Patent Application: US-201515315832-A

Abstract:
an explosive device composed of : a flux compression generator operative to produce a high intensity electric current when activated ; and an electrical payload connected to the generator and constructed to receive the high intensity electric current and cause energy in the current to generate a plate or shaped projectile in the payload and to launch the projectiles into an explosive or insensitive reactive material target for the purpose of initiating the reactive material at single or multiple points .

Description:
the basic components of an explosive device for powering electrical initiators according to the invention are shown in fig1 . the device includes a flux compression generator , electrical loads composed of initiators either of kinetic energy or hot wire types , a means to detonate the high explosives of the fcg , a means to distribute electrical energy to various initiators through a switching network , and an electronic unit to produce starting seed current for the generator . as shown in fig1 , the fcg portion of the system has an electrically conducting armature 1 , an outer stator 2 that includes helical wire windings and a coaxial section 3 , an input end plate 4 , an input insulated channel 5 , an output end plate 6 , and an output insulated channel 7 . channels 5 and 7 may be insulated with mylar or kapton material . armature 1 , stator 2 , end plate 4 , and end plate 6 form a cavity 8 that represents the inductance of the fcg . armature 1 is filled with conventional explosives 9 . detonator 10 is used to initiate and detonate explosives 9 . power to activate detonator 10 is supplied by the combined action of a thermal battery 11 and a storage capacitor 12 . the fcg provides electrical current and voltage to initiate insensitive explosive or reactive material fill 13 . the initiation system for insensitive explosive fill 13 includes a detonator 14 as a single point , an axial detonator array 15 , or peripheral detonator array 16 . detonator 14 and / or axial detonator array 15 and / or a peripheral detonator array 16 are connected to the fcg through a switching network 17 . fig2 is a circuit diagram of an external power source that generates seed current to power the fcg . the circuit has a low level power source 20 , switch 21 connected in series between power source 20 a thermal battery 11 , a resistor 22 connected in parallel with battery 11 , a capacitor 12 connected in parallel with resistor 22 , output switch 23 connected in series with output lead 24 , which is connected to armature 1 , and return lead 25 connected to stator 2 . a crowbar switch is formed by the input end of armature 1 and inner edge of input endplate 4 , due to their proximity and is open initially as insulated channel 5 . the function of this element will be described in further detail below . fig3 is a diagram of a circuit that switches fcg output current to initiators or detonators in the main explosive fill . an fcg output lead 30 is connected to armature 1 , and a return lead 31 is connected to stator 2 . a single point initiator solenoid switch 32 , axial array initiator solenoid switch 33 , and peripheral array initiator solenoid switch 34 are each connected between output lead 30 and corresponding detonators . the solenoid switches are actuated by solenoids driven by current supplied by respective ones of power lead 35 for solenoid switch 32 , power lead 36 for solenoid switch 33 , and power lead 37 for solenoid switch 34 . a selected one of switches 32 - 34 will be actuated by a manual command . fig4 ( a ) and ( b ) illustrate the components of a slapper detonator that may be used as detonator 10 or detonator 14 , 15 , or 16 . a thin metallic foil 40 and mylar film 41 are sandwiched between backing material 42 and frontal material 43 . within the frontal material 43 is a cylindrical cavity 44 that functions as a gun barrel . if this slapper detonator is used as detonator 10 , then leads 46 and 47 will be connected across a series arrangement of a capacitor and a switch , and secondary explosive 45 will correspond to secondary explosive 9 of fig1 . if this slapper detonator is used as detonator 14 , 15 , or 16 , electrical lead 46 connects one side of the detonator to the output of the armature 1 , while electrical lead 47 connects the other side of the detonator to the output end of the fcg stator 2 . the current through foil 40 resulting from detonation of explosive 9 causes metallic foil 40 to explode , creating a cavity 48 , and mylar film 41 is converted into a projectile 49 . secondary explosives 45 may be contained within , and in one embodiment may be an integral part of , the slapper detonator and will initiate secondary explosive 13 of fig1 . alternatively , secondary explosives 45 need not be an integral part of the slapper detonator if this slapper detonator is used as detonator 14 , 15 , or 16 , and electrically connected to output ends of fcg armature 1 and stator 2 , then explosives 45 may be the tertiary or insensitive reactive materials 13 of fig1 . fig5 ( a ) and ( b ) show components of another detonator according to the invention in the form of a flyer plate initiator . in this embodiment , a washer liner 50 is positioned between a central electrode 51 and a confinement stator 52 . the central electrode 51 , washer liner 50 and stator 52 form an electrical path about insulated channel 53 . the electrical insulation material may be