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公开(公告)号：US20160238361A1
公开(公告)日：2016-08-18
申请号：US14768921
申请日：2014-06-15
申请人： Felix RACHLIN
发明人： Felix RACHLIN
摘要： An accelerator, having a sealed end and a nozzle, is connected to a projectile. The accelerator is used to provide an additional acceleration to the projectile. The accelerator may be detachably or non-detachably connected to the bottom surface of the projectile. The accelerator may have a bullet like form and may be utilized in a single or a multiple projectile cartridge.
摘要翻译： 具有密封端和喷嘴的加速器连接到抛射体。 加速器用于为射弹提供额外的加速。 加速器可以可拆卸地或不可拆卸地连接到射弹的底面。 加速器可以具有子弹形状并且可以用于单个或多个弹丸筒中。
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公开(公告)号：US20150330147A1
公开(公告)日：2015-11-19
申请号：US14708932
申请日：2015-05-11
申请人： HYPERSCIENCES, INC.
发明人： MARK C. RUSSELL
摘要： One or more ram accelerator devices may be used to form one or more holes in geologic or other material. These holes may be used for drilling, tunnel boring, excavation, and so forth. The ram accelerator devices propel projectiles which are accelerated by combustion of one or more combustible gasses in a ram effect to reach velocities exceeding 500 meters per second. An endcap may be deployed within a tube of the ram accelerator device to prevent incursion of formation pressure products such as oil, water, mud, gas, and so forth into a guide tube of the ram accelerator. During operation the projectile penetrates the endcap and at least a portion thereof impact a working face. In some implementations a purge gas may be used to form a ullage between the endcap and the working face.
摘要翻译： 一个或多个冲压加速器装置可用于在地质或其他材料中形成一个或多个孔。 这些孔可用于钻孔，隧道掘进，挖掘等。 冲压加速器装置推进通过一个或多个可燃气体燃烧加速的射弹，以达到每秒超过500米的速度。 端盖可以部署在柱塞加速器装置的管内，以防止诸如油，水，泥浆，气体等的地层压力产物侵入到冲压加速器的导向管中。 在操作期间，射弹穿透端盖，其至少一部分撞击工作面。 在一些实施方案中，清洗气体可用于在端盖和工作面之间形成空隙。
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公开(公告)号：US08536502B2
公开(公告)日：2013-09-17
申请号：US13430678
申请日：2012-03-26
摘要： A vehicle for launching from a gas gun having a housing; preferably incorporating a precessional attitude control system; and utilizing a flared base, fins, or active use of the attitude control system during passage through the atmosphere. Subtly canting the fins can produce desired spinning of the vehicle. The propulsion system can employ liquid, hybrid, or solid fuel. A removable aero-shell assists atmospheric flight with thermal protection being provided by anticipated ablation, an ablative aero-spike, or transpirational cooling. And a releasable sabot enhances the effectiveness of the launch.
摘要翻译： 用于从具有外壳的气枪发射的车辆; 优选地包括进动姿态控制系统; 并且在通过大气的过程中利用喇叭形底座，翅片或主动使用姿态控制系统。 细小的鳍片可以产生所需的车辆旋转。 推进系统可以采用液体，混合或固体燃料。 可移动的航空壳可以帮助大气飞行，通过预期的消融，消融空气尖峰或蒸气冷却提供热保护。 并且可释放的sabot增强了发射的有效性。
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公开(公告)号：US07464649B2
公开(公告)日：2008-12-16
申请号：US10519203
申请日：2003-06-20
IPC分类号： F42B5/03
摘要： A cartridge assembly (10) for firearms or weapons, said cartridge assembly including a support body (11) having a central longitudinal channel (16) housing a plurality of projectiles (20, 22, 24) in end-to-end orientation and having a plurality of circumferential chambers (14), wherein each chamber houses (14a, 14b, 14c) at least one propellant charge (12a, 12b, 12c) and is located adjacent to a respective projectile; fluid communication means (18) included in the support body for communicating the products of a gaseous expansion of said propellant from a respective chamber (14) into said central longitudinal channel (16); whereby, upon initiation of a selected propellant charge (12a, 12b, 12c), the communicated products of gaseous expansion from a circumferential chamber force or eject a respective projectile (20, 22, 24) from the cartridge assembly (10). The propellant charges may comprise a volume of propellant material encased in a bag with an igniter.
