WARHEAD TRIGGERING IN TARGET-TRACKING GUIDED MISSILES
    1.
    发明申请
    WARHEAD TRIGGERING IN TARGET-TRACKING GUIDED MISSILES 有权
    目标跟踪指导的MISSILES中的WARHEAD TRIGGINGING

    公开(公告)号:US20030047102A1

    公开(公告)日:2003-03-13

    申请号:US09877346

    申请日:2001-06-08

    CPC classification number: F42C9/148 F42C13/00

    Abstract: The invention relates to a method and a device for triggering a warhead in a target-tracking guided missile. The guided missile has an impact fuse and a proximity fuse for triggering detonation of the warhead. The invention triggers the warhead such that the damage caused to the target, such as an enemy fighter aircraft, becomes maximal. To this end, the miss disdance is predicted from influencing variabled detected during the flight of the guided missile. The warhead triggering delay time of the proximity fuse is set dependent on the predicted miss distance to achieve such maximum damage.

    Abstract translation: 本发明涉及一种用于在目标跟踪导弹中触发弹头的方法和装置。 导弹具有冲击保险丝和接近保险丝,用于触发弹头的爆震。 本发明触发弹头,使得诸如敌方战机等目标造成的伤害变得最大。 为此,从导弹飞行过程中检测到的变化可以预测出错过的不便。 接近保险丝的弹头触发延迟时间取决于实现这种最大损伤的预计未命中距离。

    Safety and arming mechanism
    2.
    发明授权
    Safety and arming mechanism 失效
    安全防范机制

    公开(公告)号:US3877378A

    公开(公告)日:1975-04-15

    申请号:US45899954

    申请日:1954-09-28

    Applicant: US ARMY

    Abstract: 1. In a fuze for an explosive projectile having a base section, a body section, and a nose section, a safety and arming mechanism including a firing train having a booster charge and acceleration-sensitive means for initiating fuze arming when the projectile to which the fuze is affixed is fired from a gun, the improvement comprising: an impact assembly located in the nose portion of the fuze, said impact assembly comprising a cartridge containing a dust under pressure, means for releasing said dust from said cartridge after the projectile to which the fuze is affixed is airborne, the action of the dust passing over the projectile serving to deposit an electrostatic charge upon the projectile.

    Abstract translation: 1.在具有基部,身体部分和鼻部的爆炸性射弹的引信中,包括具有增压器的火力训练器和具有加速度敏感装置的安全和布防机构,用于当弹丸发射时引发引信装置 所述引信被固定是从枪射出的,其改进包括:位于引信的鼻部的冲击组件,所述冲击组件包括在压力下容纳灰尘的药筒,用于在射弹之后从所述药筒释放所述灰尘的装置 引信是机载,尘埃通过射弹的作用,用于在射弹上沉积静电。

