US20120291616A1 - Shield kits for projectile protection - Google Patents
Shield kits for projectile protection Download PDFInfo
- Publication number
- US20120291616A1 US20120291616A1 US13/111,888 US201113111888A US2012291616A1 US 20120291616 A1 US20120291616 A1 US 20120291616A1 US 201113111888 A US201113111888 A US 201113111888A US 2012291616 A1 US2012291616 A1 US 2012291616A1
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- United States
- Prior art keywords
- shield
- cable
- frame
- kit
- flexible
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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- 238000000034 method Methods 0.000 claims abstract description 7
- 239000004753 textile Substances 0.000 claims description 9
- 238000005474 detonation Methods 0.000 claims description 6
- 239000002360 explosive Substances 0.000 claims description 6
- 239000000463 material Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 4
- 239000002131 composite material Substances 0.000 description 3
- -1 flexible Substances 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000003466 anti-cipated effect Effects 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 239000011796 hollow space material Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 241000287828 Gallus gallus Species 0.000 description 1
- 239000004705 High-molecular-weight polyethylene Substances 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 239000002274 desiccant Substances 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 239000003562 lightweight material Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 239000013077 target material Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H5/00—Armour; Armour plates
- F41H5/02—Plate construction
- F41H5/023—Armour plate, or auxiliary armour plate mounted at a distance of the main armour plate, having cavities at its outer impact surface, or holes, for deflecting the projectile
- F41H5/026—Slat armour; Nets
Definitions
- the following disclosure relates generally to shield kits for vehicles and structures, and associated systems and methods.
- Shaped-charge warheads such as RPGs, are capable of penetrating steel armor and pose a particular problem for tanks and armored personnel carriers (APC) in combat situations.
- a shaped-charge warhead consists of a cone shaped warhead having a quantity of explosive disposed behind a hollow space.
- the hollow space is typically lined with a compliant material, such as copper.
- a compliant material such as copper.
- the energy is concentrated to the center of the charge and is sufficient to transform the copper into a thin, effectively liquid, shaped-charge jet having a tip speed of up to 26,000 mph.
- the extremely high pressures generated cause the target material to yield and flow plastically, with devastating effect.
- To be most effective the shape and structure of the cone of the shaped-charge must be in tact at detonation. If the shape is somehow altered, the shaped-charge jet will not have formed properly before hitting the surface and the effect will be lessened.
- Conventional shields for defending against shaped-charge warheads make use of the fact that the shape of warheads enables the warheads to “jet” or penetrate heavy armor.
- By providing an outer shield at a short distance from the actual armor of the vehicle or other structure that can deform or crumple the cone of the warhead it is possible to cause the warhead to fail or dud, with the effect that the full design of the charge is thwarted. In effect, the warhead becomes a conventional grenade, rather than a shaped-charge.
- Bar armor includes a metal frame which is mounted at a distance of approximately 1.5 feet from the vehicle.
- the frame includes a plurality of horizontal struts or bars which are spaced apart at a distance selected to prevent penetration by shaped-charge warheads.
- bar armor When the shaped charge strikes the bar armor, the bar armor deforms the charge and interferes with the design of the detonation, reducing the damage from the shaped-charge.
- One disadvantage of bar armor is that it is relatively heavy and adds a great deal of weight to an already heavy vehicle. In addition, bar armor cannot easily be replaced or repaired in the field.
- FIG. 1 is an isometric view of a vehicle having a plurality of flexible shields replacing damaged portions of a bar armor system according to an embodiment of the present disclosure.
- FIG. 2 is a front elevation view of one of the flexible shields of FIG. 1 configured according to an embodiment of the present disclosure.
- FIG. 3 is an isometric view of a cable support system for use with the flexible shields of the present disclosure.
- FIG. 4 is a front perspective view of an installed flexible shield having a cable-reinforced seam configured according to an embodiment of the present disclosure.
- FIG. 5 is an isometric view of a seam between two shields configured according to another embodiment of the present disclosure.
- FIG. 6 a is an isometric view of a shield kit configured according to an embodiment of the present disclosure.
- FIG. 6 b is an isometric view of the shield kit of FIG. 6 a packaged for in-field deployment and configured according to an embodiment of the present disclosure.
- the present disclosure relates to various embodiments of flexible shields and shield systems which may be used to protect a target, such as a vehicle, building or other structure, from damage caused by a projectile, such as a rocket propelled grenade (RPG) or other shaped-charge.
- the shields of the present disclosure can be used as replacement shields for bar armor systems configured to interrupt the design of detonation of warheads, rendering them significantly less powerful than intended.
- the shields can be small and lightweight for portability and relatively easy in-field installation. Many specific details are set forth in the following description and in FIGS. 1-6 b to provide a thorough understanding of various embodiments of the disclosure. Other details describing well-known structures and systems often associated with bar armor systems, however, are not set forth below to avoid unnecessarily obscuring the description of the various embodiments of the disclosure.
