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1. 发明授权

EP2092266B1 WARHEAD FOR INTERCEPTING SYSTEM 有权
标题翻译：战斗HEAD拦截
公开(公告)号：EP2092266B1
公开(公告)日：2014-12-24
申请号：EP07827316.6
申请日：2007-11-04
申请人： Rafael Advanced Defense Systems Ltd.
发明人： ROTKOPF, Menachem
IPC分类号： F42B10/00 , F42B30/00 , F42B12/00 , F42B12/14 , F42B12/12 , F42B12/10 , F42B12/32 , F42B1/02 , F42B12/58
CPC分类号： F42B1/02 , F42B12/10 , F42B12/12 , F42B12/14 , F42B12/32 , F42B12/58

2. 发明公开

EP0090001A4 PROJECTILE STABILIZATION FROM SMOOTH BORE BARREL. 失效
标题翻译： FLOOR用于稳定滑膛炮。
公开(公告)号：EP0090001A4
公开(公告)日：1985-04-11
申请号：EP82903012
申请日：1982-09-13
申请人： KUHL RAYMOND D
发明人： KUHL RAYMOND D
IPC分类号： F42B12/00 , F42B5/00 , F42B5/02 , F42B10/02 , F42B12/12 , F41G9/00 , F42B13/00
CPC分类号： F42B10/025

3. 发明授权

EP1297297B1 A METHOD AND DEVICE FOR DISPERSING SUBMUNITIONS 有权
标题翻译： DEVICE AND METHOD FORSUBMUNITIONKÖRPER的分散染料
公开(公告)号：EP1297297B1
公开(公告)日：2006-02-01
申请号：EP01944027.0
申请日：2001-06-20
申请人： BAE Systems Bofors AB
发明人： RÖNN, Torsten , AXINGER, Jan
IPC分类号： F42B12/12 , F42B12/58
CPC分类号： F42B12/60
摘要： The present invention relates to a method and a device for combating a pre-determined target with submunitions directed at the target from an airborne carrier in the form of a rocket, missile or equivalent (1) whereby the submunitions (17) are of the type whose main effect in target derives from impact with the target. As claimed in the present invention the submunitions (17) are given both a lateral motion vector (34) relative to the direction of flight of the carrier and a motion vector (35) in the direction of flight of the carrier. Jointly these motion vectors give the submunitions a resultant motion vector in a direction (36) towards the target. When the present invention is used the submunitions (17) are given the actual combined motion by the rotating magazine (5) in which they are stowed that rotates up to a high rate around the direction of flight of the carrier (1) before the submunitions leave the carrier when the centrifugal force gives them their lateral motion vector and they acquire their longitudinal motion vector from the direction of flight of the carrier.

4. 发明授权

US09476682B1 Multi-charge munitions, incorporating hole-boring charge assemblies 失效
标题翻译：多重弹药，包括钻孔装料
公开(公告)号：US09476682B1
公开(公告)日：2016-10-25
申请号：US07466711
申请日：1990-01-09
申请人： Kevin Mark Powell , Edward Evans
发明人： Kevin Mark Powell , Edward Evans
IPC分类号： F42B12/10 , F42B12/12 , F42B12/16 , F42B12/14 , F42B1/028 , F42B1/032 , F42B25/00 , F42B3/08
CPC分类号： F42B12/10 , F42B1/028 , F42B1/032 , F42B3/08 , F42B12/12 , F42B12/14 , F42B12/16 , F42B25/00
摘要： Multi-charge munition suitable for defeating a concrete target consists of a detonatable array of hollow primary charges (14) of explosive supported laterally of a line of target penetration on which is disposed a secondary explosive charge (48). Simultaneous detonation of the primary charges in the array causes jet penetrators to be projected together towards the target which produce wide boreholes in concrete suitable for the subsequent emplacement and detonation of the secondary charge. The munition may be an aerially-deliverable bomb or submunition.In one preferred embodiment, the primary charges (14) are positioned in a convergent configuration behind a forwardly-tapered secondary charge (48). Detonation of the primary charges projects penetrators forwardly passed the sides of the secondary charge and thrusts the secondary charge into the borehole produced in the target by the penetrators.
摘要翻译：在一个优选实施例中，主电荷（14）位于向前锥形次级电荷（48）后面的会聚配置中。主要电荷项目的爆破穿透者向前通过二次装置的侧面，并将次要电荷推入穿透器产生的钻孔中。

