| 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 | 用于射弹编程的方法和装置 | CN201180004955.9 | 2011-01-28 | CN102686970B | 2015-12-09 | H·R·弗里克 |
| 建议电感和/或电容地进行射弹（5）的编程。建议将波导管（2、11）用于编程，因为电磁场集中在波导管中。在此所使用的编程单元（1）包括至少一个波导管（2、11），其优选位于或集成在出口的区域中、例如口制退器（6）前方。用于传递的发射耦合器（3）由信号发生器（4）供给。在调制器（18）中为射弹（5）设置的信息被调制到载波频率（f1）上。在射弹（5）中集成接收耦合器（8），其与射弹（5）中的存储器或处理器（19）电连接。接收耦合器接收调制信号并且将其传送给处理器（19）。然后在处理器中进行原本的编程。 | ||||||
| 2 | 用于射弹编程的方法和装置 | CN201180004955.9 | 2011-01-28 | CN102686970A | 2012-09-19 | H·R·弗里克 |
| 建议电感和/或电容地进行射弹（5）的编程。建议将波导管（2、11）用于编程，因为电磁场集中在波导管中。在此所使用的编程单元（1）包括至少一个波导管（2、11），其优选位于或集成在出口的区域中、例如口制退器（6）前方。用于传递的发射耦合器（3）由信号发生器（4）供给。在调制器（18）中为射弹（5）设置的信息被调制到载波频率（f1）上。在射弹（5）中集成接收耦合器（8），其与射弹（5）中的存储器或处理器（19）电连接。接收耦合器接收调制信号并且将其传送给处理器（19）。然后在处理器中进行原本的编程。 | ||||||
| 3 | 射击装置控制系统 | CN201610946207.7 | 2016-11-02 | CN106323090A | 2017-01-11 | 李萍; 陈枫; 鞠珊; 张龙; 杨晓丽; 廖红波; 张俊; 彭为; 赖明 |
| 本发明公开了射击装置控制系统，包括射控箱、射控盒、射击装置和座圈电机，座圈电机安装在座圈上，座圈上固定有射控箱和射击装置，射控箱内部设置有射击控制板、座圈控制板、IGBT和继电器，射击装置中设有射击驱动电机、行星齿轮、离合部件和供弹机构，射击驱动电机与行星齿轮啮合；射击装置的上方设置有电磁离合器和射控盒，射控盒上设置有操控面板，操控面板、射击控制板、IGBT、射击驱动电机依次相连，射击控制板还与继电器、电磁离合器相连，电磁离合器与离合部件相连，离合部件与供弹机构啮合，操控面板依次与座圈控制板、座圈电机相连。本发明的有益效果是：射速可调、360度旋转打击目标、使用环境广泛、可靠性高、打击效果好。 | ||||||
| 4 | 一种针对区域打击任务的天基动能武器回归轨道部署方法 | CN201610388969.X | 2016-06-02 | CN106052482A | 2016-10-26 | 罗建军; 姚玮; 袁建平; 朱战霞; 马卫华; 唐歌实; 胡松杰; 李革非 |
| 本发明公开了一种针对区域打击任务的天基动能武器回归轨道部署方法，本发明能够仅利用9个平台就可以完成相同任务背景下的快速打击任务。本发明利用回归轨道周期与地球自转周期的特殊关系带来的回归效应，经过一定时间后，星下点轨迹又重新回到原先通过路线上的轨道特性，使得在单个轨道面内只需一个平台就可实现天基动能武器对于区域目标打击任务的轨道部署方式，从而大幅降低任务所需的总平台数。 | ||||||
| 5 | マシンからマシンへのターゲットを維持するポジティブ識別 | JP2017549254 | 2016-03-24 | JP2018516350A | 2018-06-21 | ピーブルズ,マクドナルド ジョン; マーティン,アンドリュー; ベイカー,チャールズ ローレンス; ワン,デイジー; アギレラ,ケヴィン,ジェイ; ハンナ,マシュー アレン; ヤング,ブライアン; ソーンボーガー,エリック; オーゴード,エリック ジェイムズ |
| ターゲット方法において、第1の航空機(100)上の第1の映像センサ(102)によって潜在的なターゲット座標に関するシーンの第1の映像をキャプチャするステップと、前記第1の航空機によって前記第1の映像(232)および関連する潜在的なターゲット座標を送信するステップと、プロセッサと通信している第1のディスプレイ上で前記第1の映像を受信し、前記プロセッサは前記潜在的なターゲット座標も受信するステップと、前記第1のディスプレイ上で前記第1の映像を見ることに応答して、前記潜在的なターゲット座標を第2の航空機の実際のターゲット座標(226)として選択するステップと、第2の航空機(116)を実際のターゲット座標に導くステップとを含み、実際のターゲット座標に対応するターゲット(114)のポジティブ識別が、実際のターゲット座標の選択時から維持される。 【選択図】図1C |
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| 6 | 発射体のプログラミングのための方法及び装置 | JP2012550371 | 2011-01-28 | JP5882911B2 | 2016-03-09 | ヘンリー ロジャー フリック |
| 7 | Method and device for programming of the projectile | JP2012550371 | 2011-01-28 | JP2013518237A | 2013-05-20 | ロジャー フリック ヘンリー |
| An inductive or capacitative programming of a projectile is disclosed. A waveguide is used for the programming, the electromagnetic field being concentrated in the waveguide. The used programming unit includes at least one waveguide which is preferable located and/or integrated in the region of the muzzle, for example in front of the muzzle brake. A transmission coupler for the transmission is fed by a signal generator. The information relating to the projectile is modulated to the carrier frequency in the modulator. A reception coupler integrated on/in the projectile is electrically interconnected to a store or processor in the projectile. The reception coupler receives the modulated signal and transmits it to the processor which is where the eventual programming takes place. | ||||||
| 8 | VERFAHREN ZUR ERMITTLUNG EINES MUNITIONSBEDARFS EINES WAFFENSYSTEMS | EP18158340.2 | 2018-02-23 | EP3367046A1 | 2018-08-29 | Muser, Christoph; Bachmann, Jörg |
Verfahren zur Ermittlung eines Munitionsbedarfs eines Waffensystems (01) zur Bekämpfung eines Ziels (04) in einer Realumgebung (05), wobei eine Zielposition (06) des zu bekämpfenden Ziels (04) mit einer georeferenzierten Simulationsdatenbasis, welche eine die Realumgebung (05) geospezifisch abbildende Simulationsumgebung (11) umfasst, analysiert wird, wobei mittels einer Klassifizierung der Simulationsumgebung die Simulationsumgebung an der Zielposition (06) ausgewertet wird und der Munitionsbedarf in Abhängigkeit der Auswertung bestimmt oder angepasst wird.
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| 9 | A NETWORKED BATTLE SYSTEM WITH HEADS UP DISPLAY | EP16798995.3 | 2016-05-26 | EP3304941A1 | 2018-04-11 | DOWNING, Warren |