- FIG. 1 is an isometric view of a vehicle 110 having a plurality of flexible shields 140 (identified individually as first shield 140 a and second shield 140 b ) replacing damaged portions of a bar armor system 100 according to embodiments of the present disclosure.
- the flexible shields 140 can be the same as or similar to the textile armor described in U.S. patent application Ser. No. 10/584,605, filed Aug. 9, 2007, published as U.S. Patent Application Publication No. 2009/0217811, claiming priority to GB Patent Application No. GB 0601030.0, filed Jan. 17, 2006, both of which are incorporated herein by reference in their entirety.
- the bar armor system 100 can include conventional armor bars or slats 124 suspended from a perimeter frame 121 that is attached to the vehicle 110 by standoff arms 122 (shown in FIG. 1 ).
- the standoff arms 122 project outward from the vehicle 110 a predetermined standoff distance, such as about one foot or more. The standoff distance can vary depending on the nature of the expected projectile attack and on the dimensions of the vehicle 110 .
- the bars 124 , the frame 121 , and the standoff arms 122 are collectively referred to herein as armor 120 .
- the armor 120 can be divided into discrete panels 123 , each panel being defined by a section of the frame 121 and covered by the bars 124 . Virtually any suitable panel dimension and bar shape and size can be used.
- one of the panels 123 covers the entire rear, side, or front of the vehicle 110 .
- the individual panels 123 cover a smaller area of the vehicle 110 , and in some cases two or more of the panels 123 together cover the entire rear, side, or front of the vehicle 110 .
- the armor 120 is configured to substantially cover the vehicle 110 from anticipated angles of attack. In some embodiments, the angle of attack cannot be anticipated so the armor 120 can cover the entire vehicle 110 . In other embodiments, such as shown in FIG. 1 , a lower perimeter of the vehicle 110 is covered by the armor 120 in anticipation that an attack will come from the ground and not the air.
- the shaped charge When a projectile such as a shaped charge strikes the armor 120 , the shaped charge is deformed by the armor 120 , thus preventing the shaped charge from “jetting.”
- the projectile's destructive power is therefore reduced to generally equivalent to a hand grenade, which can be withstood by the conventional armor of the vehicle 110 .
- the armor 120 may be damaged or otherwise rendered inoperable by the blast. Other circumstances can also damage the armor 120 , such as contact with rough terrain. Carrying replacement bars or slats for such a contingency is generally impractical.
- the shields 140 of the present disclosure can be packaged in a kit, conveniently carried on board the vehicle 110 , and deployed in the field to cover an exposed portion of the vehicle 110 when a portion of the armor 120 is damaged.
- the shields 140 can be flexible shields and can therefore cover panels 123 of varying sizes.
- the first shield 140 a can protect a portion of the front of the vehicle 110
- the second shield 140 b can protect a side of the vehicle 110 .
- the size and attachment points of the shields 140 a, 140 b when installed may vary according to the size of the damaged area of the armor 120 .
- the first shield 140 a and second shield 140 b are similar in size before deployment and are packaged similarly.
- FIG. 2 is a front elevation view of one of the shields 140 of FIG. 1 according to an embodiment of the present disclosure.
- the shield 140 is made from a textile material such as a net having interwoven strands 141 forming square, diamond, or hexagonal holes between the strands 141 .
- the holes can range from about 0.5 inch to 2.5 inches, or about one inch across.
- the size of the holes in the shield 140 can be selected to defeat a particular type of shaped charge.
- the holes in the shield 140 can be made slightly larger than a nose of an expected shaped charge projectile, but smaller than the body of the shaped projectile.
- the strands 141 can be made of various suitable materials, including flexible, lightweight materials such as polyethylene (e.g., high molecular weight polyethylene). In some embodiments, the strands 141 do not stretch appreciably and therefore interrupt the designed detonation of the projectile.
- polyethylene e.g., high molecular weight polyethylene
- the strands 141 can be aligned in a first direction, wherein each strand 141 is woven with adjacent strands 141 alternating left and right along the length of the strand 141 , with a knotless intersection between strands 141 , similar to chicken wire or a chain-link fence.
- these strands 141 are known as warp strands.
- warp strands of a textile are woven in a first direction, and the textile can optionally include weft (or fill) strands interwoven with the warp strands in a second direction transverse to the first direction.
- the shield 140 is a textile having warp strands 141 and does not include weft strands. In other embodiments, the shield 140 includes both warp strands 141 and weft strands (not shown).
- any suitable hole can be used as an attachment point for fastening the shield 140 to the frame 121 .
