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41. 发明申请

US20130055916A1 PAYLOAD DELIVERY SYSTEM WITH FORWARD FOLDING STABILIZER FOR CARTRIDGES 审中-公开
标题翻译： PAYLOAD交付系统与前向折叠稳定器
公开(公告)号：US20130055916A1
公开(公告)日：2013-03-07
申请号：US13599815
申请日：2012-08-30
申请人： James Y. Menefee, III
发明人： James Y. Menefee, III
IPC分类号： F42B12/00 , F42B14/00 , F42B10/06 , F42B12/42 , F42B12/40 , F42B12/38 , F42B12/02 , F42B12/20 , F42B12/22 , F42B12/46 , F42B7/04 , F42B12/04 , F42B10/02 , F42B12/44
CPC分类号： F42B7/08 , F42B12/76
摘要： This disclosure provides for payload delivery systems and cartridges and methods that incorporate the payload delivery systems. The payload delivery system can comprise a stabilizer having a longitudinally cut side wall defining a series of vanes that are folded forward in the pre-launched configuration. Other aspects combine a payload cup nested within the forward folding stabilizer. Still other aspects integrate the payload portion and the stabilizer portion into a single piece that constitutes a stabilized payload cup. The disclosed cartridges can be used to deliver payloads such as solid projectiles, shot of all sizes, powders, gels, liquids, and other payloads to exploit their specific function.
摘要翻译：本公开提供了包括有效载荷传送系统的有效载荷传送系统和盒和方法。有效载荷传送系统可以包括稳定器，其具有限定一系列叶片的纵向切割侧壁，该叶片在预先启动的构型中向前折叠。其他方面组合了一个嵌套在正向折叠稳定器内的有效载荷杯。另外的方面，将有效载荷部分和稳定器部分整合成构成稳定的有效载荷杯的单件。所公开的墨盒可用于传送有效载荷，例如固体射弹，各种尺寸的喷丸，粉末，凝胶，液体和其他有效载荷，以利用其特定功能。

42. 发明授权

US08342097B1 Caseless projectile and launching system 有权
标题翻译：无爆炸弹和发射系统
公开(公告)号：US08342097B1
公开(公告)日：2013-01-01
申请号：US12939785
申请日：2010-11-04
申请人： Jeffrey M. Widder , Christopher A. Perhala
发明人： Jeffrey M. Widder , Christopher A. Perhala
IPC分类号： F42B15/00 , F42B12/00
CPC分类号： F42B5/08 , F41A9/70 , F41A19/14 , F41A19/45 , F41A19/47 , F41A19/58 , F42B5/045
摘要： A launcher system includes a launcher having a barrel adapted to receive a projectile with a charge of propellant and a magazine adapted to hold additional projectiles, with each projectile including a piston shiftably mounted for movement relative to a main body. When propellant in the projectile is ignited, either mechanically or electrically, the propellant forces the piston from a retracted position during a period of initial thrust and then the propellant exits through at least one vent hole to provide an additional thrust for the projectile upon the piston moving to a fully extended position and safely discharge pressure from within the projectile. The projectile may be fired at lethal or non-lethal velocities.
摘要翻译：发射器系统包括发射器，其具有适于接收具有推进剂的弹丸的枪管和适于保持另外的射弹的弹匣，每个射弹包括可移动地安装成相对于主体运动的活塞。当抛射体中的推进剂以机械方式或电气点燃时，推进剂在初始推力期间迫使活塞从缩回位置，然后推进剂通过至少一个通气孔排出，以便为活塞上的弹丸提供额外的推力移动到完全伸出的位置，并安全地从弹丸内排出压力。射弹可能以致命或非致命的速度射击。

