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    • 1. 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。
    • 6. 发明授权
    • Projectile equipped with braking parachute
    • 抛射体配备制动降落伞
    • US4889053A
    • 1989-12-26
    • US272777
    • 1988-10-17
    • Werner GrosswendtKlaus UntersteinWalter Simon
    • Werner GrosswendtKlaus UntersteinWalter Simon
    • F42B10/56
    • F42B10/56
    • The invention relates to a projectile including a cylindrical receiving chamber (4) delimited by an interior wall (3) for a braking parachute (17) which can be ejected by way of a piston (9) that is longitudinally displaceable in the projectile, with the piston (9) being chargeable by an ignitable pyrotechnic charge (10). The braking parachute (17) is encased in a longitudinally divided sleeve (18) one side of which is in engagement with the piston (9). In order to completely or partially recover the projectile and not to impede deployment of the braking parachute (17), it is provided that the rear of the receiving chamber (4) is sealed by a cover (23) which can be ejected by way of the piston (9), is equipped with a rotational imbalance (26) and is in engagement with the other side of the sleeve (18). The braking parachute (17) is fastened to the piston (9). The projectile or a part (1) thereof connected with projectile components to be recovered is provided with a catch ring (21) disposed at the rear exit end of the receiving chamber (4) for the piston (9). The sleeve (18) is able to pass through the catch ring. Guides (19, 28) for the sleeve (18) are provided at the interior wall (3) of the receiving chamber (4).
    • PCT No.PCT / EP88 / 00022 Sec。 371日期:1988年10月17日 102(e)日期1988年10月17日PCT提交1988年1月14日PCT公布。 出版物WO88 / 06267 日本1988年8月25日。本发明涉及一种抛射物,其包括由用于制动降落伞(17)的内壁(3)限定的圆柱形容纳室(4),其可以通过活塞(9) 可在弹丸中纵向移动,活塞(9)可由点燃的烟火充电(10)充电。 制动降落伞(17)被封装在纵向分开的套筒(18)中,其一侧与活塞(9)接合。 为了完全或部分地回收抛射物并且不妨碍制动降落伞(17)的部署,设置接收室(4)的后部由盖(23)密封,盖(23)可以通过 活塞(9)配备有旋转不平衡部(26)并且与套筒(18)的另一侧接合。 制动降落伞(17)固定在活塞(9)上。 与要回收的射弹部件连接的射弹或其部分(1)设置有设置在用于活塞(9)的接收室(4)的后出口端的卡环(21)。 套筒(18)能够穿过卡环。 用于套筒(18)的导向件(19,28)设置在容纳室(4)的内壁(3)处。