公开(公告)号：US20040200341A1

公开(公告)日：2004-10-14

申请号：US10386644

申请日：2003-03-12

发明人： Craig T. Walters ,  Jeff L. Dulaney ,  David W. Sokol

IPC分类号： B64D001/04 ,  F41F005/00

CPC分类号： F41H11/12 ,  F41H11/32 ,  F41H13/0062

摘要： A system for neutralizing a buried mine includes a laser that is configured to generate laser energy that communicates through the covering ground material and accesses the mine in a manner sufficient to neutralize the mine. Neutralization can occur by deflagration or detonation. The laser includes a solid-state lasing medium that is run substantially uncooled during the lasing run. Namely, the lasing medium is operated without cooling until the lasing medium reaches a temperature where thermal population in a lower laser level begins to significantly lower inversion density. Following completion of the lasing run, the lasing medium is cooled at a rate limited only by a thermal stress fracture level of the lasing medium. Operation of the laser in this manner permits the laser to deliver high-irradiance, high-repetition rate pulses according to a burst mode operation that successfully accomplishes neutralization in a desired time period. The burst mode also facilitates preferential selection of the mechanism of laser energy-material interaction to promote rapid penetration rates.

摘要翻译： 用于中和埋地矿的系统包括激光器，其被配置为产生激光能量，所述激光能量通过覆盖的地面材料进行通信并以足以中和矿井的方式进入矿井。 中和可以通过爆燃或爆炸发生。 激光器包括在激光运行期间基本上未冷却的固态激光介质。 即，激光介质在没有冷却的情况下运行，直到激光介质达到较低激光水平的热量开始显着降低反转密度的温度。 在激光运行完成之后，激光介质以仅由激光介质的热应力断裂水平限制的速率冷却。 以这种方式操作激光器允许激光器根据在期望的时间段内成功实现中和的突发模式操作来传送高辐照，高重复率脉冲。 突发模式还有助于优先选择激光能量 - 材料相互作用的机制，以促进快速渗透速率。

公开(公告)号：US20040118270A1

公开(公告)日：2004-06-24

申请号：US10324553

申请日：2002-12-20

发明人： John L. Barrett

IPC分类号： B64D001/04 ,  F41F005/00

CPC分类号： F41H13/005 ,  F41H11/02 ,  F42B10/66

摘要： A method for deflecting a projectile from an initial trajectory. Such a projectile has a first surface area and a second surface area and moves through a gaseous atmosphere with a surrounding plasma sheath. This method includes the step of directing electromagnetic radiation toward the projectile, wherein the electromagnetic radiation has a wavelength which is absorbed by the plasma sheath but is not substantially absorbed by the gaseous atmosphere.

摘要翻译： 一种使弹丸从初始轨迹偏转的方法。 这种抛射体具有第一表面积和第二表面积，并且通过周围的等离子体鞘移动通过气态气氛。 该方法包括朝向射弹引导电磁辐射的步骤，其中电磁辐射具有被等离子体鞘吸收但不被气体气氛基本吸收的波长。

公开(公告)号：US20030233931A1

公开(公告)日：2003-12-25

申请号：US10172600

申请日：2002-06-14

发明人： Igor Z. Nemtsev

IPC分类号： B64D001/04 ,  F41F005/00

CPC分类号： F41H13/0062

摘要： The Synchronized Photo-pulse Detonation (SPD) method employs several fundamental techniques that are able to dramatically improve the kill-ratio of Laser Supported Detonation (LSD) of hostile targets, such as: missiles, aircraft, ships, and other land based targets, all the while reducing the chemical energy consumption and time needed per kill by thousands of times, thus making its deployment cost effective. The SPD to use 2 (two) synchronized laser pulses to create a Laser Supported Detonation Wave (LSDW) in a mixture of target vapors and atmospheric air. The first pulse creates an ignition plasma spark (in a mixture of air and target vapors), while the second (higher powered) pulse serves to create and support a shock wave from the heated plasma. This shock wave heats the surrounding air layer (mixture of air and target vapors) so that it begins to absorb the laser beam and to create from itself the next plasma layer with the formation of a new shock wave. The several thousands of tons of force generated by the LSDW are more than capable of destroying any object, such as an ICBM, aircraft, or build.

摘要翻译： 同步光脉冲爆震（SPD）方法采用几种基本技术，能够显着提高敌对目标的激光支持爆轰（LSD）的杀伤率，如：导弹，飞机，船舶等陆地目标， 同时将化学能量消耗和每次杀死所需的时间减少数千次，从而使其部署成本有效。 SPD使用2（2）个同步激光脉冲在目标蒸汽和大气中混合制造激光支持的爆震波（LSDW）。 第一个脉冲产生点火等离子体火花（在空气和目标蒸气的混合物中），而第二个（较高功率的）脉冲用于产生和支持来自加热的等离子体的冲击波。 这种冲击波加热了周围的空气层（空气和目标蒸汽的混合物），使得它开始吸收激光束，并且通过形成新的冲击波自身产生下一个等离子体层。 由LSDW产生的数千吨的力量超过能够摧毁任何物体，如ICBM，飞机或建造物。

