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    • 1. 发明申请
    • AVALANCHE TRIGGERING SYSTEM
    • AVALANCHE触发系统
    • US20110005423A1
    • 2011-01-13
    • US12280598
    • 2007-02-21
    • Werner Greipl
    • Werner Greipl
    • F42B12/52
    • F42D3/00
    • The invention relates to an avalanche triggering system comprising a frame (4) fitted with means of attachment (5) for transporting the system, especially by helicopter with the aid of a cable (3), the frame (4) comprising, at the top, a storage area (6) for at least one gas container (7) designed to form an explosive mixture and, at the bottom, a holding system (8) for holding a plurality of balloons (9), each having an inflation sleeve and each being separated from the others, means (7, 13, 14) for conveying the explosive mixture to the inflation sleeve of a balloon (9), an injection nozzle (12), and means for igniting the explosive mixture, the balloon holding system (8) being mounted movably on the frame (4) to bring the inflation sleeve of each balloon (9) in succession up to the injection nozzle (12) and to the ignition means.
    • 本发明涉及一种雪崩触发系统,其包括装配有用于传送系统的装置(5)的框架(4),特别是借助于电缆(3)的直升机,所述框架(4)包括在顶部 ,用于至少一个设计成形成爆炸性混合物的气体容器(7)的存储区域(6),并且在底部具有用于保持多个气囊(9)的保持系统(8),每个气囊具有充气套筒和 每个与其他物体分开,用于将爆炸性混合物输送到气囊(9)的充气套筒,喷射喷嘴(12)和用于点燃炸药混合物的装置(7,13,14),所述气囊保持系统 (8)可移动地安装在框架(4)上,以将每个气球(9)的充气套筒连续地连接到喷射喷嘴(12)和点火装置。
    • 2. 发明授权
    • Chemical initiation of detonation in fuel-air explosive clouds
    • 燃料 - 空气爆炸云中爆炸的化学引发
    • US5168123A
    • 1992-12-01
    • US553811
    • 1990-07-19
    • John H. Lee
    • John H. Lee
    • F41H11/12F42B12/52
    • F42B12/52F41H11/12
    • 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.
    • 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。
    • 3. 发明授权
    • Munition for the distribution of an incendiary mixture
    • 分配燃料混合物的弹药
    • US5160803A
    • 1992-11-03
    • US618479
    • 1990-11-27
    • Noel FulchironBernard NaillonPatrick Nadaud
    • Noel FulchironBernard NaillonPatrick Nadaud
    • F42B12/44F42B12/50F42B12/52
    • F42B12/44F42B12/50F42B12/52
    • 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.
    • 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。
    • 4. 依法登记的发明
    • Small fuel-air explosive bottle
    • USH161H
    • 1986-11-04
    • US825422
    • 1986-02-03
    • John D. Sullivan, Jr.
    • John D. Sullivan, Jr.
    • F42B12/52
    • F42B12/52
    • 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.
    • 8. 发明申请
    • Multi-mission payload system
    • 多任务有效载荷系统
    • US20050223930A1
    • 2005-10-13
    • US10741955
    • 2003-12-19
    • Thomas BootesJesse Waddell
    • Thomas BootesJesse Waddell
    • F42B12/00F42B12/08F42B12/16F42B12/44F42B12/52
    • F42B12/16F42B12/08F42B12/44F42B12/52
    • 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.
    • 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。
    • 10. 发明授权
    • Fuel-air type bomb
    • 燃油型炸弹
    • US4132169A
    • 1979-01-02
    • US89140
    • 1970-11-06
    • Leon L. GayPeriam B. HardyDonald Hutchinson
    • Leon L. GayPeriam B. HardyDonald Hutchinson
    • F42B12/52F42B25/12
    • F42B12/52
    • A highly destructive fuel-air type drop bomb which requires no retardation or restriction of its terminal velocity for efficient detonation; which utilizes a normally non-explosive, normally liquid fuel dispersed in air for its explosive power; which centrally carries a low brisance heaving type fuel dispersing explosive surrounded by the body of liquid fuel; which includes a proximity fuse to detonate the low brisance explosive to break the fuel container and to disperse the fuel into the surrounding air in minute particles to form an aerosol cloud of large volume and of substantially uniform density in close proximity to the target; and which carries a time delay detonator for detonating the aerosol cloud after it has formed.
    • 一种高度破坏性的燃料空气型液滴炸弹,其不需要延迟或限制其终点速度以进行有效的爆炸; 其利用分散在空气中的通常为非爆炸性的通常为液体的燃料用于其爆炸力; 其中心地具有由液体燃料体围绕的低爆炸型燃料分散炸药; 其包括接近保险丝以引爆低爆炸性爆炸物以破坏燃料容器并将燃料以微小颗粒分散到周围空气中,以形成大体积且密度接近目标的基本均匀密度的气溶胶云; 并且其携带用于在其形成之后引爆气溶胶云的时间延迟雷管。