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公开(公告)号：US20230213321A1
公开(公告)日：2023-07-06
申请号：US18093277
申请日：2023-01-04
发明人： Ian B. Vabnick
IPC分类号： F42B33/06
CPC分类号： F42B33/06
摘要： Disclosed is a method for rendering safe an Improvised Explosive Device (IED) via a powered mechanical press. The method includes identifying and classifying the IED and placing the IED into the press and determining a position of the IED within the press based on the classification of the IED. The method further includes activating the press until a fracturing device of the press reaches a fracture position with respect to the IED and holding the position of the press for a predetermined period of time when the fracturing device reaches the fracture position. Further, the method includes removing, after the IED has fractured, the fractured IED and explosive filler of the fractured IED.
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公开(公告)号：US10794660B2
公开(公告)日：2020-10-06
申请号：US16366487
申请日：2019-03-27
发明人： Ian B. Vabnick
摘要： Provided herein are fluid jet enhancement adapters for use with a propellant driven disrupter, and more particularly muzzle blast suppressor. The fluid jet enhancement muzzle blast suppressor may comprise a suppressor bore extending between the proximal end and the distal end with an inner suppressor surface that defines the suppressor bore. An outer suppressor surface opposably faces the inner suppressor surface, with a suppressor chamber positioned between the inner and outer suppressor surfaces. A plurality of passages connect the suppressor bore with the suppressor chamber, wherein the plurality of passages are sized to allow gas to move from the suppressor bore to the suppressor chamber and minimize liquid movement from the suppressor bore to the suppressor chamber.
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公开(公告)号：US10760872B2
公开(公告)日：2020-09-01
申请号：US16570589
申请日：2019-09-13
发明人： Ian B. Vabnick
摘要： Provided herein are fluid jet enhancement adapters for use with a propellant driven disrupter. The adapter may comprise: a first end operably connected to a muzzle end of a propellant driven disrupter barrel and a second end, wherein a longitudinal region extends between the first end and the second end. The longitudinal region has: a longitudinal region inner surface that defines a longitudinal region lumen; a longitudinal region outer surface opposably facing the longitudinal region inner surface, with a longitudinal region wall having a wall thickness that separates the longitudinal region inner surface from the longitudinal region outer surface. The longitudinal region lumen has a first end inner diameter that is substantially equivalent to a muzzle inner diameter. The longitudinal region wall forms a continuous surface that radially isolates the longitudinal region lumen from a surrounding environment.
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公开(公告)号：US20230258443A1
公开(公告)日：2023-08-17
申请号：US18109438
申请日：2023-02-14
发明人： Ian B. Vabnick , Phillip R. Quillen
CPC分类号： F42D5/04 , B30B1/007 , B30B15/065 , B30B15/04
摘要： A press device having a cradle, a base plate, a fracturing device, an actuator, a switch, and a body. The base plate is located at a first end of the cradle. The fracturing device is proximally located at a second end of the cradle. The cradle is adapted to work in communication with the base plate to maintain alignment between the baseplate and the fracturing device. The actuator is proximally located to the second end of the cradle. The switch is operably connecting the actuator to the fracturing device. The body holds the cradle, base plate, fracturing device, actuator driven ram, and switch. The preferred embodiment uses a hydraulic ram.
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公开(公告)号：US10921089B1
公开(公告)日：2021-02-16
申请号：US16853362
申请日：2020-04-20
摘要： Provided herein are shaped charges for focusing a fluid mass and related methods of using the shaped charges for disruption of an explosive target. The shaped charge comprises a plastic shell having a special geometric shape configured to support a shape-conforming explosive. A cylindrical plastic body has an interior volume for containing a fluid and the plastic shell. The plastic body closed distal end has a geometric shape that is substantially matched to the shape of the plastic shell.