公开(公告)号：US20030145717A1

公开(公告)日：2003-08-07

申请号：US10220741

申请日：2002-12-05

发明人： Naoki Yamamoto ,  Yves Riberon

IPC分类号： F41F005/00

CPC分类号： F41H11/18

摘要： The invention concerns a device mounted on a carrier vehicle equipped with at least a support (4) whereon a frame (6) is mounted in articulation, with interposed a pressure actuator (8), the frame being equipped at its bottom end with a plurality of vertical bars (24) whereof the lower ends (26) are provided with feet (28) and whereof the upper ends are provided each with a piston (15) mounted sliding into a cylinder (13). A mechanical component (10) called a proportioning unit, wherein are arranged the cylinders (13) used for fixing the pistons (15) disposed at the upper ends of the bars (24), and comprising a chamber (14) communicating said cylinders, is mounted sliding between stop elements (12, 13) in the frame, parallel to the axes of the cylinders (13), the mechanical component forming a proportioning unit (10) is directly subjected to the action of the thrust forces of the actuator (8) via the frame stops (12).

摘要翻译： 本发明涉及一种安装在载体车辆上的装置，该车辆配备有至少一个支架（4），其中框架（6）以铰接方式安装，插入有压力致动器（8），该框架在其底端装有多个 下端（26）设置有脚（28）的竖直杆（24），并且其上端设置有滑动地安装到气缸（13）中的活塞（15）。 一种称为配比单元的机械部件（10），其中布置有用于固定设置在杆（24）的上端的活塞（15）的气缸（13），并且包括连通所述气缸的室（14） 在框架中的平行于气缸（13）的轴线的止动元件（12,13）之间滑动，形成配比单元（10）的机械元件直接受到致动器的推力的作用（ 8）通过框架挡块（12）。

公开(公告)号：US20030089219A1

公开(公告)日：2003-05-15

申请号：US10001533

申请日：2001-11-14

发明人： Richard Gorman

IPC分类号： B64D001/04 ,  F41F005/00

CPC分类号： F41H11/02

摘要： The present invention is a method and system for disabling time critical and moving targets and an air deployed guided missile launcher. A system for disabling a time critical target at a site within a geographical area in accordance with the invention includes a plurality of spaced apart mostly buried missile launchers located within or adjacent to the geographical area with each spaced apart mostly buried mobile missile launcher containing a guided missile, any site within the geographical area being located at a distance from at least one spaced apart missile launcher not more than a maximum distance of travel of a guided missile launched from at least one of the spaced apart missile launchers to the site, the time of travel of a missile from the missile launcher to the site requiring less time than a maximum time required to enable the time critical target at the site.

摘要翻译： 本发明是一种用于禁用时间关键和移动目标的方法和系统，以及空中部署的导弹发射器。 根据本发明的用于禁用在地理区域内的地点的时间关键目标的系统包括位于地理区域内或邻近地理区域的多个间隔开的大部分掩埋的导弹发射器，每个间隔开的大部分埋藏的移动导弹发射器包含导向 所述地理区域内的任何站点距离至少一个间隔开的导弹发射器一定距离，该导弹发射器不超过从至少一个间隔开的导弹发射器发射到该地点的导弹的最大行进距离，时间 导弹从导弹发射器到现场的旅行时间要比在现场实现时间关键目标所需的最长时间少。

公开(公告)号：US20030019350A1

公开(公告)日：2003-01-30

申请号：US09834425

申请日：2001-04-13

发明人： Deepak Khosla

IPC分类号： F41F005/00 ,  B64D001/04

CPC分类号： F41H11/02 ,  F41G3/04

摘要： A system and method for automatic weapon allocation and scheduling of the present invention. The inventive method includes the steps of providing data with respect to threats, weapons, weapon allocation options; weapon allocation rules; and temporally dependent constraints with respect thereto; evaluating the data; and temporally allocating the weapons to the threats automatically in accordance with the evaluation. The invention computes the optimal pairing and the best time to deploy each weapon system against threat(s) it is paired with in arriving at the pairing. This results in an optimal assignment where weapon resource constraints are not exceeded and therefore guarantee availability of sufficient resources for engagement of every threat that is paired with a weapon system.

摘要翻译： 本发明的自动武器分配和调度的系统和方法。 本发明的方法包括提供关于威胁，武器，武器分配选项的数据的步骤; 武器分配规则; 和时间依赖的约束; 评估数据; 并根据评估自动将武器临时分配给威胁。 本发明计算出最佳配对和最佳时间来部署每个武器系统以抵御与之配对的威胁。 这导致了不超过武器资源限制的最佳分配，因此保证了与武器系统配对的每个威胁的参与的足够资源的可用性。

公开(公告)号：US20020139239A1

公开(公告)日：2002-10-03

申请号：US09569840

申请日：2000-05-12

发明人： Joseph Dwayne Vogl

IPC分类号： F41F005/00 ,  B64D001/04

CPC分类号： B63C9/26 ,  F41A1/04

摘要： This invention is a line throwing rescue gun which is inexpensive and easy and efficient to use. The rescue gun utilizes a combustible gas which is sprayed into a chamber of the rescue gun and then igniting thereby propelling a projectile attached to a line over a substantial distance. The invention is also a method for using a rescue gun wherein the projectile is greased and ramrodded into the barrel of the rescue gun, whereby an aerosol combustible gas is sprayed into the chamber of the rescue gun, the chamber is sealed and the gas is ignited thereby propelling the projectile through the barrel towards a specified target.

