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    • 1. 发明申请
    • OPTICAL PROXIMITY FUZE
    • 光临近度燃料
    • US20110185935A1
    • 2011-08-04
    • US12595003
    • 2009-08-06
    • Martyn Robert JenningsLee Douglas Miller
    • Martyn Robert JenningsLee Douglas Miller
    • F42C13/02G01S17/02G01S17/06H01J40/14
    • G01S7/4818F42C13/02G01S17/026G01S17/87G01S17/89
    • Described herein is an optical fuze for a guided missile that comprises an array of a large number of optical apertures distributed about the outer surface of the missile. An optical waveguide network selectively couples the array of apertures to a laser source and to a photodetector such that light from the laser source is emitted by selected ones of said apertures, and light returned from a target is received by selected ones of said apertures and directed by said optical waveguide network to said photodetector. These apertures might be arranged to form a composite target images in a particular direction, and/or may be arranged to perform a sensing operation along selected directions. The optical proximity fuze described herein provides inherent flexibility in the way the fuze can be configured in the missile for optimisation for different applications.
    • 这里描述的是用于导弹的光引信,其包括围绕导弹的外表面分布的大量光学孔的阵列。 光波导网络选择性地将孔阵列耦合到激光源和光电检测器,使得来自激光源的光由选定的所述孔发射,并且从目标返回的光被选定的所述孔接收并被定向 通过所述光波导网络到所述光电检测器。 这些孔可以被布置成在特定方向上形成复合目标图像,和/或可被布置为沿着选定的方向执行感测操作。 这里描述的光学邻近引信提供了在导弹中可以配置引信以便针对不同应用进行优化的方式的固有的灵活性。
    • 2. 发明授权
    • Method for increasing the probability of impact when combating airborne
targets, and a weapon designed in accordance with this method
    • 增加打击机载目标的冲击概率的方法,以及按照这种方法设计的武器
    • US6044765A
    • 2000-04-04
    • US43852
    • 1998-06-23
    • Chirster Regebro
    • Chirster Regebro
    • F42C13/02
    • F42C13/02
    • The present invention relates to a method and a device for combating aircraft (4). According to the invention, use is made of a projectile which rotates in the trajectory (5) towards the target (4) and which is provided with a direction-sensing proximity fuse whose direction of impact has been coordinated with a defined splinter-scattering direction for the explosive charge (8) of the projectile. In a preferred embodiment, the projectile concerned is a projectile which is fired by means of rocket technology, backblast technology or, alternatively, by means of a gas generator, and which is included in a one-man weapon or team-operated weapon of the single-shot type.
    • PCT No.PCT / SE96 / 01257 Sec。 371日期1998年6月23日第 102(e)1998年6月23日PCT PCT 1996年10月4日PCT公布。 公开号WO97 / 13116 PCT 日期:1997年04月10日本发明涉及一种对抗飞机(4)的方法和装置。 根据本发明,使用在轨迹(5)中朝向目标(4)旋转并且设置有方向感测接近保险丝的射弹,其方向感测接近保险丝已经与限定的分散散射方向协调 用于射弹的炸药(8)。 在一个优选实施例中,所涉及的射弹是通过火箭技术,反射技术或替代地通过气体发生器进行射击的射弹,并且其包括在一人的武器或团队操作的武器中 单枪型
    • 4. 发明授权
    • Target detection and fire control system for parachute-suspended weapon
    • 降落伞悬挂武器的目标检测和消防系统
    • US5339742A
    • 1994-08-23
    • US321001
    • 1981-11-13
    • Garry N. HuldermanHugh L. Ord
    • Garry N. HuldermanHugh L. Ord
    • F42C13/00F42C13/02F42C13/04F42B10/56
    • F42C13/02F42C13/006F42C13/042
    • A system for controlling the arming and firing of a weapon that is suspended from a parachute at an oblique angle and spun so as to be aimed over a spiral rotational scanning pattern on the earth as the parachute descends toward the earth. The weapon is supported by a platform so that the weapon is aimed in a predetermined direction relative to the platform. A detection system is supported by the platform and aimed in the same direction as the weapon for detecting predetermined radiation characteristics from targets of opportunity. A ranging system is supported by the platform and aimed in the same direction as the weapon for determining the range to the earth in such direction. A first circuit is coupled to the ranging system for enabling the weapon to be armed in response to the ranging system determining that the range to the earth in the direction that the weapon is aimed is less than a first predetermined distance; and a second circuit is coupled to the detection system and the ranging system for enabling an armed weapon to be fired in response to either the detection system detecting the predetermined radiation characteristics or the ranging system determining that the range to the earth in the direction that the weapon is aimed is less than a second predetermined distance that is shorter than the first predetermined distance.