- Fasteners 142 such as cable ties (e.g., zip ties) or other suitable strap fasteners can extend through a hole in the shield 140 and around a portion of the frame 121 to hold the shield 140 to the frame 121 .
- the size of the deployed shield 140 can therefore be adjusted to fit any size of breach in the armor 120 with any suitable level of tension by selectively installing fasteners 142 in available holes and securing the shield 140 to the frame 121 .
- the shield 140 can include loops or eyelets or other suitable attachment points (not shown) at any suitable position, including around a periphery of the shield 140 , that can engage the fasteners 142 to attach the shield 140 to the frame 121 .
- the shield 140 can be pulled taut across the frame 121 and fastened with an appropriate amount of slack so that the shield 140 deflects a small amount, but less than the standoff distance, when a projectile strikes the shield 140 .
- An operator can perform a convenient test for the proper slack by pressing on the shield 140 with his hand.
- the shield 140 can be sufficiently taut that the shield 140 deflects slightly, but the operator's hand does not reach more than about half the standoff distance between the shield 140 and a hull or sidewall of the vehicle 110 . This test can be performed in the field without using tools or any other specialized equipment.
- FIG. 3 is an isometric view of a first cable 144 , second cable 145 , and a cable joiner 146 for use with the shield 140 configured according to embodiments of the present disclosure.
- the cables 144 , 145 can be made of steel, polyethylene, cable, and/or other suitable materials.
- the cable joiner 146 can include two through-holes or channels configured to receive the first and second cables 144 , 145 extending therethrough. The channels can be mirrored on opposite sides of the cable joiner 146 to receive the first and second cables 144 , 145 .
- the cable joiner 146 can have spring-loaded rollers or wedges in the channels configured to permit the cables 144 , 145 to move through the cable joiner 146 in one direction only and grip the cables 144 , 145 when pulled in the opposite direction.
- the cable joiner 146 is a conventional gripple as provided by, e.g., Gripple Ltd. of Sheffield, England.
- the cables 144 , 145 can be fastened to opposing portions of the frame 121 shown in FIG. 2 .
- a first portion 144 a of the first cable 144 extends between the frame 121 and the cable joiner 146
- a second portion 144 b of the first cable 144 is trimmed near the cable joiner 146 .
- a first portion 145 a of the second cable 145 can similarly extend between the frame 121 and the cable joiner 146
- a second portion 145 b of the second cable 145 can also be trimmed near the cable joiner 146 .
- the first portions 144 a, 145 a can be tensioned by pulling the second portions 144 b , 145 b away from the cable joiner 146 as shown by arrows A.
- the cables 144 , 145 can be interwoven with the shield 140 .
- the shield 140 can be attached to the cables 144 , 145 with the fasteners 142 via holes, loops, eyelets, or another suitable attachment point on the shield 140 as described above.
- the second portions 144 b, 145 b of the first and second cables 144 , 145 can be secured to other portions of the frame 121 to pull the cables 144 , 145 away from the shield 140 to further tension the shield 140 .
- the shield 140 can therefore be enlarged and shaped.
- an edge 143 of the shield 140 can be non-linear, following the shape of the first portions 144 a, 145 a of the cables 144 , 145 .
- This method can also be used to achieve proper tension in the shield 140 .
- the cables 144 , 145 therefore form a replacement frame that holds the shield 140 in place. Accordingly, even when a portion of the frame 121 is damaged or missing, the cables 144 , 145 support the shield 140 with a desired tension in the shield 140 .
- FIG. 4 is a front perspective view of a shield installation with a cable-reinforced seam 200 configured according to an embodiment of the present disclosure.
- the first and second shields 140 a, 140 b can be fastened to the frame 121 with a plurality of the fasteners 142 installed along three sides of each shield 140 a, 140 b with the remaining side of the shields 140 a, 140 b positioned adjacent to one another in the middle of the frame 121 .
- a first cable 144 can be fastened to the frame 121 at a first cable attachment point 150
- a second cable 145 can be fastened to a second cable attachment point 151 opposite the first cable attachment point 150 .
- first and second cables 144 , 145 can be wrapped around any available portion of the frame 121 and tied off.
- the first and second cable attachment points 150 , 151 can be specifically designed to engage and anchor the respective end portions of the cables 144 , 145 .
- the cable attachment points 150 , 151 can be knobs, hooks, or cleats.
- the cables 144 , 145 can be woven through holes along the adjacent edges of the shields 140 a, 140 b and joined together with the cable joiner 146 and tensioned as described above.
- the second portions 144 b, 145 b of the first and second cables 144 , 145 can either be trimmed or can be attached to some portion of the frame 121 or the shields 140 a, 140 b.
- the first and second shields 140 a, 140 b together form a composite shield 140 c covering the entire panel 123 .
- the cables 144 , 145 provide additional rigidity and tension to the composite shield 140 c.
