-
公开(公告)号：US08997773B2
公开(公告)日：2015-04-07
申请号：US13623843
申请日：2012-09-20
申请人： Stojan Kotefski , Cathleen Reda
发明人： Stojan Kotefski , Eugene R Reda
CPC分类号： F16K17/003 , B65D51/1633 , B65D90/36 , F16K17/383 , F42B27/00 , F42B39/14 , F42B39/20 , Y10T137/1797 , Y10T137/1812
摘要： The present invention relates in general to a pressure discharge mechanism for closed vessels having an internal chamber designed to hold volatile and/or explosive substances in a sealed manner comprised of an at least one eutectic composition and a threaded joint designed to open or vent the closed vessel when the contents of the closed vessel reaches a predetermined temperature while maintaining full structural integrity during normal operation. In one aspect, the closed vessel is a munitions casing which functions as intended under normal operating environments, but then when exposed to extreme temperatures, reduces the munition's high order explosion capability, and is transformed into a safe, low order reaction with significantly less reactive potential. In one aspect, the closed vessel is a transport tanker which should not release substances contained therein. However, if the tanker catches fire, the pressure relief mechanism of the present invention reduces risk of explosion.
摘要翻译： 本发明一般涉及一种用于封闭容器的压力释放机构，其具有设计成以密封方式容纳挥发性和/或爆炸性物质的内部腔室，所述密封容器包括至少一种共晶组合物和螺纹接头，该接头被设计成打开或排出封闭的 当密封容器的内容物达到预定温度同时在正常操作期间保持完整的结构完整性时，容器。 一方面，封闭式船只是在正常作业环境下正常运作的弹药套管，但是当暴露于极端温度时，可降低弹药的高阶爆炸能力，并转化为安全，低阶反应，反应活性明显较低 潜在。 一方面，密闭容器是运输罐车，其不应释放其中所含的物质。 然而，如果油罐车起火，则本发明的减压机构降低了爆炸的风险。
-
公开(公告)号：US20140008247A1
公开(公告)日：2014-01-09
申请号：US14006678
申请日：2012-03-27
申请人： Liam McNelis , Arash Shahinpour
发明人： Liam McNelis , Arash Shahinpour
摘要： The invention relates to a packing having a top side, a base side and face sides for hollow charges for use in blasting applications in boreholes. In order that fragments are retained in the packing in the event of an unintentional ignition of the hollow charges, the packing withstands the pressure which is generated and permits a dissipation of pressure, it is proposed according to the invention that a) the hollow charges are embedded in a solid material which captures the fragments generated during a detonation of the hollow charges, b) the solid material has pressure relief openings through which the pressure wave of the gas volume generated during a detonation of the hollow charges can escape, c) the solid material is covered with shock-absorbing material on the top side and on the base side of the packing, d) the hollow charges are packed in pairs such that there are always two hollow charges situated opposite the openings, e) the axes of symmetry of the hollow charges are arranged in a plane perpendicular to the top side and base side, and f) the solid material is inserted with the hollow charges and the shock-absorbing material into a cage, preferably a bar-grate-type cage.
