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公开(公告)号：US06679155B1
公开(公告)日：2004-01-20
申请号：US10278958
申请日：2002-10-24
IPC分类号： F41F304
CPC分类号： F41A1/04
摘要： A launcher (10) is provided having a separation unit (15) and a launch tube (16) in fluid communication with the separation unit (15). The separation unit (15) has a pressure sensing chamber (23) for sensing the pressure within the separation unit (15), a separation chamber (24) in fluid communication with the pressure sensing chamber (23), and a combustion chamber (26) in fluid communication with the separation chamber (24). The combustion chamber (26) is in fluid communication with the launch tube (16) through opening (28). The rocket launcher (10) also includes a hydrogen separation circuit (21) and an ignition circuit (22). The hydrogen separation circuit (21) includes a battery pack (44) electrically coupled to a fuel cell (45) which when powered separates water into hydrogen gas and oxygen gas. The ignition circuit (22) includes a piezoelectric spark generator (61) for igniting the hydrogen gas produced by the fuel cell and contained within the combustion.
摘要翻译： 发射器（10）具有分离单元（15）和与分离单元（15）流体连通的发射管（16）。 分离单元（15）具有用于检测分离单元（15）内的压力的压力检测室（23），与压力检测室（23）流体连通的分离室（24）和燃烧室 ）与分离室（24）流体连通。 燃烧室（26）通过开口（28）与发射管（16）流体连通。 火箭发射器（10）还包括氢气分离回路（21）和点火回路（22）。 氢分离回路（21）包括电耦合到燃料电池（45）的电池组（44），当电力被分配成氢气和氧气时。 点火电路（22）包括压电火花发生器（61），用于点燃由燃料电池产生并包含在燃烧内的氢气。
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公开(公告)号：US06321631B1
公开(公告)日：2001-11-27
申请号：US09420913
申请日：1999-10-20
申请人： Gary G. Deel
发明人： Gary G. Deel
IPC分类号： F41F304
CPC分类号： F41F3/04 , B64F1/04 , B64G5/00 , F41F3/0413
摘要： A launch vehicle mounting system for use in launching either of first and second launch vehicles having different booster diameters is disclosed. In one embodiment, the launch vehicle mounting system includes a mounting frame and a plurality of arms pivotally interconnectable to the mounting frame for supporting either of the first and second launch vehicles positionable thereon. In particular, the launch vehicle mounting system of the present invention is adapted to support either the first or the second launch vehicle as the arms are at least radially adjustable relative to the mounting frame to at least first and second radial positions corresponding to the booster diameters of the first and second launch vehicles.
摘要翻译： 公开了一种用于发射具有不同增压器直径的第一和第二运载火箭的运载火箭安装系统。 在一个实施例中，运载火箭安装系统包括安装框架和可枢转地连接到安装框架的多个臂，用于支撑可定位在其上的第一和第二运载工具中的任一个。 特别地，本发明的运载火箭安装系统适于支撑第一或第二运载火箭，因为臂相对于安装框架至少可径向调整至少对应于增压器直径的第一和第二径向位置 的第一和第二个运载火箭。
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公开(公告)号：US06769345B2
公开(公告)日：2004-08-03
申请号：US10136330
申请日：2002-05-02
IPC分类号： F41F304
摘要： The invention relates to a container for propellant charge modules to be loaded into a weapon using conveyance means. It comprises protection means insulating said modules from the conveyance means, constituted by a rigid tubular body, a sheath intended to receive the modules and means to block the modules in the sheath. The sheath is made of a deformable material. The blocking means ensure the deformation of the sheath to immobilize the modules. Application to charge module conveyance.
摘要翻译： 本发明涉及一种用于使用输送装置装载到武器中的推进剂充电模块的容器。其包括保护装置，用于将所述模块与传送装置隔离，所述保护装置由刚性管状体，用于接收模块的护套和阻挡装置 护套中的模块。 护套由可变形材料制成。 阻塞意味着确保护套的变形以固定模块。应用模块运送。
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公开(公告)号：US06691600B2
公开(公告)日：2004-02-17
申请号：US10316476
申请日：2002-12-11
IPC分类号： F41F304
CPC分类号： F41A23/42
摘要： A multi-purpose missile launcher system for a military land vehicle that has the capability for direct targeting both short and medium range land targets, as well launching missiles against longer-range land targets or air targets using indirect targeting. The multi-purpose missile launcher system is deployed as part of a modular weapon system that mates with a modular bed of the military land vehicle.
