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1. 发明公开

EP1922665A4 METHOD AND APPARATUS FOR IMPACT DETECTION AND PRIORITIZATION OF IMPACT INFORMATION TRANSMITTED TO A RECEIVING STATION 有权
标题翻译：方法和装置碰撞检测和优先次序，以一台发送的影响的信息
公开(公告)号：EP1922665A4
公开(公告)日：2010-08-18
申请号：EP06851401
申请日：2006-06-09
申请人： ITT MFG ENTERPRISES INC
发明人： PADEREWSKI GARY , LESAGE JOHN
IPC分类号： G08B13/08 , F42B12/36 , F42B30/00
CPC分类号： F42B12/365 , F42B30/006

2. 发明授权

EP1322903B1 DUAL-FREQUENCY MILLIMETER WAVE AND LASER RADIATION RECEIVER 有权
标题翻译： FOR两个频率爆炸毫米波和激光辐射接收器
公开(公告)号：EP1322903B1
公开(公告)日：2010-05-12
申请号：EP00981527.5
申请日：2000-12-05
申请人： Alenia Marconi Systems Incorporated
发明人： SANDERS, Ross, J. , SHMOLDAS, John, Dusan , WICKS, Dean, Arthur
IPC分类号： F41G7/22 , F41G7/00 , G01S13/86
CPC分类号： F41G7/226 , F41G7/008 , F41G7/2286 , F41G7/2293 , F42B30/006 , G01S3/00 , H01Q1/281 , H01Q3/16 , H01Q19/19

3. 发明授权

EP1241435B1 Projektil und Verfahren zu dessen Herstellung 有权
标题翻译：弹丸及制造方法
公开(公告)号：EP1241435B1
公开(公告)日：2007-01-17
申请号：EP02002216.6
申请日：2002-01-30
申请人： RWM Schweiz AG
发明人： Ettmüller, Peter
IPC分类号： F42B12/76 , F42C19/02
CPC分类号： F42B30/006 , F42B12/76 , F42C19/02

4. 发明授权

EP1178279B1 Munitionsartikel mit Antenne für die Satellitennavigation 有权
标题翻译：弹药文章天线用于卫星导航
公开(公告)号：EP1178279B1
公开(公告)日：2004-11-10
申请号：EP01118654.1
申请日：2001-08-03
申请人： Diehl Munitionssysteme GmbH & Co. KG
发明人： Koch, Volker , Hertel, Martin , Wiesbeck, Werner, Dr. , Gschwendtner, Eberhard
IPC分类号： F42C19/00
CPC分类号： H01Q1/286 , F42B30/006 , F42C19/00 , H01Q13/10

5. 发明公开

EP1322903A1 DUAL-FREQUENCY MILLIMETER WAVE AND LASER RADIATION RECEIVER 有权
标题翻译： FOR两个频率爆炸毫米波和激光辐射接收器
公开(公告)号：EP1322903A1
公开(公告)日：2003-07-02
申请号：EP00981527.5
申请日：2000-12-05
申请人： Alenia Marconi Systems Incorporated
发明人： SANDERS, Ross, J. , SHMOLDAS, John, Dusan , WICKS, Dean, Arthur
IPC分类号： F41G7/22 , F41G7/00 , G01S13/86
CPC分类号： F41G7/226 , F41G7/008 , F41G7/2286 , F41G7/2293 , F42B30/006 , G01S3/00 , H01Q1/281 , H01Q3/16 , H01Q19/19
摘要： A tandem dual-frequency sensor for a missile that uses a steerable dichroic primary millimeter wave reflector to reflect millimeter wave energy to a secondary reflector while passing laser light in the infra-red region through a dichroic region of the reflector to multiple staring laser detectors mounted behind the primary reflector.

