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公开(公告)号：US4440296A
公开(公告)日：1984-04-03
申请号：US446936
申请日：1982-12-06
CPC分类号： F42B39/14
摘要： Propagation of detonation between pallets of munition such as artillery sls is prevented by interposing an inert material having adequate density to render the fragments from a detonating pallet non-lethal when they reach explosive devices in a neighboring pallet. The material must be of a type which does not itself form lethal fragments and the material must be placed sufficiently close to the explosive devices that the fragments from an explosive have not had time to separate into individual pieces but, instead, produce a plate impact on the material. This latter requirement reduces or eliminates the need for any substantial strength in the material.
摘要翻译： 通过插入具有足够密度的惰性材料来防止在诸如炮弹等弹药的托盘之间的爆炸传播，使碎片从引爆托盘处于非致死状态，当它们到达相邻托盘中的爆炸装置时。 材料必须是本身不形成致死碎片的材料，并且材料必须放置得足够靠近爆炸装置，使得爆炸物的碎片没有时间分离成单独的碎片，而是产生板撞击 材料。 后一种要求降低或消除了材料中任何实质强度的需要。
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公开(公告)号：US4248342A
公开(公告)日：1981-02-03
申请号：US78350
申请日：1979-09-24
CPC分类号： F42B39/14
摘要： Manufactures, apparatus and processes for shielding the hazards of explosives, pyrotechnics and propellants during manufacture, demolition, demilitarization storage, transportation and use.
摘要翻译： 在制造，拆除，非军事化储存，运输和使用过程中屏蔽爆炸物，烟火和推进剂的危害的制造，设备和工艺。
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公开(公告)号：US4114369A
公开(公告)日：1978-09-19
申请号：US794165
申请日：1977-05-05
申请人： Donald P. Crowley
发明人： Donald P. Crowley
CPC分类号： F42B39/14 , C09D5/00 , F02K9/34 , F02K9/38 , F42B39/18 , Y10S428/92 , Y10T428/2495 , Y10T428/251 , Y10T442/3415
摘要： A flexible composite sheet coating for providing cook-off protection time r rocket motors, etc., comprising intumescent material in liquid form including mica flakes sprayed in sequence onto aluminum foil and glass cloth and bonded to the wall of a rocket structure.
摘要翻译： 一种用于为火箭发动机等提供灭火保护时间的柔性复合片材涂层，其包括液体形式的膨胀材料，包括依次喷涂在铝箔和玻璃布上并结合到火箭结构壁上的云母片。
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公开(公告)号：US3738276A
公开(公告)日：1973-06-12
申请号：US3738276D
申请日：1971-11-17
申请人： US ARMY
摘要： A composite semi-liquid system for thickening halogenated organic liquids, such as Freon 113 (a registered trademark of E. I. DuPont de Nemours & Co.) to improve safety in the formulation and handling of certain highly-sensitive-to-detonation mixtures, for example, a mixture of secondary and primary explosives, or a combination of a solid sensitive oxidizer with a pyrotechnic fuel. The thickened halocarbon is used in two stages, first a selected combination of gelling agents such as Cab-O-Sil M-5 (a registered trademark of the Cabot Corporation) and Bentone 38 (a registered trademark of N. L. Industries, Inc.) is incorporated into the halocarbon and the resultant slurry is then used to desensitize the explosive by admixture. The desensitized explosive is packaged in a container which is permeable to the halocarbon vapor and this package is immersed in a vessel containing a halocarbon gel obtained by selective gellation with gellants such as Alumagel (a registered trademark of Witco Chemical Co.); this second gel provides a means for preventing a rapid escape of the liquid from the vessel if a leak occurs.