摘要翻译： 一种用于军用陆地车辆的多用途导弹发射系统，具有直接瞄准中短程地面目标的能力，并使用间接瞄准对较长距离的地面目标或空中目标发射导弹。 多用途导弹发射系统被部署为与军用陆地车辆的模块化床相配合的模块化武器系统的一部分。
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公开(公告)号：US06679154B1
公开(公告)日：2004-01-20
申请号：US10302960
申请日：2002-11-25
申请人： Buddy R. Paul
发明人： Buddy R. Paul
IPC分类号： F41F304
CPC分类号： F41F3/055
摘要： The passive dynamically disconnecting arm features an arm having two ends wherein attached to the first end is a housing having both a plunger and an electrical connector providing positive engagement force during shock or vibration. The second end of the arm features a trunnion and torsion spring. The arm features a slot wherein a rod is placed inside operatively coupled to both the plunger and trunnion. When an object is attached to the electrical connector, the spring-loaded plunger compresses preventing the rod from moving and causing the second end of the rod to couple with a divot within the trunnion. When the object moves a predetermined distance, the spring-loaded plunger decouples from the rod and the electrical connector detaches from the object. The arm, by means of a torsion spring attached to the arm's second end, translates and rotates out of the object's path without striking the object.
摘要翻译： 被动动态断开臂的特征在于具有两端的臂，其中附接到第一端是具有柱塞和电连接器的壳体，其在冲击或振动期间提供正的接合力。 臂的第二端具有耳轴和扭转弹簧。 臂具有狭槽，其中杆被放置在操作性地联接到柱塞和耳轴的位置。 当物体附接到电连接器时，弹簧加载的柱塞压缩以防止杆移动并导致杆的第二端与耳轴内的凸缘相连。 当物体移动预定距离时，弹簧加载的柱塞与杆分离并且电连接器与物体分离。 臂通过连接到臂的第二端的扭力弹簧平移并旋转离开物体的路径而不会撞击物体。
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公开(公告)号：US06561074B1
公开(公告)日：2003-05-13
申请号：US05823885
申请日：1977-07-28
IPC分类号： F41F304
CPC分类号： F41G7/2246 , F41F3/0406 , F41F3/073 , F41F3/077 , F41G7/2206 , F41G7/2286 , G01S7/03 , G01S13/225 , G01S13/30 , G01S13/426 , G01S13/4463 , G01S13/449 , G01S13/72 , G01S13/78 , G01S13/86 , G01S13/87 , G01S2013/0272
摘要： A combined defense and navigational system on a naval vessel is disclosed. The disclosed system includes a track-while-scan pulse radar which is controlled to provide either navigational information or tracking information on selected targets. Additionally, the disclosed system includes a plurality of guided missiles, each of which may be vertically launched and directed toward intercept of a selected target either by commands from the track-while-scan radar or from an active guidance system in each such missile. The invention herein described was made in the course of or under a contract or subcontract thereunder, with the Department of Defense.
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公开(公告)号：US06776079B1
公开(公告)日：2004-08-17
申请号：US10627142
申请日：2003-07-25
IPC分类号： F41F304
CPC分类号： F41F3/08
摘要： An elastomeric disk for use in an elastomeric ejection system in which a thickened curvature protrudes from both sides of a central plane of the disk. Integral to each curvature is an annulet which dovetails from the curvatures to a periphery of the disk. The thickness of the annulet in regard to the central plane is greater on the fluid pressure side of the disk thereby shifting material strain to the center of the disk during expanding deformation. The annulet shape is attachable to the elastomeric ejection system by a clamp of the system.
摘要翻译： 用于弹性体弹射系统的弹性体盘，其中增厚的曲率从盘的中心平面的两侧突出。 每个曲率的积分是从曲率到盘的周边相互衔接的圆环。 在圆盘的流体压力侧，相对于中心平面的圆环的厚度更大，从而在膨胀变形期间将材料应变转移到圆盘的中心。 环形形状可通过系统的夹具附接到弹性体弹出系统。
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公开(公告)号：US06568309B2
公开(公告)日：2003-05-27
申请号：US10077712
申请日：2002-02-14
IPC分类号： F41F304
摘要： The detachable shock-absorbing ram-plate is used in a projectile launching system to mitigate launching impact forces and to prevent ram-plate re-strike during launch. The detachable shock-absorbing ram-plate is detachably coupled to the projectile using break-away fasteners that allow the ram-plate to be attached to the projectile during launch and detached from the projectile at the end of the launch. One embodiment of the detachable shock-absorbing ram-plate is a single impact, viscous fluid ram-plate including a cylinder, a perforated piston, and a viscous fluid disposed between the cylinder and the perforated piston. Upon receiving a high initial launch impact force, the piston compresses causing the viscous fluid to be forced through the perforated piston, thereby absorbing the shock of the initial launching impact force. Another embodiment of the detachable shock-absorbing ram-plate is a gas spring ram-plate having a cylinder and piston that compresses a gas to absorb shock caused by launching forces. A further embodiment of the shock-absorbing ram-plate is made from a compressible elastic material.