- the seam 200 can be used when a portion of the frame 121 is missing. For example, when a portion of the frame 121 between adjacent panels 123 (see FIG. 1 ) may be missing or damaged. Accordingly, the composite shield 140 c and cable-reinforced seam 200 can be used to cover the vehicle 110 when portions of the frame 121 are unavailable.
- FIG. 5 is an isometric view of a shield seam 300 configured according to another embodiment of the present disclosure.
- the fasteners 142 can directly attach the first shield 140 a to the second shield 140 b, without using a cable or cable joiner. More specifically, the operator can pull the shields 140 a, 140 b together with the desired tension and place the fasteners 142 at any appropriate hole of the shields 140 a, 140 b to maintain the desired tension.
- FIG. 6 a is an isometric view of a kit 160 according to embodiments of the present disclosure.
- the kit 160 includes a shield 140 that is wrapped or rolled into a compact package, fasteners 142 , a cable 144 , and cable joiners 146 .
- the kit 160 can also include a desiccant material 145 , any suitable printed instructions 147 , and a marker 148 for indicating when the shield 140 was installed or other information.
- the kit 160 weighs approximately 3.5 pounds and is therefore easily portable. In other embodiments including a larger shield 140 , the kit can be approximately 7 pounds.
- FIG. 6 b is an isometric view of the kit 160 of FIG. 6 a as packaged conveniently for deployment in the field.
- the shields can be made of various suitable materials and can have various dimensions.
- specific elements of any of the foregoing embodiments can be combined or substituted for elements in other embodiments.
- Certain aspects of the disclosure are accordingly not limited to automobile or aircraft systems.
- advantages associated with certain embodiments of the disclosure have been described in the context of these embodiments, other embodiments may also exhibit such advantages, and not all embodiments need necessarily exhibit such advantages to fall within the scope of the invention. Accordingly, the disclosure is not limited, except as by the appended claims.
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Abstract
Description
- The present application hereby claims priority to United Kingdom Patent Application No. ______, filed on May 17, 2011, which is incorporated herein in its entirety by reference.
- The following disclosure relates generally to shield kits for vehicles and structures, and associated systems and methods.
- Shaped-charge warheads, such as RPGs, are capable of penetrating steel armor and pose a particular problem for tanks and armored personnel carriers (APC) in combat situations. A shaped-charge warhead consists of a cone shaped warhead having a quantity of explosive disposed behind a hollow space. The hollow space is typically lined with a compliant material, such as copper. When detonated, the energy is concentrated to the center of the charge and is sufficient to transform the copper into a thin, effectively liquid, shaped-charge jet having a tip speed of up to 26,000 mph. The extremely high pressures generated cause the target material to yield and flow plastically, with devastating effect. To be most effective the shape and structure of the cone of the shaped-charge must be in tact at detonation. If the shape is somehow altered, the shaped-charge jet will not have formed properly before hitting the surface and the effect will be lessened.
- Conventional shields for defending against shaped-charge warheads make use of the fact that the shape of warheads enables the warheads to “jet” or penetrate heavy armor. By providing an outer shield at a short distance from the actual armor of the vehicle or other structure that can deform or crumple the cone of the warhead, it is possible to cause the warhead to fail or dud, with the effect that the full design of the charge is thwarted. In effect, the warhead becomes a conventional grenade, rather than a shaped-charge.
- Any outer shield that interrupts the detonation design of the shaped-charge will offer some degree of protection. The shield itself merely needs to deform or crumple a portion of the cone of the shaped charge, reducing the impact of the shaped charge to a simple grenade; it is not meant to act as additional armor. In recent times it has become common to fit so-called “bar armor” to tanks and other military vehicles. Bar armor includes a metal frame which is mounted at a distance of approximately 1.5 feet from the vehicle. The frame includes a plurality of horizontal struts or bars which are spaced apart at a distance selected to prevent penetration by shaped-charge warheads. When the shaped charge strikes the bar armor, the bar armor deforms the charge and interferes with the design of the detonation, reducing the damage from the shaped-charge. One disadvantage of bar armor is that it is relatively heavy and adds a great deal of weight to an already heavy vehicle. In addition, bar armor cannot easily be replaced or repaired in the field.
