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    • 1. 发明授权
    • Submunition for a spin stabilized carrier projectile
    • 用于旋转稳定运载器项目的分支
    • US5183962A
    • 1993-02-02
    • US884141
    • 1992-05-18
    • Klaus D. KariusArmin EskamKarl-Heinz Vogt
    • Klaus D. KariusArmin EskamKarl-Heinz Vogt
    • F42B30/00F42C19/04
    • F42C19/04F42B30/003
    • A submunition unit for a spin stabilized carrier projectile (1), with the submunition unit including an antenna disposed at the nose of its casing (7), and with the antenna (5) being covered by a protective cover (6). The casing (7) and the protective cover (6) are provided with respective axially overlapping collars (8, 9) which are each provided with respective opposed circumferential grooves (14, 15) to form an annular recess to accommodate an elastic securing ring (16). The securing ring, which is normally positioned within the innermost of the circumferential grooves, expands under the influence of centrifugal forces to connect the casing and protective cover together in a form-locking manner.
    • 一种用于自旋稳定的载体射弹(1)的子弹药单元,子弹药单元包括设置在其壳体(7)的鼻部处的天线,并且天线(5)被保护盖(6)覆盖。 壳体(7)和保护盖(6)设置有相应的轴向重叠的轴环(8,9),每个轴环重叠的轴环(8,9)分别设置有相应的相对的周向槽(14,15),以形成环形凹部以容纳弹性固定环( 16)。 通常位于圆周槽的最内侧的固定环在离心力的影响下膨胀,从而将壳体和保护罩以形状锁定的方式连接在一起。
    • 3. 发明授权
    • Self-deploying stabilizing-vane assembly for projectile
    • 用于射弹的自展式稳定叶片组件
    • US4693434A
    • 1987-09-15
    • US779228
    • 1985-09-23
    • Michael SchwenzerArmin EskamWalter SimonWilfried Becker
    • Michael SchwenzerArmin EskamWalter SimonWilfried Becker
    • F42B10/14F42B13/32
    • F42B10/14Y10T403/11
    • A vane assembly for a projectile has a carrier carrying a plurality of pivots, having at the pivots respective carrier elements, and adapted to be secured to an end of the projectile. Respective vane elements are each pivotal on the pivots between an inner position lying immediately adjacent the respective carrier element and within a projection of the projectile and an outer deployed position projecting beyond the projection. Respective heat-destructible pins engaged between the vane elements and the respective carrier elements normally retain the vanes in the inner position and release the vanes for movement into the outer position when destroyed by heat. The carrier element is a rib of the carrier against which the respective vane lies when not deployed. In addition, relative to a normal longitudinal direction of travel of the projectile carrying the assembly, the vanes extend longitudinally in the direction and have relative to the direction front leading ends engaging the respective pins and rear trailing ends at the respective pivots.
    • 用于抛射体的叶片组件具有承载多个枢轴的载体,所述枢轴在枢转相应的载体元件处并且适于固定到射弹的端部。 相应的叶片元件各自在位于紧邻相应的承载元件的内部位置之间并且在射弹的突出部内的突出部和突出超过突出部的外部展开位置之间的枢轴上枢转。 接合在叶片元件和相应载体元件之间的相应的可热破坏的销通常将叶片保持在内部位置,并且当被热量破坏时释放叶片以移动到外部位置。 载体元件是载体的肋,当未展开时,相应的叶片位于该肋上。 此外,相对于承载组件的弹丸的正常的纵向运动方向,叶片沿着该方向纵向延伸并且相对于在相应枢轴处与相应销和后尾端接合的前方前端的方向。