| 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 | 用于火箭筒的整套演习教练器材 | CN200680004737.4 | 2006-02-02 | CN100545572C | 2009-09-30 | V·V·科连科夫; S·V·谢尔吉延科; V·M·乌沙科夫; P·N·万科夫; V·A·兹纳库尔科; N·N·伊韦内夫 |
| 本发明涉及兵器技术领域并可以用作为火箭发射器的演习教练器材。手持反坦克火箭筒射击用的整套演习教练器材由发射装置(1)和演习教练弹(2)构成。发射装置的前部是导向发射管(3)，其上装有模拟实弹弹体的备换零件(4)。发射装置的后部是发射装药(18)的可更换药室(7)，并配有喷孔(9)和排气道(10)。演习教练弹弹体(5)同时是发射装置(1)的导向发射管(3)的延伸部分和模拟火箭弹的运输容器。发射装置的各组成部分预先或在装到火箭筒上之前直接与演习教练弹弹体相连。本发明能完全模拟技术性能、人机工程学指标和各项准备工序，即使使用实弹类似物也会排除发射管磨损，从而能保证多次使用发射装置。 | ||||||
| 2 | 整套演习教练器材 | CN200680004737.4 | 2006-02-02 | CN101120228A | 2008-02-06 | V·V·科连科夫; S·V·谢尔吉延科; V·M·乌沙科夫; P·N·万科夫; V·A·兹纳库尔科; N·N·伊韦内夫 |
| 本发明涉及兵器技术领域并可以用作为火箭发射器的演习教练器材。手持反坦克火箭筒射击用的整套演习教练器材由发射装置(1)和演习教练弹(2)构成。发射装置的前部是导向发射管(3)，其上装有模拟实弹弹体的备换零件(4)。发射装置的后部是发射装药(18)的可更换药室(7)，并配有喷孔(9)和排气道(10)。演习教练弹弹体(5)同时是发射装置(1)的导向发射管(3)的延伸部分和模拟火箭弹的运输容器。发射装置的各组成部分预先或在装到火箭筒上之前直接与演习教练弹弹体相连。本发明能完全模拟技术性能、人机工程学指标和各项准备工序，即使使用实弹类似物也会排除发射管磨损，从而能保证多次使用发射装置。 | ||||||
| 3 | JPS62148897U - | JP3541486 | 1986-03-13 | JPS62148897U | 1987-09-19 | |
| 4 | VERFAHREN ZUR REDUKTION DES GEFAHRENBEREICHS GELENKTER ÜBUNGSMUNITION; ÜBUNGSMUNITION; SYSTEM | EP15001662.4 | 2015-06-03 | EP2960617A1 | 2015-12-30 | Kuhn, Thomas; Knutzen, Björn; Noll, Matthias; Rumsauer, Wolfgang |
Verfahren zur Reduktion des Gefahrenbereichs (GG) gelenkter Übungsmunition, umfassend folgende Schritte: |
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| 5 | ÜBUNGSSET | EP06716856.7 | 2006-02-02 | EP1852671B1 | 2014-12-24 | KORENKOV, Vladimir Vladimirovich; SERGIENKO, Sergei Vladimirovich; USHAKOV, Vyacheslav Mikhailovich; VANKOV, Petr Nikolaevich; ZNAKHURKO, Valery Alekseevich; IVENEV, Nikolai Nikolaevich |
| 6 | TRAININGS-ÜBUNGSSET | EP06716856.7 | 2006-02-02 | EP1852671A1 | 2007-11-07 | KORENKOV, Vladimir Vladimirovich; SERGIENKO, Sergei Vladimirovich; USHAKOV, Vyacheslav Mikhailovich; VANKOV, Petr Nikolaevich; ZNAKHURKO, Valery Alekseevich; Ivenev, Nikolai Nikolaevich |
Die Erfindung bezieht sich auf einen praktischen Lehrgerätesatz zum Schießen mit einem Panzerabwehrhandgranatwerfer. Der Lehrgerätesatz weist eine Starteinrichtung und ein praktisches Lehrgeschoss auf. Die Starteinrichtung besteht aus Bestandteilen, die mit dem Gehäuse des praktischen Lehrschusses vorher oder unmittelbar vor der Einbringung in den Granatwerfer zu verbinden sind. Das Vorderteil der Starteinrichtung weist einen Leitlauf auf, auf dem Auswechselteile angebracht sind, die das Gehäuse des Kampfschusses imitieren, dass der hintere Teil der Starteinrichtung einen abnehmbaren Sprengstoffladeraum des Wurfschusses bildet und mit einer Düse und einer Gasleitung versehen ist. Das verbindende Gehäuse des praktischen Lehrschusses bildet gleichzeitig die Fortsetzung des Leitlaufs der Starteinrichtung und der Beförderungsbehälter der imitierten R-Abschussgranate mit Leitwerk. |
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| 7 | METHOD FOR PERFORMING EXO-ATMOSPHERIC MISSILE INTERCEPTION TRIALS | EP09722577.5 | 2009-03-17 | EP2288865A2 | 2011-03-02 | ROVINSKY, Jacob; TOURGEMAN, Yoav |
| An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile geometry. | ||||||
| 8 | TRAININGS-ÜBUNGSSET | EP06716856 | 2006-02-02 | EP1852671A4 | 2010-07-28 | KORENKOV VLADIMIR VLADIMIROVICH; SERGIENKO SERGEI VLADIMIROVICH; USHAKOV VYACHESLAV MIKHAILOVICH; VANKOV PETR NIKOLAEVICH; ZNAKHURKO VALERY ALEKSEEVICH; IVENEV NIKOLAI NIKOLAEVICH |
| 9 | Übungsrakete | EP83101908.8 | 1983-02-26 | EP0090184A2 | 1983-10-05 | Mathey, Christoph |
Übungsrakete zum Abschuß aus einem Original-Werferrohr für den scharfen Schuß, bei welcher der äußere Durchmesser kleiner als derjenige der Originalrakete für den scharfen Schuß ist und die Übungsrakete zur Führung im Werferrohr mit - in Längsrichtung betrachtet - im Abstand voneinander angeordneten, beim Abschuß an der Werferrohrwandung entlang gleitenden Distanzelementen versehen ist. |
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| 10 | METHOD FOR PERFORMING EXO-ATMOSPHERIC MISSILE INTERCEPTION TRIALS | EP09722577.5 | 2009-03-17 | EP2288865B1 | 2016-12-21 | ROVINSKY, Jacob; TOURGEMAN, Yoav |
