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公开(公告)号：US09784523B2
公开(公告)日：2017-10-10
申请号：US15106360
申请日：2014-12-19
申请人： ENIG ASSOCIATES INC.
摘要： A hybrid gun device composed of two barrels (1,10) that accept energy from combustion of standard propellant (6), one barrel (10) being operative to produce a high intensity electric current to add accelerating energy to a projectile (7) in the second barrel (1) and at least one coil (8) stage to convert energy between electrical and kinetic to cause the projectile (7) to be launched at hypervelocity.
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公开(公告)号：US09599444B2
公开(公告)日：2017-03-21
申请号：US14768921
申请日：2014-06-15
申请人： Felix Rachlin
发明人： Felix Rachlin
摘要： A multi-part projectile accelerator to be used in the single or multiple projectile mode, constructed of the hollow and tubular body which may either self-disconnect, once the projectile leaves the barrel, or stay with the projectile for the duration of the flight; which may also include the ring member designed to fit into the grooves of the rifled barrel in order to assist in maintaining the rotation of an accelerator.
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公开(公告)号：US09567108B2
公开(公告)日：2017-02-14
申请号：US14659572
申请日：2015-03-16
申请人： QUICKLAUNCH, INC.
摘要： A gas gun launcher has a pump tube and a launch tube with a first end of the launch tube slidably inserted into a second end of the pump tube. The pump tube may hold a heat exchanger to heat a light gas used to launch a vehicle. A sliding seal can be employed to manage recoil and to retain the gas within the launch tube and the pump tube. A fast-closing muffler at the second end of the launch tube can conserve the light gas utilized for launching a vehicle, enabling the light gas to be recycled. A launch tube alignment system is preferably automatic, ensuring the survival of the launch vehicle.
摘要翻译： 气枪发射器具有泵管和发射管，发射管的第一端可滑动地插入泵管的第二端。 泵管可以容纳热交换器以加热用于发射车辆的轻质气体。 可以使用滑动密封件来管理反冲并将气体保持在发射管和泵管内。 发射管第二端的快速关闭消音器可以节省用于发射车辆的轻质气体，从而使轻型气体得以回收利用。 发射管对准系统优选是自动的，确保运载火箭的存活。
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公开(公告)号：US09567107B2
公开(公告)日：2017-02-14
申请号：US14642720
申请日：2015-03-09
申请人： QUICKLAUNCH, INC.
发明人： Harry E. Cartland
IPC分类号： B64G1/00 , F41F3/04 , F41F1/00 , F41B11/723 , F41A1/02 , F41B11/60 , F41F3/077 , B64G5/00 , F41B11/68 , F42B10/26 , F42B10/66 , F42B14/06 , F42B15/00
CPC分类号： B64G1/002 , B64G5/00 , F41A1/02 , F41B11/60 , F41B11/68 , F41B11/723 , F41F1/00 , F41F3/04 , F41F3/0413 , F41F3/077 , F42B10/26 , F42B10/66 , F42B14/06 , F42B15/00
摘要： A gas gun launcher has a pump tube and a launch tube with a first end of the launch tube slidably inserted into a second end of the pump tube. The pump tube may hold a heat exchanger to heat a light gas used to launch a vehicle. A sliding seal can be employed to manage recoil and to retain the gas within the launch tube and the pump tube. A fast-closing muffler at the second end of the launch tube can conserve the light gas utilized for launching a vehicle, enabling the light gas to be recycled. A launch tube alignment system is preferably automatic, ensuring the survival of the launch vehicle.
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公开(公告)号：US20150307213A1
公开(公告)日：2015-10-29
申请号：US14659572
申请日：2015-03-16
申请人： QUICKLAUNCH, INC.
摘要： A gas gun launcher has a pump tube and a launch tube with a first end of the launch tube slidably inserted into a second end of the pump tube. The pump tube may hold a heat exchanger to heat a light gas used to launch a vehicle. A sliding seal can be employed to manage recoil and to retain the gas within the launch tube and the pump tube. A fast-closing muffler at the second end of the launch tube can conserve the light gas utilized for launching a vehicle, enabling the light gas to be recycled. A launch tube alignment system is preferably automatic, ensuring the survival of the launch vehicle.
摘要翻译： 气枪发射器具有泵管和发射管，发射管的第一端可滑动地插入泵管的第二端。 泵管可以容纳热交换器以加热用于发射车辆的轻质气体。 可以使用滑动密封件来管理反冲并将气体保持在发射管和泵管内。 发射管第二端的快速关闭消音器可以节省用于发射车辆的轻质气体，从而使轻型气体得以回收利用。 发射管对准系统优选是自动的，确保运载火箭的存活。
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公开(公告)号：US08664576B2
公开(公告)日：2014-03-04
申请号：US13963893
申请日：2013-08-09
申请人： Quicklaunch, Inc.
