| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 一种多通道全向探测的激光引信及其方法 | CN201510801523.0 | 2015-11-19 | CN105509578A | 2016-04-20 | 姜毅; 孙超君; 刘锡民; 高洁; 张大庆 |
| 本发明公开了一种多通道全向探测的激光引信，包含：激光发射机，用于向待探测目标发射探测激光光束；激光接收机，用于接收待探测目标的回波及干扰的回波；信号处理单元，分别与所述激光发射机及激光接收机连接，用于产生激光光束发射基准时序，以控制激光发射机发射探测激光光束，还用于对激光接收机接收到的待探测目标的回波及干扰的回波进行分析处理，以完成对待探测目标的识别以及实现抗环境干扰和超低空抗海杂波干扰。本发明还公开了一种采用激光引信进行探测目标的方法。本发明具备大视场全向探测，作用距离长，抗光点和环境干扰能力强，并且适用于超低空领域。 | ||||||
| 2 | 激光引信设备 | CN201710508714.7 | 2017-06-28 | CN107328320A | 2017-11-07 | 王日金; 王双; 陈丽; 施向南; 汤爱平 |
| 本发明公开了一种激光引信设备，包括主控板组件及与主控板组件电连接的激光发射接收装置，其中，激光发射接收装置，用于根据主控板组件发送的多路脉冲驱动信号，对应产生多路脉冲激光，使用多路脉冲激光对目标进行辐射；并对碰到目标后被漫反射回来的多路脉冲激光进行光电转换，将多路脉冲激光转换为多路电脉冲信号；主控板组件，用于接收激光发射接收装置传来的多路电脉冲信号，识别多路电脉冲信号中的干扰信号和目标信号，并根据目标信号判断导弹有效杀伤半径内是否存在目标，若存在，则产生起爆信号，引爆战斗部，对目标进行击毁。本发明提供的激光引信设备，可快速、有效判别目标，提高抗干扰能力。 | ||||||
| 3 | 小型化大视场激光引信收发光学系统 | CN201611001433.4 | 2016-11-14 | CN106646863A | 2017-05-10 | 高洁; 刘锡民 |
| 本发明涉及一种小型化大视场激光引信收发光学系统，由三路发射光学系统和三路接收光学系统构成，在圆周方向上依次排列设置，每路发射光学系统与每路接收光学系统之间相邻交错设置，相邻两路发射光学系统的中心光轴之间的夹角为120°，相邻两路接收光学系统的中心光轴之间的夹角为120°；在弧矢方向上，每路发射光学系统采用120°的发射视场，每路接收光学系统采用120°的接收视场；在子午方向上，每路发射光学系统采用1°的发射视场；每路接收光学系统采用2°～8°的接收视场。本发明实现了激光引信对任意目标的大视场、周向360°无漏探测技术，并且满足激光引信小型化的要求，具有目标定位准确、探测精度高、抗干扰能力强的特点。 | ||||||
| 4 | 红外地雷 | CN201510911283.X | 2015-12-11 | CN105352378A | 2016-02-24 | 不公告发明人 |
| 一种红外地雷，属国防领域。解决了地雷的红外触发的问题。弹药体（5）上面是拉头叉（4），拉头叉（4）的叉口间是撞针（8），撞针与弹簧（7）连接；拉头叉另一端连接拉绳（3）的一端，拉绳的另一端与齿条（9）连接；齿条上有棱齿（2）；棱齿被套叉（1）的套着，套叉的另一端连接电机（6）；地雷体外有人体红外探头（17），探头上用导线连接到红外信号放大模块（16）；红外信号放大模块用导线通过电阻连接三极管的基极。用于国防。 | ||||||
| 5 | Sector type approach detection method to target, detection apparatus and weapon using the same | JP35801491 | 1991-12-27 | JPH0688864A | 1994-03-29 | DANIERU UISOO |
| PURPOSE: To detect a moment when a flying misile most approaches a target to emit the trigger of warhead explosion. CONSTITUTION: A rotating flying misile has an optical device 8 catching light incident at a certain angle with respect to a main axis XX' in an advance direction. This apparatus condenses the light incident from a window 2 to a condensing lens 12 through mirrors M1, M2 and an image is formed on one set of mosaic like detectors to which detection spaces are respectively allotted and radiation is detected from a target. The detected signal is transmitted to a logic 11 through a signal converter 10 to be processed. | ||||||
