • Figs. 1 , 5, and 6 depict a fourth embodiment, armor subsystem 325, of armor system 10.
  • armor subsystem 325 may include a modular array 330, a support system 335 for providing structural support to modular array 330, and a filling system 340 for providing modular array 330 with fill.
  • modular array 330 may include a ballistic module 345, a plurality of fill modules 350, and a spall module 355.
  • Ballistic module 345 may provide protection against ballistic threats to vehicle 11
  • fill modules 350 may provide additional protection against threats to vehicle 11
  • spall module 355 may provide protection against spalling of armor system 10.
  • Ballistic module 345, fill modules 350, and spall module 355 may be connected by any suitable technique known in the art such as, for example, by welding or by mechanical fasteners.
  • Ballistic module 345 may be a ballistic-resistant layer that leads fill modules 350 relative to trajectory 15, and may include a plurality of layers 360 and 365.
  • Layers 360 and 365 may be of any suitable material and thickness for resisting ballistic threats to vehicle 11.
  • layers 360 and 365 may include high strength metals such as aluminum, copper, steel, stainless steel, magnesium, molybdenum, copper, zirconium, titanium, nickel, and other high strength materials such as glass fiber and polymer.
  • Layers 360 and 365 may have any thickness suitable for ballistic protection such as, for example, a thickness of between about 1/8" and about 4".
  • Fill modules 350 may follow ballistic module 345 relative to trajectory 15, and may lead spall module 355 relative to trajectory 15.
  • Each fill module 350 may include a first layer 370 and a second layer 375. First layer 370 and second layer 375 may seal together to form a cavity 380 that holds a fill 385. First layer 370, second layer 375, cavity 380, and fill 385 may be similar to first layer 35, second layer 40, cavity 50, and fill 55, respectively, of armor subsystem 25.
  • Each fill module 350 may be an individual cell containing fill 385. Fill modules 350 may be disposed adjacently to each other in armor subsystem 325. Fill 385 may have a dimensional thickness 388 that is greater than an MDT of fill 385.
  • Spall module 355 may be a spall-resistant layer that follows fill modules 350 relative to trajectory 15. Spall module 355 may have a layer 390 that includes similar materials and has a similar thickness as layers 360 and 365 of ballistic module 345.
  • Support system 335 may include a separation element 395 and a frame 400. Separation element 395 may support fill modules 350 within frame 400.
  • Separation element 395 may be any suitable material for insulating fill modules 350 from adjacent threat detonations such as, for example, a
  • Separation element may be disposed between fill modules 350, and may also include transparent materials. Separation element 395 may be a thin layer separating fill modules 350, and thereby substantially reduce
  • fill modules 350 may be removably attachable from armor subsystem 325, thereby allowing compromised fill modules 350 to be replaced with new fill modules 350 within a combat area.
  • Frame 400 may include any suitable material for structurally supporting armor subsystem 325 such as, for example, structural steel or aluminum. Referring back to Fig. 1 , frame 400 may be configured to mount armor subsystem 325 within an aperture of vehicle 11 as a window, or may be mounted to an exterior of vehicle 11 , for example, as a louver. Fill modules 350 may be sealed against frame 400 by a seal 405 that may include similar materials as seal 240 of armor subsystem 225.
  • filling system 340 may include a plurality of passageways 410 and a plurality of valves 415. Passageways 410 may connect adjacent fill modules 350 to facilitate filling of fill modules 350 with fill 385.
  • Passageways 410 may have an internal diameter that is less than an MDT of a given fill 385.
  • Valves 415 may be disposed in passageways 410 to substantially prevent leakage from fill modules 350 that may be compromised by threat projectiles. Valves 415 may be any valve suitable for substantially reducing leakage such as, for example, one-way check valves.
  • filling system 340 may facilitate filling fill modules 350 simultaneously via passageways 410, and may prevent leakage from compromised fill modules 350 via valves 415.
  • Fig. 7 depicts an alternative embodiment, fill module 420, of armor subsystem 325.
  • Fill module 420 may be similar to fill module 350, and may include a cavity 425 having a fill 430, which may be similar to cavity 380 and fill 385, respectively, of fill module 350. Materials and thicknesses of fill module 420 may be selected in order to substantially minimize aberrations due to differences in material properties (e.g., differences in the index of refraction) between the various materials included in fill module 420. Fill modules 420 may be configured to be removably attachable to armor subsystem 325. Fill modules 420 may be pre-filled with fill 430 during manufacturing. Thus, a given pre-filled module 420 may be removed from frame 400 if it becomes compromised, and replaced with a new pre- filled module 420.
  • Fig. 8 illustrates an exploded view of armor subsystem 325, which depicts a length 435 of fill module 350. Keyholes 440 and 445 are also depicted, which may result from an impact of projectile 12 into armor subsystem 325 along trajectory 15. Length 435 may be at least twice as large as a length of keyholes 440 and 445. As projectile 12 travels along a projected path 450, keyhole 440 may be formed in layer 360 and layer 365, and keyhole 445 may be formed in layer 390. Keyholes 440 and 445 may be formed because layers of armor subsystem 325 may shift with respect to each other as projectile 12 impacts armor subsystem 325. For example, as projectile 12 impacts, layers 360 and 365 may shift upward, thereby causing keyhole 440 to have a keyhole shape as projectile 12 passes through moving layers 360 and 365. Keyhole 445 may be similarly formed.
  • Figs. 1 and 9 depict a fifth embodiment, armor subsystem 525, of armor system 10.
  • armor subsystem 525 may include a material 550 having a dimensional thickness 560.
  • Armor subsystem 525 may also include a mount assembly for mounting armor subsystem 525 to vehicle 11.
  • Material 550 may include a reactive and/or nonreactive liquid or gas, and may include materials similar to fill 55 of armor subsystem 25.
  • Material 550 may be a liquid in a highly viscous form such as, for example, gel form.
  • Material 550 may be a gelled block of material having dimensional thickness 560.
  • Material 550 may be gelled such that it may substantially retain a shape such as, for example, a block shape having thickness 560, without being contained in a housing or confined between structural elements.
  • Material 550 may include any suitable material such as, for example, substantially entirely transparent materials. [071]
  • Material 550 may disrupt a projectile such as, for example, an HC jet of projectile 12.
  • Dimensional thickness 560 may be large enough to exceed a minimum detonation thickness (MDT) of material 550, which may include reactive material, such that material 550 may react to disrupt the jet of projectile 12.
  • An appropriate dimensional thickness 560 may vary based on, for example, a type of reactive material included within material 550 and/or a volume of material 550. Dimensional thickness 560 may be greater than an MDT of material 550.
  • a shape and/or material types of material 550 and/or a value of thickness 560 may be sized such that material 550 reacts over a duration of time that is sufficient to disrupt an entire jet of projectile 12.
  • material 550 may have a sufficient size and be of a sufficient material to react relatively gradually as a jet is encountered, such that the reaction lasts long enough to disrupt an entire jet of projectile 12.
  • thickness 560 may be of a relatively large thickness such as, for example, between about 1" and about 6", between about 1" and about 12", or in excess of 12", depending on the material and geometric properties of material 550 such as, for example, the minimum detonation thickness of material 550.
  • Figs. 1 and 10 depict a sixth embodiment, armor subsystem 625, of armor system 10.
  • armor subsystem 625 may include a housing 640 and a material 650 having a dimensional thickness 660.
  • Armor subsystem 625 may also include a mount assembly for mounting armor subsystem 625 to vehicle 11.
  • Material 650 and thickness 660 may be similar to material 550 and thickness 560 of armor subsystem 525, respectively.
  • Material 650 may be in a gelled form or in a non-gelled form.
  • Material 650 may be housed in housing 640.
  • Dimensional thickness 660 may be greater than an MDT of material 650.
  • Housing 640 may be a thin-walled vessel suitable for containing a gelled and/or a non-gelled material. Housing 640 may be formed from a single element, or may be formed from several elements that are attached by any suitable method such as, for example, by welding. Housing 640 may include thin walls such as, for example, about 3/4", about 1/2", about 3/8", about 1/4", about 1/8", about 1/16", about 3/32", about 1/32", and/or about 1/64".
  • Figs. 1 and 11 depict a seventh embodiment, armor subsystem 725, of armor system 10.
  • armor subsystem 725 may include a first layer 735, a second layer 740, and a plurality of spacing elements 745.
  • First layer 735, second layer 740, and spacing elements 745 together may form a cavity 750 that holds a fill 755.
  • Armor subsystem 725 may also include a mount assembly for mounting armor subsystem 725 to vehicle 11.
  • Spacing elements 745 may be similar to spacing elements 45 of armor subsystem 25.
  • Cavity 750 may be similar to cavity 50 of armor subsystem 25.
  • Cavity 750 may have a dimensional thickness 760 that may be sized similarly to thickness 60 of armor subsystem 25.
  • First layer 735 and second layer 740 may be similar to first layer 35 and second layer 40 of armor subsystem 25.
  • First layer 735 and second layer 740 may include, for example, opaque materials.
  • First layer 735 and/or second layer 740 may also include one or more apertures 767 for draining and filling cavity 750 with fill 755.
  • Aperture 767 may be similar to aperture 67 of armor subsystem 25, and may include a stopper 768 that may be similar to stopper 68 of armor subsystem 25.
  • Fill 755 may include, for example, opaque reactive materials.
  • Fill 755 may include relatively insensitive explosives with detonation velocities of about 4,000 m/s (at about 1 atm pressure) to about 7,000 m/s (at about 1 atm pressure).
  • fill 755 may include materials such as ammonium nitrate, potassium chlorate, urea nitrate, urea, and tetranitro-isopropanol.
  • Fill 755 may also include mixtures of one or more of these materials with fuels and/or sensitizers.
  • Dimensional thickness 760 may be greater than an MDT of fill 755, and may support a continuation detonation of fill 755 following an initial detonation of fill 755 by a tip and/or jet of projectile 12.
  • a shock sensitivity of fill 755 may depend on, for example, a degree of pressurization and/or confinement of fill 755 within cavity 750 and/or the material properties and proportions of materials included in fill 755.
  • Fill 755 may include materials which, although not classified as explosives, may behave as explosives when exposed to a severe shock such as, for example, the impact of an HC jet from projectile 12.
  • a shape and/or material types of fill 755 and/or a value of dimensional thickness 760 may be sized such that fill 755 reacts over a predetermined length of time that is sufficient to disrupt an entire jet of projectile 12.
  • Fill 755 may also be a gelled material that may retain a shape such as a block shape similar to material 550 of armor subsystem 525. Fill 755 may thereby retain a shape without being contained in a housing or between structural elements. Fill 755 may additionally be a gelled or non-gelled material that may be housed in a thin-walled vessel similar to housing 640 of armor subsystem 625.
  • Figs. 1 and 12 depict an eighth embodiment, armor subsystem 825, of armor system 10. As best seen in Fig. 12, armor subsystem 825 may include a first layer 835, a second layer 840, and a plurality of spacing elements 845.
  • First layer 835, second layer 840, and spacing elements 845 together may form a cavity 850 that has a thickness 860 and holds a fill 855 of thickness 860.
  • the elements of armor subsystem 825 may be similar to the elements of armor subsystem 725.
  • Dimensional thickness 860 may be greater than an MDT of fill 855.
  • Armor subsystem 825 may be an armor panel that is attached to hull 20 of vehicle 11.
  • an exterior surface 865 of second layer 840 may be attached to an exterior surface of hull 20 by any method suitable in the art such as, for example, mechanical fasteners, welding, and/or adhesives.