43. 发明授权

US08119956B2 Multi-stage hyper-velocity kinetic energy missile 有权
标题翻译：多级超速动能导弹
公开(公告)号：US08119956B2
公开(公告)日：2012-02-21
申请号：US12563855
申请日：2009-09-21
申请人： Richard Janik , Doron Strassman
发明人： Richard Janik , Doron Strassman
IPC分类号： F42B15/01 , F42B15/04 , F42B12/32 , F42B15/00 , F42B12/00
CPC分类号： F42B12/06 , F41G7/32 , F42B12/625 , F42B15/01 , F42B15/04
摘要： A multi-stage hyper-velocity kinetic energy missile (HVKEM) uses a ‘missile in a missile’ architecture in which the HVKEM includes a 1st stage flight missile and a 2nd stage kill missile that includes a KE-rod penetrator. The flight missile cruises at a relatively low velocity (less than Mach 1.5, typically less than Mach 1) to conserve propellant (weight) and to allow for effective guidance and maneuvering until the missile is in close proximity to the target. When the missile is within the lethal range of the KE-rod penetrator, the kill missile separates and boosts to a much higher velocity (greater than Mach 3, typically greater than Mach 5) and flies unguided to impact the target in less than a second. Waiting to boost the KE-rod until “the last second” reduces the total propellant (weight) needed to deliver the KE-rod on target and simplifies the guidance. The missile may be configured for use with different platforms and different guidance systems but is particularly well suited for use with the existing base of TOW launch containers and platforms satisfying all of the physical, operational and CLOS guidance constraints while maintaining the performance of the KE-rod penetrator.
摘要翻译：多级高速动能导弹（HVKEM）使用“导弹”导弹，其中HVKEM包括第一级飞行导弹和第二级杀伤导弹，其中包括一个KE杆穿透器。飞行导弹以相对较低的速度（小于马赫1.5，通常小于马赫数1）巡航，以节省推进剂（重量），并允许有效的引导和机动，直到导弹靠近目标。当导弹处于KE杆穿透器的致命范围内时，杀死导弹分离并提升到更高的速度（大于Mach 3，通常大于Mach 5），并且在不到一秒钟内不引导飞行物撞击目标。等待提升KE杆直到“最后一秒”减少了将KE杆放在目标上所需的总推进剂（重量），并简化了指导。导弹可以配置为用于不同的平台和不同的导向系统，但特别适用于现有的TOW发射容器和平台的基础，满足所有的物理，操作和CLOS指导约束，同时保持KE- 杆穿透器。

44. 发明申请

US20110271825A1 SUICIDE BOMBER BLAST THREAT MITIGATION SYSTEM 有权
标题翻译： SUICIDE BOMBER BLAST威胁减轻系统
公开(公告)号：US20110271825A1
公开(公告)日：2011-11-10
申请号：US13102070
申请日：2011-05-06
申请人： Charles A. Howland
发明人： Charles A. Howland
IPC分类号： F41H5/04 , F42B12/00 , F41H5/08 , F42B14/06
CPC分类号： F42D5/05 , F41B15/10 , F41H13/0006 , F42B12/625 , F42B14/06
摘要： A non-lethal, sabot-deployed blast shield mitigates a suicide bomber by wrapping around the bomber and positioning a plurality of protective layers over an explosive device to absorb emitted heat, shock waves, and projectiles if the device is detonated. Stand-offs such as inflatable beams or pillows provide break-away zones between the protective layers, allowing some layers to expand to a point of failure and absorb the maximum possible energy. Inner layers absorb shock waves and heat. One or more outer layers resist projectile penetration. Protective layers can be positioned on opposing sides of a suspect in case two explosive devices are present. Shields can deploy with sufficient energy to knock down a bomber. In embodiments, a plurality of shields can be applied without interference therebetween. In some embodiments, a round shield includes bolas which spread the shield in flight in a cast-net dynamic and wrap around the suspect for shield attachment.
摘要翻译：非致命的，破坏部署的防风罩通过缠绕轰炸机并通过爆炸装置定位多个保护层来减轻自杀炸弹手，以吸收发射的热量，冲击波和射弹（如果装置被引爆）。诸如充气梁或枕头的支架在保护层之间提供了隔离区域，允许一些层膨胀到故障点并吸收最大可能的能量。内层吸收冲击波和热量。一个或多个外层抵抗射弹穿透。在存在两个爆炸装置的情况下，保护层可以位于嫌疑犯的相对侧上。盾牌可以用足够的能量部署以击倒轰炸机。在实施例中，可以施加多个屏蔽，而不会妨碍它们之间的干扰。在一些实施例中，圆形护罩包括弹药，其将屏蔽物在飞行中以铸网动态传播并围绕嫌疑人缠绕以进行盾构附接。