| 6 | JPS4948200A - | JP4078173 | 1973-04-10 | JPS4948200A | 1974-05-10 | |
| 7 | JPS5652275B2 - | JP11172376 | 1976-09-20 | JPS5652275B2 | 1981-12-10 | |
| 8 | Active light proximity fuse | JP11172376 | 1976-09-20 | JPS5338200A | 1978-04-07 | WATANABE YASUO; KIHARA TAKEMITSU; NAKAYAMA KIYOSHI; KOBAYASHI ATSUHIRO; KOBAYASHI TAKESHI; WAKAYAMA YOUJI; FUKUMIZU KEIICHI |
| PURPOSE:To reduce the weight of a light proximity fuse and ensure accurate action thereof through the formation of a receiving view free of non-sensitive zone around the axis thereof with the detection of a laser beam reflected on a target by a receiving section of narrow view and by means of a means discriminating background noise. | ||||||
| 9 | Judotekijohokensakukinsetsushinkan | JP7921475 | 1975-06-24 | JPS5163672A | 1976-06-02 | OOKE HAA PEE BURONKUFUISUTO; BERUTEIRU TEE ERIKUTSUSON |
| 10 | 접근하는 발사체를 향하여 방어용 포탄의 탄두를 발사하기위한 근접 센서 | KR1020037016774 | 2003-02-15 | KR1020040086155A | 2004-10-08 | 슈토이에르라이마르; 바름베른트 |
| 근접 센서(11)는 보호받을 물체로부터 공격용 발사체에 대하여 발사되어 공격체의 기능을 방해하거나 완전히 파괴하기 위한 방어용 포탄의 반경 방향으로 작동되는 탄두를 초기화하기 위한 것이다. 이러한 목적을 위해, 상기 근접 센서(11)는 포탄에 의해 방어될 공격체가 그 비행 방향으로 나타나도 아직 응답해서는 안되고, 작동될 수 있는 최적의 거리로 방어될 공격체가 전방에서 경사지게 감지되었을 때에만 응답해야 한다. 환형의 검출기 부재(12)가 원통형 볼록 렌즈(14) 뒤의 이미지 초점 평면에 배열되는 경우에 중공 원뿔 벽 형태의 이러한 응답 특성이 제공된다. | ||||||
| 11 | 광학식 근접신관 점검장치의 셔터 치구 구동회로 | KR2019960054186 | 1996-12-23 | KR2019980041096U | 1998-09-15 | 이상현 |
| 본고안은광학식근접신관점검장치에관한것으로, 더상세하게는 4개의채널의광학송수신장치를갖는광학식신관에있어서, 비또는구름등의외부조건을모의적으로인가하고이에따른신관의정상작동여부를용이하게측정하기위한검사장치에대한것이다. 본고안은, 광학식근접신관의비, 구름조건에다른정상작동여부를시험하기위하여점검우물, 이점검우물에피 검사대상신관을장착하고, 그신관에연결하여그 신관의전기광학적특성및 그동작상태를점검하기위한장치에있어서, 상기광학식근접신관의 4개의채널에대하여각각동작하는 4개의셔터스위치; 상기셔터스위치를온으로하면턴 온되어셔터구동릴레이의코일에전류회로를연결하기위한셔터구동트랜지스터; 상기셔터구동트랜지스터가턴 온됨에따라그 코일이자화되어접점을연결시키는셔터구동릴레이; 상기셔터구동릴레이의접점이연결됨에따라상기점검장치의셔터를열어주기위한셔터구동솔레노이드; 그리고, 상기셔터구동솔레노이드의구동에따른셔터열림을사용자에게알리기위한경보회로부를포함하여구성되는것을특징으로하는광학식신관의비, 구름조건에따른정상작동여부를검사하기위한검사장치를제공한다. | ||||||
| 12 | Procédé de commande d'un module d'attaque et module d'attaque mettant en oeuvre un tel procédé | EP09290743.5 | 2009-09-30 | EP2175226B1 | 2012-12-26 | Bredy, Thierry |
| 13 | Optical proximity fuze | EP09275015.7 | 2009-03-12 | EP2228619A1 | 2010-09-15 | The designation of the inventor has not yet been filed |
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.