  • Fig. 13 depicts distribution subsystem 30 that may be disposed within an interior portion of vehicle 11.
  • Distribution subsystem 30 may include a pump 455, a plurality of passageways 460, a fill reservoir 465, and a waste reservoir 470.
  • Pump 455 may pressurize and pump liquid such as fills 55, 150, 255, 385, 650, 755, and/or 855 from fill reservoir 465 and through passageways 460.
  • Pump 455 may be any suitable pump known in the art such as, for example, a piston type pump or an impeller type pump. Pump 455 may be driven, for example, via a crankshaft from an engine of vehicle 11 or by an independent power source. Pump 455 may be fluidly connected to the plurality of passageways 460 and fill reservoir 465, and may draw fill from fill reservoir 465.
  • Passageways 460 may be disposed in an interior portion of vehicle 11 such as, for example, a vehicle spine. Passageways 460 may be housed in a protective jacket that may provide protection from external threats such as, for example, bullets, shrapnel, mine blasts, HC jets, and EFP projectiles.
  • Passageways 460 may have an internal diameter that is less than an MDT of the fill that is being transferred.
  • passageways 460 may be a stainless steel tube having an internal diameter of about 1/4", if the MDT of the fill is greater than 1/4".
  • the plurality of passageways 460 may fluidly connect pump 455 with the armor subsystems of vehicle 11 such as armor subsystems 25, 125, 225, 325, 525, 625, 725, and/or 825.
  • distribution subsystem 30 may drain and re-fill armor system 10 with fill upon demand.
  • Fill reservoir 465 may be a protected reservoir for storing fill such as fills 55, 150, 255, 385, 650, 755, and/or 855 and for supplying the fill to pump 455.
  • Fill reservoir 465 may include a reinforced and/or armored lining to resist penetration by ballistics and other threats. Fill reservoir 465 may include sufficient fill to iteratively fill cavities 50, 1 5, 250, 380, 750, and/or 850 and/or housing 640 numerous times during a given operation time of vehicle 11. It is contemplated that fill reservoir 465 may have an elongated shape and have an internal diameter that is less than an MDT of a stored fill.
  • Waste reservoir 470 may be a protected reservoir similar to fill reservoir 465. Waste reservoir 470 may be fluidly connected to armor subsystems 25, 125, 225, 325, 625, 725, and/or 825 via drainage passageways (not shown) that may be similar to passageways 460. Fill may be drained from armor subsystems 25, 125, 225, 325, 625, 725, and/or 825 and delivered to waste reservoir 470 via the drainage passageways.
  • the drainage passageways and/or passageways 460 may include check valves to control flow of fill during drainage and filling of armor subsystems 25, 125, 225, 325, 625, 725, and/or 825 during an operation of distribution subsystem 30.
  • Figs. 14-16 illustrate yet another exemplary embodiment of an armor subsystem 925 for armor system 10.
  • armor subsystem 925 may include a plurality of modules 1000 having a plurality of bags 002, a support vessel 1001 , a separation element 1003, and a cover 1004.
  • Fig. 15 illustrates a disassembled view of armor subsystem 925.
  • support vessel 1001 may include an appropriate volume for housing the plurality of modules 1000. More particularly, support vessel 1001 may contain the plurality of bags 1002 and separation element 1003, with cover 1004 positioned over support vessel 1001 to encapsulate the plurality of modules 1000 within support vessel 1001. Support vessel 1001 may follow cover 1004 and lead an exterior surface of vehicle 11 relative to trajectory 15.
  • support vessel 1001 may be a substantially transparent, lightweight, and/or relatively frangible material, such as, for example, polymethylmethacrylate, glass,
  • Armor subsystem 925 may be coupled to vehicle 11 in a similar manner as armor system 325.
  • support vessel 1001 and thus armor subsystem 925, may be configured to be mounted within an aperture of vehicle 11 as a window, or may be mounted to an exterior of vehicle 11 , for example, as a louver.
  • armor subsystem 925 may include any number of rows and columns of modules 1000.
  • Cover 1004 may be a substantially transparent material and may lead the plurality of bags 1002 and support vessel 001 relative to trajectory 15.
  • Cover 1004 may be a sheet-like layer and may be thin, lightweight, and/or relatively frangible.
  • cover 004 may be a thin sheet of
  • Cover 1004 may be removably connected to support vessel 1001 by any suitable technique known in the art, such as, for example, by mechanical fasteners or removable welds.
  • Support vessel 1001 and cover 1004 may also include any thickness suitable for ballistic protection, such as, for example, a thickness between 1/8" and about 4". However, it should be appreciated that cover 1004 may include a thickness thinner relative to a thickness of a rear wall of support vessel 1001.
  • cover 1004 may shatter into relatively small, non-lethal fragments, while the rear wall of support vessel 1001 may be provide impact and ballistic protection for vehicle 11.
  • Cover 1004 may preferably have a thickness between 1 mm to 100 mm, and the rear wall of support vessel 1004 may preferably have a thickness between 1 mm to 100 mm.
  • cover 1004 may have a suitable thickness and/or structural rigidity to prevent detonation by certain projectiles.
  • cover 1004 may have a sufficient thickness and rigidity to prevent small mass and low velocity projectiles, such as bullets from small-arms weapons, from impacting and detonating bags 1002.
  • support vessel 1001 and cover 1004 may include a substantially transparent, lightweight, and relatively frangible material, such as glass, support vessel 1001 and cover 1004 may provide substantial visibility from inside vehicle 11, while also reducing the amount of overpressure to vehicle 11 and reactive fragments expelled from armor subsystem 1 1 upon detonation of a bag 1002.
  • frangible materials such as glass, may create a large debris field upon detonation of bags 1002, thereby disrupting the trajectory of a projectile and damage to vehicle 11.
  • the brittle nature of such frangible materials may also be less lethal to those around the debris field. Therefore, the threat of damage to vehicle 11 and injury to the occupants of vehicle 11 and persons around vehicle 11 may be minimized.
  • the mass of each individual piece of debris in the debris field may be substantially the same to promote improved disruption of the projectile.
  • the plurality of bags 1002 may be formed of a thin and transparent material and may contain fill material 1055 similar to fill 55 of armor subsystem 25. That is, fill material 1055 may be a miscible fluid capable of detonating upon an appropriate agitation. In one embodiment, fill material 1055 may be clear and transparent, such that one may see through bag 1002 and fill material 1055. One may also see through bag 1002 and fill material 1055 through, for example, night vision goggles. It should also be appreciated that in certain embodiments, fill material 1055 may include an opaque mixture of one or more liquids, including, as examples, ammonium nitrate and urea nitrate, if transparency is not required.
  • fill material 1055 may cause detonation.
  • fill material 1055 may include a suitable thickness to prevent detonation by certain projectiles.
  • fill material 1055 may be sufficiently thick to prevent small mass and low velocity projectiles, such as bullets from small-arms weapons, from inducing sufficient Shockwaves and causing detonation of fill material 1055 upon impact.
  • said thickness may allow projectiles having a sufficient mass and velocity, such as, for example, a hollow-charged jet, shaped-charged jets, and explosively-formed penetrators, to induce sufficient Shockwaves in fill material 1055 and cause detonation.
  • projectiles having a sufficient mass and velocity such as, for example, a hollow-charged jet, shaped-charged jets, and explosively-formed penetrators, to induce sufficient Shockwaves in fill material 1055 and cause detonation.
  • fill material 1055 may be relatively thin such that fill material 1055 may be more sensitive to detonation. That is, sufficient Shockwaves may be more easily induced to cause detonation of fill material 1055. Such a feature may, for example, prevent Shockwaves from propagating between modules 1000 and causing undesired detonation of neighboring modules. Impact between a projectile and a single module 1000 may detonate fill material 1055 before Shockwaves induced in that module 1000 propagate and induce the detonation of neighboring modules 1000.
  • Fill material 1055 may also have a relatively slower detonation velocity. Accordingly, fill material 1055 may produce a greater and longer
  • fill material 1055 may be a reactive material
  • the use of a separate energy source to detonate fill material 1055 may be eliminated.
  • Projectile detection units, such as radars, are also not necessary. Therefore, armor subsystem 925 provides a more simplistic design.
  • Fill material 1055 may also be a liquid in a highly viscous form such as, for example, gel form or slurry form, to prevent leakage from plastic bags 1002.
  • the plurality of plastic bags 1002 may be of a chemical resistant material. As such, the material of the plurality of bags 1002 may be inhibited from chemically reacting with fill 1055, thereby maintaining the
  • bags 1002 may be formed of polycarbonate, polymethylmethacrylate, derline, polyethylene, polyurethane, or any other suitable chemical resistant material. In certain embodiments, bags 1002 may be coated with the chemical resistant material.
  • Each of the bags 1002 may enclose fill 1055 and be fluidly sealed from the environment and one another.
  • the plurality of bags 1002 may be connected together and form a "quilted" configuration of bags 1002. For example, each bag 1002 may share a fluidic seal with an adjacent bag. In other words, the plurality of bags 1002 may be integrally formed of one or more materials.
  • each bag 1002 may be separately connected to the other by, for example, stitching, welding, or any other suitable means. Such a configuration may allow all of the bags 1002 to be removed together when, for example, the bags 1002 are damaged or discolored, thus providing eased assembly and disassembly of modules 1000.
  • utilizing bags 1002 that may be formed of a thin and lightweight material may advantageously reduce the overall weight and bulk of armor subsystem 925. In turn, the strain on the engine and drive train of vehicle 11 may be reduced, and a favorable mass efficiency may be provided.
  • Separation element 1003 may be any suitable material for insulating modules 1000 from detonations of adjacent bags 1002 such as, for example, a polycarbonate material. Separation element 1003 may be disposed between modules 1000, and may also include transparent materials. Separation element 1003 may be a thin layer separating modules 1000 from each other along the seams of the plurality of bags 1002, and thereby substantially reduce sympathetic detonation of a given module 1000 in the case that an adjacent module 1000 detonates due to impact of a threat projectile. It is contemplated that separation element 1003 may be removably attachable to support vessel, thereby allowing compromised bags 1002 to be replaced with new bags 1002 within a combat area.
  • bags 1002 may themselves be configured to reduce and/or prevent sympathetic detonation.
  • the seals between bags 1002 may be of an appropriate thickness and/or lateral length, while maintaining sufficient flexibility, to protect against detonation of one or more neighboring bags 002.
  • the seams may be formed of multiple layers of bag 1002 material folded and welded together, or may include separate materials directly stitched, welded, or otherwise connected to the seams of bags
  • support vessel 1001 , cover 1004, and bags 1002 may be formed of one or more substantially opaque materials.
  • Such opaque materials may be lightweight, frangible, and chemical resistant, and may include, as examples, acetal and any other suitable polymer, composite, or ceramic.
  • one or both of support vessel 1001 and cover 1004 may be scored to prevent the creation of large fragments upon detonation of bags 1002.
  • Fig. 16 illustrates a section view of Fig. 5.
  • Each bag 1002 may be supported and contained between support vessel 1001 , separation element 1003, and cover 1004.
  • the volume surrounding each bag 1002 may be filled with an inert liquid 1005.
  • Inert liquid 1005 may be substantially transparent and configured to minimize visual aberrations by maintaining the appropriate indexes of refraction within each module 1000. Thus, sufficient visibility and transparency through each module 1000 may be provided.
  • Inert liquid 1005 may also act as an appropriate buffer to prevent sympathetic detonation between neighboring bags 1002 and dissipate the blast energy of fill material 1055 transmitted to vehicle 11.