| A networked battle system includes a communication network, a first rifle and a sensor pack attached to the rifle that includes a sensor for determining a bearing of the first rifle, a sensor for an accelerometer and a rate gyroscope. The system also includes a communication element coupled to the rifle allowing the sensor pack to provide sensor information to the communication network, a battle management system in communication with the first rifle through the communication network that receives the sensor information from the sensor pack updates a battle plan based on the sensor information to form an updated battle plan and a heads up display unit at least in operative communication with the communication network and the communication element and that displays the updated battle plan to a user. | ||||||
| 10 | A NETWORKED BATTLE SYSTEM OR FIREARM | EP14889015 | 2014-10-17 | EP3129740A4 | 2017-12-27 | DOWNING WARREN; COMPTON DAVID WALTER |
| A firearm includes one or more rails to which accessories may be mounted. The rails provide a communication path over which data may be transferred between the accessories and a processor located in the rails or in the firearm. The processor may cause the data to be sent to another location and may receive other data from other locations to provide a network of intercommunicating firearms that may deployed in a battlefield environment. | ||||||
| 11 | A NETWORKED BATTLE SYSTEM OR FIREARM | EP14851134 | 2014-09-09 | EP3044905A4 | 2017-09-20 | COMPTON DAVID WALTER; TEED BRENTON STEWART; DOWNING WARREN; CROCKER GARY EDWARD |
| 12 | A NETWORK OF INTERCOMMUNICATING BATTLEFIELD DEVICES | EP14841869.2 | 2014-09-03 | EP3044904A1 | 2016-07-20 | COMPTON, David Walter; TEED, Brenton Stewart; DOWNING, Warren; CROCKER, Gary Edward |
| A plurality of battlefield devices that communicate with a battle management system using a communications network to form a network of intercommunicating battlefield devices that may be deployed in a battlefield environment. Each battlefield device comprising one or more rails to which accessories may be mounted. The rails provide a communication path over which data may be transferred between the accessories and a processor located in the rails or in the battlefield device. The processor configured to cause the data to be sent to another location and to process other data received from other locations over said communications network. | ||||||
| 13 | INTEGRATED COMBAT RESOURCE MANAGEMENT SYSTEM | EP13801186 | 2013-06-07 | EP2859746A4 | 2016-03-16 | TURCOTTE STEPHANE; BLANCHETTE REMI; BELANGER DAVID; RIOUX FRANCOIS; RIVEST MARTIN; ROMANO PAUL; CURRY BILL |
| An integrated combat resource management device is in the form of a smartphone with a display screen and user input device. The smartphone has a set of integrated applications stored therein which when executed provide an interactive display offering dynamic real-time situational awareness information to the user. Configuration files contain user-specific profiles. A launcher application offers access control and the management of several user profiles on the same smartphone such that upon successful login the appropriate user-specific profile is applied. | ||||||
| 14 | METHOD AND SYSTEM OF MISSION PLANNING | EP12876509 | 2012-05-11 | EP2847644A4 | 2015-12-16 | ERIKSSON JAN ERIK; LUNDBERG KRISTIAN |
| 15 | WAFFENVERBUNDSYSTEM UND VERFAHREN ZUR STEUERUNG DESSELBEN | EP13773650.0 | 2013-09-23 | EP2906899A1 | 2015-08-19 | GLÖSMANN, Philipp; TROUVAIN, Boris |
| The invention relates to a composite weapon system (1) having at least one monitoring system (3) with a monitoring system control station (31), at least one active system (4) with an active system control station (41), and a composite control system (2) which is connected to the control stations (31, 41) of the monitoring (3) and active systems (4). The composite control system (2) has a computing unit (21) and a display device (22) which are designed to display data from the control stations (31, 41) of the monitoring (3) and active systems (4) and to display at least one input field (F09) for instructions for the control station (41) of an active system (4). | ||||||