    • 一种用于控制武器的布防和射击的系统,其以倾斜角悬挂在降落伞上并且随着降落伞向地球下降而被旋转以在地球上的螺旋旋转扫描图案上瞄准。 武器由平台支撑,使得武器瞄准相对于平台的预定方向。 检测系统由平台支撑并且瞄准与用于从机会目标检测预定辐射特征的武器相同的方向。 平台支持测距系统,瞄准与确定朝这个方向的地球范围相同的方向。 第一电路耦合到测距系统,用于响应于测距系统确定武器所瞄准的方向上的地球范围小于第一预定距离,使武器能够被布防; 并且第二电路耦合到检测系统和测距系统,用于响应于检测系统检测到预定的辐射特性而使武器武器被点火,或者测距系统确定到地球沿着 武器的目标小于比第一预定距离短的第二预定距离。
    • 5. 发明授权
    • Device for the detection of objects and the firing of horizontal mines
    • 用于检测物体和水平矿物的装置
    • US5153372A
    • 1992-10-06
    • US569859
    • 1990-08-20
    • Matthias DeussHelmut Pfaff
    • Matthias DeussHelmut Pfaff
    • F42C11/00F42C13/02F42C13/06G01S3/808
    • F42C13/02F42C11/007F42C13/06G01S3/808
    • A device for detecting an object such as a tank in a target area and for causing a horizontal mine to be fired at the object, comprises first and second microphones which detect noise, including noise from a tank, in the target area, in infrared sensor having a directional characteristic which is narrow with respect to the target area and which extends towards the center of the target area to define a target window, and an electronic evaluation unit. The electronic evaluation unit receives acoustic signals from the microphones and calculates a correlation function from the acoustic signal. If a property derived from the calculated correlation function, for example, the correlation or the correlation gradient, exceeds a predetermined threshold, the firing mechanism of the horizontal mine is enabled. If the infrared sensor also detects the presence of an object within its target window, the electronic evaluation unit will cause the horizontal mine to be fired.
    • 一种用于检测目标区域中的诸如罐的物体并且用于使水平矿井在物体上被点燃的装置包括:第一和第二麦克风,其在红外传感器中检测包括目标区域中的来自罐的噪声的噪声 具有相对于目标区域窄且朝向目标区域的中心延伸以限定目标窗口的方向特性,以及电子评估单元。 电子评估单元从麦克风接收声信号,并根据声信号计算相关函数。 如果从计算的相关函数导出的属性,例如相关性或相关梯度超过预定阈值,则能够使水平矿井的击发机构。 如果红外线传感器也检测到目标窗内物体的存在,则电子评估单元将导致水平矿被点燃。
    • 6. 发明授权
    • Infrared proximity fuze with double field of view for moving carrier
applications
    • 具有双重视野的红外接近燃料,用于移动运载器应用
    • US5078052A
    • 1992-01-07
    • US480096
    • 1990-02-14
    • Giulio Brogi
    • Giulio Brogi
    • F42C13/02
    • F42C13/02
    • Infrared proximity fuze, obtained by joining two infrared IR proximity sensors, preferably of the open field type, which have different fields of view (F.O.V.) so that the target sources presence signal is given by the simultaneous presence of an alarm signal coming from the greater field of view sensor and a time gate generated by an alarm signal coming from the lessor F.O.V. sensor. Given the carrier-to-target movement characteristics and the aperture of the two fields of view it is possible to electronically generate a time gate which rejects false targets (fires, flares, etc.) placed at considerable distances from the line of sight. The system is intrinsically protected against the effects of solar radiation combined with the nutation and precession movements of the carrier because it requires simultaneous signal presence within both fields of view.The open field fuze signal processor checks for the simultaneous presence of a positive IR signal and of a negative rate of change of the IR signal, both characteristic of an emitter coming out of the sensor F.O.V.
    • 10. 发明授权
    • Fuze signal processing circuit
    • Fuze信号处理电路
    • US3908552A
    • 1975-09-30
    • US38095764
    • 1964-07-07
    • US NAVY
    • DICK JOHN O
    • F42C13/02
    • F42C13/02
    • 1. In a fuze system having an infrared detector means and a firing circuit means, the improvement comprising a processing circuit that is not influenced by the high degree of modulation present in the signals from said detector means as the result of said detector scanning a jet engine exhaust plume, said processing circuit comprising: A. AN INPUT TERMINAL CONNECTED TO AND TO RECEIVE AN INPUT SIGNAL PROPORTIONAL TO INFRARED ENERGY RECEIVED FROM SAID INFRARED DETECTOR MEANS AS THE JET ENGINE EXHAUST PLUME IS SCANNED BY SAID DETECTOR, B. A FIRST DIODE COUPLED TO SAID INPUT TERMINAL AND BEING POLARIZED TO PASS A NEGATIVE GOING AND TO BLOCK POSITIVE SIGNALS, C. A STORAGE CAPACITOR COUPLED TO SAID DIODE AND BEING CHARGED TO PEAK AMPLITUDE OF SAID INPUT SIGNAL, D. AN OUTPUT TERMINAL CONNECTED TO SAID FIRING CIRCUIT MEANS, E. A NORMALLY CLOSED GATE CIRCUIT COUPLED ACROSS SAID STORAGE CAPACITOR AND COUPLED TO SAID OUTPUT TERMINAL, F. A SECOND DIODE COUPLING SAID INPUT TERMINAL TO SAID GATE CIRCUIT AND BEING POLARIZED TO PASS A POSITIVE VOLTAGE TO OPEN SAID GATE CIRCUIT AND DISCHARGE SAID STORAGE CAPACITOR IN RESPONSE TO A POSITIVE OVERSHOOT AT THE TERMINATION OF SAID INPUT SIGNAL.
    • 在具有红外检测器装置和点火电路装置的引信系统中,改进包括处理电路,其不受来自所述检测器装置的信号中存在的高度调制的影响,因为所述检测器扫描喷射 发动机排气羽流,所述处理电路包括: