公开(公告)号：US20150241185A1

公开(公告)日：2015-08-27

申请号：US13929313

申请日：2013-06-27

申请人： Exquadrum, Inc.

发明人： Robert L. GEISLER ,  Kevin E. MAHAFFY

IPC分类号： F42B12/44

CPC分类号： F42B12/44 ,  F42B12/52 ,  F42B12/58

摘要： A kinetic fireball incendiary munition is provided having an outer shell or bomb casing, one or more incendiary sub munitions therein, and an igniter therefore. Each of the submunitions includes an incendiary portion, at least one rocket motor that propels the submunition inside of a target volume, and an oxidizer for the incendiary portion and rocket motor. The submunitions liberate sufficient heat to produce elevated temperatures inside of a target structure to thermalize the contents thereof without creating a substantial overpressure or explosive effect.

摘要翻译： 提供了一种动力火球燃烧弹药，具有外壳或炸弹外壳，其中包括一个或多个燃烧弹药，因此也提供点火器。 每个子弹药包括燃烧部分，至少一个将目标体积内的子弹药推进的火箭发动机，以及用于燃烧部分和火箭发动机的氧化剂。 子弹药释放足够的热量以在目标结构内产生升高的温度，以使其内容物热化，而不产生显着的超压或爆炸效应。

公开(公告)号：US07571680B1

公开(公告)日：2009-08-11

申请号：US11515699

申请日：2006-09-05

申请人： Samuel Barran Tafoya

发明人： Samuel Barran Tafoya

IPC分类号： F42B10/00

CPC分类号： F42B12/52 ,  F42B10/06

摘要： A fuel-storing ordnance canister for release from military aircraft that does not explode upon impact, its collapsible accordion-like structure instead forcefully dispersing atomized fuel in an upwardly direction in the impact zone after descent for dispersal in, around, and beyond the impact zone. When the fuel from multiple canisters is released into a drop zone and later ignited by a dropped or ground-based incendiary device, all life in the dispersal area is eliminated. Tail fins assure nose-down flight and provide handles for easy canister handling and loading onto airplanes. The configuration of a pop-open tail plug allows for its partial release upon canister collapse to create a spray nozzle that atomizes the fuel stored in the canister as it is being dispersed. The most preferred application is by the U.S. Military to eliminate terrorists hiding in caves, hidden ordnance, and other areas previously resistant to air-released ordnance.

摘要翻译： 用于从军用飞机上释放的储存燃料的弹药筒，其不会在冲击时爆炸，其可折叠的类风琴式结构反而在下降之后强力地将雾化燃料分散在冲击区域中，以将其分散在冲击区域内部，之外和之外 。 当来自多个罐的燃料被释放到下降区域中并且随后被落地或地基燃烧装置点燃时，消除了分散区域中的所有寿命。 尾翼确保了下降的飞行，并提供手柄，便于罐子处理和装载到飞机上。 弹开式尾塞的构造允许其在罐崩溃时的部分释放以产生喷雾喷嘴，其在储存在罐中的燃料在其被分散时雾化。 最优选的应用是由美国军方消除躲在洞穴，隐藏的武器以及其他以前抵抗空中弹药的地区的恐怖分子。

公开(公告)号：US5168123A

公开(公告)日：1992-12-01

申请号：US553811

申请日：1990-07-19

申请人： John H. Lee

发明人： John H. Lee

IPC分类号： F41H11/12 ,  F42B12/52

CPC分类号： F42B12/52 ,  F41H11/12

摘要： The invention relates to the chemical initiation of detonation of a fuel-in-air (FAE) cloud such as might be used in a minefield breaching system. A component of the system is adapted to carry fuel to the breaching site and is also adapted to carry a compatible chemical, either gaseous or liquid. Upon detonation of a suitable explosive within the component the fuel is dispersed outwardly to form the cloud and the chemical is jetted outwardly into the cloud in a turbulent manner. A chemical reaction between the chemical initiator and the fuel-air mixture leads almost instantaneously to an explosive shock wave that propagates through the cloud causing detonation thereof. Such detonation neutralizes the minefield along a desired path. With the invention it is not necessary to utilize secondary charges and hence a more efficient and reliable breaching system is achieved.

摘要翻译： 本发明涉及可用于雷场破坏系统中的燃料空气（FAE）云的爆炸的化学引发。 系统的一个部件适于将燃料运送到破裂部位，并且还适于携带气体或液体的相容化学物质。 在组件内爆炸合适的炸药时，燃料向外分散形成云，化学物质以湍流的方式向外喷射到云中。 化学引发剂和燃料 - 空气混合物之间的化学反应几乎瞬间导致爆炸性冲击波，其通过云传播引起其爆炸。 这种爆炸沿所需的路径中和雷区。 利用本发明，不需要利用二次电荷，因此实现更有效和可靠的破坏系统。

公开(公告)号：US5160803A

公开(公告)日：1992-11-03

申请号：US618479

申请日：1990-11-27

申请人： Noel Fulchiron ,  Bernard Naillon ,  Patrick Nadaud

发明人： Noel Fulchiron ,  Bernard Naillon ,  Patrick Nadaud

IPC分类号： F42B12/44 ,  F42B12/50 ,  F42B12/52

CPC分类号： F42B12/44 ,  F42B12/50 ,  F42B12/52

摘要： The invention concerns the domain of a charges which can be released, for example, from an aircraft to which they are fixed, and in particular a munition containing an incendiary gel made of hydrocarbons and gelatinizing agents, intended to have an incendiary effect on various targets on the ground.The invention enables the munition to be broken up above the ground thanks to means of distribution constituted of a detonating cord, gas-generating grains, a shield and a rod. These means of distribution ensure regular scattering of the incendiary gel before the impact on the ground. The invention also enables ignition of the incendiary gel on break-up of the munition thanks to means of ignition composed of ignition capsules.Application to munitions containing an incendiary gel, also to munitions containing a product to be scattered.

摘要翻译： 本发明涉及可以例如从其被固定的飞机释放的费用的领域，特别是包含由碳氢化合物和凝胶化剂制成的燃烧凝胶的弹药，旨在对各种目标具有燃烧效果 在地上。 本发明使得能够通过由引爆绳，气体产生颗粒，屏蔽和杆构成的分配装置将地弹分解成地面以上。 这些分配方式可确保在对地面造成撞击之前固化火焰凝胶。 本发明还能够通过由点燃胶囊组成的点火装置使火焰分解，从而燃烧燃烧胶。 适用于含有燃烧凝胶的弹药，以及含有分散产品的弹药。

公开(公告)号：USH161H

公开(公告)日：1986-11-04

申请号：US825422

申请日：1986-02-03

申请人： John D. Sullivan, Jr.

发明人： John D. Sullivan, Jr.

IPC分类号： F42B12/52

CPC分类号： F42B12/52

摘要： The invention comprises a plastic bottle having a threaded cap with a holen its center and two hollow plastic tubes having the same diameter. One of the hollow tubes is empty and is used to seal the device in transit. The other hollow tube is filled with an explosive fluid and capped with a detonator with wires that connect to a power source. The device is designed to create a volatile mist of air and combustible fluid by dispersing the combustible fluid by means of an explosive charge. The explosive charge is made up of an explosive fluid and is an integral part of the device. The device can be manufactured from commercially available, inexpensive materials and requires no skill or tools. The device can be safely operated. It is made entirely of plastic materials; there is no metal which may fragment. This device is the smallest to be successfully tested to achieve an unconfined fuel-air explosion; it requires approximately one-half the amount of combustible fluid as similar devices to create the same desired result.

公开(公告)号：US4297949A

公开(公告)日：1981-11-03

申请号：US62395

申请日：1979-07-31

申请人： Cecil A. Glass ,  Dallas D. Burns

发明人： Cecil A. Glass ,  Dallas D. Burns

IPC分类号： F41H11/12 ,  F42B12/52 ,  F42C15/184 ,  F42B25/12 ,  F42B15/12

CPC分类号： F42C15/184 ,  F41H11/12 ,  F42B12/52

摘要： A detonation system for explosive rounds, such as a fuel air explosive, is made by providing a sealed launch tube detonator assembly arrangement. The cloud detonator provides for a booster charge which is attached to a pyro delay detonator. The pyro delay detonator permits the booster charge to be hurled a discrete distance into the fuel air cloud to insure proper cloud detonator position while at the same time waiting an appropriate time interval to permit complete cloud formation. The detonator assembly is self-sealing in its launch tube to prevent gases, which hurl the detonator assembly out of the launch tube, from burning the fuel air cloud. The cloud detonator assembly itself contains unique safety features which will prevent premature partial burning of booster charge.

摘要翻译： 通过提供密封的发射管雷管组件装置来制造用于爆炸性的轮的爆炸系统，例如燃料空气炸药。 云雷管提供附加到火焰延迟雷管的增压装置。 火焰延迟雷管允许增压装置投入到燃料空气云中的离散距离，以确保适当的云雷管位置，同时等待适当的时间间隔以允许完全的云形成。 雷管组件在其发射管中是自密封的，以防止将雷管组件从发射管中推出的气体燃烧燃料空气云。 云雷管组件本身包含独特的安全功能，可防止增压器过早部分燃烧。

公开(公告)号：US4273048A

公开(公告)日：1981-06-16

申请号：US24132

申请日：1979-03-26

申请人： Michael H. Aley ,  James A. Bowen ,  Cecil A. Glass

发明人： Michael H. Aley ,  James A. Bowen ,  Cecil A. Glass

IPC分类号： F41H11/12 ,  F42B10/56 ,  F42B12/52 ,  F42B3/00

CPC分类号： F42B10/56 ,  F41H11/12 ,  F42B12/52

摘要： A fuel-air explosive weapon launched from a remote distance is used for clearing minefields. A set timing pattern in the operation of the minefield clearance round permits varied range through retarding the length of time that a programed sequence of events occurs at the launch site. Upon flight, the round follows a predetermined pattern in deployment of a parachute, firing cloud detonators and initiation of a burster charge. An extendable probe at the front of the round permits detonation at a predetermined level above ground. The descent by parachute provides a relatively stable launching platform for cloud detonators if they are fired prior to the burster charge detonation for dispersal of the fuel-air cloud.

