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公开(公告)号：US20130118462A1
公开(公告)日：2013-05-16
申请号：US13298124
申请日：2011-11-16
申请人： G. Wilson Flint
发明人： G. Wilson Flint
CPC分类号： F42B12/362 , F41B7/02 , F42B12/56
摘要： A system and method for propelling pellets from a launch tube includes a retainer plug for holding the pellets inside the launch tube between the retainer plug and a compressed spring. A latch is established on the launch tube to restrain forward movement of the retainer ring in response to the bias force imposed by the compressed spring. In operation, the launch tube is propelled in a forward direction by a man-powered weapon. This creates an acceleration force on the tube that moves the retainer plug and pellets in a rearward direction relative to the launch tube to further compress the spring and release the latch from the retainer plug. After the initial acceleration has subsided, force from the compressed spring provides a forward propulsion of the retainer plug and the plurality of pellets from the launch tube for travel of the pellets toward an intended target.
摘要翻译： 用于从发射管推进颗粒的系统和方法包括用于将发射管内的颗粒保持在保持器塞和压缩弹簧之间的保持器塞。 在发射管上建立闩锁，以响应于压缩弹簧施加的偏压力来限制保持环的向前运动。 在操作中，发射管由人造武器向前推进。 这在管上产生相对于发射管沿向后方向移动保持器塞和小球的加速力，以进一步压缩弹簧并且从保持器塞释放闩锁。 在初始加速度已经消退之后，来自压缩弹簧的力提供保持器塞和多个丸粒从发射管的向前推进，用于使颗粒移动到预期目标。
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公开(公告)号：US20140251296A1
公开(公告)日：2014-09-11
申请号：US13828373
申请日：2013-03-14
申请人： G. Wilson Flint , Michael T. Jones
发明人： G. Wilson Flint , Michael T. Jones
摘要： A man-powered system for pneumatically launching a pellet cluster includes a cartridge for holding the pellet cluster. A hollow propulsion shaft receives the cartridge for substantially free travel back and forth in the shaft to establish a variable-volume compression chamber in the shaft, between the cartridge and a closed end of the shaft. When a driving force acts to launch the combination of cartridge and shaft, the cartridge moves to compress gas in the compression chamber for a subsequent expansion that will propel the cartridge forward through the shaft. After launch, the compressed gas acts to separate the pellet cluster from the cartridge and to provide a pneumatic assist that increases the velocity of pellets after separation.
摘要翻译： 用于气动发射颗粒团的人造系统包括用于保持颗粒团簇的筒。 空心推进轴接收筒，用于在轴中来回地进行实质上的自由行进，以便在轴之间，在筒与轴的封闭端之间建立可变容积的压缩室。 当驱动力作用以发射筒和轴的组合时，筒移动以压缩压缩室中的气体，用于随后的膨胀，其将推动筒向前穿过轴。 发射后，压缩气体用于将颗粒团与药筒分离，并提供气动辅助，从而提高分离后颗粒的速度。
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公开(公告)号：US20140256485A1
公开(公告)日：2014-09-11
申请号：US13830599
申请日：2013-03-14
申请人： G. Wilson Flint , Michael T. Jones
发明人： G. Wilson Flint , Michael T. Jones
CPC分类号： F42B6/04 , Y10T29/49826
摘要： A projectile having a proximal tube and distal tube is described. A piston that is formed with a vent covers the distal end of the proximal tube. The piston is inserted into an open proximal end of the distal tube to establish a compression chamber in the distal tube between the axially moveable piston and a closed distal tube end. A valve is positioned at the proximal end of the proximal tube to selectively pressurize a space in the proximal tube between the valve and piston. The space, in turn, is in fluid communication with the compression chamber through the vent formed in the piston. The vent is formed as a constriction allowing fluid to flow into the compression chamber during an initial pressurization, while allowing for pressure buildup in the compression chamber during the initial relative movement between the proximal and distal tubes that occurs immediately after projectile launch.
