| 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 | Ammunition with projectile containing no explosive material in order to create a multi-spectral target signature | US14098106 | 2013-12-05 | US09513094B2 | 2016-12-06 | Lars Dierks; Christopher Zimmermann |
| An ammunition is proposed with an explosive-free missile that releases, upon dismantling at the target a fuel or fuel mixture as flammable air-fuel mixture, being caused to spontaneously react by at least one, by impact dismantling triggered, explosive-free, spark-generating ignition mechanism. The thus produced optical and thermal target signature can be detected with the naked eye, as well as with rifle scopes or other optical target detection systems, as well as with night-vision and thermal imaging devices. | ||||||
| 2 | Munition, charge for such a munition, and method of manufacturing such a munition | US14365727 | 2012-12-14 | US09476683B2 | 2016-10-25 | Marie Marchais; Olivier Bouchet; Bruno Nouguez |
| The invention provides a filler material for a munition, inluding an explosive charge, an inert charge and at least one pyrotechnic transmission unit adapted to transmit a remotely initiated detonation to said explosive charge. The invention also concerns a munition incorporating said filler material, said munition including a hollow elongate casing suitable for housing the explosive charge and the inert charge, and a firing device, at least a portion of the inert charge being interposed between the firing device and said explosive charge, and the pyrotechnic transmission unit being provided with a pyrotechnic extension and coupling the firing device to the explosive charge in order to prime detonation of the explosive charge under the action of the firing device. | ||||||
| 3 | MUNITION, CHARGE FOR SUCH A MUNITION, AND METHOD OF MANUFACTURING SUCH A MUNITION | US14365727 | 2012-12-14 | US20140331882A1 | 2014-11-13 | Marie Marchais; Olivier Bouchet; Bruno Nouguez |
| The invention provides a filler material for a munition, including an explosive charge, an inert charge and at least one pyrotechnic transmission unit adapted to transmit a remotely initiated detonation to said explosive charge. The invention also concerns a munition incorporating said filler material, said munition including a hollow elongate casing suitable for housing the explosive charge and the inert charge, and a firing device, at least a portion of the inert charge being interposed between the firing device and said explosive charge, and the pyrotechnic transmission unit being provided with a pyrotechnic extension and coupling the firing device to the explosive charge in order to prime detonation of the explosive charge under the action of the firing device. | ||||||
| 4 | Autonomous weapon effects planning | US14011543 | 2013-08-27 | US09372053B2 | 2016-06-21 | Erwin M. De Sa; David K. Barnett; Jeffrey B. Saunders; David E. Bossert |
| A method for autonomous weapon effects planning includes receiving the desired lethality and collateral effects information on a target and autonomously selecting at least one weapon and fuze setting from an inventory of weapons based on the received lethality and collateral effects information. The method further includes autonomously; determining which weapon with fuze setting and terminal elevation and heading angles satisfies the desired lethality and collateral effects; shaping weapon trajectory to satisfy weapon maneuverability, terrain clobber avoidance and guidance requirements and planning weapon launch conditions for the one or more autonomously selected weapons. The weapon launch conditions include at least a launch point or a launch corridor. | ||||||
| 5 | AUTONOMOUS WEAPON EFFECTS PLANNING | US14011543 | 2013-08-27 | US20150059564A1 | 2015-03-05 | Erwin M. De Sa; David K. Barnett; Jeffrey B. Saunders; David E. Bossert |
| A method for autonomous weapon effects planning includes receiving the desired lethality and collateral effects information on a target and autonomously selecting at least one weapon and fuze setting from an inventory of weapons based on the received lethality and collateral effects information. The method further includes autonomously; determining which weapon with fuze setting and terminal elevation and heading angles satisfies the desired lethality and collateral effects; shaping weapon trajectory to satisfy weapon maneuverability, terrain clobber avoidance and guidance requirements and planning weapon launch conditions for the one or more autonomously selected weapons. The weapon launch conditions include at least a launch point or a launch corridor. | ||||||