摘要翻译： 用于增稠卤化有机液体的复合半液体系统，例如Freon 113（EI DuPont de Nemours＆Co.的注册商标），以提高某些高灵敏度至爆炸混合物的配制和处理中的安全性，例如 ，次级和主要爆炸物的混合物，或固体敏感氧化剂与烟火燃料的组合。 增稠的卤化碳分两个阶段使用，首先选择凝胶剂如Cab-O-Sil M-5（Cabot Corporation的注册商标）和Bentone 38（NL Industries，Inc。的注册商标）的选定组合是 加入到卤代烃中，然后将所得的浆液用于通过混合使该炸药脱敏。 脱敏的爆炸物被包装在可渗透卤代烃蒸气的容器中，并且该包装被浸入容器中，所述容器含有通过与胶凝剂（例如Witco Chemical Co.的注册商标）的选择性凝胶获得的卤代烃凝胶; 如果发生泄漏，该第二凝胶提供了防止液体从容器快速逸出的手段。
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公开(公告)号：US2452035A
公开(公告)日：1948-10-26
申请号：US52596444
申请日：1944-03-10
IPC分类号： F42B39/14
CPC分类号： F42B39/14 , Y10T292/0853
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公开(公告)号：US11879710B2
公开(公告)日：2024-01-23
申请号：US18335548
申请日：2023-06-15
申请人： Raytheon Company
IPC分类号： F42B15/34 , H01M10/613 , H01M10/625 , F41A17/06 , F42B12/20 , F42B15/36 , F42B39/20 , G01K3/00 , H01M10/48 , F42B39/14 , F42C15/00
CPC分类号： F42B15/34 , F41A17/06 , F42B12/207 , F42B15/36 , F42B39/14 , F42B39/20 , F42C15/00 , G01K3/005 , H01M10/486 , H01M10/613 , H01M10/625
摘要： A mitigation control system, for performing an active hazard mitigation method, is arranged in an environment containing an energetic material and includes an abnormal temperature sensor for detecting an abnormal temperature of the environment, a power source that is mechanically actuated by the abnormal temperature sensor when the abnormal temperature exceeds a predetermined abnormal temperature threshold, a mitigation controller that is actuated by the power source, and a plurality of local temperature sensors that are communicatively coupled to the mitigation controller and are arranged for detecting critical temperatures in specific regions of the environment. The mitigation controller executes a mitigation action when one of the critical temperatures exceeds a predetermined critical temperature threshold for the corresponding specific region.
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公开(公告)号：US20230417524A1
公开(公告)日：2023-12-28
申请号：US18300626
申请日：2023-04-14
摘要： An ammunition cartridge comprised of a projectile inserted in, and mechanically connected to, a metal cartridge case assembly having a propulsion chamber and a base, and an energetic propellant disposed in the propulsion chamber, includes a base plug in which is mounted an igniter with an energetic primer. During manufacture of the cartridge, a fusible support ring is incorporated into a metal cavity. The cartridge base includes a cavity allowing the fusible material to solidify at ambient temperatures. When exposed to heat from an external fire, the fusible support plug liquefies losing its strength and subsequently, when a propellant or primer off-gasses or auto-ignites the pressure from the reaction ejects a metal plug or lid from the cartridge case base, creating a void that allows the propellant and primer to combust in an unconfined space.
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公开(公告)号：US10670381B1
公开(公告)日：2020-06-02
申请号：US13999547
申请日：2014-04-10
摘要： An electronic thermally-initiated venting system (ETIVS) for rocket motors includes at least one linear-shaped charge attached to a rocket motor housing. At least one exploding foil initiator (EFI) is attached to the linear-shaped charge. At least one electronic thermally-initiated venting system circuit is electrically-connected to the EFI. The EFI is configured to auto-fire when the electronic thermally-initiated venting system circuit relays a current pulse through the EFI. The linear-shaped charge is configured to initiate when the current pulse is relayed through the EFI.
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公开(公告)号：US10254097B2
公开(公告)日：2019-04-09
申请号：US14687693
申请日：2015-04-15
申请人： Raytheon Company
摘要： A release mechanism includes a frame with an interior. The release mechanism also includes a prestrained element coupled to the interior of the frame. The prestrained element creates a seal with the frame. The prestrained element is notched in one or more regions. The prestrained element is configured to fracture when heated to a predetermined temperature allowing the interior to open. The fracture is based on the notched regions of the prestrained element such that separation initiates within the notched regions. The remaining regions of the prestrained element unfractured. The shape memory alloy element can include one or more of a nickel-titanium alloy, a titanium-nickel alloy, a copper-zinc-aluminum alloy, a copper aluminum nickel alloy, and a nickel titanium hafnium alloy. Heating of the shape memory alloy element causes a stress in the shape memory alloy that causes fracturing of the prestrained alloy when sufficient heating has been achieved.
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30.发明申请公开(公告)号：US20190023415A1
公开(公告)日：2019-01-24
申请号：US16137196
申请日：2018-09-20
申请人： AEROVIRONMENT, INC.
摘要： An unmanned aerial vehicle (UAV) launch tube that comprises at least one inner layer of prepreg substrate disposed about a right parallelepiped aperture, at least one outer layer of prepreg substrate disposed about the right parallelepiped aperture, and one or more structural panels disposed between the at least one inner layer of prepreg substrate and the at least one outer layer of prepreg substrate. An unmanned aerial vehicle (UAV) launch tube that comprises a tethered sabot configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot is hollow having an open end oriented toward a high pressure volume and a tether attached within a hollow of the sabot and attached to the inner wall retaining the high pressure volume or attach to the inner base wall. A system comprising a communication node and a launcher comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node.
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