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1. 发明申请

US20160209191A1 COMMON CARRIER MUNITION 有权
标题翻译：通用运动员
公开(公告)号：US20160209191A1
公开(公告)日：2016-07-21
申请号：US14913088
申请日：2014-08-18
申请人： BAE SYSTEMS PLC
发明人： DANIEL ALEXANDER ADAMS , MATTHEW JONES , ANDY ODEN BURN , DAVID JOHN COSTIN , STUART ANDREW MCCOMBIE , JOHN WAINWRIGHT , MICHAEL SHAUN RUMFITT
IPC分类号： F42B12/62 , F42B12/42
CPC分类号： F42B12/625 , F42B12/42
摘要： The invention relates to a common carrier munition ammunition device, more particularly to common carrier payload delivery shell.There is provided a common carrier munition comprising a tail unit, a main body which comprises a payload cavity for receiving a payload, a fuze, and located between said main body and the fuze an ogive element, wherein the tail unit and main body comprise cooperatively engaging male and female threaded portions, wherein at least one of the threads is a shearable thread.
摘要翻译：本发明涉及一种共同的载体弹药装置，更具体地涉及公共载体有效载荷输送壳。提供了一种共同的载体弹药，包括尾部单元，主体，其包括用于接收有效载荷的有效载荷空腔，引信，并且位于所述主体和引信之间，其中尾部单元和主体协作地包括接合的阳螺纹和阴螺纹部分，其中至少一个螺纹是可剪切的螺纹。

2. 发明申请

US20150136913A1 Systems and Methods for Launching Space Vehicles 审中-公开
标题翻译：发射太空车的系统和方法
公开(公告)号：US20150136913A1
公开(公告)日：2015-05-21
申请号：US14084006
申请日：2013-11-19
申请人： David G. DILLON
发明人： David G. DILLON
IPC分类号： B64G1/00 , B64G1/52 , B64G1/66 , B64G5/00
CPC分类号： B64G1/002 , B64G1/58 , B64G5/00 , F41B6/00 , F41B6/006 , F42B5/045 , F42B12/625
摘要： Systems and methods for launching space vehicles into orbit involve placing a space vehicle into a protective container. The protective container is placed on a sled in a maglev tunnel and then launched into the atmosphere. Once the protective container reaches a certain height the space vehicle is released from the protective container and the space vehicle then proceeds to the desired orbital position.
摘要翻译：将空间车辆发射进入轨道的系统和方法涉及将空间车辆放入保护容器中。将保护容器放置在磁悬浮隧道中的雪橇上，然后发射到大气中。一旦保护容器达到一定高度，空间车辆就从保护容器中释放出来，然后空间车辆进入所需的轨道位置。

3. 发明申请

US20130199394A1 Segmented missile approach 有权
标题翻译：分段导弹方法
公开(公告)号：US20130199394A1
公开(公告)日：2013-08-08
申请号：US13506226
申请日：2012-04-05
申请人： Nicholas Collier
发明人： Nicholas Collier
IPC分类号： F42B12/18
CPC分类号： F42B12/18 , F42B12/625
摘要： This invention is a segmented missile that uses multiple circular linear shaped charge warheads deployed in tandem. Each warhead is capable of full-caliber holes and 5 to 15 charge diameters of penetration for each warhead, depending on the target material. The full-caliber hole capability allows for the warheads to travel down the hole made by the previous warhead. Each warhead is sequenced in its time of arrival at the bottom of the hole, allowing for a cumulative effect.
摘要翻译：本发明是一种分段导弹，其使用串联部署的多个圆形直线形充电弹头。根据目标材料，每个弹头能够具有全口径的孔和针对每个弹头的5至15个充电直径的穿透。全口径孔能力允许弹头沿着先前弹头所形成的孔行进。每个弹头在到达孔底部的时间内进行排序，从而达到累积效果。