  • Inert liquid 1005 may include, for example, water, glycol, or silicon.
  • Armor system 10 may be included in newly manufactured vehicles and existing vehicles may be retrofitted with armor system 10 to gain the benefits described herein.
  • an existing vehicle may be retrofitted with subsystems 25, 30, 125, 225, 325, 525, 625, 725, 825, and/or 925 using an assemblage of required parts specific to the vehicle, e.g., in kit form.
  • any of 25, 30, 125, 225, 325, 525, 625, 725, 825, and 925 may be coated with any suitable fire retardant.
  • a vehicle may include any combination of the subsystems of armor system 10 including, for example, armor subsystems 25, 30, 125, 225, 325, 525, 625, 725, 825, and/or 925.
  • armor subsystems 25, 30, 125, 225, 325, 525, 625, 725, 825, and/or 925 may be used in combination with each other, as additional armor within a window aperture, as a louver or a system of louvers, and/or as additional perimeter protection for opaque armor.
  • some or all of armor subsystems 25, 125, 225, 325, 525, 625, 725, 825, and/or 925 may be used in conjunction with distribution subsystem 30.
  • any of the materials of fills 55, 150, 255, 385, 430, 550, 650, 755, 855, and/or 1055 may be used in any of armor subsystems 25, 125, 225, 325, 525, 625, 725, 825, and/or 925. It is further contemplated that the disclosed elements of armor subsystems 25, 30, 125, 225, 325, 525, 625, 725, 825, and/or 925 may be used with any of the other disclosed armor subsystems.
  • Vehicle 1 1 equipped with armor system 10, may operate outside of a combat area.
  • vehicle 11 may move under its own power or be transported for example, by aircraft or rail.
  • armor system 10 may be configured to be in a non-hostile mode.
  • mount assembly 65 may be operated so that armor subsystem 25 is propped up or folded down as needed during transport or storage.
  • Mounts of armor subsystems 125 and 325 may be similarly operated.
  • stoppers 68, 180, 270, and/or 768 may be removed from armor subsystems 25, 125, 225, and/or 725, respectively, to drain reactive fill from vehicle 11 and thereby preclude "special handling" requirements for operators during transport and other activities outside of a combat area.
  • Distribution subsystem 30 may also be operated to transfer fill from the cavities of the various armor subsystems to waste reservoir 470. Reactive fill may be removed from waste reservoir 470, thereby precluding "special handling" requirements outside of a combat area.
  • fill modules 420 may be removed from vehicle 11 when outside of a combat area. It is contemplated that substantially all fill may be removed from vehicle 1 1 when in the non-hostile mode.
  • armor system 10 When vehicle 11 moves toward a combat area or other threat environment, armor system 10 may be configured to be in a hostile mode. Fill may be added to cavities and reservoirs of vehicle 1.
  • mount assemblies may be configured so that armor subsystems 25, 125, 325, 525, 625, 725, and/or 925 are adjusted to a suitable position for disrupting threat projectiles. Armor subsystems 25, 125, 325, 525, 625, 725, and/or 925 may be adjusted so that angle 100 is, for example, about 30° or about 45°.
  • fill may be added to the cavities of the armor subsystems, and stoppers 68, 180, 270, and/or 768 may be replaced into apertures 67, 175, 265, and/or 767 of armor subsystems 25, 125, 225, and/or 725, respectively.
  • Distribution subsystem 30 may also be operated to transfer fill from fill reservoir 465 to the cavities of the various armor subsystems.
  • fill modules 420 may be placed into armor subsystem 325 of vehicle 11. While vehicle 1 1 is in the field, fill may be manually drained and re-filled, or mechanically drained and re-filled by distribution subsystem 30, into cavities 50, 145, 250, 380, 750, and/or 850 and/or housing 640.
  • Fill may be drained and refilled, for example, if an armor subsystem is compromised, the fill becomes contaminated, or the fill begins to chemically break down from its intended properties. It should also be appreciated that a distribution system similar to distribution system 30 may be incorporated into armor subsystem 925 to fill and drain fill material 1055 from one or more bags 1002. Moreover, the distribution system of armor system 925 may be configured to fill and drain liquid from support vessel 1001.
  • a projectile may be directed toward vehicle 1 1 and may impact armor subsystems 25, 125, 225, 325, 525, 625, 725, 825, and/or 925. If the projectile penetrates the armor subsystems and enters cavities 50, 145, 250, 380, 425, 725, 825, and/or 925, material 550, module 1000, and/or housing 640, the projectile will detonate reactive fill disposed in the cavities. The reactive fill will detonate and disrupt the penetration of the projectile. The material properties of armor system 10 will contribute to the disruption of the projectile.
  • armor subsystems 25, 125, 225, 325, 420, 625, 750, 850, and/or 925 including glass and/or polycarbonate layers will shatter upon detonation of the fill, causing a debris field that will disrupt a projectile jet.
  • Material 550 of armor subsystem 525 will continuously detonate over substantially an entire duration of impact of an HC jet of projectile 12, thereby substantially completely disrupting the jet.
  • Armor subsystems 25, 125, 225, 325, 420, 625, 725, and/or 825 including aluminum and/or delrin layers will propel the aluminum and/or delrin layers into the projectile threat upon detonation of the fill, causing a debris field that will disrupt the projectile jet.
  • valves 415 may substantially prevent leakage of fill from adjacent modules.
  • armor system 10 may be reconstituted in the field. For example, fill may be manually drained and re-filled into cavities 50, 145, 250, 380, 750, and/or 850 and/or housing 640 or mechanically drained and re-filled by distribution subsystem 30. Also, compromised fill modules 420 and bags 1000 may be removed and replaced with operational fill modules 420 and bags 1000. Further, compromised material 550 may be removed and replaced with operational material 550.
  • armor system 10 may preclude the requirement for "special handling" by operators when vehicle 11 is outside of a combat area or other threat environment.
  • Armor system 10 provides additional threat protection that is modular and that may be incorporated in new vehicles or retrofitted into existing vehicles.
  • armor system 10 may be used to provide additional protection to both transparent armor and opaque armor.

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Abstract

An armor system for protecting a vehicle from a projectile and employing the use of an insensitive reactive material as the primary means of disturbing the projectile is disclosed. The armor system includes a plurality of modules. Some modules may include a bag, wherein each module shares at least one seal with an adjacent module, and a material contained in the module and capable of being detonated. By manipulating the sensitivity of the reactive material, the Shockwave interaction with the chemical energy can be optimized for design packaging and defeating a threat. A transparent or opaque system provides multi-hit capability against chemical energy weapons or high velocity projectiles that maintains a narrow profile and provides a clear field of view. The reactive armor system requires no special energy source or detection system to provide protection from shaped-charge threats or RPGs thus minimizing any potential for failure as opposed to DAS.

Description

TRANSPARENT AND OPAQUE REACTIVE ARMOR
Cross-Reference to Related Application
[001] This application claims priority to U.S. Patent Application No.
13/024,640, filed on February 10, 2011 , and to U.S. Patent Application No.
13/326,573, filed on December 15, 2011 , the contents of which are incorporated herein by reference.
Technical Field
[002] The present disclosure relates to an armor system that resists penetration by projectiles including, as examples, shaped charges, explosively formed penetrators, and other energetic or high-velocity projectiles.
Background
[003] Conventional armor systems may be applied to armored fighting vehicles to protect against a variety of anti-tank munitions. An example of anti-tank munitions is the RPG-7, a Russian-origin rocket propelled grenade with a shaped- charge (or hollow-charge) warhead that may penetrate several inches of armored steel. Conventional armor systems and similar systems, such as passive armors, defensive aid systems, and reactive armors, may defeat the threat from such antitank munitions like the RPG-7.
[004] Passive armor systems, such as bar or slat armor and RPG nets, may offer a relatively simple and affordable solution for defending against RPGs, but typically offer a 60-70% success rate against preventing detonation of the RPG by shorting out the fusing mechanism. In addition, these systems may add
considerable weight, increase the overall width of the vehicle, and obscure the view of the vehicle occupants.
[005] Defensive aid systems (or "hard-kill technologies") may detect incoming threats and counter those threats to prevent the vehicle from being hit. Typical defensive aid systems may include a detection unit, such as radar, countermeasures, such as missiles and blast modules, and a control system to process threat signature and activate the countermeasures. Such defensive aid systems are generally complex and expensive.
[006] Explosive reactive armor systems may be generally effective to protect the vehicle from shaped-charges. Such systems typically may include an explosive sandwich having a front and a back plate (typically metallic) separated by a thin sheet of explosive material. Upon detonation of the explosive material triggered by an impinging shaped-charge jet, the plates may be driven apart. The movement of the plates may increase the dynamic thickness of the armor system and may cause disruption of the jet by feeding material (e.g., the plates and the exploded material) into the path of the jet stream. In turn, the high-velocity jet particles may be knocked off-line and reduce the penetration of the jet into the armor and vehicle.
[007] Passive armor systems, such as non-explosive/energetic reactive armors and electromagnetic armors, may use passive materials or electromagnetic forces to cause a front and a back plate to be driven apart. Like explosive reactive armor systems, the plates may be projected outwards at high velocities and may pose a threat to those around the vehicle. Moreover, the energetic materials used in passive armor systems may be regulated under hazard classifications and may require special handling.
[008] While any anti-armor projectile may be defeated by armor of sufficient strength and thickness, extra armor thickness is heavy and expensive, adds weight to the armored vehicle using it, which, in turn, places greater strain on the vehicle engine and drive train, and thus has a low "mass efficiency."
[009] Armor solutions that offer a weight advantage against these types of weapons may be measured in how much weight of rolled-homogenous-armor (RHA) it saves when compared with the RHA needed to stop a particular weapon from penetrating. This advantage may be calculated as a protection ratio, the ratio being equal to the baseline RHA penetration of a warhead minus the residual penetration into RHA, all divided by the areal density of the armor. Such weights may be calculated per unit frontal area presented in the direction of the anticipated trajectory of the weapon.
[010] Thus, there exists a need for an armor that can defeat threats, such as shaped-charge and hollow-charge weapons, without requiring excess
thicknesses of armor, and thus have a favorable mass efficiency. Such armor may be made of materials that can be readily fabricated and incorporated into a vehicle design at a reasonable cost, and may be added to existing vehicles.
[011] The present disclosure is directed to overcoming shortcomings and/or other deficiencies in existing technology.
Summary of the Disclosure
[012] In accordance with one aspect, the present disclosure is directed toward an armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory. The armor system may include a plurality of modules. Each module may include a bag, wherein each bag shares at least one seal with an adjacent bag, and a material contained in the bag and capable of being detonated, wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory.
[013] According to another aspect, the present disclosure is directed toward an armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory. The armor system may include a plurality of modules. Each module may include a bag, wherein each bag shares at least one seal with an adjacent bag, and a material contained in the bag and capable of being detonated, wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory. The armor system may also include a vessel housing the plurality of modules, wherein the vessel is substantially transparent.
[014] According to yet another aspect, the present disclosure is directed toward an armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory. The armor system may include a plurality of modules. Each module may include a bag, wherein each bag shares at least one seal with an adjacent bag, and a material contained in the bag and capable of being detonated, wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory. The armor system may also include a vessel housing the plurality of modules, wherein the vessel includes a separation element configured to separate the plurality of modules along the seams of the bags.