mylar or kapton . an electrical lead 54 connects to the output end of armature 1 , while electrical lead 55 connects to the output end of stator 2 . current flow about cavity 53 and through central electrode 51 , washer liner 50 , and stator 52 causes washer liner 50 to form a flying plate in the form of washer projectile 56 and creates expansion cavity 57 . fig6 ( a ) and ( b ) illustrate formation of a jet initiator according to the invention . a shaped charge liner 60 is sandwiched between a central electrode 61 and an outer stator 62 . the central electrode 61 , shaped charge liner 60 , and stator 62 form an electrical path about insulated channel 63 . an electrical lead 64 is connected to the output end of fcg armature 1 and an electrical lead 65 is connected to the output end of fcg stator 2 . passage of current through central electrode 61 , shaped charge liner 60 , and stator 62 implodes liner 60 toward the device axis . shaped charge liner 60 is shown in fig6 ( b ) midway through the collapse process as liner 67 produces the formation of jet initiator 68 . fig7 is a detail of a hot wire initiator . components include a heating element 70 , base or casing 71 , an electrical lead 72 connecting to the output end of armature 1 , and an electrical lead 73 connecting to the output end of stator 2 . the embodiments shown in fig5 and 7 may be used as detonators 14 , 15 , or 16 to detonate either secondary or insensitive ( tertiary ) explosives . shown in fig8 is a schematic diagram of a possible initiating system according to the invention . the system consists of two sections , i . e ., one exterior to the self contained munition ( the console used by the gunner ), and a second system placed within the self contained munition . the gunner console has a switch used by the gunner to power the system into a ready mode . it also has a means for the gunner to select the initiation mode , being in this example , either single point , axial , or peripheral . a third means is provided to launch the weapon by gunner command to the munition launch system . within the self contained munition are placed a low level power supply , safe and arm mechanism or circuit , onboard safe condition verification module , munition proximity or contact switch , thermal battery / capacitor as a power generating source for seed current , initiator or detonator for the fcg explosives , a fcg , switching network , an insensitive reactive material / explosive filled munition , and initiators or detonators distributed throughout the explosives or reactive materials of the munition . in operation , a sequence of events begins with the gunner switch being switched to the “ on ” position . this switch closure signals the low - level power supply to furnish power to the various components within the self - contained munition . thereafter , the gunner sets initiation mode select switch to one of the three settings provided in this example . the final function of the gunner and exterior console is to activate the switch to launch the weapon . launch of the weapon separates the command system from the munition physically and electrically . during munition launch , sensors aboard the munition validate that a proper launch has taken place and send a verification signal to the electronic safe and arm module . after the munition has reached a safe distance from the gunner and verification has taken place , the safe and arm ( s & amp ; a ) places the munition in the “ armed ” condition . the arming readies all circuits to function on a proper signal to detonate the munition , which comes from the proximity or contact switch . closing of the contact switch instructs the s & amp ; a device to apply low - level power to ignite the thermal battery . action of the thermal battery in time charges the capacitor . then , the capacitor discharge into the fcg develops a seed current passing through the conductors of the fcg and seed magnet field in the fcg cavity by virtue of the current flow . subsequently , an electrical pulse is delivered to the fcg detonator to initiate the fcg explosives . upon detonation of the fcg , according to fig1 , under the force of detonating fcg explosives 9 , the input end of armature 1 initially travels radially across input gap 5 , cuts through the insulation of gap 5 , and makes electrical contact with input end plate 4 . this action constitutes the function of a “ crowbar ” switch as known in the fcg art . the action of the crowbar switch cuts out the external power generating seed current circuit from the generator at the beginning of its function . during further expansion of armature 1 , the input end of armature 1 slides with electrical contact along input end cap 4 until it reaches the input end of stator 2 . armature 1 makes successive contact , first with the input end of outer stator 2 and ultimately with the coaxial stator section 3 of stator 2 . the action of armature 2 is to reduce the volume of fcg cavity 8 , do work against the magnetic pressure contained within cavity 8 , and amplify the current flowing through armature 1 , end plate 6 , load initiator ( s ), 14 , 15 or 16 , and allow the current to return to the armature through the stator 2 and input end plate 4 . the high level of current generated by the fcg and being applied to the initiators causes the initiators to function , which in turn initiates or detonates the insensitive explosives or reactive material 13 at the location of the single point