| 6 | AMUNITION WITH PROJECTILE CONTAINING NO EXPLOSIVE MATERIAL IN ORDER TO CREATE A MULTI-SPECTRAL TARGET SIGNATURE | US14098106 | 2013-12-05 | US20140305328A1 | 2014-10-16 | Lars Dierks; Christopher Zimmermann |
| An ammunition is proposed with an explosive-free missile that releases, upon dismantling at the target a fuel or fuel mixture as flammable air-fuel mixture, being caused to spontaneously react by at least one, by impact dismantling triggered, explosive-free, spark-generating ignition mechanism. The thus produced optical and thermal target signature can be detected with the naked eye, as well as with rifle scopes or other optical target detection systems, as well as with night-vision and thermal imaging devices. | ||||||
| 7 | MUNITION, CHARGEMENT POUR UNE TELLE MUNITION ET PROCEDE DE FABRICATION D'UNE TELLE MUNITION | EP12813928.4 | 2012-12-14 | EP2791616A1 | 2014-10-22 | MARCHAIS, Marie; BOUCHET, Olivier; NOUGUEZ, Bruno |
| The invention relates to a charge for a munition (10), comprising an explosive charge (40), an inert charge (50) and at least one pyrotechnique transmission unit (60) designed to transmit a remote-initiated detonation to said explosive charge (40). The invention also relates to a munition incorporating such a charge, said munition (10) comprising an elongate hollow body (12) able to house the explosive charge (40) and the inert charge (50), and a firing device (20), at least part of the inert charge (50) being interposed between the firing device (20) and said explosive charge (40), and the pyrotechnic transmission unit (60) being provided with a pyrotechnic extension (64) and coupling the firing device (20) to the explosive charge (40) in such a way as to allow the explosive charge to be primed to detonate under the action of the firing device (20). | ||||||
| 8 | EXPLOSIVSTOFFFREIES GESCHOSS FÜR ZIELMARKIERUNG | EP13789734.4 | 2013-10-29 | EP2929286A1 | 2015-10-14 | DIERKS, Lars; ZIMMERMANN, Christopher |
| The invention relates to ammunition with an explosives-free projectile (20, 20', 30, 30', 40), which releases a fuel or a fuel mixture as an inflammable air-fuel mixture upon breaking apart at the target, said air-fuel mixture being reacted spontaneously by at least one explosives-free, spark-generating ignition mechanism (4) triggered when the projectile breaks apart on impact. The thus produced optical and thermal target signature can be detected with the naked eye and with telescopic sights or other optical target detecting systems as well as with night-vision or thermal-imaging devices. | ||||||
| 9 | Munition, chargement pour une telle munition et procédé de fabrication d'une telle munition | EP12813928.4 | 2012-12-14 | EP2791616B1 | 2016-03-09 | MARCHAIS, Marie; BOUCHET, Olivier; NOUGUEZ, Bruno |
| 10 | 발사체용 신관 결합장치 | KR20160172493 | 2016-12-16 | KR20180070158A | 2018-06-26 | KIM JAE HO; CHO CHANG YEON; PAK CHANG HO; KIM JIN WON; HEO JUN HOE; SEO IL WON; JEONG PIL GYU; LIM HYEON JUN |
| 신관과탄체조립시 탄두정렬을수행하되회전부와고정부를구비하는발사체용신관결합장치에있어서, 상기회전부는결합몸체부를포함하고, 상기고정부는센서정렬을위한홀을구비하는하우징잠금링과상기하우징잠금링과결합하는상부커플링, 소정각도의회전으로상기상부커플링과결합되는하부커플링, 및상기상부커플링과하부커플링사이에개재된커플링홀더를포함하는커플링체로구성되되, 상기커플링체는상기상부커플링과상기하부커플링의결합시 형성된환형의홈을구비하고, 상기결합몸체부는원통의내측면에환형의턱을구비하고, 상기커플링체는상기결합몸체부내로삽입되되, 상기환형의홈과턱이맞물림으로써체결되는것을특징으로하는발사체용신관결합장치를제공한다. | ||||||
| 11 | 비행 가속도 신호 및 충격 신호의 이력을 제공하는 방법 및 장치 | KR1020170156617 | 2017-11-22 | KR101837738B1 | 2018-03-12 | 박상현; 손중탁; 정명숙; 정기훈 |
| 실시예는비행가속도신호및 충격신호의이력을제공하는방법및 장치에관한것으로, 일실시예에따른신관내부의가속도센서및 충격센서를이용하고, 전원이해제되어도데이터가삭제되지않는특성을포함하는비휘발성메모리를이용하여, 별도의이력측정장치를구성할필요없이신관자체만으로비행가속도및 충격신호이력을측정하여저장하고, 그결과를탄 회수후 외부통신을통해데이터를추출할수 있다. | ||||||
| 12 | 포탄 회전량을 측정하기 위한 회전량 송신장치 | KR2019960043337 | 1996-11-29 | KR2019980030241U | 1998-08-17 | 김영원 |
| 본고안은포탄신관의텔리메터리장치에관한것으로, 더상세하게는포탄의신관에장착되고포탄의발사후포탄자체전원부의전원으로포탄의운동에관한신호를검출하여지상의관측소로송출하여주는포탄신관의텔레메터리장치에있어서그 포탄의회전량을송신하기위한송신장치에관한것이다. 본고안은, 포탄의신관에장착되어발사되어, 그포탄의회전량을측정하기위한회전량신호를송신하는텔레메트리송신장치에있어서, 수광량에따른전기적신호를발생시키기위한두개의광센서를포함하는광센서부; 상기광센서부에서발생된전기적신호를최적의변조상태로만들기위한신호처리부; 상기신호처리부에서처리된광센서신호를수GHz대의반송파주파수에변조시키기위한변조부; 상기변조부를거쳐변조된반송파를송신하기위한전력증폭을담당하는전력증폭부; 그리고, 상기반송파를송신하기위한안테나를포함하여구성되는것을특징으로하는포탄회전량을측정하기위한회전량송신장치를제공함으로써, 지상의관측소에서이 송신신호를수신하여분석하여그 포탄의비행상태를정확히분석하여파악하게하는효과를제공한다. | ||||||
QQ群二维码
意见反馈
意见反馈