[015] According to yet another aspect, the present disclosure is directed toward an armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory. The armor system may include a first element, leading relative to the expected projectile trajectory, a second element disposed behind the first element, relative to the expected projectile trajectory, wherein the first element and the second element are spaced apart to form a cavity, and a fill capable of being detonated disposed in the cavity, wherein the fill may include one or more of a desensitizer and a sensitizer.
Brief Description of the Drawings
[016] Fig. 1 is a perspective view of an exemplary disclosed armor system;
[017] Fig. 2 is a schematic, cross-sectional view of a first exemplary disclosed embodiment of the armor system of Fig. 1 ;
[018] Fig. 2A is a schematic view of another armor system;
[019] Fig. 2B is a schematic view of another armor system;
[020] Fig. 2C is a schematic view of another armor system;
[021] Fig. 2D is a schematic view of another armor system;
[022] Fig. 3 is a schematic, cross-sectional view of a second exemplary disclosed embodiment of the armor system of Fig. 1 ;
[023] Fig. 4 is a schematic, cross-sectional view of a third exemplary disclosed embodiment of the armor system of Fig. 1 ;
[024] Fig. 5 is a schematic, plan view of a fourth exemplary disclosed embodiment of the armor system of Fig. 1 ;
[025] Fig. 6 is a schematic, cross-sectional view of the fourth exemplary disclosed embodiment of Fig. 5;
[026] Fig. 7 is a schematic, detailed view of a fifth exemplary disclosed embodiment of the armor system of Fig. 1 ;
[027] Fig. 8 is a schematic, detailed view of the armor system of Fig. 5;
[028] Fig. 9 is a schematic, cross-sectional view of a fifth exemplary disclosed embodiment of the armor system of Fig. 1 ;
[029] Fig. 0 is a schematic, cross-sectional view of a sixth exemplary disclosed embodiment of the armor system of Fig. 1 ;
[030] Fig. 1 1 is a schematic, cross-sectional view of a seventh exemplary disclosed embodiment of the armor system of Fig. 1 ; [031] Fig. 12 is a schematic, cross-sectional view of an eighth exemplary disclosed embodiment of the armor system of Fig. 1 ;
[032] Fig. 13 is a schematic illustration of an exemplary disclosed armor subsystem of the armor system of Fig. 1 ;
[033] Fig. 14 is a schematic, plan view of yet another exemplary disclosed embodiment of the armor system;
[034] Fig. 15 is another view of the exemplary disclosed embodiment of Fig. 14; and
[035] Fig. 16 is a schematic, cross-sectional view of the exemplary disclosed embodiment of Fig. 14.
Detailed Description
[036] Fig. 1 illustrates an exemplary disclosed armor system 10 for protecting a vehicle 11 from a projectile 12 such as, for example, an HC jet, EFP, and Hybrid warhead. In the following discussion, projectile 2 has an expected trajectory 15 relative to vehicle 1 1. Trajectory 15 establishes a direction for understanding certain terms used in the following discussion (e.g., "leading," "rear," "behind," "front," etc.), describing the components of armor system 10 that projectile 12 successively confronts as it approaches a vehicle hull 20.
[037] Armor system 10 may include one or more armor subsystems such as armor subsystem 25 and a distribution subsystem 30 (shown dotted) that may be disposed within hull 20. Distribution subsystem 30 may provide a fill including at least one of a liquid and a gas to armor subsystem 25 of vehicle 11. Fig. 1 also depicts additional embodiments of armor subsystems in accordance with the present disclosure, which will be described below.
[038] As depicted in Figs. 1 and 2, armor subsystem 25 may include a first layer 35, a second layer 40, and a plurality of spacing elements 45. First layer 35, second layer 40, and spacing elements 45 together may form a cavity 50 that holds a fill 55. Armor subsystem 25 may also include a mount assembly 65 for mounting armor subsystem 25 to vehicle 11.
[039] First layer 35 may lead second layer 40 relative to trajectory 15. First layer 35 and second layer 40 may include, for example, transparent materials.
First layer 35 and second layer 40 may also be, for example, sheet-like layers including material such as, for example, glass, transparent ceramics, acrylic, polycarbonate, aluminum, delrin, UHMW PP (ultra high molecular weight polypropylene), UHMW PE (ultra high molecular weight polyethylene), and/or borosilicate. First layer 35 and second layer 40 may be of any suitable thickness for containing a liquid or a gas such as, for example, between about 1/2" thick and about 3" thick. For example, first layer 35 and second layer 40 may be layers having a thickness of about 1/2" and including substantially only borosilicate. First layer 35 and/or second layer 40 may also include one or more apertures 67 for draining and filling cavity 50 with fill 55. Aperture 67 may be in fluid communication with cavity 50 and may be configured to receive a removable stopper 68. It is also contemplated that aperture 67 and stopper 68 may be included on other portions of armor subsystem 25 such as, for example, spacing elements 45.
[040] Spacing elements 45 may be formed from a chemical resistant material and include any material suitable for spacing first layer 35 from second layer 40 such as, for example, delrin or UHMW PE. For example, spacing elements 45 may be delrin gaskets. Spacing elements 45 may be hollow or solid elements, and may be sealed with first layer 35 and second layer 40 by a chemical resistant sealant such as, for example, butyl rubber.
[041] Cavity 50 may be a hollow, sealed space formed by first layer 35, second layer 40, and spacing elements 45. Cavity 50 may be partially or substantially filled by fill 55. Spacing elements 45 may space first layer 35 and second layer 40 apart to provide cavity 50 with a suitable dimensional thickness 60, as discussed below.
[042] The fill disclosed in the below embodiments and used herein may include a material that is sufficiently reactive to be capable of detonation when exposed to a severe shock such as, for example, an impact of an HC jet from projectile 12. Although materials that are classified as "explosives" are not excluded from the fill material, it is not a requirement that the fill material be classified as "explosive" material. Fill 55 may include a reactive liquid such as, for example, a liquid explosive, catalyst, and/or accelerant. For example, fill 55 may include a fuel such as methanol, and/or a clear liquid explosive such as
nitromethane. Fill 55 may also be a reactive liquid such as, for example, isopropyl nitrate, nitrobenzene, nitrogen tetroxide, and/or a fuel-like toluene. For example, fill 55 may include nitrobenzene having a detonation velocity of about 7,300 m/s (at about 1 atm pressure). Additionally, for example, fill 55 may include a mixture of about 82% nitrogen tetroxide and about 18% toluene, and may have a detonation velocity of about 8,100 m/s (at about 1 atm pressure). Fill 55 may also be a liquid in a highly viscous form such as, for example, gel form. Cavity 50 may provide fill 55 with a suitable dimensional thickness 60 such as, for example between about 1" and about 8", between about 1" and about 6", and between about 1 1/2" and about 4". Thickness 60 may be any sufficient thickness to support a continuous detonation of fill 55 following an initial detonation of fill 55 by a tip and/or jet of projectile 12. The sufficient dimensional thickness to support continuous detonation may be larger than the "Minimum Detonation Thickness" (MDT), which may vary from explosive to explosive based on a given explosive's sensitivity to Shockwaves. Dimensional thickness 60 may be greater than an MDT of fill 55. For example, fill 55 may have a 1" dimensional thickness when fill 55 includes substantially only nitromethane, based on MDT. Fill 55 may also include a nonreactive liquid such as, for example, water. Fill 55 may additionally include a mixture of one or more reactive liquids and one or more nonreactive liquids such as, for example, a mixture of fuel and water. For example, fill 55 may be a mixture of about 50% methanol and about 50% water, which may be substantially resistant to freezing at cold temperatures in the field and may keep interior surfaces of layers 35 and 40 substantially clean. Also, fill 55 may include transparent liquids and may be substantially transparent.
[043] Fill 55 may also include a reactive gas such as, for example, ether, ethylene, acetylene, and/or hydrogen. Fill 55 may include a reactive gaseous mixture having a lower detonation velocity relative to reactive liquid mixtures. Fill 55 may also include a fuel that is at a gaseous state at ambient temperatures, e.g., at room temperature. Fill 55 may also include a mixture of one or more reactive gases and one or more nonreactive gases. For example, fill 55 may include a mixture of ether and oxygen having a detonation velocity of about 2,300 m/s (at about 1 atm pressure), a mixture of ethylene and oxygen having a detonation velocity of about 2,423 m/s (at about 1 atm pressure), a mixture of acetylene and oxygen having a detonation velocity of about 2,900 m/s (at about 1 atm pressure), and/or a mixture of hydrogen and oxygen having a detonation velocity of about 3,800 m/s (at about 1 atm pressure). It is contemplated that the detonation velocities of reactive gases in fill 55 may be increased by pressurizing cavity 50 above a pressure of 1 atm. For example, fill 55 may include a mixture of hydrogen and oxygen that is pressurized, for example, at between about 1.4 atm and about 2.7 atm (between about 20 psi and about 40 psi). Fill 55 including a pressurized mixture of hydrogen and oxygen may provide a detonation velocity of greater than about 3,800 m/s. Also, for example, fill 55 may include an ideal gas pressurized at about 30 psi, and containing about three times more mass and energy than the same ideal gas may contain when unpressurized. Also, fill 55 may include transparent gases and may be substantially transparent.
[044] In certain embodiments, fill 55 may include a number of materials, components, and mixtures thereof to tailor or customize the explosive sensitivity of fill 55. For example, fill 55 may include any combination of one or more sensitizers, desensitizers, and reactive materials to control the detonation velocity and/or the detonation susceptibility of fill 55. The ability to control the explosive sensitivity of fill 55 may prevent certain types of projectiles from detonating fill 55, while detonating fill 55 upon impact from other types of projectiles to protect vehicle 11. For instance, fill 55 may be desensitized by, for example, the presence of desensitizers, which may prevent detonation of fill 55 from impact from small arms fire, such as bullets and the like. In addition, desensitizing fill 55 may produce a slower detonation velocity relative to traditional reactive materials used in explosive reactive armors. For example, and without limitation, the slower detonation velocity may be 5,400 m/s (at about 1 atm pressure). Thus, the slower detonation velocity of fill 55 may cause larger Shockwaves to collide into projectile 12. One or both of first layer 35 and spacing elements 45 may be formed of a frangible material, such as glass, polycarbonate, or an acrylic, and upon detonation of fill 55, first layer 35 and spacing elements 45 may shatter into many relatively small, non-lethal fragments. When fill 55 detonates, the larger Shockwaves, the many fragments created by the shattered first layer 35 and spacing elements 45, and the density of fill 55, may reduce the penetration ability of projectile 12 into vehicle 11. In addition, the slower detonation velocity and density of fill 55 may allow the
Shockwaves and fill 55 to engulf the tail end of projectile 2 to further protect vehicle 11. It should also be appreciated that the dimensional thickness of fill 55 may be larger than its MDT. For example, the dimensional thickness of the desensitized fill 55 may be between 1 mm and 100 mm. [045] As alluded to above, fill 55 may include any combination of sensitizers, desensitizers, and reactive materials to vary the explosive sensitivity of fill 55. The reactive materials may include liquid explosives, such as, for example, nitromethane, and/or reactive liquid such as, for example, isopropyl nitrate, nitrobenzene, nitrogen tetroxide, and/or a fuel like toluene. Desensitizers may include less reactive liquids, such as methanol, fire retardants, and/or nonreactive liquids, such as water. In addition, structures, such as plates and/or sheets, formed of low speed of sound materials, such as rubber or polymers, may be contained within fill 55 to act as a desensitizer. The plates and/or sheets may include varying thicknesses ranging from 1 mm to 25 mm. Sensitizers may also include structures, such as sheets, spheres and/or cylindrical rods, formed of high speed of sound materials, such as ceramics, glass, aluminum, and/or steel. The cross-sectional diameters of the sheets, spheres and/or cylindrical rods may range from 10 m to 50 mm.