    Bomb fuzing system
    3.
    发明授权
    Bomb fuzing system 失效
    BOMB燃油系统

    公开(公告)号:US3613589A

    公开(公告)日:1971-10-19

    申请号:US55521655

    申请日:1955-12-23

    Applicant: US ARMY

    CPC classification number: F42C9/14 F42C9/148 F42C11/06 F42C13/04 F42C19/12

    Abstract: 1. An aircraft bomb fuzing system that permits the selection of alternative arming-delay and detonation-delay-after-impact times at any time prior to release of the bomb, said system comprising in combination: a first circuit point aboard said aircraft; a DC power source aboard said aircraft connected to said first circuit point for energization thereof with DC voltage; an AC generator aboard said aircraft also connected to said first circuit point, said generator being capable of selectively applying to said first circuit point any predetermined combination of a number of AC signals of different frequencies; means on said bomb and said aircraft for supporting said bomb prior to release thereof; an electrical input terminal aboard said bomb; an extensible and disconnectable conductor means connected between said input terminal and a grounded point on said aircraft for maintaining said input terminal grounded prior to release of said bomb, said conductor means being so constructed and arranged that as the bomb falls away from said aircraft after release thereof, said conductor means first disconnects itself from said grounded point on said aircraft as the bomb begins to fall, the makes momentary electrical contact with said first circuit point after said bomb has fallen a short predetermined distance, and then disconnects itself from said input terminal after said bomb has fallen an additional predetermined short distance, the DC voltage of said DC power source and the predetermined combination of AC signal frequencies from said AC generator thereby being momentarily applied to said input terminal aboard said bomb as said bomb falls away from said aircraft; capacitive storage means within said bomb connected to said input terminal, said capacitive storage means being adapted to charge to the DC voltage of said power source as a result of the momentary application of said DC power source to said input terminal as the bomb falls away from the aircraft; an arming-delay resistance means and an armingdelay capacitor in series across said capacitive storage means; an arming-delay gas diode and an impulse responsive arming means in series across said arming-delay capacitor, said DC voltage on said capacitive storage means flowing through said arming-delay resistance means to charge said arming-delay capacitor which upon attaining a voltage equal to the firing voltage of said armingdelay diode rapidly discharges through said diode and said arming means, said arming means being adapted to thereupon arm said bomb, the arming-delay time thus being the time taken by said arming-delay capacitor to charge to saId firing voltage; a normally open impact switch, a detonation-delay resistance means and a detonation-delay capacitance in series across said capacitive storage means; a detonation-delay gaS diode and a detonator in series across said detonation-delay capacitor, said impact switch being adapted to close on impact so that said capacitive storage means flows through said detonation-delay resistance means to charge said detonation-delay capacitor which upon attaining a voltage equal to the firing voltage of said detonation-delay diode rapidly discharges through said diode and said detonator, said detonator being adapted to thereupon detonate said bomb, the detonation-delay-after-impact time thus being the time taken by said detonation-delay capacitor to charge to the firing voltage of said detonation-delay diode; a plurality of parallel-connected frequency-sensitive switch devices connected to said input terminal, each of said switch devices comprising a tuned circuit and an irreversible impulse-responsive switch, each tuned circuit being tuned to a different one of the signal frequencies capable of being applied to said first circuit point by said generator, said switch devices being so constructed and arranged that the momentary application of the predetermined combination of AC signal frequencies applied to said input terminal as said bomb falls away causes irreversible actuation of the impulse-responsive switches of those switch devices whose tuned circuit is tuned to one of the signal frequencies present in the predetermined combination applied by said generator; said arming-delay resistance means and said detonation-delay resistance means each comprising a plurality of resistors, the resistors of said arming-delay resistance means being adapted to cooperate with a first number of said impulse-responsive switches so that the resistance provided by said arming-delay resistance means is determined by the number of said first number of impulse-responsive switches which are actuated, and the resistors of said detonation-delay resistance means being adapted to cooperate with a second number of impulse-responsive switches so that the resistance provided by said detonation-delay resistance means is determined by the number of said second number of impulse-responsive switches which are actuated, the arming-delay and detonation-delay-after-impact times, which are dependent on the resistances of said arming-delay resistance means and said detonation-delay resistance means, respectively, thus being selectively variable by choice of the predetermined combination of signal frequencies applied to said first circuit point by said generator.

    Warhead triggering in target-tracking guided missiles
    6.
    发明授权
    Warhead triggering in target-tracking guided missiles 有权
    目标跟踪导弹中的弹头触发

    公开(公告)号:US06584906B2

    公开(公告)日:2003-07-01

    申请号:US09877346

    申请日:2001-06-08

    CPC classification number: F42C9/148 F42C13/00

    Abstract: The invention relates to a method and a device for triggering a warhead in a target-tracking guided missile. The guided missile has an impact fuse and a proximity fuse for triggering detonation of the warhead. The invention triggers the warhead such that the damage caused to the target, such as an enemy fighter aircraft, becomes maximal. To this end, the miss disdance is predicted from influencing variabled detected during the flight of the guided missile. The warhead triggering delay time of the proximity fuse is set dependent on the predicted miss distance to achieve such maximum damage.