摘要翻译： 从远处发射的燃油爆炸武器用于清雷雷区。 排雷周期运行中的设定时间模式允许通过延迟发射现场发生的编程顺序事件的时间长短来改变范围。 在飞行中，圆形按照预定的方式进行降落伞的部署，发射云雷管并引发爆胎。 在圆形前部的可伸缩探头允许在地面以上预定水平的爆震。 降落伞的下降为云雷管提供了一个相对稳定的发射平台，如果它们在燃烧空气云散布爆炸炸药爆炸之前被射击。

公开(公告)号：US3713392A

公开(公告)日：1973-01-30

申请号：US3713392D

申请日：1971-02-09

申请人： US NAVY

发明人： PARSONS K

IPC分类号： F42C19/08 ,  F42B3/10

CPC分类号： F42B12/52 ,  F42C19/0838

摘要： A metal fuse extension with an explosive-filled channel passing through it. The channel is small on one end and large on the other end. The small end is adjacent a fuse and the large end is adjacent a burster charge. Upon detonation of the explosive material in the channel, the small end is sealed closed due to metal flow, thus preventing a backfire of the burster charge through the small end.

公开(公告)号：US09423224B2

公开(公告)日：2016-08-23

申请号：US13929313

申请日：2013-06-27

申请人： Exquadrum, Inc.

发明人： Robert L Geisler ,  Kevin E Mahaffy

IPC分类号： F42B12/44 ,  F42B12/58 ,  F42B12/52

CPC分类号： F42B12/44 ,  F42B12/52 ,  F42B12/58

摘要： A kinetic fireball incendiary munition is provided having an outer shell or bomb casing, one or more incendiary sub munitions therein, and an igniter therefore. Each of the submunitions includes an incendiary portion, at least one rocket motor that propels the submunition inside of a target volume, and an oxidizer for the incendiary portion and rocket motor. The submunitions liberate sufficient heat to produce elevated temperatures inside of a target structure to thermalize the contents thereof without creating a substantial overpressure or explosive effect.

摘要翻译： 提供了一种动力火球燃烧弹药，具有外壳或炸弹外壳，其中包括一个或多个燃烧弹药，因此也提供点火器。 每个子弹药包括燃烧部分，至少一个将目标体积内的子弹药推进的火箭发动机，以及用于燃烧部分和火箭发动机的氧化剂。 子弹药释放足够的热量以在目标结构内产生升高的温度，以使其内容物热化，而不产生显着的超压或爆炸效应。

公开(公告)号：US07418905B2

公开(公告)日：2008-09-02

申请号：US10741955

申请日：2003-12-19

申请人： Thomas H. Bootes ,  Jesse T. Waddell

发明人： Thomas H. Bootes ,  Jesse T. Waddell

IPC分类号： F42B12/16

CPC分类号： F42B12/16 ,  F42B12/08 ,  F42B12/44 ,  F42B12/52

摘要： A missile, such as a cruise missile, has a nose payload portion having a frangible nose cover and a relatively hard target penetration nose cone. The nose cone may have a liquid fuel tank within, and a chemical energy explosive charge, such as a shaped charge, aft of the liquid fuel tank. The target penetration nose cone enables perforation of certain types of targets prior to detonation of the chemical energy explosive and the liquid fuel. The frangible nose cover is configured to be easily perforated or otherwise removed by the explosive force of the chemical energy explosive charge when the missile system is utilized for the attack of hard targets. The nose payload portion may have a fragmentation case, with one or more features designed to enhance fragmentation during detonation of the explosive and/or the liquid fuel.

摘要翻译： 诸如巡航导弹的导弹具有具有易碎鼻罩和相对硬的目标穿透鼻锥的鼻部净荷部分。 鼻锥可能在其内部具有液体燃料箱，以及化学能量的爆炸装料，例如液体燃料箱的成形装料。 目标穿透鼻锥体能够在爆炸化学能量爆炸物和液体燃料之前穿透某些类型的目标。 当导弹系统用于硬目标的攻击时，易碎的鼻罩构造成容易穿孔或以化学能量炸药的爆炸力去除。 鼻部有效载荷部分可以具有碎裂情况，其中一个或多个特征被设计成在炸药和/或液体燃料爆炸期间增强碎裂。