[046] In addition to varying the explosive sensitivity of fill 55 by selecting a combination of sensitizers, desensitizers, and reactive materials, the MDT and detonation velocity of fill 55 may be varied by selecting a combination of sensitizers, desensitizers, and reactive materials. For example, fill 55 may be desirably desensitized by including a suitable amount of desensitizers and sensitizers, thus decreasing the detonation velocity and the MDT of fill 55. By decreasing the MDT of fill 55, a housing holding fill 55 may be made thinner, thus reducing the weight on vehicle 11 and material costs. For example, and with reference to Fig. 2, one or more of first layer 35, second layer 40, and spacing elements 45 may have a thickness substantially between 1 mm and 100 mm.
[047] As discussed above, sheets, rods and/or spheres may be used as a sensitizer for fill 55, and plates and/or sheets may be used as a desensitizer for fill 55. It should also be appreciated that the rods, spheres, plates, and/or sheets may also be used to manipulate the direction of the Shockwaves induced from the detonation reaction of fill 55. For example, and as shown in Fig. 2A, upon impact of projectile 12 with armor subsystem 25, fill 55 may detonate and induce
Shockwaves 2000. Sheets, Spheres and/or rods 2010 may divert the direction of Shockwaves 2000, in for example, a radial direction relative to spheres and/or rods 2010. It should be appreciated that sheets, spheres and/or rods 2010 may be arranged in a symmetrical or random configuration within fill 55, and may vary in cross-sectional diameter. As shown in Fig. 2B, Shockwaves 2000 induced by the detonation of fill 55 may be diverted by sheets and/or plates 2020. For example, the direction of Shockwaves 2000 may be directed away from the surfaces of sheets and/or plates 2020. It should also be appreciated that sheets and/or plates 2020 may be arranged in any other suitable configuration within fill 55, such as, for example, diagonally stacked (Fig. 2C), or may be a single sheet and/or plate 2020 arranged diagonally across fill 55 (Fig. 2D). Moreover, sheets and/or plates 2020 may vary in cross-sectional diameter.
[048] Referring back to Fig. 1 , armor subsystem 25 may be mounted to vehicle 11 by a mounting apparatus such as, for example, mount assembly 65. Mount assembly 65 may include a mount 75, a hinge 80, and a frame 85. Mount 75 may be operably connected to hinge 80, which may be connected to armor subsystem 25 by any suitable means known in the art. For example, armor subsystem 25 may be framed by a structural frame 85 on which hinge 80 is rotatably mounted. Armor subsystem 25 may thus be rotated about hinge 80. Mount 75 may also be raised or lowered about a pivot point 90. Therefore, armor subsystem 25 may be adjusted as a louver system in front of an exterior surface 70 of vehicle 11 , as depicted in Fig. 2. Armor subsystem 25 may be adjusted by mount assembly 65 by any suitable means in the art. For example, mount assembly 65 may be manually adjusted by an operator, or may be mechanically adjusted by a motor 95. Armor subsystem 25 may be configured to adjust to provide clearance for the various systems of vehicle 11 such as, for example, emergency egress windows and antennas. Armor subsystem 25 may be used to provide additional protection at any suitable location of vehicle 11 such as, for example, additional protection for transparent armor of windows of vehicle 11 and additional perimeter protection for opaque armor on a side of vehicle 11.
[049] As depicted in Fig. 2, armor subsystem 25 may be rotatably mounted via mount assembly 65 at an angle 00, relative to trajectory 15, where trajectory 15 may be substantially perpendicular to vehicle exterior surface 70. Armor subsystem 25 may be rotatably adjusted so that angle 100 is oriented, for example, at about 30°, 45°, 60°, or 90°
[050] Figs. 1 and 3 depict a second embodiment, armor subsystem 125, of armor system 10. As best seen in Fig. 3, armor subsystem 125 may include a first element 130, a second element 135, and a plurality of spacing elements 140. First element 130, second element 135, and spacing elements 140 may form a cavity 145 that holds a fill 150. Armor subsystem 125 may also include a mount assembly similar to mount assembly 65 of armor subsystem 25. Spacing elements 140 may be similar to spacing elements 45 of armor subsystem 25, and cavity 145 may be similar to cavity 50 of armor subsystem 25.
[051] First element 130 may lead second element 135 relative to trajectory 15. First element 130 may include a plurality of layers 155 and an intermediate layer 160 that may be disposed between layers 155. Layers 155 may be sheet-like layers including material such as, for example, glass, transparent ceramics, acrylic, polycarbonate, aluminum, delrin, UHMW PP, UHMW PE, and/or borosilicate.
Layers 155 may be suitable thin-walled layers for containing a liquid or a gas. For example, layers 155 may be glass sheets having a thickness of about 1/8".
Intermediate layer 160 may include a nonreactive liquid or gas. For example, intermediate layer 160 may include a nonreactive liquid such as, for example, water. It is also contemplated that intermediate layer 160 may include a reactive liquid or gas. Intermediate layer 160 may have any suitable thickness for an armored layer such as, for example, between about 1/8" and about 6". For example, intermediate layer 160 may have a thickness of about 1/2". Second element 135 may include a plurality of layers 165 and an intermediate layer 170 that may be disposed between layers 165. Layers 165 of second element 135 may be similar to layers 155 of first element 130, and intermediate layer 170 of second element 135 may be similar to intermediate layer 160 of first element 130, respectively. It is contemplated that armor subsystem 125 may be mounted at an exterior of vehicle 11 , as a louver as shown in Fig. 1 , and/or as a window module in a shaped aperture of vehicle 11 , as discussed henceforth in relation to armor subsystem 225.
[052] Returning to Fig. 3, first element 130 and/or second element 135 may also include one or more apertures 175, each configured to receive a removable stopper 180. Aperture 175 and stopper 180 may be similar to aperture 67 and stopper 68, respectively, of armor subsystem 25. It is also contemplated that aperture 175 and stopper 180 may be included on other portions of armor subsystem 125 such as, for example, spacing elements 140.
[053] Fill 150 may include a reactive and/or nonreactive liquid or gas, and may be similar to fill 55 of armor subsystem 25. For example, fill 150 may include a reactive liquid such as, for example, nitromethane and/or isopropyl nitrate. Fill 150 may have a dimensional thickness 185 that is greater than an MDT of fill 150.
[054] Figs. 1 and 4 depict a third embodiment, armor subsystem 225, of armor system 10. Referring to Fig. 4, armor subsystem 225 may include a layer 230, at least one transparent armor layer 235, at least one seal 240, and at least one frame element 245. Layer 230, transparent armor layer 235, and seal 240 may be supported by frame element 245 and may form a cavity 250 that holds a fill 255.
[055] Layer 230 may lead transparent armor layers 235 relative to trajectory 15, and layer 230 may be similar to first layer 35 and second layer 40 of armor subsystem 25. To facilitate use in a window of vehicle 11 , layer 230 may include a transparent material. Layer 230 may be spaced apart from the at least one transparent armor layer 235.
[056] The one or more transparent armor layers 235 may include glass, transparent ceramics, acrylic, polycarbonate, and/or borosilicate. Transparent armor layer 235 may be of any suitable thickness such as, for example, between about 1/8" and about 6" thick.
[057] The one or more seals 240 may include materials similar to spacing elements 45 of armor subsystem 25. For example, the one or more seals 240 may include a single gasket or a plurality of seals. The one or more seals 240 may form a seal between layer 230, transparent armor layers 235, and one or more frame elements 245 to seal fill 255 within cavity 250. For example, seal 240 may be a single rubber gasket that surrounds and seals layer 230 and transparent armor layers 235, and fits within frame element 245. Frame element 245 may support armor subsystem 225 within a shaped aperture 260 of vehicle 1 1. Shaped aperture 260 may extend into an interior of vehicle 1 1. Thus, armor subsystem 225 may provide a transparent armored window for vehicle 1 1 , as shown in Fig. 1 , but may also be used in a louver configuration as shown in armor subsystems 25 and 125. Seal 240 and/or frame 245 may include one or more apertures 265 and stoppers 270, for draining and/or filling fill 255 in cavity 250. Apertures 265 and stoppers 270 may be similar to aperture 67 and stopper 68 of armor subsystem 25.
[058] Fill 255 may be similar to fill 55 of armor subsystem 25. Fill 255 may include a reactive or nonreactive liquid or gas. For example, fill 255 may include substantially only nitromethane and may have a thickness such as, for example, 1 1/2". Alternatively, fill 255 may include, for example, substantially only isopropyl nitrate. Fill 255 may have a dimensional thickness 272 that is greater than an MDT of fill 255.
[059] Figs. 1 , 5, and 6 depict a fourth embodiment, armor subsystem 325, of armor system 10. Referring to Figs. 5 and 6, armor subsystem 325 may include a modular array 330, a support system 335 for providing structural support to modular array 330, and a filling system 340 for providing modular array 330 with fill.
[060] As depicted in Fig. 6, which is a sectional view of Fig. 5, modular array 330 may include a ballistic module 345, a plurality of fill modules 350, and a spall module 355. Ballistic module 345 may provide protection against ballistic threats to vehicle 11 , fill modules 350 may provide additional protection against threats to vehicle 11 , and spall module 355 may provide protection against spalling of armor system 10. Ballistic module 345, fill modules 350, and spall module 355 may be connected by any suitable technique known in the art such as, for example, by welding or by mechanical fasteners.
[061] Ballistic module 345 may be a ballistic-resistant layer that leads fill modules 350 relative to trajectory 15, and may include a plurality of layers 360 and 365. Layers 360 and 365 may be of any suitable material and thickness for resisting ballistic threats to vehicle 11. For example, layers 360 and 365 may include high strength metals such as aluminum, copper, steel, stainless steel, magnesium, molybdenum, copper, zirconium, titanium, nickel, and other high strength materials such as glass fiber and polymer. Layers 360 and 365 may have any thickness suitable for ballistic protection such as, for example, a thickness of between about 1/8" and about 4".
[062] Fill modules 350 may follow ballistic module 345 relative to trajectory 15, and may lead spall module 355 relative to trajectory 15. Each fill module 350 may include a first layer 370 and a second layer 375. First layer 370 and second layer 375 may seal together to form a cavity 380 that holds a fill 385. First layer 370, second layer 375, cavity 380, and fill 385 may be similar to first layer 35, second layer 40, cavity 50, and fill 55, respectively, of armor subsystem 25. Each fill module 350 may be an individual cell containing fill 385. Fill modules 350 may be disposed adjacently to each other in armor subsystem 325. Fill 385 may have a dimensional thickness 388 that is greater than an MDT of fill 385. [063] Spall module 355 may be a spall-resistant layer that follows fill modules 350 relative to trajectory 15. Spall module 355 may have a layer 390 that includes similar materials and has a similar thickness as layers 360 and 365 of ballistic module 345.
[064] Support system 335 may include a separation element 395 and a frame 400. Separation element 395 may support fill modules 350 within frame 400.