5. 发明授权

US4413565A Projectile with a tubular-shaped projectile body 失效
标题翻译：射弹与管状射弹体
公开(公告)号：US4413565A
公开(公告)日：1983-11-08
申请号：US373122
申请日：1982-04-29
申请人： Philippe Matthey , Robert Salmon , Niklaus Buhlmann
发明人： Philippe Matthey , Robert Salmon , Niklaus Buhlmann
IPC分类号： F42B12/12 , F42B10/34 , F42B13/16 , F42B11/00
CPC分类号： F42B10/34
摘要： Firing of a tubular-shaped projectile body containing a sharp-edged annular end surface previously created difficulties, because firing the end surface of the tubular-shaped projectile body was damaged by the sabot base portion by virtue of the large acceleration forces. This difficulty is avoided in that the invention contemplates incorporating an at least bipartite ring-shaped wedge member between a cone-shaped portion of the sabot base portion and a cone-shaped rear wall of the tubular-shaped projectile body.
摘要翻译：由于大的加速力，筒状射弹体的端面由于烧毁基座部分而被烧毁，所以发射包含尖锐的环形端面的管状的射弹体预先产生困难。避免了这个困难，因为本发明设想在膛体基部的锥形部分和管状射弹体的锥形后壁之间并入至少二分的环形楔形构件。

6. 发明授权

US4372239A Undersea weapon with hydropulse system and periodical seawater admission 失效
标题翻译：海底武器与水力脉冲系统和定期海水进入
公开(公告)号：US4372239A
公开(公告)日：1983-02-08
申请号：US126782
申请日：1980-03-03
申请人： Allen C. Hagelberg , Clark E. Allardt , Walter A. Lobitz , Robert O. Thornburg , George F. Zimmerman , Gary L. Letterman , John W. Helbron
发明人： Allen C. Hagelberg , Clark E. Allardt , Walter A. Lobitz , Robert O. Thornburg , George F. Zimmerman , Gary L. Letterman , John W. Helbron
IPC分类号： F41G7/22 , F42B12/12 , F42B17/00 , F42B19/00 , F42B19/01 , F42B19/12 , F42B19/26 , F42B19/46
CPC分类号： F41G7/228 , F42B17/00 , F42B19/26
摘要： An undersea weapon comprising a warhead, a rocket motor, detection, homing and control systems and a hydropulse underwater propulsion system in an integral unit. The weapon is launched at a previously detected target, such as a submarine, on a ballistic trajectory through the air by means of the rocket motor. The weapon enters the water near the submarine, which is thereafter detected by an on-board system incorporating active and/or passive detection. The thus-determined submarine direction is utilized by the control system to guide the weapon toward the submarine under water. A hydropulse motor utilizes the empty rocket motor as the propulsion chamber and provides the underwater propulsion to propel the weapon through the water toward the submarine, where the warhead then detonates on contact with the submarine. Alternatively, the weapon may be air dropped near a previously detected target, in which case there need be no propellant in the rocket motor. The hydropulse motor operates by repeatedly filling the chamber with water and expelling the water at high velocity through a converging nozzle in succeeding pulse stages. During the intervals between pulses, the detection system monitors the submarine free of noise from the on-board propulsion motor.
摘要翻译：一个海底武器，包括弹头，火箭发动机，检测，归位和控制系统以及整体单元中的水下脉冲水下推进系统。武器是通过火箭发动机通过空中的弹道轨迹在先前检测到的目标（如潜艇）上发射的。武器进入潜艇附近的水域，此后由包含有源和/或无源探测的车载系统进行检测。由此确定的潜艇方向由控制系统利用，以将武器引向水下的潜艇。水力冲击马达利用空的火箭发动机作为推进室，并提供水下推进力，以将武器通过水向潜艇提供，然后弹头在与潜艇接触时引爆。或者，武器可以在先前检测到的目标附近空气滴落，在这种情况下，在火箭发动机中不需要推进剂。水力脉冲电动机通过反复充满水并通过后续脉冲阶段中的会聚喷嘴高速排出水来进行操作。在脉冲间隔期间，检测系统监测潜艇没有来自车载推进电机的噪音。

7. 发明授权

US2633465A Penicillin salts of aminophenylpiperidine 失效
标题翻译：氨基苯基哌啶的青霉素盐
公开(公告)号：US2633465A
公开(公告)日：1953-03-31
申请号：US27142752
申请日：1952-02-13
申请人： LILLY CO ELI
发明人： RHODEHAMEL JR HARLEY W
IPC分类号： C07D499/00 , C07D499/26 , F42B12/12 , F42B15/00
CPC分类号： C07D499/00

