Patent Application
20130104765
Embodiments of the present invention relate generally to explosively formed projectiles. More particularly, embodiments of the present invention relate to explosively formed projectiles, devices for generating explosively formed projectiles including reactive materials and reactive material configurations suitable for increasing the velocity of explosively formed projectiles.
Explosively formed projectiles (“EFP”) (also known as explosively formed penetrators, and explosively formed perforators) are provided by so-called “shaped charges” which utilize explosive energy to deform a liner disposed over a concave-shaped explosive material into a coherent projectile while simultaneously accelerating it to extremely high velocities. An EFP offers a method of employing a kinetic energy projectile without the use of a large gun. A conventional EFP device is comprised of a metallic liner, a case, an explosive material, and an initiator. The case may also contain a retaining ring to position and hold the liner-explosive subassembly in place. EFP devices are normally designed to produce a single massive, high velocity projectile that has a high kinetic energy capable of penetrating solid objects, such as, for example, a target in the form of an armored vehicle or a subterranean formation. Upon detonation, the explosive material creates enormous pressures that accelerate the liner while simultaneously reshaping it into a projectile of a rod-like or other desired shape. On impact with a target, the EFP delivers a high mechanical power in an extremely focused manner, enabling penetration of target materials which are impervious to conventional explosives.
The liner of the EFP device is formed from a solid material that is formed into a projectile responsive to detonation of the explosive charge. The liner material is typically a high-density, ductile material, such as a metal, a metal alloy, a ceramic, or a glass. The metals commonly used in liners include iron, copper, aluminum, molybdenum, depleted uranium, tungsten, and tantalum. Depending on the mechanical strength characteristics of the target, penetration by the liner may heavily damage or destroy the target in the vicinity of impaction by the projectile formed from the liner. However, if the target is an armored vehicle or other heavily armored target, the liner may not cause the desired degree of damage. The destructive capability of the EFP may be limited by the geometry and weight of the projectile formed from the liner by the EFP device and the velocity imparted to the projectile by the detonation of the explosive material. Further, aerodynamic drag will generally act to decrease the velocity of projectile as the projectile travels toward the target.
In some applications, in order to improve the destructive capability of the warhead, the liner may be provided with the ability to produce secondary reactions that cause additional damage. These secondary reactions commonly include incendiary reactions. As disclosed in U.S. Pat. No. 4,807,795 to LaRocca et al., pyrophoric metals are added to the liner to provide the desired incendiary effects. In LaRocca et al., a double-layered liner is disclosed, where a layer of dense metal provides the penetration ability and a layer of light metal, such as aluminum or magnesium, produces the incendiary effects.
While metals have been commonly used in liners, reactive materials have also been used. Upon impact with a target, the reactive material of the liner produces a high burst of energy. Such reactive materials for use in penetrating warheads are disclosed, for example, in U.S. Pat, No. 6,962,634, issued Nov. 8, 2005, entitled “Low Temperature, Extrudable, High Density Reactive Materials” and assigned to the assignee of the present invention, the entire disclosure of which patent is incorporated herein by this reference.
In accordance with some embodiments of the present invention, a liner assembly for an explosively formed projectile device may include a reactive material liner comprising a reactive material and a primary liner. The primary liner may be configured to, upon initiation of an explosive material used to form an explosively formed projectile, deform into an outer portion of the projectile at least partially surrounding a portion of the reactive material liner. At least a portion of the reactive material liner may be configured and formulated to increase a velocity of the projectile in excess of a velocity generated by the explosive material.
In additional embodiments, the present invention includes an ordnance device for generating an explosively formed projectile including a case, an explosive material at least partially disposed within the case, a reactive material liner comprising a reactive material at least partially disposed within the case, and a primary liner at least partially disposed within the case and abutting at least a portion of a surface of the reactive material liner. The primary liner may be configured to deform into an outer portion of a projectile at least partially surrounding a portion of the reactive material liner after being expelled from the case responsive to initiation of the explosive material. At least a portion of the reactive material liner may be configured and formulated to increase a velocity of the projectile in excess of a velocity generated by the explosive material.
