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    • 1. 发明授权
    • Extended charge cartridge assembly
    • 扩展充电盒组件
    • US5183961A
    • 1993-02-02
    • US803806
    • 1991-12-09
    • Ralph F. CampoliJohn T. McGovern
    • Ralph F. CampoliJohn T. McGovern
    • F42B5/067F42B14/06F42C19/08
    • F42B14/061F42B5/067F42C19/08F42C19/0834
    • A cartridge assembly for propelling a subscaliber penetrator through a gun tube which has a portion of the propellant charge contained in an annular cavity surrounding the sabot is disclosed. The annular cavity is defined by the scoop shaped front bourrelet, the aft bourrelet which has three radially extending support posts and bore riding shoes, and a combustible tubular case extension over the aft bourrelet extending forward to the front bourrelet. The assemlby includes cartridge case having a multistrand ignition system having a plurality of flexible combustible ignition strand. The strands extend through the propellant charge in the case and extend between the posts of the aft bourrelet into the annular cavity to simultaneously ignite the propellant charge contained therein with the portion of the charge in the cartridge case.
    • 公开了一种用于推动子午线穿透器通过枪管的药筒组件,该枪管具有包围在围绕着刺刀的环形空腔中的推进剂电荷的一部分。 环形空腔由勺形前膛,后膛具有三个径向延伸的支撑柱和钻孔骑行鞋以及在向后延伸到前膛的后膛上的可燃管状延伸部限定。 组件包括具有多个点火系统的多个柔性可燃点火线的盒壳体。 线束在壳体中延伸穿过推进剂装料,并在尾部的支柱之间延伸到环形空腔中,以同时点燃容纳在其中的推进剂电荷,同时将暗盒中的部分电荷点燃。
    • 4. 发明授权
    • Segmented cartridge assembly
    • 分段墨盒组件
    • US5179250A
    • 1993-01-12
    • US816003
    • 1992-01-02
    • Ralph F. Campoli
    • Ralph F. Campoli
    • F42B5/045F42B5/073F42B5/18F42C19/08
    • F42B5/181F42B5/045F42B5/073F42B5/18F42C19/0834
    • The cartridge assembly of the present invention comprises two or more combustible cartridge case segments, the front of which is fastened to the projectile assembly and the rear of which contains a primer assembly and a charge of propellant. The two segments are automatically joined together during loading into a gun chamber via velcro rings at a butted interface between the segments. Extending axially throughout each of the segments is a distributed plurality of flexible combustible ignition strands which, when ignited, propagate the ignition flame front at an extremely high rate, on the order of between 3 to 6 thousand feet per second, ensuring virtually simultaneous ignition of the propellant in each segment.
    • 本发明的暗盒组件包括两个或更多个可燃的盒壳段,其前部固定到射弹组件,并且其后部包含底漆组件和推进剂装料。 在通过节段之间的对接界面处的涡旋环加载到枪室期间,两个段自动连接在一起。 在每个段中轴向延伸的是分布的多个柔性可燃点火线,当被点燃时,以非常高的速率将点火火焰前沿传播大约在3至6千英尺/秒之间,确保几乎同时点燃 每个部分的推进剂。
    • 5. 发明授权
    • Cartridge assembly
    • 卡特彼勒大会
    • US5129324A
    • 1992-07-14
    • US644726
    • 1991-01-23
    • Ralph F. Campoli
    • Ralph F. Campoli
    • F42B5/045F42B5/073F42B5/18F42C19/08
    • F42B5/181F42B5/045F42B5/073F42B5/18F42C19/0826F42C19/0834
    • A cartridge assembly is provided, in one embodiment, comprising a combustible casing with an open forward end and an open breech end, enclosed at the breech end by a thin metal stub casing, a projectile assembly mounted in the forward end, an igniter assembly, a resilient obturator pop riveted to the casing, an annular sabot, and a plurality of flexible combustible priming tubes immersed in a propellant charge and extending the length of the casing. In another embodiment, the combustible casing comprises two separate casings joined together with fasteners, each casing having a set of flexible combustible priming tubes, an interface portion defined between the two where respective ends of combustible priming tubes abut. In both embodiments, the priming tubes combust rapidly producing complete ignition of the propellant charge and resultant stable projectile flight.