45. 发明申请

US20110067592A1 INDUSTRIAL AMMUNITION 有权
标题翻译：工业弹药
公开(公告)号：US20110067592A1
公开(公告)日：2011-03-24
申请号：US11475854
申请日：2006-06-27
申请人： Douglas D. Olson , Jack D. Dippold , Randant D. Huelsmann
发明人： Douglas D. Olson , Jack D. Dippold , Randant D. Huelsmann
IPC分类号： F42B30/00 , F42B12/00
CPC分类号： F27D25/006 , F41A9/40 , F41A15/00 , F42B5/067 , F42B5/28 , F42B8/04
摘要： A projectileless ammunition system (20; 320) includes a metallic case (22; 322). A propellant charge (26; 326) is carried by the case and covered by an over-powder member (24; 324) in the absence of a separate projectile. The ammunition is advantageously used with an industrial ballistic tool operating so that each spent case serves as the effective projectile to be propelled by firing of the next round of ammunition.
摘要翻译：无弹药弹药系统（20; 320）包括金属外壳（22; 322）。推进剂装料（26; 326）由壳体承载并且在没有单独的抛射体的情况下被过粉末构件（24; 324）覆盖。这种弹药有利地用于工业弹道工具的操作，使得每个废弃的壳体作为通过下一轮弹药的射击而被推动的有效射弹。

46. 发明授权

US07883593B1 Non-toxic pyrotechnic delay compositions 失效
标题翻译：无毒烟火延迟组合物
公开(公告)号：US07883593B1
公开(公告)日：2011-02-08
申请号：US12315488
申请日：2008-11-26
申请人： James E. Rose , Magdy Michay , Jan Puszynski
发明人： James E. Rose , Magdy Michay , Jan Puszynski
IPC分类号： C06B45/00 , C06B33/00 , D03D23/00 , D03D43/00 , F42D1/055 , F42B10/00 , F42B12/00 , F42B30/00 , F42B27/00
CPC分类号： F42C9/10 , C06B33/00 , C06C5/06
摘要： A novel pyrotechnic delay composition for use in metal delay fuse cartridges, including as its primary constituent Si—Al—Fe3O4 prepared from powdered form. The delay composition yields a progressive burning zone and burns substantially gas-free, is safe to handle, is resistant to moisture and degradation over time, can be incorporated within the confines of existing detonator shells, and poses no environmental hazards.
摘要翻译：一种用于金属延迟保险丝盒的新型烟火延迟组合物，包括作为其粉末形式制备的主要成分Si-Al-Fe 3 O 4。延迟组合物产生逐步燃烧区域并且基本上无气体燃烧，安全处理，耐潮湿和随时间退化，可以并入现有的雷管壳体的范围内，并且不会对环境造成危害。

47. 发明授权

US07739955B2 Device adjacent to an explosive charge with at least two liners 失效
标题翻译：设备与至少两个衬垫的爆炸装置相邻
公开(公告)号：US07739955B2
公开(公告)日：2010-06-22
申请号：US10558754
申请日：2004-06-03
申请人： Torsten Rönn , Christer Thuman
发明人： Torsten Rönn , Christer Thuman
IPC分类号： F42B12/00
CPC分类号： F42B1/028
摘要： An explosive charge (3) can be equipped with two liners (4, 5) that can be attached to one another. The primary liner (4) is so devised that when choosing a first choice (11) of being able to work independently and by employing a symmetrical form achieving a forward-aimed Shaped Charge Warhead (SCW) effect upon explosive charge initiation by means of the material (7, 8) indicated for the primary liner. A secondary liner (5) is devised with a second choice (12) to be able to work together with the primary liner and together cause an asymmetric form that distributes the material (18, 19) from the liners at different velocities to thereby cause a forward-directed fragmentation effect. The ammunition unit (1) can, thus, be designed or prepared for two different combat cases in a technologically simple and unambiguous manner.
摘要翻译：爆炸物（3）可以配备两个可以相互连接的内衬（4,5）。主衬套（4）的设计使得当选择能够独立工作的第一选择（11）并且通过采用对称形式实现在爆炸装药启动时的前向目标成形弹头（SCW）效应，借助于材料（7,8）表示为主衬里。第二选择（12）设计成能够与主衬套一起工作并且一起产生以不同速度从衬套分配材料（18,19）的不对称形式的第二选择（5），从而导致前向碎片效应。因此，弹药单位（1）可以以技术上简单和明确的方式为两个不同的作战情况设计或准备。