摘要： A vehicle for launching from a gun such as a gas gun and 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： 用于从诸如气枪和枪具等的枪上发射的车辆; 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：US07814835B2
公开(公告)日：2010-10-19
申请号：US12037085
申请日：2008-02-26
申请人： Zhongwei Shi
发明人： Zhongwei Shi
CPC分类号： F02K9/763 , F02K9/28 , F05D2240/40 , F41A1/00 , F41A1/02 , F42B10/38 , F42B15/00 , F42B15/10 , F42B15/36
摘要： A rocket includes a front warhead, a rear propellant actuator, and a propulsion enhancement arrangement which comprises at least two propulsion impulse generators longitudinally cascadedly mounted between the warhead and the rear propellant actuator, wherein each propulsion impulse generator comprises a storage barrel for storing a predetermined amount of explosive materials to provide propelling impulse upon controlled explosion thereof, and a time-internal control arrangement comprising a time-interval control device mounted on a bottom of the front warhead, a time-interval trigger wire operatively connected with the time-interval control device, and at least two time-interval triggers mounted along the time-interval trigger wire and inside of each of the storage chambers respectively, wherein the time-interval triggers trigger the explosion of the explosive material stored in the storage chamber from the bottom propelling impulse generator to the top propelling impulse generator one by one at a predetermined time intervals, so as to further propels the front warhead to the predetermined position at a predetermined velocity and after each explosion.
摘要翻译： 火箭包括前弹头，后推进剂致动器和推进增强装置，其包括纵向级联地安装在弹头和后推进剂致动器之间的至少两个推进脉冲发生器，其中每个推进脉冲发生器包括存储筒， 爆炸物质的数量，以便在其受控爆炸时提供推进冲击;以及时间内部控制装置，包括安装在前弹头底部的时间间隔控制装置，与时间间隔控制可操作地连接的时间间隔触发线 装置以及沿着时间间隔触发线和每个存储室内部安装的至少两个时间间隔触发器，其中时间间隔触发器触发从底部推进存储在存储室中的爆炸物质的爆炸 脉冲发生器到顶部推进脉冲发生器 以预定的时间间隔一个，以便以预定速度和每次爆炸之后进一步将前弹头推进到预定位置。
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公开(公告)号：US07775148B1
公开(公告)日：2010-08-17
申请号：US11327479
申请日：2006-01-09
申请人： Patrick P. McDermott
发明人： Patrick P. McDermott
IPC分类号： F41A1/02
摘要： Launching payloads at high velocity uses high-pressure gas or combustion products for propulsion, with injection of high pressure gas at intervals along the path behind the payload projectile as it accelerates along the barrel of the launcher. An inner barrel has an interior diameter equal to the projectile diameter or sabot containing the projectile. An outer casing surrounds the inner barrel. Structures at intervals attach the outer casing and the inner barrel. An axial gas containment chamber (AGC) stores high pressure gas between the inner barrel wall, the outer casing wall, and enclosure bulkheads. Pressure-activated valves along the barrel sequentially release the high pressure gas contained in the AGC in to the barrel to create a continuously refreshed high energy pressure heads behind the projectile as it moves down the barrel. A frangible cover at the exit end of the barrel allows the barrel to be evacuated prior to launch. The launcher is rapidly recyclable. The valves close automatically after the projectile has exited the barrel, allowing a new projectile to be introduced into the breech and the AGC to be recharged with high-pressure gas.
摘要翻译： 以高速启动有效载荷使用高压气体或燃烧产物进行推进，随着沿着发射器的炮筒加速沿着有效载荷弹道的路径间隔注入高压气体。 内筒具有等于抛射体直径的内径或包含弹丸的内筒。 外壳围绕内筒。 间隔的结构附着外壳和内筒。 轴向气体容纳室（AGC）在内筒壁，外壳壁和外壳隔板之间存储高压气体。 沿着桶的压力激活的阀顺次将包含在AGC中的高压气体释放到桶中，以在弹丸向下移动时产生连续刷新的高能量压头。 在桶的出口处的易碎盖子允许桶在发射之前被排空。 发射器迅速回收。 射弹弹出枪管后，阀门自动关闭，允许将新的射弹引入后膛，并将AGC放入高压气体中。
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公开(公告)号：US5841058A
公开(公告)日：1998-11-24
申请号：US592575
申请日：1996-01-26
申请人： John Robert Manis
发明人： John Robert Manis
IPC分类号： F41A1/02 , F41A21/00 , F41A21/28 , F42B5/02 , F42B10/24 , F42B14/00 , F42B30/02 , F41F1/00 , F42B10/00
摘要： The construction and arrangement of 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在射弹界面的凹面表面腔室的前后方向与由凹槽分隔的孔壁区域的界面相结合，共同影响部署/运输/分散/开发/调制和转换 的爆炸性推进剂装料，其顺序地起始并沿着钻孔和钻孔壁室向后和向前激发，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，同时沿钻孔激发弹丸运动 在用于自由飞行的热力学推进剂能量的封闭系统中。
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