6. 发明公开

EP0816762A2 Radome nose cone probe apparatus for use with electrostatic sensor 失效
标题翻译：探测器雷达接收器
公开(公告)号：EP0816762A2
公开(公告)日：1998-01-07
申请号：EP97110242.1
申请日：1997-06-23
申请人： ALLIANT TECHSYSTEMS INC.
发明人： Crist, Scott D.
IPC分类号： F24C13/00
CPC分类号： F42B30/006 , F42C13/003
摘要： A radome probe apparatus for use with an electrostatic proximity sensor is disclosed. The apparatus comprises a radome nose cone probe connected to a projectile and having an inner surface. The nose cone is made of a dielectric material. Single or multiple electrically conducting areas are connected to the inner surface of the nose cone. The conducting areas are dielectrically isolated. Electronics are utilized to sense the time rate of change voltage or current between the areas due to the intrinsic electrostatic charge on a target aircraft.
摘要翻译：公开了一种用于静电接近传感器的雷达探测器。该装置包括连接到射弹并具有内表面的天线罩鼻锥探头。鼻锥由电介质材料制成。单个或多个导电区域连接到鼻锥的内表面。导电区域是介电隔离的。电子装置用于感测由于目标飞行器上的固有静电电荷引起的区域之间的时间变化电压或电流的时间速率。

7. 发明公开

EP3264024A1 NOSE CONE COMPRISING ELECTRONIC CIRCUIT BOARDS ARRANGED RADIALLY 无效
标题翻译：包括电子电路板在内的鼻锥体
公开(公告)号：EP3264024A1
公开(公告)日：2018-01-03
申请号：EP16275091.3
申请日：2016-06-28
申请人： BAE SYSTEMS plc
发明人： The designation of the inventor has not yet been filed
IPC分类号： F42B15/01 , F42B30/00 , G06F15/78 , G06F15/80 , H05K7/14 , H05K7/20 , F42B10/46 , F42B19/00
CPC分类号： F42B15/01 , F42B10/46 , F42B19/005 , F42B30/006 , H05K1/141 , H05K3/366 , H05K7/1434 , H05K2201/048
摘要： The invention relates to A nose cone assembly for a munition, comprising a transducer array operably linked to a transmission assembly, wherein the transducer array is operably connected to a transducer housing, said transducer housing comprising a first and second surface, wherein said transmission assembly is reversibly operably connected to the second surface of said transducer housing,
said transmission assembly comprising a control board and a plurality of electronic circuit boards, wherein at least one electronic circuit board is a transceiver circuit board,
said electronic circuit boards being reversibly connected to the control board and being arranged along their longest dimension, at an axis substantially perpendicular to the control board and further arranged such that the electronic circuit boards extend radially inwardly to a substantially rotational centre of the control board.
摘要翻译：本发明涉及一种用于弹药甲鼻锥体组件，其包括换能器阵列可操作地连接到传动组件，其中，所述换能器阵列被可操作地连接到换能器壳体，所述换能器壳体，其包括第一和第二表面，其中，所述传动组件是可逆地可操作地连接到所述换能器壳体的第二表面，所述传动组件包括一个控制基板和多个电子电路板，其中，至少一个电子电路板是收发器电路板，所述电子电路板被可逆地连接到所述控制沿着其最长尺寸布置在基本上垂直于控制板的轴线上，并且还布置成使得电子电路板径向向内延伸至控制板的大致旋转中心。

8. 发明公开

EP2871438A1 Rocket or artillery launched smart reconnaissance pod 失效转让
标题翻译：通过火箭或枪的手段击落智能集装箱侦察
公开(公告)号：EP2871438A1
公开(公告)日：2015-05-13
申请号：EP14192253.4
申请日：2014-11-07
申请人： Lonestar Inventions L.P.
发明人： Akcasu, Osman Ersed , Uslu, Ibrahim Onur , Leblebici, Yusuf
IPC分类号： F42B10/56 , F42B12/36 , F42B12/58 , F42B10/50
CPC分类号： F42B12/365 , B64D17/00 , F42B5/025 , F42B10/50 , F42B10/56 , F42B12/58 , F42B30/006
摘要： A modular reconnaissance capsule or reconnaissance pod (10) is provided that is suitable for deployment by means of an artillery launching platform, such as a conventional 40 mm grenade launcher or 155 mm cannon wherein a parachute (24) is deployed at a pre-calculated observation altitude, the parachute (24) being designed to yield a sufficiently slow rate of descent to permit live video capture and transmission of images as forward observation information. Alternatively, pods according to the invention may also be air dropped from an aircraft, either piloted or pilotless, thus allowing the aircraft to operate at a safe distance and yet provide close reconnaissance even under a cloud cover. Accurate information about targeting dynamics is made available to the user through commercially available products. The invention complements other reconnaissance methods and provides easy-to-use real-time visual information for a desired area of interest.
摘要翻译：提供了一种模块化的侦察胶囊或侦察吊舱（10）所做的是适于部署由火炮发射平台的方式，检查作为worin降落伞（24）被部署在预先计算的一个传统的40mm榴弹发射或155毫米炮观察高度，降落伞（24）被设计成产生下降的足够慢的速度，以允许实时视频捕获和图像作为正向观察信息的传输。可替代地，豆荚gemäß发明因此可以是空气从飞机下降到，无论是驾驶或无人驾驶，因此允许飞机在安全距离操作，但甚至在云盖提供接近侦察。有关定位动态的准确信息，通过市售的产品提供给用户。本发明补充了其他的侦察方法，并提供期望的感兴趣区域易于使用的实时视觉信息。