48. 发明申请

US20100078004A1 Method and apparatus for launching solid body and multiple solid bodies using compressed gas 失效
标题翻译：使用压缩气体发射固体和多个固体的方法和装置
公开(公告)号：US20100078004A1
公开(公告)日：2010-04-01
申请号：US12564782
申请日：2009-09-22
申请人： Vladislav Oleynik , Gennadiy Albul
发明人： Vladislav Oleynik , Gennadiy Albul
IPC分类号： F41B11/00 , F42B12/00 , F42B14/00 , F42B10/00
CPC分类号： F41B11/68 , F41B11/723 , F41B11/73 , F41F7/00 , F42B12/58
摘要： An apparatus for launching projectiles may incorporate a hermetically sealed launch tube, projectile or projectiles within the launch tube with their payload inside or connected via meaning of socket to projectile from outside. The space between the outer surface of the projectile inside the launch tube and the inner surface of the launch tube is filled with compressed gas and hermetically sealed with a fast removable lid. If outside payload is used, then it will be attached to inside projectile via a socket where inside projectile is located inside the launch tube and outside payload connected to the protruded via fast acting valve, portion of projectile and connected to it via the socket. Projectile may incorporate another meaning of control via controllable surfaces or propulsion or constant acting engines. The exhaust gas would be in addition to use for projectile stabilization or additional propulsion, by incorporation a exhaust gas organizers.
摘要翻译：用于发射弹丸的装置可以在发射管内并入密封的发射管，射弹或射弹，其内部具有有效载荷，或通过插座的意思从外部连接到射弹。发射管内的射弹的外表面与发射管的内表面之间的空间被填充有压缩气体，并用快速可拆卸的盖密封。如果使用外部有效载荷，那么它将通过一个插座安装在射弹内部，该插座内部的射弹位于发射管内部，外部有效负载与突出的快速作用阀，弹丸部分和通过插座相连。抛射体可以通过可控表面或推进或恒定作用发动机引入控制的另一个含义。通过并入废气组织者，排气将是除了用于弹丸稳定或额外推进之外的。

49. 发明授权

US07679037B2 Personal rifle-launched reconnaisance system 失效
标题翻译：个人步枪发射侦察系统
公开(公告)号：US07679037B2
公开(公告)日：2010-03-16
申请号：US10539340
申请日：2003-12-18
申请人： Benjamin Z. Eden , Ronen Ben-Horin
发明人： Benjamin Z. Eden , Ronen Ben-Horin
IPC分类号： F42B12/36 , F42B12/00 , F42B15/00
CPC分类号： F42B12/365
摘要： A reconnaissance system includes a projectile having an opening through which images of a target area are acquired, a portable launcher having a mechanism for affixing the launcher to a rifle for launching the projectile to fly along and above the target area, an image acquiring device within the projectile for acquiring images of the target area through the opening, a transmitter within the projectile for transmitting during its flight the acquired images to a remote station, a stabilizing mechanism for stabilizing at least one of the projectile and the image acquiring device while flying in a ballistic trajectory above the target area and a remote station. The remote station includes a receiver for receiving the images transmitted from the projectile and a monitor having a display for displaying the received images.
摘要翻译：侦察系统包括具有目标区域的图像的开口的射弹，具有用于将发射器固定到用于发射射弹以在目标区域上方飞行的步枪的机构的便携式发射器，用于通过开口获取目标区域的图像的射弹，用于在飞行期间发射所获取的图像到远程站的射弹内的发射器，用于在飞行期间稳定至少一个射弹和图像获取装置的稳定机构在目标区域上方的弹道轨迹和远程站。远程站包括用于接收从射弹发射的图像的接收器和具有用于显示接收到的图像的显示器的监视器。

50. 发明申请

US20090301337A1 NANO-ENHANCED KINETIC ENERGY PARTICLES 有权
标题翻译：纳米增强动力能量颗粒
公开(公告)号：US20090301337A1
公开(公告)日：2009-12-10
申请号：US11813611
申请日：2006-01-10
申请人： Dennis Eugene Wilson , Kurt A. Schroder , Darrin Lee Willauer , Stephan Bless , Rodney Thompson Russell
发明人： Dennis Eugene Wilson , Kurt A. Schroder , Darrin Lee Willauer , Stephan Bless , Rodney Thompson Russell
IPC分类号： F42B12/00 , F42B12/44 , F42B30/00
CPC分类号： F42B12/74 , F42B12/06
摘要： The current invention relates to the fields of ballistic and kinetic energy (KE) weapons. Specifically a novel apparatus and use of nanomaterials has been developed to make significant improvements over existing weapons. By incorporating nano-scale particles as a filler material for kinetic energy weapons several advancements are realized.
摘要翻译：本发明涉及弹道和动能（KE）武器领域。具体来说，已经开发了一种新型的纳米材料的设备和用途，以便对现有武器进行显着改进。通过纳入纳米级粒子作为动能武器的填充材料，实现了几个进步。

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