摘要翻译： 一种用于火器或武器的盒组件（10），所述盒组件包括支撑体（11），所述支撑体具有中心纵向通道（16），所述中心纵向通道以端对端取向容纳多个射弹（20,22,24） 多个周向室（14），其中每个室容纳（14a，14b，14c）至少一个推进剂装料（12a，12b，12c）并且邻近相应的抛射体定位; 流体连通装置（18），包括在支撑体中，用于将所述推进剂的气态膨胀产物从相应的室（14）连通到所述中心纵向通道（16）中; 由此，在开始选择的推进剂装料（12a，12b，12c）时，来自周向室的气体膨胀的连通产物产生作用力，或者将相应的抛射体（20,22,24）从盒组件（10）喷出。 推进剂装料可包括一包装有带点火器的袋中的推进剂材料的体积。
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公开(公告)号：US20060124020A1
公开(公告)日：2006-06-15
申请号：US10519203
申请日：2003-06-20
申请人： Ben Bishop , Ramon Bambach , James O'Dwyer , Vinod Puri
发明人： Ben Bishop , Ramon Bambach , James O'Dwyer , Vinod Puri
IPC分类号： F42B12/58
摘要： A cartridge assembly (10) for firearms or weapons, said cartridge assembly including a support body (11) having a central longitudinal channel (16) housing a plurality of projectiles (20, 22, 24) in end-to-end orientation and having a plurality of circumferential chambers (14), wherein each chamber houses (14a, 14b, 14c) at least one propellant charge (12a, 12b, 12c) and is located adjacent to a respective projectile; fluid communication means (18) included in the support body for communicating the products of a gaseous expansion of said propellant from a respective chamber (14) into said central longitudinal channel (16); whereby, upon initiation of a selected propellant charge (12a, 12b, 12c), the communicated products of gaseous expansion from a circumferential chamber force or eject a respective projectile (20, 22, 24) from the cartridge assembly (10). The propellant charges may comprise a volume of propellant material encased in a bag with an igniter.
摘要翻译： 一种用于火器或武器的盒组件（10），所述盒组件包括支撑体（11），所述支撑体具有中心纵向通道（16），所述中心纵向通道以端对端取向容纳多个射弹（20,22,24） 多个周向室（14），其中每个室容纳（14a，14b，14c）至少一个推进剂装料（12a，12b，12c）并位于相应的抛射体附近; 流体连通装置（18），包括在支撑体中，用于将所述推进剂的气态膨胀产物从相应的室（14）连通到所述中心纵向通道（16）中; 由此，在所选择的推进剂装料（12a，12b，12c）开始时，来自圆周室的气体膨胀的所产生的气流产生力，或者将相应的抛射体（20,22,24）从盒组件（10）喷出， 。 推进剂装料可包括一包装有带点火器的袋中的推进剂材料的体积。
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公开(公告)号：US6085630A
公开(公告)日：2000-07-11
申请号：US168323
申请日：1998-08-26
申请人： John R. Manis
发明人： John R. Manis
IPC分类号： F41A1/02 , F41A21/00 , F41A21/28 , F42B5/02 , F42B10/24 , F42B14/00 , F42B30/02 , F41F1/00 , F42B3/00
摘要： The construction and arrangement of the projectile bearing surface interfaces rearward and forward of a recessed surface chamber of the projectile interface conjointly with the interfaces of bore wall areas segmented by recessed bore chambers which in conjunction effect the deployment/transport/dispersement/development/modulation and transformation of explosive propellant charges sequentially primed and activated rearward and forwardly of the projectile along the bore and in bore wall chambers captively converting high static gas pressure to expansively relieved dynamic propellant gas pressure directly at the projectile reducing firearm barrel recoil while energizing projectile movement along the bore in a closed-system of thermodynamic propellant energy for free flight purposes.
摘要翻译： 射弹支座表面的结构和布置与射弹界面的凹面表面腔室的后方和前方相接合，与由凹孔腔分隔的孔壁区域的界面相结合，这些孔壁区域部分/运输/分散/开发/调制和 爆炸性推进剂费用的转换依次地引导并沿着钻孔和钻孔壁室向后和向前激活，将高静态气体压力直接转换为在弹丸减少枪械枪筒反冲下向膨胀释放的动力推进剂气体压力，同时沿着 以自由飞行的目的在一个封闭系统的热力学推进剂能量。
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公开(公告)号：US5322002A
公开(公告)日：1994-06-21
申请号：US56426
申请日：1993-04-30
CPC分类号： F41A1/02
摘要： A tube launched rocket system which uses a plurality of small propellant charges located within the tube to propel the rocket. The charges form part of the outer wall of a traveling propulsion chamber. The rest of the chamber is substantially defined by a propulsion housing, which includes a forward plate that abuts the projectile, and an aft nozzle for venting gases from the interior of the chamber. Alternative embodiments also contain baffles for directing the flow of combustion gases, and may employ an electronic ignition system for igniting the propellant charges in sequence. As charges adjoining the propulsion chamber are ignited, the resulting combustion gases thrust into the interior of the chamber, forcing the housing forward as they flow aftward through the nozzle. As the propulsion housing travels through the tube, additional propellant charges are ignited as they effectively become part of the outer wall of the propulsion chamber. The housing pushes the projectile ahead of it through the tube. Use of a sequence of small propellant charges in the tube rather than a conventional rocket motor in the projectile makes the system's noise level manageable, permits the use of nontoxic propellant compositions, and eliminates the risk that a user will be burned by rocket motor exhaust as the projectile exits the tube. The teachings of the present invention also apply to closed breech systems.