In yet additional embodiments, the present invention includes an explosively formed projectile including a deformed primary liner substantially forming an outer portion of the projectile and a deformed reactive material liner at least partially disposed within the deformed primary liner. An ignited portion of the deformed reactive material liner may increase a velocity of the projectile in excess of a velocity generated by an explosive material used to form the projectile.
In yet additional embodiments, the present invention includes a method of configuring an explosively formed projectile device including arranging an explosive material at least partially within a case, arranging a reactive material liner at least partially on the explosive material, and arranging a primary liner at least partially on the reactive material liner. The method further includes configuring the primary liner and the reactive material liner to form a explosively formed projectile, configuring and formulating a portion of the reactive material liner to ignite when the reactive material liner is explosively expelled from the case, and configuring the ignited portion of the reactive material liner to increase the velocity of the explosively formed projectile after the forming explosively formed projectile is explosively expelled from the case.
In yet additional embodiments, the present invention includes a method of explosively forming a projectile including explosively expelling a primary liner and a secondary liner from a case, deforming the primary liner to at least partially surround a portion of the secondary liner, and increasing a velocity of the projectile by combusting at least a portion of the secondary liner.
While the specification concludes with claims particularly pointing out and distinctly claiming that which is regarded as the present invention, the advantages of this invention may be more readily ascertained from the following description of embodiments of the invention when read in conjunction with the accompanying drawings in which:
The illustrations presented herein are not meant to be actual views of any particular material, apparatus, system, or method, but are merely idealized representations which are employed to describe embodiments of the present invention. Additionally, elements common between figures may retain the same numerical designation.
An embodiment of an ordnance device such as a device for generating an EFP, which may be termed an “EFP device” 100 is illustrated in
At least a portion of the case 102 may be filled with the explosive material 106. The explosive material 106 may be formed within the interior of the case 102 and may comprise an explosive material 106 such as polymer-bonded explosives (“PBX”), LX-14, C-4, OCTOL, trinitrotoluene (“TNT”); cyclo-1,3,5-trimethylene-2,4,6 trinitramine (“RDX”); cyclotetramethylene tetranitramine (“HMX”); hexanitrohexaazaisowurtzitane (“CL 20”), C-4, combinations thereof, or any other suitable explosive material. In some embodiments, the explosive material 106 may also be formed to have a countersunk recess in a forward surface of the explosive material 106 to receive the placement of a liner or liners. As used herein, the term “forward surface” is meant to describe the surface of the material or liner that faces the open end of the case 102 from which a forming projectile is expelled. The case 102 may also include a detonator such as the initiator 104 located, for example, at the rear surface of the case 102. The initiator 104 may comprise any known detonation device sufficient to detonate the explosive material 106 within the case 102 including, but not limited to, explosives such as pentaerythritol tetranitrate (“PETN”), PBXN-5, CH-6, blasting caps, and electronic detonators (e.g., exploding foil initiators).
As shown in
In some embodiments, the reactive material liner 110 may include reactive materials including, for example, at least one fuel and, optionally, an oxidizer. In some embodiments, the reactive material utilized in the reactive material liner 110 may include two or more components selected from a fuel, an oxidizer, and a class 1.1 explosive. Binders, polymers, plasticizers, and matrix materials may also be incorporated with various embodiments of the invention as part of the reactive materials or as support structures for the reactive materials. In addition, the reactive material may include an ignition initiator suitable for igniting or initiating combustion of the reactive material.
Fuels that may be used to form reactive materials according to embodiments of the invention may include, but are not limited to, metals, fusible metal alloys, organic fuels, and mixtures thereof. Suitable metals that may be used as fuels in reactive materials include metals such as, for example, hafnium, tantalum, nickel, zinc, tin, silicon, palladium, bismuth, iron, copper, phosphorous, aluminum, tungsten, zirconium, magnesium, boron, titanium, sulfur, magnalium, and mixtures thereof An organic fuel that may be incorporated into the reactive materials may include, but is not limited to, a mixture of phenolphthalein and hexamine cobalt(III)nitrate (HACN). Fusible metal alloys may include an alloy of a metal selected from the group of gallium, bismuth, lead, tin, cadmium, indium, mercury, antimony, copper, gold, silver, and zinc.