摘要翻译： 本发明涉及一种具有用于在钻孔中喷砂应用的中空装料的顶侧，底侧和正面的填料。 为了在中空电荷的无意点燃的情况下将碎片保持在包装中，密封件可以承受所产生的压力并且允许压力的消散，根据本发明提出：a）中空电荷是 嵌入固体材料中，其捕获在中空电荷引爆期间产生的碎片，b）固体材料具有压力释放开口，在中空电荷爆炸期间产生的气体体积的压力波可通过该开口逃逸，c） 固体材料在填料的顶侧和底部侧覆盖有减震材料，d）中空电荷成对填充，使得总是位于与开口相对的两个中空电荷，e）对称轴 的空心电荷布置在垂直于顶侧和底侧的平面中，f）固体材料插入中空电荷和减震垫 卡入笼子，最好是棒状笼子。
-
公开(公告)号：US07107909B2
公开(公告)日：2006-09-19
申请号：US10897937
申请日：2004-07-23
申请人： Detlef Haeselich
发明人： Detlef Haeselich
摘要： A cartridge munition, particularly practice round, includes a cartridge shell (3) and a projectile (2) inserted into it. A propulsion chamber (4) is provided within the cartridge shell that receives a propulsive charge (5) that may be ignited by means of a pyrotechnic igniter (13) and that develops propulsive gases that act on the base (8) of the projectile, driving it out of the cartridge shell. In order to prevent the pyrotechnic igniter from igniting spontaneously, and from igniting the propulsive charge (5) because of the ambient temperature or because of a fire, which would cause the cartridge shell and projectile to be separated and fly apart, it is proposed by the invention to provide exhaust channels (14) between the propulsion chamber and the exterior of the cartridge shell (3) that are filled with a fusible material, particularly a fusible metal (15). The fusible material has a lower melting point than the ignition point of the igniter (13) and of the propulsive charge (5). If the ambient temperature of the cartridge shell rises above the melting point of the fusible material, it melts, releasing the exhaust channels (14), so that, upon delayed ignition of the propulsive charge, it burns without pressure buildup, and the cartridge shell and projectile remain together.
摘要翻译： 弹药弹，特别是围绕着弹药，包括插入其中的弹药筒（3）和射弹（2）。 推进室（4）设置在盒壳体内，其接收可以通过烟火点火器（13）点燃的推进装药（5），并且产生作用在射弹的基座（8）上的推进气体， 将其从墨盒外壳中推出。 为了防止烟火点火器自发点燃，并且由于环境温度或由于火灾引起推进装料（5），这将导致暗盒壳和射弹分离和飞散，故由 本发明提供了在推进室和盒壳体（3）的外部之间设置有用易熔材料，特别是可熔金属（15）填充的排气通道（14）。 可熔材料的熔点低于点火器（13）和推进装料（5）的点火点。 如果盒壳的环境温度升高到可熔材料的熔点之上，则其熔化，释放排气通道（14），使得在推进式电荷的延迟着火时，其燃烧而没有压力累积，并且盒壳 和射弹保持在一起。
-
14.发明授权公开(公告)号：US06952995B2
公开(公告)日：2005-10-11
申请号：US10042391
申请日：2002-01-11
摘要： Passive venting apparatus and method for a rocket motor or ordnance device containing propellant or explosive material enclosed in a case, which presents an explosion hazard when subjected to external heat. A combustible strip is secured to the exterior surface of the case and is constructed to burn and generate sufficient heat when exposed to predetermined external heat to weaken the adjacent portion of the case and effect rupture of the case to vent interior gases therein prior to autoignition of the propellant or explosive.
摘要翻译： 用于包含封装在壳体内的推进剂或爆炸性材料的火箭发动机或弹药装置的被动通风装置和方法，当受到外部热量时，其具有爆炸危险。 可燃条被固定到壳体的外表面，并被构造为当暴露于预定的外部热量时燃烧并产生足够的热量，以削弱壳体的相邻部分并且在自动点火之前实现壳体的内部气体泄放 推进剂或爆炸物。
-
公开(公告)号：US5786544A
公开(公告)日：1998-07-28
申请号：US659756
申请日：1996-06-06
申请人： Moshe Gill , Itzhak Avnon , Yehuda Katz , Tamar Yarom
发明人： Moshe Gill , Itzhak Avnon , Yehuda Katz , Tamar Yarom
CPC分类号： F42B39/20
摘要： A device for imparting non-explosive and non-propulsive properties to a warhead during a slow cook-off test, which comprises a pyrotechnic pellet located inside a tube having a predetermined ignition temperature of at least 130.degree. C. but below the violent ignition temperature of the material under slow cook-off conditions, whereby the venting holes present in the aft closure of said tube, are covered by a composite material that loses its strength below the predetermined temperature, causing a pressure relief and a non-propulsive burning of said warhead.
