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1. 发明授权

US3808972A Dual function bomb 失效
标题翻译：双功能物料清单
公开(公告)号：US3808972A
公开(公告)日：1974-05-07
申请号：US88045969
申请日：1969-11-25
申请人： US NAVY
发明人： CAMMACK T , DONAHUE W , GRATTON P
IPC分类号： F42B12/10 , F42B12/58 , F42C1/09 , F42C9/14 , F42C15/24 , F42C15/29 , F42B25/16
CPC分类号： F42C9/142 , F42B12/10 , F42B12/58 , F42C1/09 , F42C15/24 , F42C15/29
摘要： 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.
摘要翻译：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。

2. 发明授权

US3768415A Fuze arming device 失效
标题翻译： FUZE ARMING DEVICE
公开(公告)号：US3768415A
公开(公告)日：1973-10-30
申请号：US3768415D
申请日：1965-04-15
申请人： US NAVY
发明人： CZAJKOWSKI N , DONAHUE W , CAMMACK T , PICKLER W
IPC分类号： F42C9/04 , F42C9/14 , F42C15/192 , F42C15/22 , F42C15/295 , F42C19/06 , F42C15/12
CPC分类号： F42C15/22 , F42C9/048 , F42C9/147 , F42C15/192 , F42C15/295 , F42C19/06
摘要： 1. In a fuze for a bomb adapted to be dropped from an aircraft and armed in free fall flight, A CASING, AN ARMING ROTOR ROTATABLY MOUNTED IN SAId casing for movement from an initial safe position to an armed position in incremental distances, A TIME DELAY MECHANISM CONNECTED TO THE ROTOR FOR PREVENTING MOVEMENT OF THE ROTOR FOR A PREDETERMINED TIME INTERVAL, SAID TIME DELAY MECHANISM INCLUDING A STORED ENERGY SPRING MEANS FOR MOVING THE ROTOR THROUGH A FIRST INCREMENTAL DISTANCE PRIOR TO SAID TIME INTERVAL AND FOR MOVING THE ROTOR THROUGH A SECOND INCREMENTAL DISTANCE AT THE EXPIRATION OF SAID TIME INTERVAL, A ROTOR LOCKING MEANS CONNECTED TO SAID ROTOR FOR RELEASING SAID ROTOR FOR MOVEMENT THROUGH SAID FIRST INCREMENTAL DISTANCE BY SAID STORED ENERGY MEANS WHEN THE BOMB IS SUBJECTED TO A PREDETERMINED MINIMUM AIR VELOCITY AND FOR STARTING SAID TIME DELAY MECHANISM, AND AN ENVIRONMENTALLY POWERED DRIVING MEANS MOUNTED UPON SAID CASING AND POSITIONED FOR DRIVING ENGAGEMENT WITH THE ROTOR WHEN THE ROTOR HAS BEEN MOVED THROUGH SAID SECOND INCREMENTAL DISTANCE FOR DRIVING THE ROTOR TO SAID ARMED POSITION, WHEREBY SAID BOMB IS ARMED AFTER THE EXPIRATION OF A PREDETERMINED TIME INTERVAL SUBSEQUENT TO RELEASE OF THE BOMB BY THE AIRCRAFT AT NORMAL LAUNCHING AIR SPEEDS.
摘要翻译： 1.在一枚适用于从飞机上坠落并在自由落体飞行中装备的炸弹的引信中，A CASING，AN ARMING ROTOR ROTATABLY安装在SAId套管中，用于从初始安全位置向增量距离的武装位置运动，A TIME 延迟机构连接到转子，用于防止转子在预定的时间间隔中的运动，具体的时间延迟机制包括存储能量弹簧装置，用于在通过第二个时间间隔移动转子之前通过第一个增量距离移动转子在达到时间间隔期间的增加距离，转向器的连接方式连接到转子上，用于通过按照存储的能量方式通过第一次增加的距离来释放转向器，当物料清单受到预定的最低空速和启动时间时延迟机制和环境驱动装置安装在外壳上并定位用于与ROTO的驱动接合 R当转子已经通过确定驱动转子以确定武装位置的第二次增加距离时，由于飞机在正常启动空速下发布预定的时间间隔后才能装载BOMB。