-
FIG. 1 is an isometric view of a vehicle having a plurality of flexible shields replacing damaged portions of a bar armor system according to an embodiment of the present disclosure. -
FIG. 2 is a front elevation view of one of the flexible shields ofFIG. 1 configured according to an embodiment of the present disclosure. -
FIG. 3 is an isometric view of a cable support system for use with the flexible shields of the present disclosure. -
FIG. 4 is a front perspective view of an installed flexible shield having a cable-reinforced seam configured according to an embodiment of the present disclosure. -
FIG. 5 is an isometric view of a seam between two shields configured according to another embodiment of the present disclosure. -
FIG. 6 a is an isometric view of a shield kit configured according to an embodiment of the present disclosure. -
FIG. 6 b is an isometric view of the shield kit ofFIG. 6 a packaged for in-field deployment and configured according to an embodiment of the present disclosure. - The present disclosure relates to various embodiments of flexible shields and shield systems which may be used to protect a target, such as a vehicle, building or other structure, from damage caused by a projectile, such as a rocket propelled grenade (RPG) or other shaped-charge. The shields of the present disclosure can be used as replacement shields for bar armor systems configured to interrupt the design of detonation of warheads, rendering them significantly less powerful than intended. The shields can be small and lightweight for portability and relatively easy in-field installation. Many specific details are set forth in the following description and in
FIGS. 1-6 b to provide a thorough understanding of various embodiments of the disclosure. Other details describing well-known structures and systems often associated with bar armor systems, however, are not set forth below to avoid unnecessarily obscuring the description of the various embodiments of the disclosure. - Many of the details and features shown in the Figures are merely illustrative of particular embodiments of the disclosure. Accordingly, other embodiments can have other details and features without departing from the spirit and scope of the present disclosure. In addition, those of ordinary skill in the art will understand that further embodiments can be practiced without several of the details described below. Furthermore, various embodiments of the disclosure can include structures other than those illustrated in the Figures and are expressly not limited to the structures shown in the Figures. Moreover, the various elements and features illustrated in the Figures may not be drawn to scale.
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FIG. 1 is an isometric view of avehicle 110 having a plurality of flexible shields 140 (identified individually asfirst shield 140 a andsecond shield 140 b) replacing damaged portions of abar armor system 100 according to embodiments of the present disclosure. Theflexible shields 140 can be the same as or similar to the textile armor described in U.S. patent application Ser. No. 10/584,605, filed Aug. 9, 2007, published as U.S. Patent Application Publication No. 2009/0217811, claiming priority to GB Patent Application No. GB 0601030.0, filed Jan. 17, 2006, both of which are incorporated herein by reference in their entirety. Thebar armor system 100 can include conventional armor bars orslats 124 suspended from aperimeter frame 121 that is attached to thevehicle 110 by standoff arms 122 (shown inFIG. 1 ). Thestandoff arms 122 project outward from the vehicle 110 a predetermined standoff distance, such as about one foot or more. The standoff distance can vary depending on the nature of the expected projectile attack and on the dimensions of thevehicle 110. Thebars 124, theframe 121, and thestandoff arms 122 are collectively referred to herein asarmor 120. Thearmor 120 can be divided intodiscrete panels 123, each panel being defined by a section of theframe 121 and covered by thebars 124. Virtually any suitable panel dimension and bar shape and size can be used. In some embodiments, one of thepanels 123 covers the entire rear, side, or front of thevehicle 110. In other embodiments, theindividual panels 123 cover a smaller area of thevehicle 110, and in some cases two or more of thepanels 123 together cover the entire rear, side, or front of thevehicle 110. - The
armor 120 is configured to substantially cover thevehicle 110 from anticipated angles of attack. In some embodiments, the angle of attack cannot be anticipated so thearmor 120 can cover theentire vehicle 110. In other embodiments, such as shown inFIG. 1 , a lower perimeter of thevehicle 110 is covered by thearmor 120 in anticipation that an attack will come from the ground and not the air. - When a projectile such as a shaped charge strikes the