摘要翻译： 一种用于在慢速烹饪测试期间向弹头施加非爆炸性和非推进性的装置，其包括位于管内的烟火颗粒，其具有至少130℃但低于暴露点火温度的预定点火温度 的材料，由此存在于所述管的后盖中的通气孔被失去其强度低于预定温度的复合材料覆盖，导致所述压力释放和非推进燃烧所述 弹头。
-
16.发明授权Method and apparatus for minimizing blast damage caused by an explosion in aircraft cargo bay 失效用于最小化飞机货舱爆炸造成的爆炸破坏的方法和装置
公开(公告)号：US5769257A
公开(公告)日：1998-06-23
申请号：US583470
申请日：1996-01-05
CPC分类号： B64D45/0015 , B64D9/00 , B65D88/14 , B65D90/325 , F42B39/20 , B64D2045/005 , Y02T50/46
摘要： Method and apparatus for minimizing blast damage caused by an explosive device carried in luggage or other cargo loaded on an aircraft. A first cargo container is provided which includes a non-explosion-resistant panel. A second cargo container, also including a non-explosion-resistant panel is paired with the first container and both containers are loaded in the cargo bay such that the non-explosion-resistant panels face inboard, oppose and align with one another. The method provides a controlled venting feature whereby explosive products are vented into the adjacent container in the cargo bay of an aircraft through non-explosion-resistant panel on the inboard side of the container. The container is constructed of lightweight, high-strength materials and may be joined to a supporting structure with threaded fasteners, allowing for efficient replacement of damaged panels. The container may also incorporate edge and corner joint designs that exceed panel strength and will not fail under reasonable probable blast pressures, yet require no special manufacturing or maintenance techniques.
摘要翻译： 用于最小化由装在飞机上的行李或其他货物中携带的爆炸装置引起的爆炸破坏的方法和装置。 提供了包括非防爆面板的第一货物集装箱。 另外还包括一个非防爆面板的第二个货物集装箱与第一个集装箱配对，两个集装箱都装载在货舱中，使得防爆板面向内侧相对并相互对齐。 该方法提供了一种受控的排气功能，其中爆炸产品通过在容器的内侧上的非防爆面板排放到飞机的货舱中的相邻容器中。 容器由轻质的高强度材料构成，并且可以通过螺纹紧固件连接到支撑结构上，从而有效地更换损坏的板。 容器还可以包括超过面板强度的边缘和角接头设计，并且在合理的可能的鼓风压力下不会失效，但不需要特殊的制造或维护技术。
-
公开(公告)号：US5337672A
公开(公告)日：1994-08-16
申请号：US974259
申请日：1992-11-10
申请人： Bruno Boissiere , Michel Bossus
发明人： Bruno Boissiere , Michel Bossus
CPC分类号： F42B39/20
摘要： Ignition means being provided to ignite pyrotechnic materials, this ignition is produced by the activation of these ignition means. As long as the ignition means have not been activated, the casing is maintained firmly attached to a closing plug only by a first set of locking means so that at pressures within the casing in excess of a given pressure, the plug is ejected from the casing. As soon as the ignition means have been activated, the casing is maintained firmly attached to the plug by a second set of locking means at pressures within the casing in excess of the given pressure.
摘要翻译： 点火装置用于点燃烟火材料，这种点火是通过激活这些点火装置产生的。 只要点火装置没有被激活，壳体仅通过第一组锁定装置被保持牢固地附接到闭合塞，使得在壳体内的压力超过给定压力的情况下，插塞从壳体 。 一旦点火装置被激活，壳体通过第二组锁定装置在壳体内的压力下被保持牢固地附接到插头，超过给定的压力。
-
公开(公告)号：US5311820A
公开(公告)日：1994-05-17
申请号：US642523
申请日：1991-01-17
申请人： Warren Ellingsen
发明人： Warren Ellingsen
CPC分类号： F02K9/38 , F02K9/343 , F42B39/20 , Y10T403/11
摘要： A heat sensitive case/nozzle interface is provided for an insensitive propellant-loaded munition such that the interface loses its structural integrity when high external heat is applied. The joint between a rocket case housing a rocket motor and nozzle forming the interface is received by an internal spring retainer positioned in a first groove in the case or nozzle in cooperation with a fusible material housed in an aligned second groove in the nozzle or case, respectively. A plurality of aligned openings extend into said first and second grooves. When the rocket is exposed to a high ambient temperature greater than melt temperature of the fusible material but lower than the auto-ignition temperature of the rocket, the fusible material melts and is forced through said holes by the spring retainer permitting the nozzle to separate from the case rendering the rocket motor safe if it auto-ignites.