[065] Separation element 395 may be any suitable material for insulating fill modules 350 from adjacent threat detonations such as, for example, a
polycarbonate material. Separation element may be disposed between fill modules 350, and may also include transparent materials. Separation element 395 may be a thin layer separating fill modules 350, and thereby substantially reduce
sympathetic detonation of a given fill module 350 in the case that an adjacent fill module 350 detonates due to impact of a threat projectile. It is contemplated that fill modules 350 may be removably attachable from armor subsystem 325, thereby allowing compromised fill modules 350 to be replaced with new fill modules 350 within a combat area.
[066] Frame 400 may include any suitable material for structurally supporting armor subsystem 325 such as, for example, structural steel or aluminum. Referring back to Fig. 1 , frame 400 may be configured to mount armor subsystem 325 within an aperture of vehicle 11 as a window, or may be mounted to an exterior of vehicle 11 , for example, as a louver. Fill modules 350 may be sealed against frame 400 by a seal 405 that may include similar materials as seal 240 of armor subsystem 225.
[067] As depicted in Fig. 5, filling system 340 may include a plurality of passageways 410 and a plurality of valves 415. Passageways 410 may connect adjacent fill modules 350 to facilitate filling of fill modules 350 with fill 385.
Passageways 410 may have an internal diameter that is less than an MDT of a given fill 385. Valves 415 may be disposed in passageways 410 to substantially prevent leakage from fill modules 350 that may be compromised by threat projectiles. Valves 415 may be any valve suitable for substantially reducing leakage such as, for example, one-way check valves. Thus, filling system 340 may facilitate filling fill modules 350 simultaneously via passageways 410, and may prevent leakage from compromised fill modules 350 via valves 415. [068] Fig. 7 depicts an alternative embodiment, fill module 420, of armor subsystem 325. Fill module 420 may be similar to fill module 350, and may include a cavity 425 having a fill 430, which may be similar to cavity 380 and fill 385, respectively, of fill module 350. Materials and thicknesses of fill module 420 may be selected in order to substantially minimize aberrations due to differences in material properties (e.g., differences in the index of refraction) between the various materials included in fill module 420. Fill modules 420 may be configured to be removably attachable to armor subsystem 325. Fill modules 420 may be pre-filled with fill 430 during manufacturing. Thus, a given pre-filled module 420 may be removed from frame 400 if it becomes compromised, and replaced with a new pre- filled module 420.
[069] Fig. 8 illustrates an exploded view of armor subsystem 325, which depicts a length 435 of fill module 350. Keyholes 440 and 445 are also depicted, which may result from an impact of projectile 12 into armor subsystem 325 along trajectory 15. Length 435 may be at least twice as large as a length of keyholes 440 and 445. As projectile 12 travels along a projected path 450, keyhole 440 may be formed in layer 360 and layer 365, and keyhole 445 may be formed in layer 390. Keyholes 440 and 445 may be formed because layers of armor subsystem 325 may shift with respect to each other as projectile 12 impacts armor subsystem 325. For example, as projectile 12 impacts, layers 360 and 365 may shift upward, thereby causing keyhole 440 to have a keyhole shape as projectile 12 passes through moving layers 360 and 365. Keyhole 445 may be similarly formed.
[070] Figs. 1 and 9 depict a fifth embodiment, armor subsystem 525, of armor system 10. As best seen in Fig. 9, armor subsystem 525 may include a material 550 having a dimensional thickness 560. Armor subsystem 525 may also include a mount assembly for mounting armor subsystem 525 to vehicle 11.
Material 550 may include a reactive and/or nonreactive liquid or gas, and may include materials similar to fill 55 of armor subsystem 25. Material 550 may be a liquid in a highly viscous form such as, for example, gel form. Material 550 may be a gelled block of material having dimensional thickness 560. Material 550 may be gelled such that it may substantially retain a shape such as, for example, a block shape having thickness 560, without being contained in a housing or confined between structural elements. Material 550 may include any suitable material such as, for example, substantially entirely transparent materials. [071] Material 550 may disrupt a projectile such as, for example, an HC jet of projectile 12. Dimensional thickness 560 may be large enough to exceed a minimum detonation thickness (MDT) of material 550, which may include reactive material, such that material 550 may react to disrupt the jet of projectile 12. An appropriate dimensional thickness 560 may vary based on, for example, a type of reactive material included within material 550 and/or a volume of material 550. Dimensional thickness 560 may be greater than an MDT of material 550. A shape and/or material types of material 550 and/or a value of thickness 560 may be sized such that material 550 reacts over a duration of time that is sufficient to disrupt an entire jet of projectile 12. For example, material 550 may have a sufficient size and be of a sufficient material to react relatively gradually as a jet is encountered, such that the reaction lasts long enough to disrupt an entire jet of projectile 12. For example, thickness 560 may be of a relatively large thickness such as, for example, between about 1" and about 6", between about 1" and about 12", or in excess of 12", depending on the material and geometric properties of material 550 such as, for example, the minimum detonation thickness of material 550.
[072] Figs. 1 and 10 depict a sixth embodiment, armor subsystem 625, of armor system 10. As best seen in Fig. 10, armor subsystem 625 may include a housing 640 and a material 650 having a dimensional thickness 660. Armor subsystem 625 may also include a mount assembly for mounting armor subsystem 625 to vehicle 11. Material 650 and thickness 660 may be similar to material 550 and thickness 560 of armor subsystem 525, respectively. Material 650 may be in a gelled form or in a non-gelled form. Material 650 may be housed in housing 640. Dimensional thickness 660 may be greater than an MDT of material 650.
[073] Housing 640 may be a thin-walled vessel suitable for containing a gelled and/or a non-gelled material. Housing 640 may be formed from a single element, or may be formed from several elements that are attached by any suitable method such as, for example, by welding. Housing 640 may include thin walls such as, for example, about 3/4", about 1/2", about 3/8", about 1/4", about 1/8", about 1/16", about 3/32", about 1/32", and/or about 1/64".
[074] Figs. 1 and 11 depict a seventh embodiment, armor subsystem 725, of armor system 10. As best seen in Fig. 11 , armor subsystem 725 may include a first layer 735, a second layer 740, and a plurality of spacing elements 745. First layer 735, second layer 740, and spacing elements 745 together may form a cavity 750 that holds a fill 755. Armor subsystem 725 may also include a mount assembly for mounting armor subsystem 725 to vehicle 11. Spacing elements 745 may be similar to spacing elements 45 of armor subsystem 25. Cavity 750 may be similar to cavity 50 of armor subsystem 25. Cavity 750 may have a dimensional thickness 760 that may be sized similarly to thickness 60 of armor subsystem 25.
[075] First layer 735 and second layer 740 may be similar to first layer 35 and second layer 40 of armor subsystem 25. First layer 735 and second layer 740 may include, for example, opaque materials. First layer 735 and/or second layer 740 may also include one or more apertures 767 for draining and filling cavity 750 with fill 755. Aperture 767 may be similar to aperture 67 of armor subsystem 25, and may include a stopper 768 that may be similar to stopper 68 of armor subsystem 25.
[076] Fill 755 may include, for example, opaque reactive materials. Fill 755 may include relatively insensitive explosives with detonation velocities of about 4,000 m/s (at about 1 atm pressure) to about 7,000 m/s (at about 1 atm pressure). For example, fill 755 may include materials such as ammonium nitrate, potassium chlorate, urea nitrate, urea, and tetranitro-isopropanol. Fill 755 may also include mixtures of one or more of these materials with fuels and/or sensitizers.
Dimensional thickness 760 may be greater than an MDT of fill 755, and may support a continuation detonation of fill 755 following an initial detonation of fill 755 by a tip and/or jet of projectile 12. A shock sensitivity of fill 755 may depend on, for example, a degree of pressurization and/or confinement of fill 755 within cavity 750 and/or the material properties and proportions of materials included in fill 755. Fill 755 may include materials which, although not classified as explosives, may behave as explosives when exposed to a severe shock such as, for example, the impact of an HC jet from projectile 12. A shape and/or material types of fill 755 and/or a value of dimensional thickness 760 may be sized such that fill 755 reacts over a predetermined length of time that is sufficient to disrupt an entire jet of projectile 12.
[077] Fill 755 may also be a gelled material that may retain a shape such as a block shape similar to material 550 of armor subsystem 525. Fill 755 may thereby retain a shape without being contained in a housing or between structural elements. Fill 755 may additionally be a gelled or non-gelled material that may be housed in a thin-walled vessel similar to housing 640 of armor subsystem 625. [078] Figs. 1 and 12 depict an eighth embodiment, armor subsystem 825, of armor system 10. As best seen in Fig. 12, armor subsystem 825 may include a first layer 835, a second layer 840, and a plurality of spacing elements 845. First layer 835, second layer 840, and spacing elements 845 together may form a cavity 850 that has a thickness 860 and holds a fill 855 of thickness 860. The elements of armor subsystem 825 may be similar to the elements of armor subsystem 725. Dimensional thickness 860 may be greater than an MDT of fill 855.
[079] Armor subsystem 825 may be an armor panel that is attached to hull 20 of vehicle 11. For example, an exterior surface 865 of second layer 840 may be attached to an exterior surface of hull 20 by any method suitable in the art such as, for example, mechanical fasteners, welding, and/or adhesives.
[080] Fig. 13 depicts distribution subsystem 30 that may be disposed within an interior portion of vehicle 11. Distribution subsystem 30 may include a pump 455, a plurality of passageways 460, a fill reservoir 465, and a waste reservoir 470. Pump 455 may pressurize and pump liquid such as fills 55, 150, 255, 385, 650, 755, and/or 855 from fill reservoir 465 and through passageways 460.
[081] Pump 455 may be any suitable pump known in the art such as, for example, a piston type pump or an impeller type pump. Pump 455 may be driven, for example, via a crankshaft from an engine of vehicle 11 or by an independent power source. Pump 455 may be fluidly connected to the plurality of passageways 460 and fill reservoir 465, and may draw fill from fill reservoir 465.
[082] Passageways 460 may be disposed in an interior portion of vehicle 11 such as, for example, a vehicle spine. Passageways 460 may be housed in a protective jacket that may provide protection from external threats such as, for example, bullets, shrapnel, mine blasts, HC jets, and EFP projectiles.
Passageways 460 may have an internal diameter that is less than an MDT of the fill that is being transferred. For example, passageways 460 may be a stainless steel tube having an internal diameter of about 1/4", if the MDT of the fill is greater than 1/4". The plurality of passageways 460 may fluidly connect pump 455 with the armor subsystems of vehicle 11 such as armor subsystems 25, 125, 225, 325, 525, 625, 725, and/or 825. Thus, distribution subsystem 30 may drain and re-fill armor system 10 with fill upon demand. [083] Fill reservoir 465 may be a protected reservoir for storing fill such as fills 55, 150, 255, 385, 650, 755, and/or 855 and for supplying the fill to pump 455. Fill reservoir 465 may include a reinforced and/or armored lining to resist penetration by ballistics and other threats. Fill reservoir 465 may include sufficient fill to iteratively fill cavities 50, 1 5, 250, 380, 750, and/or 850 and/or housing 640 numerous times during a given operation time of vehicle 11. It is contemplated that fill reservoir 465 may have an elongated shape and have an internal diameter that is less than an MDT of a stored fill.
[084] Waste reservoir 470 may be a protected reservoir similar to fill reservoir 465. Waste reservoir 470 may be fluidly connected to armor subsystems 25, 125, 225, 325, 625, 725, and/or 825 via drainage passageways (not shown) that may be similar to passageways 460. Fill may be drained from armor subsystems 25, 125, 225, 325, 625, 725, and/or 825 and delivered to waste reservoir 470 via the drainage passageways. The drainage passageways and/or passageways 460 may include check valves to control flow of fill during drainage and filling of armor subsystems 25, 125, 225, 325, 625, 725, and/or 825 during an operation of distribution subsystem 30.