摘要翻译： 描述了具有近端管和远端管的射弹。 形成有通气口的活塞覆盖近端管的远端。 活塞插入到远端管的开放的近端中，以在轴向可移动的活塞和封闭的远端管端之间的远端管中建立压缩室。 阀位于近端管的近端，以选择性地加压阀和活塞之间的近端管中的空间。 空间又通过形成在活塞中的排气口与压缩室流体连通。 通气口形成为使得流体在初始加压期间流入压缩室的收缩，同时允许在弹丸发射之后立即在近端管和远端管之间的初始相对运动期间在压缩室中产生压力。
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公开(公告)号：US20140155200A1
公开(公告)日：2014-06-05
申请号：US13890053
申请日：2013-05-08
申请人： G. Wilson Flint
发明人： G. Wilson Flint
CPC分类号： F42B12/362 , F41B7/02 , F42B12/56 , Y10T29/49826
摘要： A system and method for propelling pellets from a launch tube includes a retainer plug for holding the pellets inside the launch tube between the retainer plug and a compressed spring. A latch is established on the launch tube to restrain forward movement of the retainer ring in response to the bias force imposed by the compressed spring. In operation, the launch tube is propelled in a forward direction by a man-powered weapon to further compress the spring and release the latch from the retainer plug. After the initial acceleration has subsided, force from the compressed spring provides a forward propulsion of the retainer plug and the plurality of pellets from the launch tube for travel of the pellets toward an intended target. As an added feature, the launch tube can be extended to delay separation of the pellets from the tube for a so-called “choke” effect.
摘要翻译： 用于从发射管推进颗粒的系统和方法包括用于将发射管内的颗粒保持在保持器塞和压缩弹簧之间的保持器塞。 在发射管上建立闩锁，以响应于压缩弹簧施加的偏压力来限制保持环的向前运动。 在操作中，发射管由人力武器沿向前方向推进，以进一步压缩弹簧并从保持器塞释放闩锁。 在初始加速度已经消退之后，来自压缩弹簧的力提供保持器塞和多个丸粒从发射管的向前推进，用于使颗粒移动到预期目标。 作为附加功能，发射管可以延伸以延迟颗粒与管的分离以产生所谓的“扼流”效应。
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公开(公告)号：US20130247887A1
公开(公告)日：2013-09-26
申请号：US13890035
申请日：2013-05-08
申请人： G. Wilson Flint , Michael T. Jones
发明人： G. Wilson Flint , Michael T. Jones
CPC分类号： F42B10/06 , F41B15/00 , F41F7/00 , F42B12/362 , F42B12/56 , Y10T29/49826
摘要： A system and method for propelling pellets from a launch tube in flight includes a payload section and a stabilizing section. The launch tube and its pellets are essentially the payload section. The stabilizing section is essentially the equivalent of an arrow, and it includes a connector for selectively engaging the stabilizing section with the payload section. In use, the stabilizing section is reusable with a sequence of payload sections.
摘要翻译： 用于从飞行中的发射管推进颗粒的系统和方法包括有效载荷部分和稳定部分。 发射管及其颗粒本质上是有效载荷部分。 稳定部分基本上等同于箭头，并且其包括用于选择性地将稳定部分与有效载荷部分接合的连接器。 在使用中，稳定部分可以用一系列有效负载部分重新使用。
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公开(公告)号：US20110277736A1
公开(公告)日：2011-11-17
申请号：US13084818
申请日：2011-04-12
申请人： Wilson Flint
发明人： Wilson Flint
CPC分类号： F41B5/12
摘要： A projectile launcher includes an acceleration rail with an accelerator mounted on opposite sides of the rail. Each accelerator includes an elastomeric energy generator having an end that is held stationary, while another end is connected to a string. This string then passes over a series of pulleys and crosses over the rail into the other accelerator. Thus, both accelerators act on the same string. In operation, as the string is pulled back and engaged with the projectile on the acceleration rail, the elastomeric drives are stretched. Also, each series of pulleys effectively causes a velocity multiplication that enhances the momentum of the projectile when it is launched.
摘要翻译： 射弹发射器包括一个加速轨道，其加速器安装在轨道的相对两侧。 每个加速器包括弹性能量发生器，其具有保持静止的端部，而另一端连接到弦线。 然后，该绳子经过一系列滑轮并且横过导轨进入另一加速器。 因此，两个加速器作用在相同的字符串上。 在操作中，当绳子被拉回并与加速轨道上的弹丸接合时，弹性体驱动器被拉伸。 此外，每一系列滑轮有效地引起了速度倍增，从而增加了弹丸在发射时的动量。
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公开(公告)号：US20140251295A1
公开(公告)日：2014-09-11
申请号：US13789514
申请日：2013-03-07
申请人： G. Wilson Flint , Michael Jones
发明人： G. Wilson Flint , Michael Jones
摘要： A device for transferring energy to propel a payload with added velocity after launch includes a first component having a mass (m1), and a second component having a mass (m2). As an assembly, the first and second components are positioned to establish a compression chamber between them that is dimensionally responsive to their relative movements. And, a payload is mounted on a selected component of the assembly. In operation, a driving force is exerted against one component of the assembly to propel the entire assembly along a predetermined flight path. Contemporaneously with this acceleration, the two components are moved toward each other. In turn, this compresses gas in the gas chamber to generate potential energy that is transferred as the gas expands to separate the payload from the assembly with added velocity.