9. 发明公开

EP2446505A1 HALTERUNG FÜR EINEN BEWEGBAREN SENSOR 审中-公开
标题翻译：支持对可移动的传感器
公开(公告)号：EP2446505A1
公开(公告)日：2012-05-02
申请号：EP10735182.7
申请日：2010-06-21
申请人： EADS Deutschland GmbH
发明人： AHRING, Bernhard , CHRISTOF, Horst
IPC分类号： H01Q1/18 , H01Q1/28 , F42B30/00 , H01Q3/08
CPC分类号： F42B30/006 , F41H5/26 , H01Q1/1207 , H01Q1/1242 , H01Q3/08
摘要： The invention relates to a holder for a movable sensor (1), which can be directed towards a sensor target (T), on a supporting structure (2), which holder contains at least two sensor-side bearings (22, 24; 26) at a distance to each other, at least two supporting-structure-side bearings (32, 34; 36) at a distance to each other, at least two length-adjustable actuating drive units (4, 5; 6), wherein each of the actuating drive units (4, 5; 6) is provided between an associated sensor-side bearing (22, 24; 26) and an associated supporting-structure-side bearing (32, 34; 36), and a center bearing (7; 8), which is designed in such a way that the center bearing supports the sensor (1) on the supporting structure (2) so that the sensor can be swiveled about a kinematic swivel center point about at least two spatial axes (X, Y; Z).

10. 发明公开

EP2167901A1 OPTICAL ELEMENT MOUNT AND METHOD THEREOF FOR A GUN-LAUNCHED PROJECTILE 审中-公开
标题翻译：支援，为某型高炮弹丸的光学元件及相应方法
公开(公告)号：EP2167901A1
公开(公告)日：2010-03-31
申请号：EP08836123.3
申请日：2008-06-04
申请人： Raytheon Company
发明人： JOHNSON, Gary, H. , BEARD, Douglas, M. , THOMAS, John, A. , PEREZ, Rene, D.
IPC分类号： F41G7/00 , F41G9/00 , F42B10/00 , F42B15/00 , H01Q1/42 , H01Q1/40 , F41A3/00 , G02B3/00 , G02B7/00 , G02B9/00 , G02B11/00
CPC分类号： F42B30/006 , F41G7/2253 , F41G7/226 , F41G7/2293 , G02B7/00 , G02B7/007 , G02B7/02
摘要： An optical element mount is effective in high G environments to protect brittle optical elements in which tensile stresses are generated on surface S2 without degrading optical performance. A flexible spacer formed of a relatively low-stiffness material supports an optical element having a tapered outer periphery in an optical seat having a complementary tapered surface. When the optical assembly is exposed to the high G environment, the inertial loading drives the optical element in the aft direction into the flexible spacer and seat. This puts the optical element into a plate bending condition thereby inducing tensile stress on S2 which is at least partially offset by a compressive stress caused by the reaction force normal to the tapered interface. The stresses, both compressive and tensile, placed on the optical element in the high G environment can be very large. In the absence of the tapered mount and flexible spacer, the tensile stress placed on S2 would likely fracture or shatter the brittle optical element. When the inertial loading is removed, the optical element returns to its initial unstressed position.

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