The reactive materials according to embodiments of the invention may also include oxidizers mixed with one or more fuels or with class 1.1 explosives. Oxidizers that may be used to form reactive materials according to embodiments of the invention may include, but are not limited to, inorganic oxidizers, sulfur, fluoropolymers, and mixtures thereof For example, an oxidizer may include ammonium perchlorate, potassium perchlorate, potassium nitrate, strontium nitrate, basic copper nitrate, ammonium nitrate, cupric oxide, tungsten oxides, silicon dioxide, manganese dioxide, molybdenum trioxide, bismuth oxides, iron oxide, molybdenum trioxide, hafnium oxide, zirconium oxide, polytetrafluoroethylene, thermoplastic terpolymers of tetrafluoroethylene, hexafluoropropylene, vinylidene fluoride (THV), copolymers of vinylidenefluoride-hexafluoropropylene, and mixtures thereof.
The reactive material may, optionally, include a class 1.1, detonable energetic material, such as a nitramine or a nitrocarbon. The energetic material may include, but is not limited to, trinitrotoluene (“TNT”); cyclo-1,3,5-trimethylene-2,4,6 trinitramine (“RDX”); cyclotetramethylene tetranitramine (“HMX”); hexanitrohexaazaisowurtzitane (“CL 20”); 4,10 dinitro 2,6,8,12 tetraoxa 4,10 diazatetracyclo [5.5.0.0 5,9.0 3,11] dodecane (“TEX”); 1,3,3 trinitroazetine (“TNAZ”); ammonium dinitramide (“ADN”); 2,4,6 trinitro 1,3,5 benzenetriamine (“TATB”); dinitrotoluene (“DNT”); dinitroanisole (“DNAN”); or combinations thereof.
Reactive materials according to embodiments of the invention may also include binder materials. The binder, if present, may be a curable organic binder, a thermoplastic fluorinated binder, a non-fluorinated organic binder, a fusible metal alloy, an epoxy resin, silicone, nylon, or combinations thereof. The binder may be a high-strength, inert material including, but not limited to, polyurethane, epoxy, silicone, or a fluoropolymer. Alternatively, the binder may be an energetic material, such as glycidyl azide polymer (“GAP”) polyol. The binder may enable the reactive material to be pressed, cast, or extruded into a desired shape. The thermoplastic fluorinated binder may include, but is not limited to, polytetrafluoroethylene (“PTFE”); a thermoplastic terpolymer of tetrafluoroethylene, hexafluoropropylene, and vinylidene fluoride (“THV”); perfluorosuccinyl polyether di-alcohol; a fluoroelastomer; or combinations thereof
The reactive materials used according to embodiments of the invention may, optionally, include ignition initiators which are suitable for igniting the reactive materials after the reactive material liner 110 has been explosively expelled from the case 102. The ignition initiators may be formed or mixed with the reactive materials or may be a distinct, separate material from the reactive material. The ignition initiator may be optional because the reactive material may ignite on launch due to external forces such as an explosive shockwave formed by the detonation of the explosive material 106 or the reactive material may ignite due to aerodynamic heating of the reactive material in contact with air. Ignition initiators according to embodiments of the invention include materials that are capable of producing sufficient thermal activity to ignite the reactive materials. For example, the ignition initiators may include reactive powders, electrical wires, or reactive foils. Ignition initiators incorporated with a reactive material of particular embodiments of the invention may be activated, releasing thermal energy which ignites the reactive materials.
In other embodiments of the invention, an ignition initiator is mixed or blended with a reactive material. For example, a reactive powder suitable as an ignition initiator may be mixed with components used to form a reactive material, such as with a fuel or oxidizer. Examples of reactive powders suitable as ignition initiators include a metal powder in combination with an oxidizer. The metal powder may include, but is not limited to, zirconium, aluminum, hafnium, titanium, nickel, iron, boron, silicon, tin, zinc, tungsten, copper, or combinations thereof. The oxidizer may be potassium perchlorate, potassium nitrate, bismuth oxide, hafnium oxide, iron oxide, an alkali metal nitrate, a fluoropolymer, or combinations thereof Each of the metal powder and the oxidizer may have a small particle size, such as less than approximately 20 μm. If faster rates of reactions or burn rates are desired, the metal powder and the oxidizer may have a particle size on the order of several nanometers.