摘要翻译： 管发射火箭系统，其使用位于管内的多个小推进剂装药来推进火箭。 电荷形成行进推进室的外壁的一部分。 腔室的其余部分基本上由推进壳体限定，该推进壳体包括抵靠射弹的前板，以及用于从腔室内部排放气体的后喷嘴。 替代实施例还包含用于引导燃烧气体流的挡板，并且可以采用用于依次点燃推进剂装料的电子点火系统。 当邻接推进室的电荷被点燃时，所产生的燃烧气体推入室的内部，当壳体向后流过喷嘴时迫使壳体向前。 当推进壳体穿过管时，额外的推进剂装料被点燃，因为它们有效地成为推进室的外壁的一部分。 这个房屋通过管子将其抛出。 在射弹中使用一系列小型推进剂装料，而不是传统的火箭发动机使得系统的噪音水平易于管理，允许使用无毒的推进剂组合物，并消除了用户将被火箭发动机排气燃烧的危险 射弹射出管。 本发明的教导也适用于封闭的后膛系统。
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公开(公告)号：US5131313A
公开(公告)日：1992-07-21
申请号：US635645
申请日：1990-11-28
申请人： Theodore Zimmerman
发明人： Theodore Zimmerman
摘要： A linear accelerator mounted on a launcher that injects propellant into a launcher behind a projectile causing the projectile to achieve greater distances. The launcher has apertures along its longitudinal surface allowing propellant to enter the inner cavity of the launcher. When the projectile is fired, additional propellant is introduced behind the projectile giving it additional impetus.
摘要翻译： 安装在发射器上的线性加速器，其将推进剂注射入射弹后面的发射器中，使射弹达到更大的距离。 发射器沿其纵向表面具有孔，允许推进剂进入发射器的内腔。 当射弹被射击时，在射弹后面引入额外的推进剂，给予额外的推动力。
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9.发明授权Controlled explosive, hypervelocity self-contained round for a large caliber gun 失效大口径枪的控制爆炸，超高速独立圆
公开(公告)号：US5016537A
公开(公告)日：1991-05-21
申请号：US490378
申请日：1990-03-08
申请人： George T. Pinson
发明人： George T. Pinson
摘要： A round for placement and firing in the barrel of a large caliber gun, the round comprising a cartridge case defining a cylindrical chamber having axially opposed open and closed ends, a plurality of axially-adjacent annualr explosive charges coaxially-disposed in the chamber, the charges defining a bore coaxial with said chamber and each charge being shaped to generate on detonation a predetermined shock wave in the case, a projectile disposed in the chamber proximate the closed end, the projectile having a trailing end shaped to convert shock waves generated by detonation of the annular charges to projectile acceleration, an explosive in the case for initially propelling the projectile axially through the bore toward the open, end, an electrical detonator for each annular charge responsive to an electrical signal, and a power source and circuit for generating the electrical signal in response to axial movement of the projectile in the bore.
摘要翻译： 一个用于在大口径枪的枪管中放置和击发的圆，该圆形包括限定具有轴向相对的开放和封闭端的圆柱形腔室的盒壳体，同轴地设置在腔室中的多个轴向相邻的年度炸药， 限定与所述室同轴的孔，并且每个电荷被成形为在爆炸时产生预定的冲击波，在该情况下，放置在靠近封闭端的小室中，抛射体具有成形为转换由爆炸产生的冲击波的后端 的环形电荷到弹丸加速度，在最初将射弹轴向推动通过孔朝向开放端的情况下的爆炸物，响应于电信号的每个环形电荷的电雷管，以及用于产生 响应于射弹在孔中的轴向运动的电信号。
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公开(公告)号：US3880044A
公开(公告)日：1975-04-29
申请号：US37665573
申请日：1973-07-05
申请人： US ARMY
发明人： KORR ABRAHAM L , WALKER EVAN HARRIS
CPC分类号： F41A1/02
摘要： An efficient hypervelocity weapon system is described in which a conically-based projectile is initially launched from a reusable conventional gun into an aligned cylindrical tube of high explosive which is initiated by the rotating band located at the juncture of the conical base and the rearward end of the bourrelet. As the projectile moves through the high explosive tube, the gases generated from its detonation implode upon the conical projectile base rearwardly of the rotating band and cause the projectile to accelerate to a hypervelocity range in the direction of travel.
摘要翻译： 描述了一种有效的超高速武器系统，其中最初从可重复使用的常规喷射器将基于锥体的射弹发射到由位于锥形基座的接合处的旋转带和位于圆锥形基座的后端 。子 当弹丸穿过高爆炸管时，其爆炸产生的气体会旋转在旋转带的后方的锥形弹射基座上，导致射弹加速到行进方向的超高速范围。
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