    Abstract translation: 本发明涉及一种用于在目标跟踪导弹中触发弹头的方法和装置。 导弹具有冲击保险丝和接近保险丝,用于触发弹头的爆震。 本发明触发弹头,使得诸如敌方战机等目标造成的伤害变得最大。 为此,从导弹飞行过程中检测到的变化可以预测出错过的不便。 接近保险丝的弹头触发延迟时间取决于实现这种最大损伤的预计未命中距离。

    Fuzing arrangements
    7.
    发明授权
    Fuzing arrangements 失效
    福兴安排

    公开(公告)号:US4825766A

    公开(公告)日:1989-05-02

    申请号:US23532

    申请日:1979-03-06

    Inventor: Graham J. Ruthen

    CPC classification number: F42B30/006 F42C13/08 F42C9/148

    Abstract: A submunition has a metallic body 1 a sensor 4 for sensing the presence of metal and an extendable probe (e.g. a spring 3) separating the sensor 4 and body 1 to avoid interference with the sensor. A circuit including the metal sensor and an impact sensor detonates the submunition if impact with a metal body is detected; if impact only is detected the submunition adopts the role of a mine.

    Abstract translation: 子弹药具有金属体1,用于感测金属的存在的传感器4和分离传感器4和主体1的可延伸探针(例如弹簧3),以避免与传感器的干涉。 包括金属传感器和冲击传感器的电路如果检测到金属体的碰撞则引爆子弹药; 如果检测到影响,子弹药就起着矿山的作用。

    Circuit arrangement for a combined proximity and impact fuse
    8.
    发明授权
    Circuit arrangement for a combined proximity and impact fuse 失效
    组合接近和冲击保险丝的电路布置

    公开(公告)号:US4388867A

    公开(公告)日:1983-06-21

    申请号:US246698

    申请日:1981-03-23

    Applicant: Hans Baumer

    Inventor: Hans Baumer

    CPC classification number: F42C15/40 F42C13/00 F42C9/148

    Abstract: A combined proximity and impact fuse employed in a missile, including a circuit arrangement for avoiding the actuation of a detonation upon impingement of the impact fuse on a rain drop. The circuit arrangement is connected to the proximity fuse and is respective to the signals produced by the same to prevent the generation of a detonation signal upon impact until recognition by the proximity fuse that a given release criterion for impact detonation has been met.

    Abstract translation: 在导弹中使用的组合的接近和冲击保险丝,包括用于避免在撞击保险丝撞击雨滴时引发爆震的电路装置。 电路装置连接到接近保险丝,并且与相应的信号相对应,以防止碰撞时产生爆震信号,直到接近保险丝识别已经满足给定的冲击爆炸释放标准。

    Shock-acceleration activated function selector
    9.
    发明授权
    Shock-acceleration activated function selector 失效
    触发加速功能选择器

    公开(公告)号:US3977329A

    公开(公告)日:1976-08-31

    申请号:US517994

    申请日:1974-10-25

    Inventor: Gerald L. Wilde

    CPC classification number: F42C17/04 F42C9/148

    Abstract: A mode selector device, such as might be used in a projectile, allowing a simple manual adjustment before firing time to enable a function upon firing. A safe, small, reliable, "fail-useful" mechanism using shock to activate a cutter which removes a particular short in the circuit for each of a plurality of functions.

    Semi-active electro-optical bomblet fuze
    10.
    发明授权
    Semi-active electro-optical bomblet fuze 失效
    半主动电子轰炸机引信

    公开(公告)号:US3948182A

    公开(公告)日:1976-04-06

    申请号:US766035

    申请日:1968-10-03

    CPC classification number: F42C9/148 F42C13/02

    Abstract: A pressure-armed, semiactive bomblet fuze, having both contact and proxim-fuze capability for a free-fall weapon, and utilizing both a gyro aligning fuze train and a photocell transducer for directly initiating an electric detonator.

    Abstract translation: 一个压力武装的半主动炸弹引信,具有自由落体武器的接触和接近引导能力,并且使用陀螺校准引信列车和光电管传感器直接启动电雷管。

Patent Agency Ranking