Other reactive materials, binders, polymers, plasticizers, and ignition initiators that may be incorporated with the reactive materials according to embodiments of the invention may include those materials disclosed in the following United States Patents and Patent Applications, the disclosure of each of which is incorporated herein by reference in its entirety: U.S. Pat. No. 6,593,410; U.S. Pat. No. 6,962,634; U.S. patent application Ser. No. 11/079,925, entitled “Reactive Material Enhanced Projectiles and Related Methods,” filed Mar. 14, 2005; U.S. patent application Ser. No. 11/538,763, entitled “Reactive Material Enhanced Projectiles and Related Methods,” filed Oct. 4, 2006; U.S. patent application Ser. No. 11/512,058, entitled “Weapons and Weapon Components Incorporating Reactive Materials and Related Methods,” filed Aug. 29, 2006; U.S. patent application Ser. No. 11/620,205, entitled “Reactive Compositions Including Metal” filed on Jan. 5, 2007; U.S. patent application Ser. No. 11/690,016, entitled “Reactive Material Compositions, Shot Shells Including Reactive Materials, and A Method Of Producing Same,” filed Mar. 22, 2007; U.S. patent application Ser. No. 11/697,005, entitled “Consumable Reactive Material Fragments, Ordnance Incorporating Structures for Producing the Same, and Methods of Creating the Same,” filed Apr. 5, 2007; and U.S. patent application Ser. No. 12/127,627, entitled “Reactive Material Enhanced Munition Compositions and Projectiles Containing Same” filed on May 27, 2008.
Referring again to
In some embodiments, the thickness of the liners 108 and 110 may be utilized to determine the geometry and size and the projectile 101 (
In order to retain the explosive material 106 and the primary liner 108 and the reactive material liner 110 at least partially within the case 102, the explosive material 106, the primary liner 108, and the reactive material liner 110 may be mounted together physically, for example, by a retaining ring disposed around and fixed to the open end of the case 102. In some embodiments, the explosive material 106, the primary liner 108, and the reactive material liner 110 may be held together by an adhesive, by another mechanical attachment, or by a combination of adhesive and mechanical attachments.
Referring now to
An example of a projectile 101 formed by the EFP device 100 is shown in
The pressure volume energy delivered to the primary liner 108 and the reactive material liner 110 deforms the liners 108 and 110 into a projectile shape such as the substantially elongated shape shown in
In some embodiments, the reactive material liner 110 may also be ignited as the primary liner 108 and the reactive material liner 110 are expelled from the case 102. For example, the reactive material liner 110 may be ignited by the shockwave created by the detonation of the explosive material 106. As the projectile 101 is formed, the reactive material liner 110 may start to combust. As discussed above, the reactive material utilized in the reactive material liner 110 may be formulated to provide a desired rate of reaction or “burn rate” and may also, in some embodiments, contain an ignition initiator to facilitate the ignition of the reactive material. The combustion of the reactive material liner 110 may form a propellant generated thrust such as a propulsive jet 118 shown in
The thrust produced by the reactive material in the reactive material liner 110 may increase the velocity of the projectile 101 during the flight of the projectile 101 after it has been expelled from the case 102 at an initial velocity and before the projectile 101 impacts a target. For example, an EFP device 100 may be formed to produce a projectile 101 having an initial velocity of 2.2 km/s. That is, the ignition of the explosive material 106 may form a projectile 101 from the primary liner 108 and the reactive material liner 110 and propel the liners 108 and 110 toward a target at an initial velocity of 2.2 km/s. As will be appreciated by one with ordinary skill in the art, aerodynamic drag will reduce the initial velocity of the projectile 101 as the projectile 101 travels toward the target. In some embodiments, the thrust produced by the ignition of the reactive material may increase the velocity of projectile 101 ten to forty percent (10% to 40%) higher than the initial velocity provided by the pressure volume energy imparted to liners 108 and 110. By way of example and not limitation, the ignition of the reactive material liner 110 may further increase the velocity of the explosively formed projectile 101 to a velocity of 2.75 km/s (i.e., approximately a 25% increase in velocity). The higher velocity of the projectile 101 may increase the range and destructive capability of the projectile 101 such as perforation capability and behind-armor debris effects. Additionally, upon impact with the target, any reactive material of the reactive material liner 110 that has not been burned to propel the projectile 101 may produce a high burst of energy, further increasing the destructive capability of the projectile 101. It is noted that while the embodiment shown and described with reference to