摘要翻译： 为不敏感的推进剂装载的弹药设置了一个热敏箱/喷嘴接口，使得当施加高外部热量时，界面失去其结构完整性。 容纳火箭发动机的火箭壳体和形成界面的喷嘴之间的接合部通过位于壳体或喷嘴中的第一凹槽中的内部弹簧保持器与容纳在喷嘴或壳体中对准的第二凹槽中的可熔材料协作接收， 分别。 多个对准的开口延伸到所述第一和第二凹槽中。 当火箭暴露于高于易熔材料的熔融温度但低于火箭自燃温度的高环境温度时，易熔材料通过弹簧保持器熔化并被迫穿过所述孔，允许喷嘴与 如果火箭发动机自动点火，则会使火箭发动机安全。
-
公开(公告)号：US5216965A
公开(公告)日：1993-06-08
申请号：US901619
申请日：1992-06-15
IPC分类号： F42B39/20
CPC分类号： F42B39/20
摘要： A relocatable storage magazine is provided for containing the shockwave, flagration and flying debris of an accidental explosion of stored explosives, ordnance or the like and includes a container; a debris trap attached to the container for receiving the pressure wave and for containing flying debris; an access hole communicating with the container and with the debris trap for venting the pressure wave of an explosion from the container into the debris trap and for providing access to the container; a lid cover and storage tray for storing and retrieving explosives; vent holes in the debris trap for venting the pressure wave to the atmosphere; a sliding door for providing access to the storage magazine; ears for lifting and relocating the storage magazine; hooks for retaining the lid cover and storage tray in an accessible position.
摘要翻译： 提供了一个可重新定位的存储杂志，用于容纳存储的爆炸物，弹药等的意外爆炸的冲击波，火灾和飞溅碎片，并且包括容器; 附着在容器上的用于接受压力波并用于容纳飞溅碎片的碎片陷阱; 与所述容器连通并具有用于将所述容器的爆炸压力波从所述容器排放到所述碎片陷阱中并用于提供对所述容器的通路的进入孔; 用于存储和检索炸药的盖盖和储存托盘; 通风孔在碎片陷阱中，以将压力波浪排放到大气中; 用于提供进入存储仓的滑动门; 用于提升和搬运存储杂志的耳朵; 用于将盖盖和存储托盘固定在可接近的位置的钩子。
-
公开(公告)号：US5166468A
公开(公告)日：1992-11-24
申请号：US681103
申请日：1991-04-05
申请人： Peter L. C. Atkeson
发明人： Peter L. C. Atkeson
摘要： An igniter which is triggered by a thermocouple for detonating an explosive material for forming an opening in a rocket motor case to render it non-propulsive in the event of a fire dangerously close thereto or for any other suitable purpose. The bridge therefor is preferably a suitable semiconductor bridge for handling a reduced amount of electrical energy which may be provided by the thermocouple. The thermocouple may be a plurality of pairs of dissimilar metal layers or foils alloyed together and the pairs connected in series.
摘要翻译： 一个由热电偶触发的点火器，用于引爆用于在火箭发动机壳体中形成开口的爆炸材料，以使得在火灾危险地靠近火花发动机的情况下使其非推进，或用于任何其它合适的目的。 其桥是优选用于处理可由热电偶提供的减少量的电能的合适的半导体桥。 热电偶可以是多对不同的金属层或合金化的箔，并且该对被串联连接。
-
-
-
-
-
-
-
-
-
搜索结果
181 条记录 (耗时 0.017 秒)
