公开(公告)号：US3808972A

公开(公告)日：1974-05-07

申请号：US88045969

申请日：1969-11-25

Applicant: US NAVY

Inventor： CAMMACK T ,  DONAHUE W ,  GRATTON P

IPC: F42B12/10 ,  F42B12/58 ,  F42C1/09 ,  F42C9/14 ,  F42C15/24 ,  F42C15/29 ,  F42B25/16

CPC classification number: F42C9/142 ,  F42B12/10 ,  F42B12/58 ,  F42C1/09 ,  F42C15/24 ,  F42C15/29

Abstract: A dual function bomb combining anti-personnel and armor piercing capabilities in a single bomb and capable of discriminating between targets. A frangible member in the bomb nose shears upon impact with a hard target, such as armor, and drives a firing pin into a detonator in an arming rotor to cause instantaneous initiation of an armor piercing shaped charge. Impact with soft targets, such as earth, will not shear the frangible member but causes an inertia firing pin to initiate a propellant charge and a pyrotechnic delay. The propellant charge ejects the warhead upward three to ten feet at which time the pyrotechnic delay initiates the shaped charge for optimum effect against unprotected personnel in the vicinity.

Abstract translation: 一种双重功能的炸弹将单一炸弹中的杀伤人员和穿甲能力结合在一起，能够区分目标。 炸弹的一个脆弱的成员在与一个硬的目标（如装甲）碰撞时剪切，并将一个击发针驱动到一个武装转子的雷管中，以引起一个穿甲穿甲装甲的瞬间启动。 与软性目标（例如地球）的冲击不会剪切易碎的构件，而是导致惯性撞针引发推进剂装药和烟火延迟。 推进剂装药将弹头弹起三至十英尺，此时烟火延迟启动成形装置，以对附近的未受保护的人员产生最佳效果。

公开(公告)号：US3786754A

公开(公告)日：1974-01-22

申请号：US3786754D

申请日：1968-12-20

Applicant: US NAVY

Inventor： CAMMACK T ,  SCHMIDT R ,  DONAHUE W ,  GRATTON P

IPC: F42C1/04 ,  F42C14/00 ,  F42C15/196 ,  F42C15/22

CPC classification number: F42C15/196 ,  F42C1/04 ,  F42C14/00

Abstract: A mechanical delay for point detonating fuzes for projectiles to allow penetration into aircraft or similar light target structures before detonation of the projectile. A trans-axial inertial firing pin is mounted within the projectile so that the centrifugal force exerted thereon by the spinning projectile during light target penetration will selectively determine the firing time delay. Alternatively, instantaneous detonation is provided by a second, axial firing pin when the projectile strikes an impenetrable target or one of such hardness that would break up the projectile before the trans-axial firing pin could react to provide the normal delayed detonation.

Abstract translation: 引爆点的引爆点的机械延迟，以便在弹丸引爆之前允许穿透入飞机或类似的光靶结构。 反射轴惯性撞针安装在射弹内，使得在光靶穿透期间由旋转射弹施加在其上的离心力将选择性地确定燃烧时间延迟。 或者，当射弹撞击不可穿透的目标时，瞬时爆炸由第二轴向击球提供，或者在跨轴击球针能够反应以提供正常的延迟爆震之前，这种硬度会破坏射弹。