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91. 发明申请

US20080048931A1 Helmet System for Information or Weapon Systems 审中-公开
标题翻译：信息或武器系统头盔系统
公开(公告)号：US20080048931A1
公开(公告)日：2008-02-28
申请号：US10596006
申请日：2004-11-18
申请人： Tsafrir Ben-Ari
发明人： Tsafrir Ben-Ari
IPC分类号： G09G5/00
CPC分类号： G02B27/017 , A42B3/0433 , A61B3/113 , A61B5/11 , A61B5/6814 , A61B2562/0219 , F41G3/225 , G01C21/165 , G01S5/163 , G02B2027/0187 , G06F3/012 , G06F3/013 , G06F3/0304
摘要： A helmet position measuring system for use in a predefined environment. The system includes a helmet-mounted illumination system for directing electromagnetic radiation of one or more wavelength from the helmet in one or more range of angles, a set of three or more passive reflectors deployed at fixed positions in the predefined environment to reflect electromagnetic radiation from the illumination system, a helmet-mounted imaging system sensitive to the one or more wavelength for deriving images of part of the predefined environment including electromagnetic radiation reflected from the reflectors, and a processing system associated with the imaging system for processing the images to identify regions of the images corresponding to the reflectors and hence to determine information relating to a position of the helmet within the predefined environment.
摘要翻译：一种用于预定义环境的头盔位置测量系统。该系统包括头盔安装的照明系统，用于以一个或多个角度范围从头盔引导一个或多个波长的电磁辐射，一组三个或更多个无源反射器，部署在预定环境中的固定位置，以反映来自照明系统，对于一个或多个波长敏感的头盔安装的成像系统，用于导出预定环境的一部分的图像，包括从反射器反射的电磁辐射，以及与成像系统相关联的处理系统，用于处理图像以识别区域并且因此确定与预定环境内的头盔的位置有关的信息。

92. 发明授权

US07336216B2 Parachuted radar decoy 失效
标题翻译：降落雷达诱饵
公开(公告)号：US07336216B2
公开(公告)日：2008-02-26
申请号：US11406446
申请日：2006-04-18
申请人： Gil Weisbrod
发明人： Gil Weisbrod
IPC分类号： H01Q15/00 , H04K3/00 , G01S13/00
CPC分类号： H01Q15/18 , G01S7/38 , H01Q15/20
摘要： A radar decoy having radar reflectors disposed in the interior of the inflated canopy of a descending parachute as a first set of four corner reflectors, and a second set of corner reflectors disposed on the exterior of the canopy integral with the first set of corner reflectors, to form an octahedron of eight corner reflectors. The radar decoy is pliable and folded with the parachute for stowage in the interior of a canister. When loaded on a vehicle flying in a trajectory, the canister may open at a point P on the trajectory, to release the parachute, and thereby deploy the radar decoy to become operative.
摘要翻译：雷达诱饵具有雷达反射器，其设置在下降降落伞的充气舱顶的内部，作为第一组四个角反射器，以及设置在与第一组角反射器集成的顶篷的外部上的第二组角反射器，形成八角反射器的八面体。雷达诱饵是柔韧的，并与降落伞折叠，用于装载在罐的内部。当装载在以轨迹飞行的车辆上时，罐可以在轨迹上的点P处打开，以释放降落伞，从而部署雷达诱饵使其变得可操作。