4. 发明授权

US08408139B2 Projectile 失效
标题翻译：射弹
公开(公告)号：US08408139B2
公开(公告)日：2013-04-02
申请号：US12786124
申请日：2010-05-24
申请人： Christian Baumann , Thomas Heitmann
发明人： Christian Baumann , Thomas Heitmann
IPC分类号： F42B12/22
CPC分类号： F42B12/22 , F42B12/207 , F42B12/625
摘要： A projectile (1) is optionally used as a fragmentation projectile or as a projectile that utilizes a pressure wave effect created when the explosive charge (3) explodes. The projectile (1) contains an ejection charge (12), and an explosive charge (3) arranged in a jacket (4) that can be moved axially with respect to a fragmentation casing (5). The ejection charge (12) allows the explosive charge (3) and surrounding jacket (4) to be pushed at least so far out of the projectile casing (2) that, in the event of explosion, the explosive charge does not act on the fragmentation casing (5). In order to ensure that the jacket (4) of the explosive charge (3) does not develop any fragmentation effect, or develops only a small fragmentation effect, when the explosive charge (3) is ignited, a molded part composed of plastic or a light alloy is used as the jacket (4).
摘要翻译：抛射体（1）可选地用作碎裂射弹或使用当爆炸炸药（3）爆炸时产生的压力波效应的射弹。射弹（1）包含喷射装置（12）和布置在护套（4）中的爆炸装药（3），其可以相对于碎裂壳体（5）轴向移动。喷射装置（12）允许爆炸装药（3）和周围护套（4）至少被推到射弹套管（2）外，即在爆炸的情况下，爆炸装药不会对碎片套（5）。为了确保炸药（3）的护套（4）不会产生任何碎裂效应，或仅产生小碎裂效应，当炸药（3）被点燃时，由塑料或轻合金用作护套（4）。

5. 发明申请

US20120043149A1 LAUNCHABLE REMOTE-CONTROL ATTACK DEVICE 有权
标题翻译：可启动的远程控制攻击装置
公开(公告)号：US20120043149A1
公开(公告)日：2012-02-23
申请号：US13213291
申请日：2011-08-19
申请人： Soohyun KIM , Kyung-Soo KIM , Jeehyoung KIM , Bong-soo Kang , Wonsuk JUNG , Chulyoung KIM , Yunsic HONG , Hyunsoo PARK , Kyuje YOO , Doo-Yeol Koh , Seung-Ho LEE , Min-Gu Lee
发明人： Soohyun KIM , Kyung-Soo KIM , Jeehyoung KIM , Bong-soo Kang , Wonsuk JUNG , Chulyoung KIM , Yunsic HONG , Hyunsoo PARK , Kyuje YOO , Doo-Yeol Koh , Seung-Ho LEE , Min-Gu Lee
IPC分类号： F41H13/00
CPC分类号： F41H7/005 , B25J11/002 , F41G7/30 , F41H9/04 , F42B12/20 , F42B12/365 , F42B12/50 , F42B12/58 , F42B12/625 , F42B23/005
摘要： Provided is a launchable remote-control attack device that enables an operator to remotely grasp the status of a target place and to remotely control weapons it has been equipped with to perform an attack using explosives or gas when necessary. The remote-control attack device includes a cylindrical body with a camera, drivers which are made up of two tires that are disposed on opposite sides of the body and can be driven individually, and battery units for supplying power and which are disposed in central openings of the tires of the drivers. The attack device further includes a plurality of storage units and a wireless control unit.
摘要翻译：提供了一种可发射的远程控制攻击装置，其使得操作者能够远程地掌握目标地点的状态，并且在必要时远程控制其配备的武器以使用爆炸物或气体进行攻击。遥控攻击装置包括具有相机的圆柱体，由两个轮胎构成的驱动器，两个轮胎设置在主体的相对侧上并且可以单独驱动，以及用于供电的电池单元，并且设置在中心开口的司机轮胎。攻击装置还包括多个存储单元和无线控制单元。

6. 发明授权

US5895882A Air-delivered remotely-activated infrared anti-ship missile decoy and deployment method 失效
标题翻译：空运遥控红外反舰导弹诱饵和部署方式
公开(公告)号：US5895882A
公开(公告)日：1999-04-20
申请号：US986982
申请日：1997-12-08
申请人： Robert C. Woodall, Jr.
发明人： Robert C. Woodall, Jr.
IPC分类号： F42B12/42 , F42B12/62 , F42B4/26 , F42B12/46
CPC分类号： F42B12/42 , F42B12/625
摘要： An air-delivered infrared anti-ship missile decoy is delivered from an aiaft to a desired location below sea surface ahead of advancing forces and then activated at a later time by a remotely-transmitted encoded signal to separate a payload assembly from the remainder of the decoy, float the payload assembly on the sea surface and then produce a relatively large infrared plume above the payload assembly and atop the sea surface that provides an infrared signature for decoying and deception purposes.
摘要翻译：空中交付的红外反舰导弹诱饵从飞机运送到提前力之前的海面以下的所需位置，然后在远程传输的编码信号之后被激活，以将有效载荷组件与其余部分分离诱饵，将有效载荷组件浮在海面上，然后在有效载荷组件上方和在海面顶部产生相对较大的红外线羽毛，其提供用于诱捕和欺骗目的的红外线标记。