initiator 14 , or along the axis of axial initiator array 15 , or at peripheral initiator array 16 , for example . mode switch 17 routes current produced by the fcg to the desired initiator ( s ). according to one example , solenoid switch 32 would be closed to cause single point initiator 14 to operate , while solenoid switch 33 or solenoid switch 34 would actuate axial initiator array 15 or peripheral initiator array 16 , respectively . all solenoids or any one or any combination thereof could be activated to produce a multiplicity of initiator array function . the initiators function in response to fcg output current flowing through their various components . for example , in fig4 , metallic foil 40 explodes using the exploding wire phenomenon , wherein passage of current through the metallic foil 40 via electrical leads 46 and 47 causes the foil &# 39 ; s temperature to increase beyond the vapor phase in response to rapid joule heating . the phase change causes expansion , which in turn , attempts to accelerate backing material 42 and frontal confinement 43 . since a portion of mylar film 41 is not confined by virtue of its presence at cylindrical cavity 44 , projectile 49 is formed by shearing out of mylar film 41 and is propelled to extremely high velocity . upon impact , projectile 49 has sufficient energy to initiate secondary explosives 45 of the slapper detonator while the output of the secondary explosives 45 can be sufficient to initiate insensitive explosives 13 . the function of the flying plate technique , according to the invention , is shown in fig5 . flow of fcg output current through electrical leads 54 and 55 , passes through central electrode 51 , washer liner 50 , stator 52 , and returns through electrical lead 55 . the action of current flowing in this circuit creates a very high magnetic field within the insulated channel 53 . interaction of the field and current produces an accelerating lorentz force on washer liner 50 within an expanding cavity 57 . upon exit from the device body , washer liner 50 converts into flying plate 56 , which impacts insensitive reactive material 13 ( fig1 ) with sufficiently large mass and high velocity to initiate detonation of such material . the cross section of the flying plate liner can be of varied shape to include conic sections , trumpet , hemispherical cap , or freely formed depending on the desired structure of the flying plate to be formed . fig6 shows shaped charge liner 60 wherein electrical current from the fcg through electrical lead 64 is passed about insulated channel 63 and through the central electrode 61 , through the liner 60 , through stator 62 , and returned to the fcg through electrical lead 65 . the current flow establishes a magnetic field whereby lorentz forces accelerate liner 60 toward the device axis passing through cavity 66 . as liner 60 strikes the axis some of its material flows forward to form jet penetrator 68 . jet penetrator 68 has high velocity and relatively high mass that provides a means to initiate insensitive reacting materials 13 . the jet can have great length ; therefore impact pressure can be sustained over a relative long time to assure initiation of insensitive reacting materials . the shaped charge liner 60 cross - section can have varied shape to include conic sections , tulip , trumpet , or be freely varied depending on the formed penetrator structure desired . the hot wire initiator consists of a resistive element 70 , base or encasement 71 , and electrical leads 72 and 73 to provide electrical current to the resistive element 70 . the element can be a coil of finely stretched metal such as tungsten or a solid section of high electrical resistance metal like nichrome . when large currents are passed through the resistive element , its temperature rises by joule heating . in application , the resistive element 70 is in contact with or embedded in insensitive reactive material 13 . the temperature is sufficiently high to cause ignition or initiation of the insensitive reactive material . exemplary materials for the above described components may include conducting metals such as copper or aluminum for armature 1 , wires for stator 2 , coaxial section 3 , and input and output end plates 4 and 6 . for the initiators , copper , aluminum , tungsten or any electrically conducting metal can be used for flying plate liner 50 , central electrode 51 , stator 52 , shaped charge liner 60 , central electrode 61 , and stator 62 , for example . typically , conventional primary explosive fills for the fcg explosives 9 can be tnt , comp b , octol or hmx based plastic bonded explosives ( pbxs ). the initiation system addresses insensitive materials such as tatb ( triaminotrinitrobenzene ) and derivatives based on tatb . the presently disclosed embodiments are therefore to be considered in all respects as illustrative and not restrictive , the scope of the invention being indicated by the appended claims , rather than the foregoing description , and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein . 5 . mil - std - 1316e , fuze design , safety criteria for dod , 10 jul . 1998 . 6 . t . r . gibbs and a . popolato , eds ., lasl explosive property data , university of california press , berkley , c a , 1980 . 8 . t . p . weihs , johns hopkins university , woodhead publishing limited , chapter 5 , p . 160 , 2014 . 9 . j . s . foster , jr ., u . s . pat . no . 4 , 370 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