armor 120, the shaped charge is deformed by thearmor 120, thus preventing the shaped charge from “jetting.” The projectile's destructive power is therefore reduced to generally equivalent to a hand grenade, which can be withstood by the conventional armor of thevehicle 110. However, thearmor 120 may be damaged or otherwise rendered inoperable by the blast. Other circumstances can also damage thearmor 120, such as contact with rough terrain. Carrying replacement bars or slats for such a contingency is generally impractical. Theshields 140 of the present disclosure, however, can be packaged in a kit, conveniently carried on board thevehicle 110, and deployed in the field to cover an exposed portion of thevehicle 110 when a portion of thearmor 120 is damaged. Theshields 140 can be flexible shields and can therefore coverpanels 123 of varying sizes. For example, in the illustrated embodiment thefirst shield 140 a can protect a portion of the front of thevehicle 110, and thesecond shield 140 b can protect a side of thevehicle 110. The size and attachment points of the 140 a, 140 b when installed may vary according to the size of the damaged area of theshields armor 120. In some embodiments, thefirst shield 140 a andsecond shield 140 b are similar in size before deployment and are packaged similarly. -
FIG. 2 is a front elevation view of one of theshields 140 ofFIG. 1 according to an embodiment of the present disclosure. In some embodiments, theshield 140 is made from a textile material such as a net having interwovenstrands 141 forming square, diamond, or hexagonal holes between thestrands 141. The holes can range from about 0.5 inch to 2.5 inches, or about one inch across. The size of the holes in theshield 140 can be selected to defeat a particular type of shaped charge. For example, the holes in theshield 140 can be made slightly larger than a nose of an expected shaped charge projectile, but smaller than the body of the shaped projectile. Thestrands 141 can be made of various suitable materials, including flexible, lightweight materials such as polyethylene (e.g., high molecular weight polyethylene). In some embodiments, thestrands 141 do not stretch appreciably and therefore interrupt the designed detonation of the projectile. - The
strands 141 can be aligned in a first direction, wherein eachstrand 141 is woven withadjacent strands 141 alternating left and right along the length of thestrand 141, with a knotless intersection betweenstrands 141, similar to chicken wire or a chain-link fence. In general textile terminology, thesestrands 141 are known as warp strands. In general, warp strands of a textile are woven in a first direction, and the textile can optionally include weft (or fill) strands interwoven with the warp strands in a second direction transverse to the first direction. In some embodiments, theshield 140 is a textile havingwarp strands 141 and does not include weft strands. In other embodiments, theshield 140 includes bothwarp strands 141 and weft strands (not shown). - In embodiments in which the
shield 140 is a net having holes, any suitable hole can be used as an attachment point for fastening theshield 140 to theframe 121.Fasteners 142 such as cable ties (e.g., zip ties) or other suitable strap fasteners can extend through a hole in theshield 140 and around a portion of theframe 121 to hold theshield 140 to theframe 121. The size of the deployedshield 140 can therefore be adjusted to fit any size of breach in thearmor 120 with any suitable level of tension by selectively installingfasteners 142 in available holes and securing theshield 140 to theframe 121. In other embodiments in which theshield 140 includes tightly-wovenwarp strands 141 and weft strands (not shown) without holes, theshield 140 can include loops or eyelets or other suitable attachment points (not shown) at any suitable position, including around a periphery of theshield 140, that can engage thefasteners 142 to attach theshield 140 to theframe 121. - The
shield 140 can be pulled taut across theframe 121 and fastened with an appropriate amount of slack so that theshield 140 deflects a small amount, but less than the standoff distance, when a projectile strikes theshield 140. An operator can perform a convenient test for the proper slack by pressing on theshield 140 with his hand. Theshield 140 can be sufficiently taut that theshield 140 deflects slightly, but the operator's hand does not reach more than about half the standoff distance between theshield 140 and a hull or sidewall of thevehicle 110. This test can be performed in the field without using tools or any other specialized equipment. -
FIG. 3 is an isometric view of afirst cable 144,second cable 145, and acable joiner 146 for use with theshield 140 configured according to embodiments of the present disclosure. The 144, 145 can be made of steel, polyethylene, cable, and/or other suitable materials. Thecables cable joiner 146 can include two through-holes or channels configured to receive the first and 144, 145 extending therethrough. The channels can be mirrored on opposite sides of thesecond cables cable joiner 146 to receive the first and 144, 145. Thesecond cables cable joiner 146 can have spring-loaded rollers or wedges in the channels configured to permit the 144, 145 to move through thecables cable joiner 146 in one direction only and grip the 144, 145 when pulled in the opposite direction. In some embodiments, thecables cable joiner 146 is a conventional gripple as provided by, e.g., Gripple Ltd. of Sheffield, England. - The