93. 发明申请

US20080040895A1 Highly-Filled, High-Viscosity Paste Charge, And Method And Device For Production Thereof 有权
标题翻译：高填充，高粘度糊剂，及其生产方法和装置
公开(公告)号：US20080040895A1
公开(公告)日：2008-02-21
申请号：US11747925
申请日：2007-05-14
申请人： Tamar Kaully , Dganit Shacham , Haim Baniste , David Tidhar , Corrine Nadiv
发明人： Tamar Kaully , Dganit Shacham , Haim Baniste , David Tidhar , Corrine Nadiv
IPC分类号： B01D19/00 , C06B45/06
CPC分类号： C06B21/0025 , B01D19/0036 , C06B25/34 , C06B45/00 , F42B1/036 , F42B33/025 , Y10S425/812
摘要： A highly-filled paste, and a method and device of de-aerating and injecting the paste, the paste including: (a) a solid filler; (b) an organic binder, and (c) a residual gas, wherein the paste contains at least 80 volume-% of the solid filler and has a viscosity exceeding 100 kilopascal·seconds, wherein the filler, binder, and residual gas are intimately mixed so as to form a substantially homogeneous paste, and wherein a composition of the solid filler, binder, and residual gas is selected such that the homogeneous paste has: an average density greater than 98.5% of a Theoretical Maximum Density (TMD).
摘要翻译：一种高填充糊剂，以及脱气和喷射糊剂的方法和装置，所述糊剂包括：（a）固体填料; （b）有机粘合剂，和（c）残余气体，其中所述浆料含有至少80体积％的固体填料，并且具有超过100千帕斯卡的粘度，其中填料，粘合剂和残留气体是密切的混合以形成基本上均匀的糊料，并且其中选择固体填料，粘合剂和残余气体的组合物，使得均匀的糊剂具有大于理论最大密度（TMD）的98.5％的平均密度。

94. 发明申请

US20080002858A1 Photogrammetric mapping of inaccessible terrain 审中-公开
标题翻译：不可访问地形的摄影测绘图
公开(公告)号：US20080002858A1
公开(公告)日：2008-01-03
申请号：US11453073
申请日：2006-06-15
申请人： Menachem Devir
发明人： Menachem Devir
IPC分类号： G06K9/00
CPC分类号： G01C11/02 , G01C15/02
摘要： A device for establishing a ground control point photogrammetry. The Device includes a signaling mechanism for providing a photographically recordable signature, and a navigation mechanism for determining absolute geographic coordinates of the signaling mechanism.
摘要翻译：用于建立地面控制点摄影测量的装置。该装置包括用于提供照相可记录签名的信令机制和用于确定信令机制的绝对地理坐标的导航机制。

95. 发明申请

US20070281358A1 Simultant Material and Method for Manufacture Thereof 失效
标题翻译：模拟材料及其制造方法
公开(公告)号：US20070281358A1
公开(公告)日：2007-12-06
申请号：US11660737
申请日：2005-08-08
申请人： Yael Cohen-Arazi , Tamar Kaully , Edith Sokol , Aviv Nisan
发明人： Yael Cohen-Arazi , Tamar Kaully , Edith Sokol , Aviv Nisan
IPC分类号： G01N33/22
CPC分类号： A01K15/02 , C06B23/001 , F41H11/132 , F42B8/00 , Y10T436/10
摘要： A simulant material for simulating hazardous materials, comprising a quantity of at least one explosive material and at least one inert material. The simulant material is a non-explosive material and is in the form of a homogenous, flexible and non-particulated material. The invention is also concerned with a method for manufacturing such a stimulant material
摘要翻译：一种用于模拟危险材料的模拟材料，包括至少一种爆炸性材料和至少一种惰性材料。模拟材料是非爆炸性材料，并且是均匀，柔性和无颗粒材料的形式。本发明还涉及制造这种兴奋剂材料的方法