    • 在一个实施例中,提供了一种盒组件,其包括具有敞开的前端和敞开的后膛端部的可燃壳体,其通过薄金属短截线外壳在后膛端封闭,安装在前端的射弹组件,点火器组件, 铆接到壳体上的弹性闭塞器,环形防撞器,以及浸入推进剂装料中并延伸壳体的长度的多个柔性可燃起动管。 在另一个实施例中,可燃外壳包括两个用紧固件连接在一起的独立壳体,每个壳体具有一组柔性可燃性起动管,界定部分限定在两个可燃性起动管的相应端部邻接的位置。 在两个实施例中,起动管快速燃烧,产生完全点燃的推进剂装料并由此产生稳定的射弹飞行。
    • 6. 发明授权
    • Extended charge cartridge assembly
    • 扩展充电盒组件
    • US5277120A
    • 1994-01-11
    • US990472
    • 1992-12-14
    • Ralph F. CampoliJohn T. McGovern
    • Ralph F. CampoliJohn T. McGovern
    • F42B5/067F42B14/06F42C19/08F42B5/02C06C5/00F42B14/08
    • F42B14/061F42B5/067F42C19/08F42C19/0834
    • A cartridge assembly for propelling a subcaliber penetrator through a gun tube which has a portion of the propellant charge contained in an annular cavity surrounding the sabot is disclosed. The annular cavity is defined by the scoop shaped front bourrelet, the aft bourrelet which has three radially extending support posts and bore riding shoes, and a combustible tubular case extension over the aft bourrelet extending forward to the front bourrelet. The assembly includes cartridge case having a multistrand ignition system having a plurality of flexible combustible ignition strand. The strands extend through the propellant charge in the case and extend between the posts of the aft bourrelet into the annular cavity to simultaneously ignite the propellant charge contained therein with the portion of the charge in the cartridge case.
    • 公开了一种用于推动子光学穿透器通过枪管的墨盒组件,该喷枪管具有包围在围绕着枪身的环形空腔中的推进剂电荷的一部分。 环形空腔由勺形前膛,后膛具有三个径向延伸的支撑柱和钻孔骑行鞋以及在向后延伸到前膛的后膛上的可燃管状延伸部限定。 组件包括具有多级点火系统的盒壳体,其具有多个柔性可燃点火线。 线束在壳体中延伸穿过推进剂装料,并在尾部的支柱之间延伸到环形空腔中,以同时点燃容纳在其中的推进剂电荷,同时将暗盒中的部分电荷点燃。
    • 8. 发明授权
    • Rocket launching cartridge case and assembly
    • 火箭发射筒盒和组件
    • US4640195A
    • 1987-02-03
    • US851898
    • 1986-04-11
    • Ralph F. Campoli
    • Ralph F. Campoli
    • F42B5/073F42B5/10F42B5/02
    • F42B5/073F42B5/10
    • A rocket launching cartridge case is formed by attaching a cylindrical extension member to the open end of a cartridge case. The extension member conforms to cartridge receiving chambers of conventional weapons. A rocket assembly is releasably locked within the extension member at a predetermined axial position. The rocket assembly can be slideably positioned within the extension member and locked in place prior to attachment of the extension member to the cartridge case. The locking means establishes a rocket assembly and launching case overall length for use in particular conventional weapons. An obturator member on the rocket assembly engages rifling in the conventional weapon bore imparting a stabilizing spin when the rocket assembly is fired. The obturator is connected to the rocket assembly in a manner permitting slip rotation therebetween providing a predetermined rate of stabilizing spin. The extension member and the obturator have surfaces functioning as gas seals during launching of the rocket assembly.
    • 通过将圆柱形延伸构件附接到盒壳体的开口端而形成火箭发射筒壳体。 延伸构件符合常规武器的盒容纳室。 火箭组件在预定的轴向位置处可释放地锁定在延伸构件内。 火箭组件可以可滑动地定位在延伸构件内并且在将延伸构件附接到盒壳体之前被锁定就位。 锁定装置建立了用于特定常规武器的总长度的火箭组件和发射箱。 当火箭组件被点燃时,火箭组件上的一个闭孔器件接合传统武器孔中的膛线,从而产生稳定的旋转。 封闭器以允许滑动旋转的方式连接到火箭组件,提供预定的稳定旋转速率。 延伸构件和闭孔器在发射火箭组件期间具有用作气体密封的表面。
    • 10. 发明授权
    • Ultra light weight sabot
    • 超轻重量的笨蛋
    • US5359938A
    • 1994-11-01
    • US602831
    • 1990-10-24
    • Ralph F. CampoliEdwin G. Steiner
    • Ralph F. CampoliEdwin G. Steiner
    • F42B14/06
    • F42B14/061Y10S102/703
    • An ultra light weight sabot for a subcaliber projectile comprises a sabot having three reduced mass segments each incorporating driving grooves at their inner diameter, an aft bourrelet, a central cavity beneath the aft bourrelet and an outwardly directed projection forward of the aft bourrelet to support the forward end of the projectile as it travels through a gun bore. The aft bourrelet has a balloon type obturator thereon which also fastens to the cartridge case. A bore extending through the obturator and the aft bourrelet into the annular cavity equalizes pressure between the case and the annular cavity to assist in sabot segment separation from the subcaliber projectile.
    • 用于亚型射弹的超重轻型防盗器包括具有三个减小的质量段的膛体,每个节段包括其内径处的驱动槽,后膛,后膛下方的中心腔和向后指向的后膛向前突出以支撑 射弹的前端穿过枪孔。 尾兜在其上具有气囊式闭塞器,其也固定到盒壳体上。 延伸穿过闭孔器和后膛进入环形空腔的孔使得壳体和环形空腔之间的压力相等,以帮助从亚型射线射出的分段段分离。