144, 145 can be fastened to opposing portions of thecables frame 121 shown inFIG. 2 . In some embodiments, afirst portion 144 a of thefirst cable 144 extends between theframe 121 and thecable joiner 146, and asecond portion 144 b of thefirst cable 144 is trimmed near thecable joiner 146. Afirst portion 145 a of thesecond cable 145 can similarly extend between theframe 121 and thecable joiner 146, and asecond portion 145 b of thesecond cable 145 can also be trimmed near thecable joiner 146. The 144 a, 145 a can be tensioned by pulling thefirst portions 144 b, 145 b away from thesecond portions cable joiner 146 as shown by arrows A. In some embodiments, the 144, 145 can be interwoven with thecables shield 140. In other embodiments, theshield 140 can be attached to the 144, 145 with thecables fasteners 142 via holes, loops, eyelets, or another suitable attachment point on theshield 140 as described above. - In some embodiments, the
144 b, 145 b of the first andsecond portions 144, 145 can be secured to other portions of thesecond cables frame 121 to pull the 144, 145 away from thecables shield 140 to further tension theshield 140. Theshield 140 can therefore be enlarged and shaped. For example, anedge 143 of theshield 140 can be non-linear, following the shape of the 144 a, 145 a of thefirst portions 144, 145. This method can also be used to achieve proper tension in thecables shield 140. The 144, 145 therefore form a replacement frame that holds thecables shield 140 in place. Accordingly, even when a portion of theframe 121 is damaged or missing, the 144, 145 support thecables shield 140 with a desired tension in theshield 140. -
FIG. 4 is a front perspective view of a shield installation with a cable-reinforcedseam 200 configured according to an embodiment of the present disclosure. The first and 140 a, 140 b can be fastened to thesecond shields frame 121 with a plurality of thefasteners 142 installed along three sides of each 140 a, 140 b with the remaining side of theshield 140 a, 140 b positioned adjacent to one another in the middle of theshields frame 121. Afirst cable 144 can be fastened to theframe 121 at a firstcable attachment point 150, and asecond cable 145 can be fastened to a secondcable attachment point 151 opposite the firstcable attachment point 150. In some embodiments, the first and 144, 145 can be wrapped around any available portion of thesecond cables frame 121 and tied off. In other embodiments, the first and second cable attachment points 150, 151 can be specifically designed to engage and anchor the respective end portions of the 144, 145. For example, in some embodiments the cable attachment points 150, 151 can be knobs, hooks, or cleats.cables - The
144, 145 can be woven through holes along the adjacent edges of thecables 140 a, 140 b and joined together with theshields cable joiner 146 and tensioned as described above. The 144 b, 145 b of the first andsecond portions 144, 145 can either be trimmed or can be attached to some portion of thesecond cables frame 121 or the 140 a, 140 b.shields - The first and
140 a, 140 b together form asecond shields composite shield 140 c covering theentire panel 123. The 144, 145 provide additional rigidity and tension to thecables composite shield 140 c. In some embodiments, theseam 200 can be used when a portion of theframe 121 is missing. For example, when a portion of theframe 121 between adjacent panels 123 (seeFIG. 1 ) may be missing or damaged. Accordingly, thecomposite shield 140 c and cable-reinforcedseam 200 can be used to cover thevehicle 110 when portions of theframe 121 are unavailable. -
FIG. 5 is an isometric view of ashield seam 300 configured according to another embodiment of the present disclosure. In this embodiment, thefasteners 142 can directly attach thefirst shield 140 a to thesecond shield 140 b, without using a cable or cable joiner. More specifically, the operator can pull the 140 a, 140 b together with the desired tension and place theshields fasteners 142 at any appropriate hole of the 140 a, 140 b to maintain the desired tension.shields -
FIG. 6 a is an isometric view of akit 160 according to embodiments of the present disclosure. Thekit 160 includes ashield 140 that is wrapped or rolled into a compact package,fasteners 142, acable 144, andcable joiners 146. Thekit 160 can also include adesiccant material 145, any suitable printedinstructions 147, and amarker 148 for indicating when theshield 140 was installed or other information. In some embodiments, thekit 160 weighs approximately 3.5 pounds and is therefore easily portable. In other embodiments including alarger shield 140, the kit can be approximately 7 pounds.FIG. 6 b is an isometric view of thekit 160 ofFIG. 6 a as packaged conveniently for deployment in the field. - From the foregoing, it will be appreciated that specific embodiments have been described herein for purposes of illustration, but that various modifications may be made without deviating from the spirit and scope of the various embodiments of the disclosure. For example, the shields can be made of various suitable materials and can have various dimensions. Moreover, specific elements of any of the foregoing embodiments can be combined or substituted for elements in other embodiments. Certain aspects of the disclosure are accordingly not limited to automobile or aircraft systems. Furthermore, while advantages associated with certain embodiments of the disclosure have been described in the context of these embodiments, other embodiments may also exhibit such advantages, and not all embodiments need necessarily exhibit such advantages to fall within the scope of the invention. Accordingly, the disclosure is not limited, except as by the appended claims.
