首页> 外国专利> TRIGGER CONTROLLED RELEASE OF CONTROLLED NUMBERS OF PROJECTILES AT EACH OF CONTROLLED NUMBER OF INSTANCES PER REVOLUTION IN A CENTRIFUGAL PROPULSION WEAPON

TRIGGER CONTROLLED RELEASE OF CONTROLLED NUMBERS OF PROJECTILES AT EACH OF CONTROLLED NUMBER OF INSTANCES PER REVOLUTION IN A CENTRIFUGAL PROPULSION WEAPON

机译:离心推进器中每次旋转的控制点数每触发一次控制点数的弹丸释放

摘要

A weapon 1 peripherally discharging projectiles 2a-2n, normally ball bearings, at sustained high rates under centrifugal force has at least one member 11 rotating within a housing, or guide track, 10. Each rotating member 11 has at least one channel, 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) an elongate member 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 arm 13 moves (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 arm 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,在离心力的作用下以持续的高速率旋转,至少一个构件 11 在壳体或导轨 10 中旋转。每个旋转构件 11 具有至少一个通道或轨道 16 ,其径向分量内有射弹 2 a - 2 n 径向向外发展,直到首先在 19 逸出,然后在离心力的作用下在X处弹出。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)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通道内。 16 ,并且近端凸轮从动件 13 接触(2)环形凸轮 18 的内圆周 181 旋转至壳体 10 ,并且在至少一个旋转构件 11 的旋转轴线同轴且错位的位置之间移动。细长臂 13 在至少一个旋转构件 11 的旋转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内< B> 16,其中的弹道 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,抵抗离心力径向向内拉动细长臂 13 ,直到其远端不再在通道 16内突出,沿着通道 16 <失去射弹 2 a - 2 n / B>,以便随后在 19 处转义并在X处弹出。

著录项

  • 公开/公告号US2008092866A1

    专利类型

  • 公开/公告日2008-04-24

    原文格式PDF

  • 申请/专利权人 CHARLES ST. GEORGE;

    申请/专利号US20050283445

  • 发明设计人 CHARLES ST. GEORGE;

    申请日2005-11-18

  • 分类号F41B3/04;

  • 国家 US

  • 入库时间 2022-08-21 20:15:42

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