96. 发明授权

US07273001B2 Modular launch-cell system 失效
标题翻译：模块化发射单元系统
公开(公告)号：US07273001B2
公开(公告)日：2007-09-25
申请号：US11159171
申请日：2005-06-23
申请人： Ehud Dekel
发明人： Ehud Dekel
IPC分类号： F41F3/04
CPC分类号： F41F3/042 , F42B39/00
摘要： A modular launch-cell system for a launch vehicle. The method includes a number of launch-cells, a base and an upper attachment arrangement. The launch-cells include a missile and are arranged in a structure which includes a number of layers, each of the layer includes two or more launch cells. The launch-cells are substantially directly reversibly mechanically connected to the base. One of the launch-cells includes a lower attachment arrangement configured for reversibly mechanically connecting one launch-cell to one or more of the base and another of the launch-cells disposed below the one launch-cell. The upper arrangement is designed for reversibly mechanically connecting one launch-cell to another of the launch-cells disposed above the one launch-cell.
摘要翻译：用于运载火箭的模块化发射单元系统。该方法包括许多发射单元，基座和上部附接装置。发射单元包括导弹，并且布置在包括多个层的结构中，每个层包括两个或更多个发射单元。发射单元基本上直接可逆地机械地连接到基座。其中一个发射单元包括一个较低的附接装置，其配置用于将一个发射单元可逆地机械地连接到一个或多个设置在一个发射单元下方的发射单元的基座和另一个发射单元。上部装置设计用于将一个发射单元可逆地机械地连接到设置在一个发射单元上方的发射单元的另一个。

97. 发明申请

US20070129853A1 AIRBORNE RECONNAISSANCE SYSTEM 有权
标题翻译： AIRBORNE重新建立系统
公开(公告)号：US20070129853A1
公开(公告)日：2007-06-07
申请号：US11538882
申请日：2006-10-05
申请人： Israel GREENFELD , Zvi YAVIN , Bernd UHL
发明人： Israel GREENFELD , Zvi YAVIN , Bernd UHL
IPC分类号： G01C23/00
CPC分类号： G01C11/02
摘要： A airborne reconnaissance system comprising: (1) Gimbals having at least two degrees of freedom; (2) At least one array of light sensors positioned on the gimbals, for being directed by the same within at least two degrees of freedom; (3) Map storage means for storing at least one Digital Elevation Map of an area of interest, divided into portions; (4) Inertial Navigation System for real-time providing to a gimbals control unit navigation and orientation data of the aircraft with respect to a predefined global axes system; (5) Portion selection unit for selecting, one at a time, another area portion from the area of interest; and (6) servo means for directing the gimbals. The system uses data from the inertial navigational system and from the digital elevation map for real-time calculating direction to selected area portions, and for maintaining the direction during integration of light from the terrain, and for producing corresponding images of area portions.
摘要翻译：一种机载侦察系统，包括：（1）具有至少两个自由度的万岁者; （2）定位在万向面上的至少一组光传感器，由至少两个自由度引导; （3）地图存储装置，用于存储感兴趣区域的至少一个数字高程图，被分成多个部分; （4）惯性导航系统，用于相对于预定义的全局轴系统实时提供飞行器的万向节控制单元导航和定向数据; （5）部分选择单元，用于一次一个地选择来自感兴趣区域的另一区域部分; 和（6）用于引导万向架的伺服装置。该系统使用来自惯性导航系统的数据和数字高程图的实时计算方向的数据，并且用于在来自地形的光的集成期间保持方向，并且用于产生区域部分的相应图像。

98. 发明授权

US07163731B2 Lightweight armor against firearm projectiles 失效
标题翻译：轻型装甲防弹枪
公开(公告)号：US07163731B2
公开(公告)日：2007-01-16
申请号：US09904585
申请日：2001-07-16
申请人： Yehoshua Yeshurun , Yechezkel Ashuach , Zvi Rosenberg , Moshe Rozenfeld
发明人： Yehoshua Yeshurun , Yechezkel Ashuach , Zvi Rosenberg , Moshe Rozenfeld
IPC分类号： B32B5/12 , B32B7/00 , F41H5/00 , F41H5/04
CPC分类号： F41H5/0407 , F41H5/04 , Y10S428/911 , Y10T428/24116 , Y10T428/24174 , Y10T428/24752 , Y10T428/2476 , Y10T442/20
摘要： An armor assembly for protecting a body disposed behind said armor assembly, wherein the armor assembly comprises at least one layer of material made of an essentially brittle material, said layer extending slanted relative the expected trajectory of an oncoming firearm projectile.
摘要翻译：一种用于保护设置在所述装甲组件后面的主体的装甲组件，其中所述装甲组件包括由基本上脆性材料制成的至少一层材料，所述层相对于迎面而来的枪支射弹的预期轨迹倾斜延伸。