An additional embodiment of the present invention is shown in
As shown in
Similar in manner to performance of the previously described EFP device 100, the reactive material liner 210 may also be ignited as the primary liner 208, the reactive material liner 210, and the control liner 212 are expelled from the case 202. In some embodiments, the control liner 212 may control the rate of reaction of the reactive material in the reactive material liner 210. For example, the control liner 212 may mitigate or reduce the shock pressure imparted to reactive material liner 210 from the detonation of explosive material 206 and may decrease the combustion rate of the reactive material ignited by the shockwave impulse. In some embodiments, the control liner 212 may decrease the size of the propulsive jet 218 formed by the combustion of the reactive material of the reactive material liner 210 at the posterior portion 224 of the projectile 210. The shape, size, and thickness of the control liner 212 formed in the case 201 may be varied to control the size of the propulsive jet 218 of the projectile 201 and produce the desired velocity increase provided by the ignited reactive material following the formation of the projectile 201 .
An additional embodiment of the present invention is shown in
The EFP device 300 may further include a fourth liner comprising an additional reactive material and a fifth, buffer liner comprising a buffer material. The buffer liner 314 may comprise a material configured and formulated to separate the reactive material liner 310 and the additional reactive material liner 316. The buffer liner 314 may be formed in between the reactive material liner 310 from the additional reactive material liner 316 in the case 302. The buffer liner 314 may comprise a material such as a polymer, metal, metal alloy, ceramic, etc. In some embodiments, the buffer liner 314 may comprise a substantially inert material that will tend to not react with the reactive material liner 310. The reactive material liner 310 and the additional reactive material liner 316 may comprise the same reactive material or the reactive material liner 310 may comprise a first reactive material composition while the additional reactive material liner 316 comprises a different second reactive material composition. The additional reactive material liner 316 may comprise materials similar to the reactive material liners 110 and 210 previously described with reference to
As shown in
100421 In a manner similar to the actuation of the EFP assemblies 100 and 200, previously described with reference to
The following examples serve to explain embodiments of the present invention in more detail. These examples are not to be construed as being exhaustive or exclusive, or otherwise limiting, as to the scope of this invention.
Explosively Formed Projectile Testing using a First Epoxy Based Reactive Material and a Stereolithographic Polymer
A first velocity test was performed on an EFP device similar to the EFP device shown in
The EFP device was fabricated from a modified Selectable Lightweight Attack Munitions (SLAM) warhead manufactured by the Alliant Techsystems (ATK) Corporation of Minneapolis, Minnesota. The explosive material and liners in the SLAM warhead included a LX-14 explosive material weighing 256.9 grams formed within the case. The SLAM warhead also consisted of a primary liner and a reactive material liner. The primary liner was formed from copper having a weight of 44 grams and an average axial thickness of 0.0366 inches (0.923 millimeters). The reactive material liner was formed from a first epoxy based reactive material having a weight of 44.6 grams, a density of 6.080 g/cc, and an average axial thickness of 0.0543 inches (1.379 millimeters). The first epoxy based reactive material comprised 71.434 percent by weight tungsten (about 50.004 percent tungsten having a particle size of about 90 μm and 21.430 percent tungsten having a particle size of about 6 to 8 μm), 9.988 percent by weight potassium perchlorate, about 9.988 percent by weight zirconium and 8.590 percent by weight of an epoxy material. The epoxy material included 4.419 percent by weight Araldite® LY 1556, 3.977 percent by weight Aradur® 917, 0.023 percent by weight Accelerator DY 070 (each of which are commercially available from Huntsman Advanced Materials of Brewster, N.Y.), and 0.171 percent by weight cabosil. The control liner was formed from a sterolithographic polymer having a weight of 15.3 grams, a density of 1.12 g/cc, and an average axial thickness of 0.1000 inches (2.54 millimeters). In the test, the sterolithographic polymer was formed from a liquid photopolymer manufactured under the trade name WATERSHED™ 11120 and commercially available from the DMS SOMOS® Corporation of New Castle, Del.
