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1.发明授权Telescoped ammunition round having subcaliber projectile sabot with integral piston 失效伸缩式弹药，带有一体式活塞的亚型射弹弹
公开(公告)号：US4802415A
公开(公告)日：1989-02-07
申请号：US138259
申请日：1987-12-28
CPC分类号： F42B5/045 , F42B14/061 , F42B14/067
摘要： A telescoped ammunition round comprises:a propellant charge having an axial cavity for supplying firing power to the ammunition round;a control tube means housed within the aft end of the axial cavity;a booster charge within the axial bore of the control tube, fireable in response to a primer means of the ammunition round in communication therewith; anda sabot/projectile assembly mounted within the axial cavity, its aft end extending into the control tube, wherein the sabot comprises an integral piston at its aft end to receive propulsive forces upon firing of the booster charge of the ammunition round.
摘要翻译： 一个伸缩式弹药包括：推进剂装药，具有用于向弹药提供射击动力的轴向腔; 容纳在所述轴向腔的后端内的控制管装置; 在控制管的轴向孔内的增压器充电，可响应于与其连通的弹药圆的底漆装置而被点燃; 以及安装在轴向空腔内的破坏/抛射组件，其后端延伸到控制管中，其中，所述突破在其后端包括一体的活塞，以在射击弹药加强器的充电时接收推进力。
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公开(公告)号：US4604954A
公开(公告)日：1986-08-12
申请号：US663645
申请日：1984-10-22
摘要： A telescoped ammunition round has a projectile positioned in the axial cavity of a propellant charge. A generally tubular casing surrounding the propellant charge has two longitudinal splits dividing the casing into two substantially identical halves which can separate during firing and sustain the pressure created by the propellant charge without deforming. An end cap assembly couples adjacent ends of the halves of the tubular casing to each other.
摘要翻译： 一个伸缩式弹药弹，弹丸定位在推进剂装药的轴向腔内。 围绕推进剂装料的大致管状壳体具有两个纵向分割，将壳体分成两个基本上相同的两半，其在点火期间可以分离并维持由推进剂装料产生的压力而不变形。 端盖组件将管状壳体的两半的相邻端部彼此连接。
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