首页> 外国专利> LOW-MASS-TRIGGER CONTROLLED RELEASE OF PROJECTILES HAVING VARIABLE ENERGIES AND NUMBERS IN A CENTRIFUGAL PROPULSION WEAPON, AND METHODS OF WEAPON USE

LOW-MASS-TRIGGER CONTROLLED RELEASE OF PROJECTILES HAVING VARIABLE ENERGIES AND NUMBERS IN A CENTRIFUGAL PROPULSION WEAPON, AND METHODS OF WEAPON USE

机译:离心推进武器中具有可变能量和数量的弹药的低质量触发控制释放及其使用方法

摘要

A weapon 1 peripherally discharging projectiles 2a-2n, normally ball bearings, at sustained high rates under centrifugal force preferably has two opposed members 11 each rotating within a housing, or guide track, 10. Each rotating member 11 preferably has at least two channels, or track, 16 with a radial component within which projectiles 2a-2n received near the center of rotation progress radially outwards until first escaping at 19, and then being ejected at X, under centrifugal force at the periphery of the at least one rotating member 11. A projectile release mechanism controls the timing, locations, and numbers of projectiles released per rotation of the at least one rotating member. This mechanism uses (1) opposed connected elongate members 13, substantially positioned along a radius line and within the at least one member 11 with its distal end protruding within the at least one channel 16 and with a proximal end cam follower 13 contacting the interior circumference 181 of (2) a ring cam 18, non-rotating to the housing 10 and movable between positions both coaxial, and displaced, to the rotational axis of the at least one rotating member 11. The elongate members 13 move (1) radially outward under centrifugal force of the rotation of the at least one rotating member 11 until its distal end protrudes within the at least one channel 16, therein obstructing passage of projectiles 2a-2n along the channel 16 and any ejection of these projectiles 2a-2n from the periphery of the at least one rotating member 11, until (2) the cam follower 14 of the elongate arm 13 contacts during rotation the cam 181 surface of the ring cam 18, pulling the elongate member 13 against centrifugal force radially inwards until its distal end ceases to protrude within the channel 16, losing passage of projectiles 2a-2n along the channel 16 for subsequent escape at 19 and for ejection at X.
机译:武器 1 沿圆周发射弹丸 2 a - 2 n 的武器,通常为滚珠轴承在离心力下以持续高速率运转时,最好有两个相对的构件 11 ,每个在壳体或导轨 10 中旋转。每个旋转构件 11 优选具有至少两个通道或轨道 16 ,其具有径向分量,射弹 2 a 在其中在旋转中心附近接收到的I>- 2 n 径向向外发展,直到首先在 19 逸出,然后在离心力下在X处弹出。力在至少一个旋转构件 11 的外围。弹丸释放机构控制至少一个旋转构件的每次旋转释放的弹丸的时间,位置和数量。该机构使用(1)相对的连接的细长构件 13 ,该细长构件 13 基本上沿着半径线设置并且在至少一个构件 11 内,并且其远端突出在至少一个构件内通道 16 且其近端凸轮从动件 13 与(2)环形凸轮 18 181 接触>,不相对于壳体 10 旋转,并且可在与至少一个旋转构件 11 的旋转轴同轴且错位的位置之间移动。细长构件 13 在至少一个旋转构件 11 的旋转的离心力的作用下径向向外移动(1),直到其远端突出到至少一个通道< B> 16 ,其中会阻止弹丸 2 a - 2 n 沿着通道< B> 16 以及这些弹丸 2 a - 2 n 的任何弹射至少一个旋转部件 11 ,直到(2)在旋转凸轮时细长臂 13 的凸轮从动件 14 接触环形凸轮 18 的181 表面,抵抗离心力沿径向向内拉动细长构件 13 ,直到其远端不再在通道 16内突出,失去了弹道2 a -2 n 沿着通道 16 的通道,随后在 19 并在X处弹出。

著录项

  • 公开/公告号US2008257326A1

    专利类型

  • 公开/公告日2008-10-23

    原文格式PDF

  • 申请/专利权人 CHARLES ST. GEORGE;

    申请/专利号US20060475831

  • 发明设计人 CHARLES ST. GEORGE;

    申请日2006-06-26

  • 分类号F41B3/04;

  • 国家 US

  • 入库时间 2022-08-21 20:16:11

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