[085] Figs. 14-16 illustrate yet another exemplary embodiment of an armor subsystem 925 for armor system 10. As shown in Fig. 14, armor subsystem 925 may include a plurality of modules 1000 having a plurality of bags 002, a support vessel 1001 , a separation element 1003, and a cover 1004.
[086] Fig. 15 illustrates a disassembled view of armor subsystem 925. As depicted in Fig. 15, support vessel 1001 may include an appropriate volume for housing the plurality of modules 1000. More particularly, support vessel 1001 may contain the plurality of bags 1002 and separation element 1003, with cover 1004 positioned over support vessel 1001 to encapsulate the plurality of modules 1000 within support vessel 1001. Support vessel 1001 may follow cover 1004 and lead an exterior surface of vehicle 11 relative to trajectory 15. In addition, support vessel 1001 may be a substantially transparent, lightweight, and/or relatively frangible material, such as, for example, polymethylmethacrylate, glass,
polycarbonate, acrylic, polyurethane, or a transparent ceramic. Armor subsystem 925 may be coupled to vehicle 11 in a similar manner as armor system 325. For example, and with reference to Fig. 1 , it should be appreciated that support vessel 1001 , and thus armor subsystem 925, may be configured to be mounted within an aperture of vehicle 11 as a window, or may be mounted to an exterior of vehicle 11 , for example, as a louver. Furthermore, although illustrated as including a single row of modules 1000, it should be appreciated that armor subsystem 925 may include any number of rows and columns of modules 1000.
[087] Cover 1004 may be a substantially transparent material and may lead the plurality of bags 1002 and support vessel 001 relative to trajectory 15. Cover 1004 may be a sheet-like layer and may be thin, lightweight, and/or relatively frangible. For example, cover 004 may be a thin sheet of
polymethylmethacrylate, glass, polycarbonate, acrylic, or a transparent ceramic. Cover 1004 may be removably connected to support vessel 1001 by any suitable technique known in the art, such as, for example, by mechanical fasteners or removable welds.
[088] Support vessel 1001 and cover 1004 may also include any thickness suitable for ballistic protection, such as, for example, a thickness between 1/8" and about 4". However, it should be appreciated that cover 1004 may include a thickness thinner relative to a thickness of a rear wall of support vessel 1001.
Accordingly, upon detonation of one or more bags 1002, cover 1004 may shatter into relatively small, non-lethal fragments, while the rear wall of support vessel 1001 may be provide impact and ballistic protection for vehicle 11. Cover 1004 may preferably have a thickness between 1 mm to 100 mm, and the rear wall of support vessel 1004 may preferably have a thickness between 1 mm to 100 mm. Furthermore, cover 1004 may have a suitable thickness and/or structural rigidity to prevent detonation by certain projectiles. For example, cover 1004 may have a sufficient thickness and rigidity to prevent small mass and low velocity projectiles, such as bullets from small-arms weapons, from impacting and detonating bags 1002.
[089] Furthermore, since support vessel 1001 and cover 1004 may include a substantially transparent, lightweight, and relatively frangible material, such as glass, support vessel 1001 and cover 1004 may provide substantial visibility from inside vehicle 11, while also reducing the amount of overpressure to vehicle 11 and reactive fragments expelled from armor subsystem 1 1 upon detonation of a bag 1002. In addition, frangible materials, such as glass, may create a large debris field upon detonation of bags 1002, thereby disrupting the trajectory of a projectile and damage to vehicle 11. The brittle nature of such frangible materials may also be less lethal to those around the debris field. Therefore, the threat of damage to vehicle 11 and injury to the occupants of vehicle 11 and persons around vehicle 11 may be minimized. In certain embodiments, the mass of each individual piece of debris in the debris field may be substantially the same to promote improved disruption of the projectile.
[090] The plurality of bags 1002 may be formed of a thin and transparent material and may contain fill material 1055 similar to fill 55 of armor subsystem 25. That is, fill material 1055 may be a miscible fluid capable of detonating upon an appropriate agitation. In one embodiment, fill material 1055 may be clear and transparent, such that one may see through bag 1002 and fill material 1055. One may also see through bag 1002 and fill material 1055 through, for example, night vision goggles. It should also be appreciated that in certain embodiments, fill material 1055 may include an opaque mixture of one or more liquids, including, as examples, ammonium nitrate and urea nitrate, if transparency is not required.
[091] Agitation of fill material 1055 may cause detonation. In other words, once Shockwaves running through fill material 1055 reach a certain threshold magnitude, fill material 1055 may detonate. Such Shockwaves may be caused by projectiles colliding with armor subsystem 925. Accordingly, fill material 1055 may include a suitable thickness to prevent detonation by certain projectiles. For example, fill material 1055 may be sufficiently thick to prevent small mass and low velocity projectiles, such as bullets from small-arms weapons, from inducing sufficient Shockwaves and causing detonation of fill material 1055 upon impact. On the other hand, said thickness may allow projectiles having a sufficient mass and velocity, such as, for example, a hollow-charged jet, shaped-charged jets, and explosively-formed penetrators, to induce sufficient Shockwaves in fill material 1055 and cause detonation.
[092] In certain embodiments, however, fill material 1055 may be relatively thin such that fill material 1055 may be more sensitive to detonation. That is, sufficient Shockwaves may be more easily induced to cause detonation of fill material 1055. Such a feature may, for example, prevent Shockwaves from propagating between modules 1000 and causing undesired detonation of neighboring modules. Impact between a projectile and a single module 1000 may detonate fill material 1055 before Shockwaves induced in that module 1000 propagate and induce the detonation of neighboring modules 1000. [093] Fill material 1055 may also have a relatively slower detonation velocity. Accordingly, fill material 1055 may produce a greater and longer
Shockwaves upon detonation onto a projectile over a longer period of time, thus reducing the penetration ability of the projectile.
[094] In addition, because fill material 1055 may be a reactive material, the use of a separate energy source to detonate fill material 1055 may be eliminated. Projectile detection units, such as radars, are also not necessary. Therefore, armor subsystem 925 provides a more simplistic design.
[095] Fill material 1055 may also be a liquid in a highly viscous form such as, for example, gel form or slurry form, to prevent leakage from plastic bags 1002.
[096] Furthermore, the plurality of plastic bags 1002 may be of a chemical resistant material. As such, the material of the plurality of bags 1002 may be inhibited from chemically reacting with fill 1055, thereby maintaining the
transparency of and visibility through bags 1002 by preventing bags 1002 from becoming cloudy and/or opaque due to chemical reactions for applications when transparency may be required. For example, bags 1002 may be formed of polycarbonate, polymethylmethacrylate, derline, polyethylene, polyurethane, or any other suitable chemical resistant material. In certain embodiments, bags 1002 may be coated with the chemical resistant material. Each of the bags 1002 may enclose fill 1055 and be fluidly sealed from the environment and one another. Moreover, the plurality of bags 1002 may be connected together and form a "quilted" configuration of bags 1002. For example, each bag 1002 may share a fluidic seal with an adjacent bag. In other words, the plurality of bags 1002 may be integrally formed of one or more materials. However, it should also be appreciated that each bag 1002 may be separately connected to the other by, for example, stitching, welding, or any other suitable means. Such a configuration may allow all of the bags 1002 to be removed together when, for example, the bags 1002 are damaged or discolored, thus providing eased assembly and disassembly of modules 1000. In addition, utilizing bags 1002 that may be formed of a thin and lightweight material may advantageously reduce the overall weight and bulk of armor subsystem 925. In turn, the strain on the engine and drive train of vehicle 11 may be reduced, and a favorable mass efficiency may be provided.
[097] Separation element 1003 may be any suitable material for insulating modules 1000 from detonations of adjacent bags 1002 such as, for example, a polycarbonate material. Separation element 1003 may be disposed between modules 1000, and may also include transparent materials. Separation element 1003 may be a thin layer separating modules 1000 from each other along the seams of the plurality of bags 1002, and thereby substantially reduce sympathetic detonation of a given module 1000 in the case that an adjacent module 1000 detonates due to impact of a threat projectile. It is contemplated that separation element 1003 may be removably attachable to support vessel, thereby allowing compromised bags 1002 to be replaced with new bags 1002 within a combat area.
[098] It should also be appreciated that bags 1002 may themselves be configured to reduce and/or prevent sympathetic detonation. For example, the seals between bags 1002 may be of an appropriate thickness and/or lateral length, while maintaining sufficient flexibility, to protect against detonation of one or more neighboring bags 002. For example, the seams may be formed of multiple layers of bag 1002 material folded and welded together, or may include separate materials directly stitched, welded, or otherwise connected to the seams of bags
1002. Such a configuration may therefore obviate the need for separation element
1003, thus minimizing the number and weight of components in armor subsystem 925.
[099] In certain embodiments not requiring transparency, support vessel 1001 , cover 1004, and bags 1002 may be formed of one or more substantially opaque materials. Such opaque materials may be lightweight, frangible, and chemical resistant, and may include, as examples, acetal and any other suitable polymer, composite, or ceramic. Moreover, one or both of support vessel 1001 and cover 1004 may be scored to prevent the creation of large fragments upon detonation of bags 1002.
[0100] Fig. 16 illustrates a section view of Fig. 5. Each bag 1002 may be supported and contained between support vessel 1001 , separation element 1003, and cover 1004. The volume surrounding each bag 1002 may be filled with an inert liquid 1005. Inert liquid 1005 may be substantially transparent and configured to minimize visual aberrations by maintaining the appropriate indexes of refraction within each module 1000. Thus, sufficient visibility and transparency through each module 1000 may be provided. Inert liquid 1005 may also act as an appropriate buffer to prevent sympathetic detonation between neighboring bags 1002 and dissipate the blast energy of fill material 1055 transmitted to vehicle 11. Inert liquid 1005 may include, for example, water, glycol, or silicon. Although Fig. 16 illustrates bags 1002 substantially abutting against the back of support vessel 1001 , it should also be appreciated that a suitable gap may be provided between bags 1002 and support vessel 1001 to further dissipate the blast energy of fill material 1055 transmitted to vehicle 11.
[0101] Armor system 10 may be included in newly manufactured vehicles and existing vehicles may be retrofitted with armor system 10 to gain the benefits described herein. For example, an existing vehicle may be retrofitted with subsystems 25, 30, 125, 225, 325, 525, 625, 725, 825, and/or 925 using an assemblage of required parts specific to the vehicle, e.g., in kit form. It should also be appreciated that any of 25, 30, 125, 225, 325, 525, 625, 725, 825, and 925 may be coated with any suitable fire retardant.
[0102] A vehicle may include any combination of the subsystems of armor system 10 including, for example, armor subsystems 25, 30, 125, 225, 325, 525, 625, 725, 825, and/or 925. For example, armor subsystems 25, 30, 125, 225, 325, 525, 625, 725, 825, and/or 925 may be used in combination with each other, as additional armor within a window aperture, as a louver or a system of louvers, and/or as additional perimeter protection for opaque armor. On a given vehicle, some or all of armor subsystems 25, 125, 225, 325, 525, 625, 725, 825, and/or 925 may be used in conjunction with distribution subsystem 30. It is also contemplated that any of the materials of fills 55, 150, 255, 385, 430, 550, 650, 755, 855, and/or 1055 may be used in any of armor subsystems 25, 125, 225, 325, 525, 625, 725, 825, and/or 925. It is further contemplated that the disclosed elements of armor subsystems 25, 30, 125, 225, 325, 525, 625, 725, 825, and/or 925 may be used with any of the other disclosed armor subsystems.