摘要翻译： 本发明是一种廉价，易于使用的投掷式救援枪。 救护枪使用可燃气体，喷射到救援枪的一个腔室中，然后点燃，从而推动连接在一段距离上的射弹。 本发明还是一种使用救援枪的方法，其中抛射体被润滑并撞击救援枪的枪管，由此将气溶胶可燃气体喷射到救护枪的腔室中，该腔室被密封并且气体被点燃 从而将射弹通过枪管推向特定目标。

公开(公告)号：US20020129695A1

公开(公告)日：2002-09-19

申请号：US09809886

申请日：2001-03-16

发明人： Carlton William Naab ,  Paul Grant Schamell

IPC分类号： B64D001/04 ,  F41F005/00

CPC分类号： F16K31/00 ,  F16K3/02 ,  F16K13/06 ,  Y10T137/0318 ,  Y10T137/1647 ,  Y10T137/1782

摘要： A contamination-free pyrovalve having first tubing section and a second tubing section. The first and second tubing sections are disposed in spaced-apart relation such that a conveying path between the first and second tubing section is established. An opening is disposed between the first and second tubing sections. A valve body is fixedly attached to the first and second tubing sections. The valve body has a bore. A ram is disposed inside the bore of the valve body. A slug is disposed in the opening between the first tubing section and the second tubing section. The slug is held in position by a frictional fit. A combustion chamber is disposed in operative relation to the ram such that when an explosive material is ignited the pressure inside the chamber causes the ram to move through the bore to strike the slug and to displace it from the opening between the first and second tubing sections such that the valve is opened.

摘要翻译： 具有第一管段和第二管段的无污染火山灰。 第一和第二管段以间隔开的关系设置，使得第一和第二管段之间的输送路径被建立。 开口设置在第一和第二管段之间。 阀体固定地附接到第一和第二管段。 阀体具有孔。 柱塞设置在阀体的孔内。 在第一管段和第二管段之间的开口中设置有塞子。 通过摩擦配合将块塞保持在适当的位置。 燃烧室被设置成与冲头有效的关系，使得当爆炸材料被点燃时，腔室内的压力使得冲头移动穿过孔以撞击塞子并使其从第一和第二管段之间的开口移位 使阀门打开。

公开(公告)号：US20020100360A1

公开(公告)日：2002-08-01

申请号：US09771739

申请日：2001-01-29

发明人： James A. Rochen ,  Kare-Jonny Haugvaldstad ,  Timothy W. Sampson

IPC分类号： B64D001/04 ,  F41F005/00

CPC分类号： E21B43/116

摘要： A stackable thru-tubing perforating gun system for use in perforating in a large diameter cased wellbore below a smaller diameter production tubing string. The system comprises a thru-tubing retrievable bridge plug for supporting a lower perforating gun section. The system further comprises at least one additional gun section stacked on top of the lower gun section. After firing, individual gun sections may be retrieved from the wellbore through the tubing string.

摘要翻译： 用于在较小直径的生产油管柱下方的大直径套管井筒中穿孔的可堆叠通管穿孔枪系统。 该系统包括用于支撑下部射孔枪部分的通管可回收桥塞。 该系统还包括堆叠在下部枪部分的顶部上的至少一个附加枪部分。 在燃烧之后，可以通过油管柱从井筒中取出各个喷枪段。

公开(公告)号：US20020040634A1

公开(公告)日：2002-04-11

申请号：US09501290

申请日：2000-02-09

发明人： Alan R. Pinkus ,  Harry L. Task ,  Peter L. Marasco

IPC分类号： B64D001/04 ,  F41F005/00

CPC分类号： F41G7/226 ,  F41G7/2293

摘要： A laser energy window arrangement especially usable in a tactical aircraft having night vision equipment-aided cockpit visual information input requirements. The laser energy window arrangement enables use of laser apparatus directed external to the aircraft for target designation or other purposes while minimizing the amount of energy from such laser returning spuriously inside the cockpit where it inherently acts a noise signal for night vision equipment. The laser energy window limits the portion of the aircraft windshield or canopy exposed to laser radiation and its effects to a relatively small area, an obscurable area generating significantly reduced amounts of spurious return energy in comparison with use of the laser directly through an unlimited windshield, canopy, or other type of transparency. Transmission of spurious return energy from the laser energy window to remaining portions of the windshield or canopy is precluded by interruption of transmission paths within the windshield or canopy material and transducing the interrupted path energy into heat dissipated within or outside of the aircraft and not affecting the remainder of the canopy. Potentially increased aircraft to target standoff range, reduce need for aircrew use of laser eye protection gear, reduced laser induced windshield or canopy degradation and other benefits are identified for aircraft uses of the invention. Use of the window invention in other non aircraft and non military aircraft settings is also contemplated.