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    • 1. 发明申请
    • METHOD FOR PACKING FIN-STABILIZED PENETRATORS IN A CARRIER SHELL
    • 用于在载体壳中包装稳定稳定的穿孔器的方法
    • WO2011115542A1
    • 2011-09-22
    • PCT/SE2011/000047
    • 2011-03-10
    • BAE Systems Bofors ABTHURMAN, Christer
    • THURMAN, Christer
    • F42B12/62F42B10/06
    • F42B12/58F42B10/06F42B10/08F42B12/06F42B12/362F42B12/60Y10S102/703
    • The present invention relates to a method for packing fin-stabilized penetrators (8) in a carrier shell (1), which penetrators (8) comprise a front penetrator part (10) and a rear fin part (9, 9') comprising fin sides (14, 14'), so that the empty space between the penetrators (8) and problems with the penetrators upon the release of the penetrators (8) from the carrier shell (1) are minimized, wherein the penetrators (8) are packed in groups (7) and are joined together to form larger packing units (6), in which each group (7) is arranged with a centrally located penetrator (8) flanked by at least three outer penetrators (8), which outer penetrators (8) are arranged so that their front penetrator parts (10) lie side to side against the fin sides (14, 14') of the centrally located penetrator (8). The method is characterized in that the rear fin parts (9, 9') of the penetrators (8) are made shorter than the front penetrator parts (10) of the penetrators (8), and in that the front penetrator parts (10) are made cylindrical for the distribution of load stresses, upon firing of the carrier shell, from the centrally located penetrator (8) rearwards in the direction of firing via the front penetrator parts (10) of the flanking penetrators (8).
    • 本发明涉及一种用于在载体壳体(1)中包装翅片稳定的穿透器(8)的方法,所述穿透器(8)包括前穿透部分(10)和包括翅片的后翅片部分(9,9') 使得穿透器(8)之间的空白空间和穿透器(8)从载体壳体(1)释放时与穿透器的问题最小化,其中穿透器(8)是 包装在组(7)中并且连接在一起以形成较大的包装单元(6),其中每个组(7)布置有侧面为至少三个外部穿透器(8)的位于中心的穿透器(8),该外部穿透器 (8)被布置成使得它们的前穿透部件(10)相对于位于中心的穿透器(8)的翅片侧面(14,14')一侧到另一侧。 该方法的特征在于,穿透器(8)的后翅片部件(9,9')制成比穿透器(8)的前穿透部件(10)短,并且前穿透部件(10) 被制成圆柱形,用于在穿过侧面穿透器(8)的前穿透部件(10)的方向上从位于中心的穿透器(8)向后方施加载体壳体的载荷应力分布。