Claims (22)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB1108349.5 | 2011-05-17 | ||
| GB201108349 | 2011-05-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20120291616A1 true US20120291616A1 (en) | 2012-11-22 |
Family
ID=47178369
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US13/111,888 Abandoned US20120291616A1 (en) | 2011-05-17 | 2011-05-19 | Shield kits for projectile protection |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US20120291616A1 (en) |
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| US20110123355A1 (en) * | 2008-08-04 | 2011-05-26 | Edwards Limited | Vacuum pump |
| US20120011993A1 (en) * | 2008-04-16 | 2012-01-19 | Joseph Vincent Malone | Vehicle and structure shield with a cable frame |
| US20120255431A1 (en) * | 2011-04-07 | 2012-10-11 | Nexter Systems | Ballistic protection grid having an access hatch |
| US8443708B2 (en) | 2006-01-17 | 2013-05-21 | Amsafe Bridport Limited | Textile armour |
| US8573125B1 (en) * | 2012-07-13 | 2013-11-05 | Blast Control Systems, L.L.C. | Blast control blanket |
| US20140338520A1 (en) * | 2011-09-12 | 2014-11-20 | Ten Cate Advanced Armour Uk Ltd. | Armour Module for Vehicle |
| US20150292838A1 (en) * | 2014-04-13 | 2015-10-15 | Plasan Sasa Ltd. | Armor coupler |
| US20160187106A1 (en) * | 2014-10-03 | 2016-06-30 | Response Solutions & Innovations, Inc. | Frame configurable for use as a ballistic shield and related methods |
| US9476679B2 (en) * | 2011-09-06 | 2016-10-25 | Thomas Frederick Hafer | Ultra light bar armor |
| CN111776475A (en) * | 2018-02-27 | 2020-10-16 | 蓝箭航天技术有限公司 | Rocket packaging method and packaging box section preparation method |
| US11402177B2 (en) * | 2019-12-03 | 2022-08-02 | Michael Cohen | Composite grid/slat-armor |
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| US8752468B2 (en) | 2006-01-17 | 2014-06-17 | Amsafe Bridport Limited | Textile Armour |
| US9310169B2 (en) | 2006-01-17 | 2016-04-12 | Amsafe Bridport Limited | Textile armour |
| US8881638B2 (en) | 2006-01-17 | 2014-11-11 | Amsafe Bridport Limited | Textile armour |
| US8443708B2 (en) | 2006-01-17 | 2013-05-21 | Amsafe Bridport Limited | Textile armour |
| US8468927B2 (en) * | 2008-04-16 | 2013-06-25 | QinetiQ North America, Inc. | Vehicle and structure shield with a cable frame |
| US20120011993A1 (en) * | 2008-04-16 | 2012-01-19 | Joseph Vincent Malone | Vehicle and structure shield with a cable frame |
| US8783156B1 (en) | 2008-04-16 | 2014-07-22 | Foster-Miller, Inc. | Vehicle and structure shield with a cable frame |
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| US8746121B2 (en) * | 2011-04-07 | 2014-06-10 | Nexter Systems | Ballistic protection grid having an access hatch |
| US20120255431A1 (en) * | 2011-04-07 | 2012-10-11 | Nexter Systems | Ballistic protection grid having an access hatch |
| US9476679B2 (en) * | 2011-09-06 | 2016-10-25 | Thomas Frederick Hafer | Ultra light bar armor |
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| US8573125B1 (en) * | 2012-07-13 | 2013-11-05 | Blast Control Systems, L.L.C. | Blast control blanket |
| US20150292838A1 (en) * | 2014-04-13 | 2015-10-15 | Plasan Sasa Ltd. | Armor coupler |
| US9587914B2 (en) * | 2014-04-13 | 2017-03-07 | Plasan Sasa Ltd. | Armor coupler |
| US20160187106A1 (en) * | 2014-10-03 | 2016-06-30 | Response Solutions & Innovations, Inc. | Frame configurable for use as a ballistic shield and related methods |
| CN111776475A (en) * | 2018-02-27 | 2020-10-16 | 蓝箭航天技术有限公司 | Rocket packaging method and packaging box section preparation method |
| US11402177B2 (en) * | 2019-12-03 | 2022-08-02 | Michael Cohen | Composite grid/slat-armor |
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Legal Events
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Owner name: AMSAFE BRIDPORT LIMITED, UNITED KINGDOM Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:ANDREWARTHA, MICHAEL I.;STEWART, DOUGLAS J.;SIGNING DATES FROM 20110620 TO 20110621;REEL/FRAME:026490/0251 |
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| AS | Assignment |
Owner name: ARES CAPITAL CORPORATION, AS ADMINISTRATIVE AGENT, Free format text: SECURITY AGREEMENT;ASSIGNORS:AMSAFE, INC.;AMSAFE COMMERCIAL PRODUCTS. INC.;AMSAFE AVIATION, INC.;REEL/FRAME:026637/0591 Effective date: 20110722 |
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Owner name: AMSAFE AVIATION, INC., GEORGIA Free format text: TERMINATION AND SECURITY RELEASE;ASSIGNOR:ARES CAPITAL CORPORATION;REEL/FRAME:027830/0048 Effective date: 20120215 Owner name: AMSAFE, INC., ARIZONA Free format text: TERMINATION AND SECURITY RELEASE;ASSIGNOR:ARES CAPITAL CORPORATION;REEL/FRAME:027830/0048 Effective date: 20120215 Owner name: AMSAFE COMMERCIAL PRODUCTS, INC., INDIANA Free format text: TERMINATION AND SECURITY RELEASE;ASSIGNOR:ARES CAPITAL CORPORATION;REEL/FRAME:027830/0048 Effective date: 20120215 |
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