8. 发明申请

WO02003013A1 A METHOD AND DEVICE FOR DISPERSING SUBMUNITIONS 审中-公开
标题翻译：一种分散子系统的方法和装置
公开(公告)号：WO02003013A1
公开(公告)日：2002-01-10
申请号：PCT/SE2001/001399
申请日：2001-06-20
IPC分类号： F42B12/60 , F42B12/12 , F42B12/58
CPC分类号： F42B12/60
摘要： The present invention relates to a method and a device for combating a pre-determined target with submunitions directed at the target from an airborne carrier in the form of a rocket, missile or equivalent (1) whereby the submunitions (17) are of the type whose main effect in target derives from impact with the target. As claimed in the present invention the submunitions (17) are given both a lateral motion vector (34) relative to the direction of flight of the carrier and a motion vector (35) in the direction of flight of the carrier. Jointly these motion vectors give the submunitions a resultant motion vector in a direction (36) towards the target. When the present invention is used the submunitions (17) are given the actual combined motion by the rotating magazine (5) in which they are stowed that rotates up to a high rate around the direction of flight of the carrier (1) before the submunitions leave the carrier when the centrifugal force gives them their lateral motion vector and they acquire their longitudinal motion vector from the direction of flight of the carrier.
摘要翻译：本发明涉及一种用于以火箭，导弹或等同物形式从空中载体以目标指向目标的子弹药来对预定目标进行打击的方法和装置（1），其中子弹药（17）是类型其目标的主要影响来自于与目标的冲击。如本发明所要求的，子弹药（17）给予相对于载体的飞行方向的横向运动矢量（34）和在载体的飞行方向上的运动矢量（35）。这些运动向量联合地向子弹药提供朝向目标的方向（36）的合成运动矢量。当使用本发明时，子弹药（17）通过其存放的旋转刀库（5）被给予实际的组合运动，其在子弹药之前围绕载体（1）的飞行方向旋转高速率当离心力给出它们的横向运动矢量时，离开载体，并且它们从载体的飞行方向获取它们的纵向运动矢量。

9. 发明申请

WO2017103323A1 WEAPON/HAND GRENADE 审中-公开
标题翻译：武器/手刨
公开(公告)号：WO2017103323A1
公开(公告)日：2017-06-22
申请号：PCT/FI2016/000029
申请日：2016-12-08
申请人： KAMILA, Ilmari
发明人： KAMILA, Ilmari
IPC分类号： F42B12/12 , F42B12/32 , F42B27/00 , G01S19/18
CPC分类号： G01S19/18 , F42B10/26 , F42B12/12 , F42B12/207 , F42B12/32 , F42B12/56 , F42B23/16 , F42B27/00 , F42B27/08
摘要： The invention relates to a weapon/hand grenade (10) consisting of a substantially spherical shell containing a fragment-dispersing charge (3). The fragment-dispersing charge (3) and the electronics (2) of the weapon form a single unit, which is mounted onto bearings (5) within the shell and weighted so as to be allowed to rotate freely, with the fragment-dispersing charge (3) remaining always in vertical upright position under the effect of gravitation.
摘要翻译：本发明涉及一种武器/手榴弹（10），其由包含碎片分散装药（3）的基本上为球形的外壳组成。该武器的碎片分散装药（3）和电子装置（2）形成一个单元，该单元安装在壳体内的轴承（5）上并且被加权以允许其自由旋转，碎片分散装药（3）在万有引力的作用下始终处于垂直竖直位置。

10. 发明申请

WO2022125155A1 SYMPATHETICALLY DETONATED SELF-CENTERING EXPLOSIVE DEVICE 审中-公开
公开(公告)号：WO2022125155A1
公开(公告)日：2022-06-16
申请号：PCT/US2021/047435
申请日：2021-08-25
申请人： RAYTHEON COMPANY [US]/[US]
发明人： SADLER, Coulton , MOFFET, Mitchell , KIM, Henri Y.
IPC分类号： E21B43/117 , F42B1/02 , F42B3/08 , F42B12/10 , F42B12/12
摘要： An explosive device includes a housing having an outer surface and defining an inner space; a plurality of primary liners arranged on the outer surface in a spaced pattern and having primary energetic material inwardly positioned in the housing relative to the primary liners; an initiation mechanism in the inner space for initiating the primary energetic material to drive the primary liners; and a plurality of additional liners positioned in the spaced pattern between the primary liners and having additional energetic material positioned in proximity to the primary energetic material such that the additional energetic material is sympathetically initiated by initiation of the primary energetic material. The device can find useful application in a military setting and also in the perforation of well casings in subterranean wells.

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