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| 14 | ANNÄHERUNGSSENSOR, INSBESONDERE FÜR DIE ZÜNDAUSLÖSUNG DES GEFECHTSKOPFES EINER ABWEHRGRANATE GEGEN EIN ANFLIEGENDES PROJEKTIL | EP03742524.6 | 2003-02-15 | EP1476713A2 | 2004-11-17 | STEUER, Raimar; WARM, Berndt |
| The invention relates to a proximity sensor (11) for initiating the warhead of an anti-missile shell that is launched from the object to be protected in the direction of an approaching attacking projectile, in order to disturb or even destroy the functionality of the attacker. The proximity sensor (11) should not yet respond to the appearance of the adversary to be fought of ahead of the course thereof; rather, the proximity sensor should respond only when the adversary to be fought of is detected at a distance and at an angle ahead that is optimal for the effect of the anti-missile shell. Such a hollow cone wall-shaped response characteristic is achieved when an annular detector element (12) is disposed in the image focus plane behind a positive cylindrical lens (14). | ||||||
| 15 | Projectile dont la charge explosive est déclenchée au moyen d'un désignateur de cible | EP97400767.6 | 1997-04-03 | EP0800054B1 | 2001-09-19 | Bilbaut, Jean-Noel; Laurend, Pascal |
| 16 | METHOD FOR INCREASING THE PROBABILITY OF IMPACT WHEN COMBATING AIRBORNE TARGETS, AND A WEAPON DESIGNED IN ACCORDANCE WITH THIS METHOD | EP96933715.0 | 1996-10-04 | EP0864073A1 | 1998-09-16 | REGEBRO, Chirster |
| 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. | ||||||
| 17 | Sensor system | EP94850154.9 | 1994-09-07 | EP0644396A3 | 1997-01-15 | Almqvist, Bo Nilsson; Nilsson, Björn |
The invention relates to a sensor system with a number of sensor stations for surveillance of an area intended to include an object to be protected. The sensor stations (1-4) are essentially distributed along the periphery of a circle (5). Each sensor station comprises a detector unit (11) arranged to scan the arc in an azimuth sector allocated to it in two detection fields (9,10). The time of passage T of a target which passes the two detection fields is measured and the target position is calculated on the basis of the measured time T, the target speed Vmissile, the angle between the detection fields a and the angle to the target β. In the sensor system, the scanning is carried out from below and up towards the background of the sky. This implies that the scanning is not interfered by the surrounding terrain and that a large IR area is obtained. The sensor system according to the invention increases the possibilities of detecting low-flying missiles and similar targets in comparison with conventional technology |
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| 18 | Procédé et dispositif de détection de proximité sectorielle d'une cible et munition utilisant le dispositif | EP91403540.7 | 1991-12-26 | EP0493256B1 | 1995-12-06 | Wisshaupt, Daniel |
| 19 | Sous-munition à effet dirigé | EP93402200.5 | 1993-09-09 | EP0589746A1 | 1994-03-30 | Redaud, Chirstophe |
Une sous-munition à effet dirigé se déplace selon une direction sensiblement verticale V avec une vitesse de translation v parallèle à V et une vitesse de rotation r autour d'un axe parallèle à V. La sous-munition comporte une charge formée (2) d'axe D formant un angle aigu t avec l'axe V et un dispositif de détection d'axe d formant avec l'axe D un angle u, des moyens (21 à 24 ; 26) pour détecter une cible (5) et des moyens (8) pour déclencher la charge formée (2). La sous-munition comporte en outre des moyens (28) pour déterminer à tout instant la vitesse de translation v et des moyens de calcul (29) pour calculer en fonction de v une valeur ui de l'angle u minimisant l'écart (e) entre la position (M) d'une cible détectée à l'instant considéré et le point d'impact (M') du noyau de la charge formée (2) si celle-ci était déclenchée à l'instant considéré, ainsi que des moyens pour donner à l'angle u ladite valeur ui. Application à une charge à effet dirigé permettant d'augmenter notablement la probabilité d'atteindre une cible telle qu'un véhicule terrestre. |
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| 20 | Vorrichtung für die Zielerkennung und Zündauslösung von abzufeuernden Horizontal-Minen für die Panzerabwehr | EP90115977.2 | 1990-08-21 | EP0414203B1 | 1994-03-30 | Deuss,Matthias; Pfaff,Helmut |