[0103] Vehicle 1 1 , equipped with armor system 10, may operate outside of a combat area. For example, vehicle 11 may move under its own power or be transported for example, by aircraft or rail. While outside of a combat area and/or during transport, armor system 10 may be configured to be in a non-hostile mode. For example, mount assembly 65 may be operated so that armor subsystem 25 is propped up or folded down as needed during transport or storage. Mounts of armor subsystems 125 and 325 may be similarly operated. Also, for example, stoppers 68, 180, 270, and/or 768 may be removed from armor subsystems 25, 125, 225, and/or 725, respectively, to drain reactive fill from vehicle 11 and thereby preclude "special handling" requirements for operators during transport and other activities outside of a combat area. Distribution subsystem 30 may also be operated to transfer fill from the cavities of the various armor subsystems to waste reservoir 470. Reactive fill may be removed from waste reservoir 470, thereby precluding "special handling" requirements outside of a combat area. Additionally, fill modules 420 may be removed from vehicle 11 when outside of a combat area. It is contemplated that substantially all fill may be removed from vehicle 1 1 when in the non-hostile mode.
[0104] When vehicle 11 moves toward a combat area or other threat environment, armor system 10 may be configured to be in a hostile mode. Fill may be added to cavities and reservoirs of vehicle 1. For example, mount assemblies may be configured so that armor subsystems 25, 125, 325, 525, 625, 725, and/or 925 are adjusted to a suitable position for disrupting threat projectiles. Armor subsystems 25, 125, 325, 525, 625, 725, and/or 925 may be adjusted so that angle 100 is, for example, about 30° or about 45°. Also, for example, fill may be added to the cavities of the armor subsystems, and stoppers 68, 180, 270, and/or 768 may be replaced into apertures 67, 175, 265, and/or 767 of armor subsystems 25, 125, 225, and/or 725, respectively. Distribution subsystem 30 may also be operated to transfer fill from fill reservoir 465 to the cavities of the various armor subsystems. Additionally, fill modules 420 may be placed into armor subsystem 325 of vehicle 11. While vehicle 1 1 is in the field, fill may be manually drained and re-filled, or mechanically drained and re-filled by distribution subsystem 30, into cavities 50, 145, 250, 380, 750, and/or 850 and/or housing 640. Fill may be drained and refilled, for example, if an armor subsystem is compromised, the fill becomes contaminated, or the fill begins to chemically break down from its intended properties. It should also be appreciated that a distribution system similar to distribution system 30 may be incorporated into armor subsystem 925 to fill and drain fill material 1055 from one or more bags 1002. Moreover, the distribution system of armor system 925 may be configured to fill and drain liquid from support vessel 1001.
[0105]During the hostile mode, as depicted in Fig. 8, a projectile may be directed toward vehicle 1 1 and may impact armor subsystems 25, 125, 225, 325, 525, 625, 725, 825, and/or 925. If the projectile penetrates the armor subsystems and enters cavities 50, 145, 250, 380, 425, 725, 825, and/or 925, material 550, module 1000, and/or housing 640, the projectile will detonate reactive fill disposed in the cavities. The reactive fill will detonate and disrupt the penetration of the projectile. The material properties of armor system 10 will contribute to the disruption of the projectile. For example, armor subsystems 25, 125, 225, 325, 420, 625, 750, 850, and/or 925 including glass and/or polycarbonate layers will shatter upon detonation of the fill, causing a debris field that will disrupt a projectile jet. Material 550 of armor subsystem 525 will continuously detonate over substantially an entire duration of impact of an HC jet of projectile 12, thereby substantially completely disrupting the jet. Armor subsystems 25, 125, 225, 325, 420, 625, 725, and/or 825 including aluminum and/or delrin layers will propel the aluminum and/or delrin layers into the projectile threat upon detonation of the fill, causing a debris field that will disrupt the projectile jet. If a given module of armor subsystem 325 or 925 is compromised by a projectile, separation elements 395 (for armor system 325) and 1003 (for armor system 925) will substantially reduce the threat of sympathetic detonation to adjacent modules. Moreover, in armor subsystem 325, valves 415 may substantially prevent leakage of fill from adjacent modules.
[0106] Between engagements with threats during the hostile mode, armor system 10 may be reconstituted in the field. For example, fill may be manually drained and re-filled into cavities 50, 145, 250, 380, 750, and/or 850 and/or housing 640 or mechanically drained and re-filled by distribution subsystem 30. Also, compromised fill modules 420 and bags 1000 may be removed and replaced with operational fill modules 420 and bags 1000. Further, compromised material 550 may be removed and replaced with operational material 550.
[0107]Several benefits may be associated with armor system 10. For example, armor system 10 may preclude the requirement for "special handling" by operators when vehicle 11 is outside of a combat area or other threat environment. Armor system 10 provides additional threat protection that is modular and that may be incorporated in new vehicles or retrofitted into existing vehicles. Also, armor system 10 may be used to provide additional protection to both transparent armor and opaque armor.
[0108] Any aspect set forth in any embodiment may be used with any other embodiment set forth herein. It will be apparent to those skilled in the art that various modifications and variations can be made to the disclosed apparatus and method. Other embodiments will be apparent to those skilled in the art from consideration of the specification and practice of the disclosed method and apparatus. It is intended that the specification and examples be considered as exemplary only, with a true scope being indicated by the following claims and their equivalents.

Claims

WHAT IS CLAIMED IS:
1. An armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory, the armor system comprising:
a plurality of modules, each module including:
a bag, wherein each bag shares at least one seal with an adjacent bag; and
a material contained in the bag and capable of being detonated, wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory.
2. The armor system of claim 1 , wherein the bag is substantially transparent and formed of a chemical resistant material.
3. The armor system of claim 2, wherein the chemical resistant material is one of delrin and polyethylene.
4. The armor system of claim 1 , wherein each of the bags is fluidly sealed off from one another.
5. The armor system of claim 1 , wherein the material is a liquid in one of gel form and slurry form.
6. The armor system of claim 1 , wherein the material is substantially entirely transparent.
7. The armor system of claim 1 , wherein the material includes one or more of ammonium nitrate, potassium chlorate, urea nitrate, urea, and tetranitro-isopropanol.
8. The armor system of claim 1 , wherein the material includes one or more of nitromethane, isopropyl nitrate, nitrobenzene, nitrogene tetroxide, and toluene.
9. The armor system of claim 1 , wherein the material includes a mixture of about 82% nitrogen tetroxide and about 18% toluene.
10. The armor system of claim 1 , wherein the material includes a mixture of about 50% methanol and 50% water.
11. An armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory, the armor system comprising:
a plurality of modules, each module including:
a bag, wherein each bag shares at least one seal with an adjacent bag; and
a material contained in the bag and capable of being detonated, wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory; and
a vessel housing the plurality of modules, wherein the vessel is substantially transparent.
12. The armor system of claim 11 , wherein the vessel is configured to cover the plurality of modules and includes one of glass, polycarbonate, acrylic, and
transparent ceramics.
13. The armor system of claim 11 , wherein the vessel is filled with an inert liquid configured to maintain appropriate indexes of refraction for visibility.
14. The armor system of claim 13, wherein the inert liquid includes one or more of water, glycol, and silicon gel.
15. The armor system of claim 11 , wherein the vessel includes a separation element configured to separate the plurality of modules along the seams of the bags.
16. An armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory, the armor system comprising:
a plurality of modules, each module including: a bag, wherein each bag shares at least one seal with an adjacent bag; and
a material contained in the bag and capable of being detonated, wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory; and
a vessel housing the plurality of modules, wherein the vessel includes a separation element configured to separate the plurality of modules along the seams of the bags.
17. The armor system of claim 16, wherein the separation element is configured to prevent sympathetic detonation between bags.
18. The armor system of claim 16, wherein the separation element is formed of a substantially transparent material.
19. The armor system of claim 16, wherein all of the bags are configured to be installed or removed together.
20. The armor system of claim 16, wherein the vessel is substantially transparent and configured to cover the plurality of modules.
21. An armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory, the armor system comprising:
a plurality of modules, each module including:
a bag, wherein each bag shares at least one seal with an adjacent bag, and wherein each bag is substantially transparent; and
a material contained in the bag and capable of being detonated, wherein the material is substantially transparent, and wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory; and
a vessel housing the plurality of modules, wherein the vessel is substantially transparent.
22. The armor system of claim 21 , wherein each bag is chemical resistant and includes one or more of polycarbonate, polymethylmethacrylate, and polyurethane.
23. The armor system of claim 21 , wherein the vessel is formed of one or more of glass, transparent ceramics, polycarbonate, polymethylmethacrylate, and
polyurethane.
24. The armor system of claim 21 , wherein the material is a liquid in one of gel form and slurry form.
25. The armor system of claim 21 , wherein the at least one seal includes a thickness configured to prevent sympathetic detonation of a neighboring bag.
26. The armor system of claim 21 , further comprising a gap between each bag and a wall of the vessel, wherein the gap is configured to dissipate blast energy from the detonation of one or more of the bags.
27. The armor system of claim 21 , wherein the vessel is filled with a liquid configured to dissipate blast energy from the detonation of one or more of the bags.
28. An armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory, the armor system comprising:
a plurality of modules, each module including:
a bag, wherein each bag shares at least one seal with an adjacent bag, and wherein each bag is substantially opaque; and
a material contained in the bag and capable of being detonated, wherein the material is substantially opaque, and wherein the bag and the material lead a vehicle exterior surface relative to the expected projectile trajectory; and
a vessel housing the plurality of modules, wherein the vessel is substantially opaque.
29. The armor system of claim 28, wherein each bag is chemical resistant.
30. The armor system of claim 28, wherein the vessel is formed of one or more of acetal, opaque polymers, opaque composites, and opaque ceramics.
31. The armor system of claim 28, wherein the material is one of ammonium nitrate and urea nitrate.
32. The armor system of claim 28, wherein the material is a liquid in one of gel form and slurry form.
33. The armor system of claim 28, wherein the at least one seal includes a thickness configured to prevent sympathetic detonation of a neighboring bag.
34. The armor system of claim 28, further comprising a gap between each bag and a wall of the vessel, wherein the gap is configured to dissipate blast energy from the detonation of one or more of the bags.
35. The armor system of claim 28, wherein the vessel is filled with a liquid configured to dissipate blast energy from the detonation of one or more of the bags.
36. An armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory, the armor system comprising:
a first element, leading relative to the expected projectile trajectory;
a second element disposed behind the first element, relative to the expected projectile trajectory, wherein the first element and the second element are spaced apart to form a cavity; and
a fill capable of being detonated disposed in the cavity, wherein the fill includes one or more of a desensitizer and a sensitizer.
37. The armor system of claim 36, wherein the fill includes the desensitizer, and wherein the desensitizer includes methanol.
38. The armor system of claim 37, wherein the fill includes the sensitizer, and wherein the sensitizer includes glass spheres.
39. The armor system of claim 37, wherein the first and second elements include plates, each having a thickness between 1 mm to 100 mm.
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US13/024,640 US20120204711A1 (en) 2011-02-10 2011-02-10 Apparatus for Defeating Threat Projectiles
US13/024,640 2011-02-10
US201113326573A 2011-12-15 2011-12-15
US13/326,573 2011-12-15

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