摘要翻译： 可拆卸的减震柱塞板用于射弹发射系统，以减轻发射冲击力，并防止发射时撞击板重击。 可拆卸的减震拉杆板使用断开紧固件可拆卸地联接到抛射体，该紧固件允许在发射期间将撞板附接到射弹，并在发射结束时与射弹分离。 可拆卸的减震冲压板的一个实施例是单个冲击粘性流体柱塞板，其包括气缸，穿孔活塞和设置在气缸和穿孔活塞之间的粘性流体。 在接收到高的初始发射冲击力时，活塞压缩，使得粘性流体被迫穿过穿孔活塞，从而吸收初始发射冲击力的冲击。 可拆卸式减震冲压板的另一实施例是具有气缸和活塞的气弹簧冲压板，其压缩气体以吸收由发射力引起的冲击。 减震拉杆板的另一实施例由可压缩的弹性材料制成。
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9.发明授权Missile launcher with piezoelectric launcher pulse power source and inductive launcher/missile coupling 有权导弹发射器具有压电发射器脉冲电源和感应发射器/导弹联轴器公开(公告)号：US06439097B1
公开(公告)日：2002-08-27
申请号：US09549886
申请日：2000-04-17
申请人： Ronald E Loving
发明人： Ronald E Loving
IPC分类号： F41F304
CPC分类号： F41A19/62
摘要： A missile system includes a launcher having a built-in pulse power source and an electrical connection to a missile. The pulse power source is used to send activation and firing pulses to the missile. The pulse power source utilizes a piezoelectric crystal which produces a pulse of energy when struck by a spring-loaded hammer that is released by an operator. In one version, a first piezoelectric crystal produces a first pulse to activate the system when struck by a first hammer, and a second piezoelectric crystal produces a second pulse to fire the missile when struck by a second hammer. The energy pulses are conducted from the launcher to the missile through an inductive coupling between a primary induction coil in the launcher and a facing secondary induction coil in the missile.
摘要翻译： 导弹系统包括具有内置脉冲电源和与导弹的电气连接的发射器。 脉冲电源用于向导弹发送激活和发射脉冲。 脉冲电源利用压电晶体，当被操作者释放的弹簧锤撞击时产生能量脉冲。 在一个版本中，第一压电晶体产生第一脉冲以在被第一锤撞击时激活该系统，并且第二压电晶体产生第二脉冲以在被第二锤击打时引燃该导弹。 能量脉冲从发射器通过发射器中的初级感应线圈和导弹的面对的次级感应线圈之间的感应耦合从发射器传导到导弹。
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公开(公告)号：US06311604B1
公开(公告)日：2001-11-06
申请号：US07516405
申请日：1990-04-30
申请人： Victor G. Foris , Takeshi Tokiyama
发明人： Victor G. Foris , Takeshi Tokiyama
IPC分类号： F41F304
CPC分类号： F41F3/077
摘要： A missile launch system is described in which a missile launch tube has the launch end thereof protected by a hollow launch tube cover. The launch tube cover is divided into a plurality of segments which are frangible and are dispersed during launch of a missile 62. The surfaces of the individual segments are coated with water repellant material such as tetrafluoroethylene or silicone to prevent ice buildup. Moreover the outer surface of the head of the launch tube cover can be coated with a layer of metallic material to prevent electro magnetic interference or radio frequency interference. The launch tube cover is constructed of a light weight, water proof material such as an expanded closed cell foam including polyurethane foam.
摘要翻译： 描述了一种导弹发射系统，其中导弹发射管的发射端由空心发射管盖保护。 发射管盖被分成多个段，这些段在导弹62的发射期间是易碎的并分散的。各个段的表面涂覆有防水材料，例如四氟乙烯或硅树脂，以防止积冰。 此外，发射管盖的头部的外表面可以涂覆有一层金属材料，以防止电磁干扰或射频干扰。 发射管盖由重量轻，防水的材料构成，例如膨胀的闭孔泡沫，包括聚氨酯泡沫。
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