7. 发明授权

US5656792A Projectile 失效
标题翻译：射弹
公开(公告)号：US5656792A
公开(公告)日：1997-08-12
申请号：US714239
申请日：1996-09-16
申请人： Max Rentzsch , Manfred Schildknecht , Hans Strauss , Rainer Himmert
发明人： Max Rentzsch , Manfred Schildknecht , Hans Strauss , Rainer Himmert
IPC分类号： F42B12/62
CPC分类号： F42B12/625
摘要： A ballistic projectile including a subcaliber-sized penetrator which is coaxially carried in the casing of the projectile, and in which the penetrator additionally carries an explosive charge. The projectile possesses a proximity fuze at its tip which electrically triggers a penetrator-propellent charge which is arranged in the projectile base and which fills the volume of the projectile base, which accelerates the penetrator through a therebetween arranged propellant base, and in which the penetrator additionally possesses an impact detonator.
摘要翻译：一种弹道射弹，包括同轴携带在射弹套管中的亚尺寸穿透器，其中穿透器另外携带爆炸物。射弹在其尖端处具有接近引信，其电触发穿透器 - 推进剂装料，其布置在抛射体基体中并且填充射弹基座的体积，其通过其间布置的推进剂基底加速穿透器，并且其中穿透器另外还具有冲击雷管。

8. 发明授权

US5594197A Secondary projectile for a tandem warhead 失效
标题翻译：串联弹头的二次射弹
公开(公告)号：US5594197A
公开(公告)日：1997-01-14
申请号：US540935
申请日：1995-10-11
申请人： Klaus Lindstadt , Manfred Klare
发明人： Klaus Lindstadt , Manfred Klare
IPC分类号： F42B12/32 , F42B12/62 , F42B12/20
CPC分类号： F42B12/625 , F42B12/32
摘要： The present invention relates to a secondary projectile for a tandem warhead including a forwardly located active charge, a rearwardly located active charge and a fuze which is arranged therebetween, and whose triggering direction is oriented towards the forwardly located active charge, whereby the transmission of the ignition or triggering is implemented forwardly through the intermediary of a booster charge and towards the rear through the use of a cross-triggering device. The booster charge which is triggered by the fuze consists of an explosive material and lies directly against the forwardly located active charge, and wherein the booster charge at the other side thereof is separated by thin cross-ignitable wall segments of a housing of the cross-triggering device from at least two tongue-shaped explosive material poles of the rearwardly located active charge.
摘要翻译：本发明涉及一种用于串联弹头的二次射弹，其包括前向定位的有源电荷，位于其后的有源电荷和引信，并且其触发方向朝向前向定位的有源电荷，由此传输点火或触发通过中间的增压器电荷向前推进，并且通过使用交叉触发装置朝向后方。由引信触发的增压装置由爆炸材料构成，并且直接抵靠位于前方的有效电荷，并且其另一侧的增压器充电由横截面的壳体的薄的可交叉点火的壁段分隔开，从位于后方的有效电荷的至少两个舌形爆炸材料极触发装置。

9. 发明授权

US4497253A Armor-piercing projectile 失效
标题翻译：穿甲射弹
公开(公告)号：US4497253A
公开(公告)日：1985-02-05
申请号：US237395
申请日：1981-02-04
申请人： Udo Sabranski
发明人： Udo Sabranski
IPC分类号： F42B12/16 , F42B12/62 , F42B11/22
CPC分类号： F42B12/16 , F42B12/625
摘要： An armor-piercing projectile having a hard core and a hollow charge disposed in front of the hard core with respect to the direction of flight. A proximity fuse is arranged in the projectile and is adapted to effect an ignition of the hollow charge prior to the impacting of the armor-piercing projectile on the target.
摘要翻译：具有相对于飞行方向在硬芯前方设置的硬芯和空心电荷的穿甲射弹。接近保险丝布置在抛射体中，并且适于在穿甲射弹在靶上的撞击之前实现空心电荷的点火。

10. 发明授权

US3377952A Probe ejecting rocket motor 失效
标题翻译：探头喷射火箭发动机
公开(公告)号：US3377952A
公开(公告)日：1968-04-16
申请号：US58866866
申请日：1966-10-19
申请人： SYDNEY R. CROCKETT
发明人： CROCKETT SYDNEY R
IPC分类号： F42B12/62
CPC分类号： F42B12/625

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