99. 发明授权

US07136726B2 Airborne reconnaissance system 有权
标题翻译：机载侦察系统
公开(公告)号：US07136726B2
公开(公告)日：2006-11-14
申请号：US10484677
申请日：2003-05-22
申请人： Israel Greenfeld , Zvi Yavin , Bernd Uhl
发明人： Israel Greenfeld , Zvi Yavin , Bernd Uhl
IPC分类号： G01C11/02 , G01S3/786 , G01C21/00
CPC分类号： G01S3/7864 , F41G5/14 , F41G7/2213 , F41G7/2253 , F41G7/2293 , G01C11/025 , G01C21/005 , G01C21/165
摘要： An airborne reconnaissance system comprising: (1) Gimbals having at least two degrees of freedom; (2) At least one array of light sensors positioned on the gimbals, for being directed by the same within at least two degrees of freedom; (3) Map storage means for storing at least one Digital Elevation Map of an area of interest, divided into portions; (4) Inertial Navigation System for real-time providing to a gimbals control unit navigation and orientation data of the aircraft with respect to a predefined global axes system; (5) Portion selection unit for selecting, one at a time, another area portion from the area of interest; and (6) servo means for directing the gimbals. The system uses data from the inertial navigation system and from the digital elevation map for real-time calculating direction to selected area portions, and for maintaining the direction during integration of light from the terrain, and for producing corresponding images of area portions.
摘要翻译：一种机载侦察系统，包括：（1）具有至少两个自由度的万用表; （2）定位在万向面上的至少一组光传感器，由至少两个自由度引导; （3）地图存储装置，用于存储感兴趣区域的至少一个数字高程图，被分成多个部分; （4）惯性导航系统，用于相对于预定义的全局轴系统实时提供飞行器的万向节控制单元导航和定向数据; （5）部分选择单元，用于一次一个地选择来自感兴趣区域的另一区域部分; 和（6）用于引导万向架的伺服装置。该系统使用来自惯性导航系统的数据和数字高程图的实时计算方向的数据，并且用于在来自地形的光的集成期间保持方向，并且用于产生区域部分的相应图像。

100. 发明申请

US20060239120A1 Flash event detection with acoustic verification 失效
标题翻译：闪存事件检测与声学验证
公开(公告)号：US20060239120A1
公开(公告)日：2006-10-26
申请号：US11347220
申请日：2006-02-06
申请人： Erez Berkovich , Ofer Solomon
发明人： Erez Berkovich , Ofer Solomon
IPC分类号： G01S3/80
CPC分类号： G01S11/12 , G01S11/14 , G01S11/16
摘要： A system for identifying flash events including an optical imaging module with one or more optical imaging array, the optical imaging module configured for monitoring a region of interest to identify a tentative flash event. The system further includes a ranging module associated with the optical imaging module and configured to derive an estimated range to a location of the tentative flash event, and an acoustic verification module associated with the ranging module and with one or more acoustic sensor. The acoustic verification module is configured to determine whether an acoustic event corresponding to the tentative flash event is detected within a time window derived from the estimated range, thereby classifying the tentative flash event as either a verified flash event or a rejected flash event.
摘要翻译：一种用于识别闪光事件的系统，包括具有一个或多个光学成像阵列的光学成像模块，所述光学成像模块被配置为监视感兴趣的区域以识别临时闪存事件。该系统还包括与光学成像模块相关联的测距模块，并且被配置为将估计的范围导出到临时闪光事件的位置，以及与测距模块相关联并与一个或多个声学传感器相关联的声学验证模块。声学验证模块被配置为确定在从估计范围导出的时间窗内是否检测到与暂定闪光事件相对应的声学事件，从而将暂定闪光事件分类为已验证的闪光灯事件或被拒绝的闪光灯事件。

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