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公开(公告)号：US10451378B2
公开(公告)日：2019-10-22
申请号：US15896760
申请日：2018-02-14
摘要： Provided herein are fluid jet enhancement adapters for use with a propellant driven disrupter. The adapter may comprise: a first end operably connected to a muzzle end of a propellant driven disrupter barrel and a second end, wherein a longitudinal region extends between the first end and the second end. The longitudinal region has: a longitudinal region inner surface that defines a longitudinal region lumen; a longitudinal region outer surface opposably facing the longitudinal region inner surface, with a longitudinal region wall having a wall thickness that separates the longitudinal region inner surface from the longitudinal region outer surface. The longitudinal region lumen has a first end inner diameter that is substantially equivalent to a muzzle inner diameter. The longitudinal region wall forms a continuous surface that radially isolates the longitudinal region lumen from a surrounding environment.
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公开(公告)号：US09470490B2
公开(公告)日：2016-10-18
申请号：US14192976
申请日：2014-02-28
发明人： Ian B. Vabnick , Jeffrey T. Curtis
CPC分类号： F42B8/28 , G09B5/02 , G09B9/003 , G09B19/003
摘要： The present invention relates to a hot-wire detonator emulator that has the capability of monitoring switching in a simulated, mock, or inert improvised explosive device (IED) powered by direct current. One purpose of the inventive emulator is to function as an energetic witness substitute by replacing the detonator in an actual IED, thus enabling bomb technicians to conduct bench top and field analyses of IEDs, and to assess the effectiveness of render-safe procedures by, for example, illustrating how a detonator would react in a render-safe procedure.
摘要翻译： 本发明涉及一种热线雷管仿真器，其具有监控由直流电驱动的模拟，模拟或惰性简易爆炸装置（IED）中的切换的能力。 本发明的仿真器的一个目的是通过在实际的IED中替换雷管来充当活力的证人，从而使炸弹技术人员能够对IED进行台面和现场分析，并评估渲染安全程序的有效性 例如，说明雷管如何在渲染安全的过程中作出反应。
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公开(公告)号：US11898830B2
公开(公告)日：2024-02-13
申请号：US17862940
申请日：2022-07-12
发明人： Ian B. Vabnick
CPC分类号： F42B33/06 , F41A21/02 , F42B12/745 , F42B12/76
摘要： Provided are methods and related devices for disrupting an explosive device using a propellant driven disrupter (PDD) that propels a rounded projectile (RP) toward an explosive device. The RP travels along a linear trajectory and impacts the target, including a barrier portion of the explosive device. The impacting between the RP and barrier forms a composite projectile via a solid state weld between a portion of the barrier and the RP distal end, thereby minimizing or avoiding spall and fragment generation into the explosive device. The projectile traverses a penetration distance along the linear trajectory, or a defined-angle relative thereto, to disrupt the explosive device without unwanted explosive detonation.
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公开(公告)号：US11274908B2
公开(公告)日：2022-03-15
申请号：US16209643
申请日：2018-12-04
发明人： Ian B. Vabnick
摘要： Provided herein are penetrator projectiles for use with explosive ordnance disposal disrupters, and related methods of making and using. The penetrator projectile has a tip, neck, shaft and base, wherein the geometry and composition of the different elements are selected to ensure the projectile is ballistically stable after firing to provide improved free-flight characteristics and corresponding explosive ordnance disruption.
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公开(公告)号：US11262155B2
公开(公告)日：2022-03-01
申请号：US16987942
申请日：2020-08-07
发明人： Ian B. Vabnick
摘要： A propellant driven disrupter (PDD) for disrupting an explosive target, comprising: a disrupter barrel having a breech and muzzle end; a projectile liquid or gas positioned in the barrel and extending a longitudinal distance in the disrupter barrel. The projectile liquid distal end is located farthest from the disrupter barrel breech end. A jet stabilizing projectile (JSP) is at least partially positioned in the barrel and operably contacts the projectile liquid distal end. The JSP has a JSP proximal end facing toward the disrupter barrel breech end and a distal end opposed to the JSP proximal end, wherein some or all of the JSP is positioned in the barrel. The PDD may contain the JSP, with an air region between the JSP distal end and the muzzle end, or an air region in an adapter that is connected to the muzzle end. Also provided are JSP's having improved flight stability for use with liquid or air-filled disrupters and methods of disrupting a target.
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