| 16 | Harmonic shuttered seeker | EP14173511.8 | 2014-06-23 | EP2816311A3 | 2015-03-18 | Ell, Todd; Rutkiewicz, Robert |
A dual-mode, semi-active, laser-based and passive image-based seeker for projectiles, missiles, and other ordnance that persecute targets by detecting and tracking energy scattered from targets. The disclosed embodiments use a single digital imager having a single focal plane array sensor to sense data in both the image-based and laser-based modes of operation. A shuttering technique allows the relatively low frame-rate of the digital imager to detect, decode and localize in the imager's field-of-view a known pulse repetition frequency (PRF) from a known designator in the presence of ambient light and other confusing target designators, each having a different PRF.
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| 17 | Harmonic shuttered seeker | EP14173511.8 | 2014-06-23 | EP2816311A2 | 2014-12-24 | Ell, Todd; Rutkiewicz, Robert |
A dual-mode, semi-active, laser-based and passive image-based seeker for projectiles, missiles, and other ordnance that persecute targets by detecting and tracking energy scattered from targets. The disclosed embodiments use a single digital imager having a single focal plane array sensor to sense data in both the image-based and laser-based modes of operation. A shuttering technique allows the relatively low frame-rate of the digital imager to detect, decode and localize in the imager's field-of-view a known pulse repetition frequency (PRF) from a known designator in the presence of ambient light and other confusing target designators, each having a different PRF.
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| 18 | SYSTEM AND METHOD FOR REUSE OF COMMAND AND CONTROL SOFTWARE COMPONENTS | EP03799810 | 2003-05-23 | EP1573481A4 | 2010-04-07 | GRAVES KENNETH P; MILLER DARIUS F; ROY RONALD |
| 19 | Close-air-support assistant | EP09162407.2 | 2009-06-10 | EP2141438A1 | 2010-01-06 | Cornett, Alan; Becker, Robert Charles; Demers, Robert E. |
A system (24) includes a signal interface (74) configured to receive first data from at least one onboard system of at least one aircraft, a display (70), and a processing device (60). The processing device is configured to render to the display a graphical representation of a target location, determine from the first data and render to the display a graphical illustration of a position of the at least one aircraft, and determine, from information describing munitions carried by the at least one aircraft, and render to the display a graphical illustration of a blast radius associated with munitions deliverable by the at least one aircraft to the target location.
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| 20 | AREA DENIAL COMMUNICATION LATENCY COMPENSATION | US15838213 | 2017-12-11 | US20180167132A1 | 2018-06-14 | Michael J. BALK; Larry G. LINDE |
| An area denial system may be operationally placed with communication latency compensation. The area denial system may include a plurality of munitions, one or more sensor devices, and a command and control unit, networked together and having a command and control latency for communication between the command and control unit and the remainder of the area denial system. Latency compensation may include determining a first target position, determining a first predicted position area for the target using the command and control latency and the first target position, receiving an authorization to arm one or more of the munitions, determining a second target position, and determining that the second target position is outside a threshold distance from a first authorized munition of the one or more authorized munitions, and in response, de-authorizing the first authorized munition. | ||||||