The predicted velocity for the tested EFP projectile without any assist from the reactive material was 2.24 km/s. The measured velocity just prior to impact with the target measured with the high-speed digital camera was 2.68 km/s.
The results of the first velocity test on the projectile formed by the EFP device having a first epoxy based reactive material liner and a stereolithographic polymer control liner indicated that the projectile including the reactive material exhibited a velocity greater than the predicted velocity of the projectile.
Explosively Formed Projectile Testing using a Second Epoxy Based Reactive Material and a Stereolithographic Polymer
A second velocity test was performed on an EFP device similar to the EFP device shown in
The EFP device was fabricated from a SLAM warhead that included a 256.9 gram LX-14 explosive material formed in the case, a primary liner, and a reactive material liner. The primary liner was formed from copper having a weight of 44 grams and an average axial thickness of 0.0366 inches (0.923 millimeters). The reactive material liner was formed from a second epoxy based reactive material having a weight of 47.6 grams, a density of 6.552 g/cc, and an average axial thickness of 0.0504 inches (1.280 millimeters). The second epoxy based reactive material comprised 72.112 percent by weight tungsten (50.478 percent tungsten having a particle size of about 90 μm and 21.634 percent tungsten having a particle size of about 6 to 8 μm), 10.000 percent by weight nickel, 10.000 percent by weight aluminum and 7.888 percent by weight of an epoxy material. The epoxy material included 4.088 percent by weight Araldite® LY 1556, 3.680 percent by weight Aradur® 917, 0.021 percent by weight Accelerator DY 070 (each of which are commercially available from Huntsman Advanced Materials of Brewster, N.Y.), and 0.100 percent by weight cabosil. The control liner was formed from a sterolithographic polymer having a weight of 15.3 grams, a density of 1.12 g/cc, and an average axial thickness of 0.1000 inches (2.54 millimeters). In the test, the sterolithographic polymer was the same as the polymer used in Example 1.
The predicted velocity for the projectile formed by the EFP device without any assist from the reactive material is 2.19 km/s. The measured velocity just after formation of the projectile was approximately 2.20 km/s. The measured velocity at the first X-ray station was 2.72 km/s.
Similar to Example 1, the results of the second velocity test on the projectile formed by the EFP device having a second epoxy based reactive material liner and a stereolithographic polymer control liner indicated that the projectile including the reactive material exhibited a velocity greater than the predicted velocity of the projectile and exhibited a velocity greater than the measured velocity just after formation.
In view of the above, embodiments of the present invention may be particularly useful in producing EFPs enhanced by reactive materials. The ignition of the reactive material creating a propulsive jet may be used to increase the velocity of an EFP beyond the initial velocity produced by the ignition of the explosive material in the case. Conventionally, the amount of explosives in the case along with the material properties of the liners and case inhibit the amount of energy that may be delivered to the liners. The ability to increase the velocity of a projectile after the projectile has been formed with an initial velocity imparted by the explosive material will enable the projectile to obtain velocities not attainable previously in similar, but conventional, EFP device configurations. The higher velocity of the projectile may increase the range and destructive capability of the projectile such as perforation capability and the behind-armor debris effects. The ignition of the reactive material provides a relatively lower g-force acceleration of the projectile than the explosive material and may accelerate the projectile without substantially damaging or breaking up the formed projectile. Further, the combustion of the reactive material may provide a tracer effect on the projectile during its flight.
While the present invention has been described herein with respect to certain preferred embodiments, those of ordinary skill in the art will recognize and appreciate that it is not so limited. Rather, many additions, deletions and modifications to the preferred embodiments may be made without departing from the scope of the invention as hereinafter claimed, and legal equivalents. In addition, features from one embodiment may be combined with features of another embodiment while still being encompassed within the scope of the invention as contemplated by the inventors.