| 11 | SURROGATE RPG | EP12811011 | 2012-07-06 | EP2729758A4 | 2014-11-19 | LAWSON WILLIAM R; QUIGLEY SCOTT PAUL; MILLIKEN JAMIE ORLANDO; CARDENAS ROBERT LEE |
| 12 | SURROGATE RPG | EP12811011.1 | 2012-07-06 | EP2729758A1 | 2014-05-14 | LAWSON, William, R.; QUIGLEY, Scott, Paul; MILLIKEN, Jamie, Orlando; CARDENAS, Robert, Lee |
| A surrogate RPG includes a warhead with an outer conductive portion and an inner conductive portion spaced from the outer conductive portion. A sabot includes an electrical circuit configured to monitor conductivity between the inner and outer conductive portions. The surrogate RPG can be used to test the effectiveness of various RPG defeat technologies. | ||||||
| 13 | Practice rocket | EP83101908 | 1983-02-26 | EP0090184A3 | 1983-11-30 | Mathey, Christoph |
| Übungsrakete zum Abschuß aus einem Original-Wer ferrohr für den scharfen Schuß, bei welcher der äußere Durchmesser kleiner als derjenige der Originalrakete für den scharfen Schuß ist und die Übungsrakete zur Führung im Werferrohr mit - in Längsrichtung betrachtet - im Ab stand voneinander angeordneten, beim Abschuß an der Werferrohrwandung entlang gleitenden Distanzelementen versehen ist. | ||||||
| 14 | 완구용 로켓 | KR2020130007540 | 2013-09-09 | KR200472554Y1 | 2014-05-07 | 정호원 |
| 완구용로켓이개시된다. 본고안의일 실시예에따른완구용로켓은, 내측에중공부가형성되는막대형상의지지대, 상기지지대의상단과하단에형성되고, 상기지지대가회전할때 상기지지대와함께회전하는고정부, 상기지지대의중간에형성되고, 상기고정부가회전하는방향과반대방향으로회전하는중간날개및 상기지지대의하단에형성된고정부의끝단에형성되는프로펠러를구비하며, 상기프로펠러가회전하는반작용에의해상기프로펠러가회전하는방향의반대방향으로상기지지대및 상기고정부를회전시키는구동부를포함하고, 상기중간날개부는상기고정부가회전하는방향과반대방향으로회전하여비행방향을조절할수 있다. | ||||||
| 15 | Method for performing exo-atmospheric missile's interception trial | US14861328 | 2015-09-22 | US10012481B2 | 2018-07-03 | Jacob Rovinsky; Yoav Tourgeman |
| An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile. | ||||||
| 16 | METHOD FOR PERFORMING EXO-ATMOSPHERIC MISSILE'S INTERCEPTION TRIAL | US15130526 | 2016-04-15 | US20170343325A1 | 2017-11-30 | Jacob ROVINSKY; Yoav TOURGEMAN |
| An inflatable dummy target comprising a chassis of inflatable ducts wrapped with a sheet. | ||||||
| 17 | Smart-store emulation unit | US13370195 | 2012-02-09 | US08967032B2 | 2015-03-03 | Edward H. Campbell |
| A smart-store emulation unit is provided for use on-board a weapon platform in place of the physical presence of a smart-store. The emulation unit may be used for operator training on or testing of the smart-store on-board an operational weapon platform such as an aircraft, tank or ship. | ||||||
| 18 | SMART-STORE EMULATION UNIT | US13370195 | 2012-02-09 | US20130211813A1 | 2013-08-15 | Edward H. CAMPBELL |
| A smart-store emulation unit is provided for use on-board a weapon platform in place of the physical presence of a smart-store. The emulation unit may be used for operator training on or testing of the smart-store on-board an operational weapon platform such as an aircraft, tank or ship. | ||||||
| 19 | METHOD FOR PERFORMING EXO-ATMOSPHERIC MISSILE'S INTERCEPTION TRIAL | US12405664 | 2009-03-17 | US20120292450A1 | 2012-11-22 | Jacob ROVINSKY; Yoav TOURGEMAN |
| An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile | ||||||
| 20 | Method and apparatus for testing engines | US10164718 | 2002-06-10 | US20030051536A1 | 2003-03-20 | Jason S. Tyll; Robert J. Bakos; Florin Girlea; Ralph Woelfel; Dean Modroukas; John I. Endos |
| A scramjet has a cowl, a center structure, and a plurality of wide pylons connecting the cowl to the center structure, with scramjet engines positioned between adjacent pylons. Leading surfaces of adjacent pylons converge to one another to provide side wall compression to air entering the engines. The center structure includes a fore body, a center body and an aft body that, with the pylons, define a basic structure either formed entirely from one piece or several securely connected pieces. A method of testing the scramjet projectile comprises using a gun to accelerate the scramjet projectile to the takeover velocity of the engines. | ||||||
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