3. 发明授权

US3786754A Firing delay for point detonating fuze 失效
标题翻译：点燃爆炸燃料的延迟
公开(公告)号：US3786754A
公开(公告)日：1974-01-22
申请号：US3786754D
申请日：1968-12-20
申请人： US NAVY
发明人： CAMMACK T , SCHMIDT R , DONAHUE W , GRATTON P
IPC分类号： F42C1/04 , F42C14/00 , F42C15/196 , F42C15/22
CPC分类号： F42C15/196 , F42C1/04 , F42C14/00
摘要： 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.
摘要翻译：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。

4. 发明授权

US3742854A Fuze 失效
公开(公告)号：US3742854A
公开(公告)日：1973-07-03
申请号：US3742854D
申请日：1965-05-26
申请人： US NAVY
发明人： DONAHUE W , CAMMACK T
IPC分类号： F42B12/10 , F42C1/14 , F42C9/04 , F42C15/188
CPC分类号： F42C9/043 , F42B12/10 , F42C1/14 , F42C15/188
摘要： 1. A shaped charge bomb comprising, AN ELONGATED HOLLOW BOMB CASING HAVING A NOSE PORTION AT ONE END AND A TAIL PORTION AT ITS OTHER END, A SHAPED EXPLOSIVE CHARGE HAVING A CONICAL METAL-LINED RECESS FORMED THEREIN, SAID SHAPED CHARGE BEING POSITIONED WITHIN SAID BOMB CASING SO THAT SAID RECESS IS ADJACENT TO THE NOSE OF THE BOMB, A CYLINDRICAL STRIKER TUBE MOUNTED UPON THE NOSE OF THE BOMB CASING FOR LONGITUDINAL SLIDING MOVEMENT RELATIVE TO THE BOMB CASING, SAID STRIKER TUBE BEING COAXIALLY ALIGNED WITH SAID CONICAL RECESS AND POSITIONED FOREWARDLY THEREOF, AND A MECHANICAL DETONATING MEANS MOUNTED UPON SAID CASING FOR DETONATING SAID SHAPED CHARGE IN RESPONSE TO MOVEMENT OF SAID STRIKER TUBE, SAID DETONATING MEANS INCLUDING AN EXPLOSIVE BOOSTER CHARGE POSITIONED IN THE TAIL PORTION OF SAID BOMB CASING IN OPERATIVE ASSOCIATION WITH SAID SHAPED CHARGE, A STAB DETONATOR TYPE FUZE POSITIONED FOR ACUTATION IN RESPONSE TO MOVEMENT OF SAID STRIKER TUBE, AND A DETONATING CORD LEADING FROM SAID STAB DETONATOR TO SAID BOOSTER CHARGE AND BEING POSITIONED EXTERIORALLY OF THE BOMB CASING, A STRIKER PIN MOUNTED UPON SAID CASING AND POSITIONED FOR MOVEMENT BY SAID STRIKER TUBE TO DETONATE SAID STAB DETONATOR, A FUZE ARMING MECHANISM MOUNTED UPON THE NOSE OF THE BOMB CASING INCLUDING A CYLINDRICAL BEARING TUBE MOUNTED UPON THE NOSE OF SAID BOMB CASING AND BEING CONCENTRICALLY DISPOSED ABOUT THE PERIPHERY PORTION OF SAID STRIKER TUBE, AN ANNULAR ARMING ROTOR ROTABLY MOUNTED UPON SAID BEARING TUBE, SAID STAB DETONATOR BEING MOUNTED UPON SAID ARMING ROTOR FOR ROTATION THEREWITH FROM AN UNARMED POSITION WHEREIN SAID STAB DETONATOR IS OUT OF LINE WITH SAID STRIKER PIN AND WITH SAID DETONATING CORD TO AN ARMED POSITION WHEREIN SAID STAB DETONATOR IS ALIGNED WITH THE STRIKER PIN AND DETONATING CORD, AND MEANS FOR DRIVING THE ROTOR FROM ITS UNARMED POSITION TO ITS ARMED POSITION, WHEREBY THE DESTRUCTIVE JET PRODUCED BY THE SHAPED CHARGE MAY IMPINGE DIRECTLY UPON THE TARGET WITHOUT INTERFERENCE.

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