摘要翻译： 用于传送能量以在发射之后以附加速度推进有效载荷的装置包括具有质量（m1）的第一部件和具有质量（m2）的第二部件。 作为组件，第一和第二部件被定位成在它们之间建立一个压缩室，其在尺寸上响应于它们的相对运动。 并且，有效载荷被安装在组件的选定部件上。 在操作中，驱动力被施加在组件的一个部件上以沿着预定的飞行路径推动整个组件。 与此加速度同时，两个组件相互移动。 反过来，这压缩了气体室中的气体，以产生随着气体膨胀而传递的势能，以便以附加的速度将有效载荷与组件分开。
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公开(公告)号：US08567376B2
公开(公告)日：2013-10-29
申请号：US13084818
申请日：2011-04-12
申请人： Wilson Flint
发明人： Wilson Flint
CPC分类号： F41B5/12
摘要： A projectile launcher includes an acceleration rail with an accelerator mounted on opposite sides of the rail. Each accelerator includes an elastomeric energy generator having an end that is held stationary, while another end is connected to a string. This string then passes over a series of pulleys and crosses over the rail into the other accelerator. Thus, both accelerators act on the same string. In operation, as the string is pulled back and engaged with the projectile on the acceleration rail, the elastomeric drives are stretched. Also, each series of pulleys effectively causes a velocity multiplication that enhances the momentum of the projectile when it is launched.
摘要翻译： 射弹发射器包括一个加速轨道，其加速器安装在轨道的相对两侧。 每个加速器包括弹性能量发生器，其具有保持静止的端部，而另一端连接到弦线。 然后，该绳子经过一系列滑轮并且横过导轨进入另一加速器。 因此，两个加速器作用在相同的字符串上。 在操作中，当绳子被拉回并与加速轨道上的弹丸接合时，弹性体驱动器被拉伸。 此外，每一系列滑轮有效地引起了速度倍增，从而增加了弹丸在发射时的动量。
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公开(公告)号：US20200378716A1
公开(公告)日：2020-12-03
申请号：US16831731
申请日：2020-03-26
申请人： Graham Wilson Flint
发明人： Graham Wilson Flint
摘要： The subject application is directed to a projectile apparatus and method for use of the same, wherein the apparatus has a first tubular component formed with a lumen and defines an axis, wherein the first component has an open end and a closed end, a second component engaged with the first component to create an assembly, wherein the assembly provides for a sliding axial movement of the second component in the lumen of the first tubular component, and the assembly establishes a gas-filled compression chamber in the lumen of the first component between the second component and the closed end of the first component, a payload mounted on a selected component of the assembly, and a release valve for regulating the gas-filled compression chamber for safety purposes.
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公开(公告)号：US20140256484A1
公开(公告)日：2014-09-11
申请号：US13790301
申请日：2013-03-08
申请人： G. Wilson Flint
发明人： G. Wilson Flint
CPC分类号： F42B6/04 , F42B6/06 , F42B6/08 , Y10T29/49826
摘要： A projectile includes an elongated shaft having a fore-end and an aft-end. A nose portion is affixed to the fore-end of the shaft, and cutting edges are attached near the aft-end of the shaft. For the present invention, the nose portion of the projectile is preferably made of a material having a greater density than the material that is used to construct the shaft of the projectile. In any event, the structure and configuration of the projectile is such that its center of gravity is located in the forward half of the projectile. Also, the cutting edges at the aft-end of the shaft can be configured to function as stabilizing fins for the projectile in flight.
摘要翻译： 抛射体包括具有前端和后端的细长轴。 鼻部部分固定在轴的前端，并且切削刃附接在轴的后端附近。 对于本发明，抛射体的鼻部优选地由具有比用于构造射弹的轴的材料的密度更高的材料制成。 无论如何，射弹的结构和结构使其重心位于射弹的前半部分。 此外，轴的后端处的切割边缘可以被配置为用作飞行中的抛射体的稳定翅片。
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