专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明公开

EP2812646A4 BRAKE PANEL FOR A DETONATOR OR A PROJECTILE 有权
标题翻译：制动盘连接保险丝和地板
公开(公告)号：EP2812646A4
公开(公告)日：2015-09-16
申请号：EP13746181
申请日：2013-01-28
申请人： BAE SYSTEMS BOFORS AB
发明人： PETTERSSON THOMAS , ENGMAN PETER , JOHANSSON BJÖRN
IPC分类号： F42B10/50 , F42C19/02
CPC分类号： F42B10/50 , F42C19/02
摘要： The invention relates to a brake panel (3, 3′) for a projectile (1), in which those surfaces (A) of the brake panel (3, 3′) which are facing in the direction of travel of the projectile are wholly or partially angled in such a way that the normal from the said surfaces (A) is not parallel with the center line (C) of the projectile (1) in order to reduce or counteract the Magnus torque generated during and after the extension of the brake panel (3, 3′). The invention further relates to a detonator (2) for a projectile (1) and a projectile (1) comprising such a brake panel.

2. 发明公开

EP2871438A1 Rocket or artillery launched smart reconnaissance pod 失效转让
标题翻译：通过火箭或枪的手段击落智能集装箱侦察
公开(公告)号：EP2871438A1
公开(公告)日：2015-05-13
申请号：EP14192253.4
申请日：2014-11-07
申请人： Lonestar Inventions L.P.
发明人： Akcasu, Osman Ersed , Uslu, Ibrahim Onur , Leblebici, Yusuf
IPC分类号： F42B10/56 , F42B12/36 , F42B12/58 , F42B10/50
CPC分类号： F42B12/365 , B64D17/00 , F42B5/025 , F42B10/50 , F42B10/56 , F42B12/58 , F42B30/006
摘要： A modular reconnaissance capsule or reconnaissance pod (10) is provided that is suitable for deployment by means of an artillery launching platform, such as a conventional 40 mm grenade launcher or 155 mm cannon wherein a parachute (24) is deployed at a pre-calculated observation altitude, the parachute (24) being designed to yield a sufficiently slow rate of descent to permit live video capture and transmission of images as forward observation information. Alternatively, pods according to the invention may also be air dropped from an aircraft, either piloted or pilotless, thus allowing the aircraft to operate at a safe distance and yet provide close reconnaissance even under a cloud cover. Accurate information about targeting dynamics is made available to the user through commercially available products. The invention complements other reconnaissance methods and provides easy-to-use real-time visual information for a desired area of interest.
摘要翻译：提供了一种模块化的侦察胶囊或侦察吊舱（10）所做的是适于部署由火炮发射平台的方式，检查作为worin降落伞（24）被部署在预先计算的一个传统的40mm榴弹发射或155毫米炮观察高度，降落伞（24）被设计成产生下降的足够慢的速度，以允许实时视频捕获和图像作为正向观察信息的传输。可替代地，豆荚gemäß发明因此可以是空气从飞机下降到，无论是驾驶或无人驾驶，因此允许飞机在安全距离操作，但甚至在云盖提供接近侦察。有关定位动态的准确信息，通过市售的产品提供给用户。本发明补充了其他的侦察方法，并提供期望的感兴趣区域易于使用的实时视觉信息。

3. 发明公开

EP2268996A1 METHODS AND APPARATUS FOR GUIDANCE OF ORDNANCE DELIVERY DEVICE 有权
标题翻译：方法和装置用于实现枪供应设备
公开(公告)号：EP2268996A1
公开(公告)日：2011-01-05
申请号：EP09734567.2
申请日：2009-04-22
申请人： Raytheon Company
发明人： GESWENDER, Chris, E. , BENNETT, Stephen, E.
IPC分类号： F42B10/50 , F42B10/64
CPC分类号： F42B10/64 , F42B10/50
摘要： A guidance system (102) according to various aspects of the present invention operates in conjunction with a suite of different ordnance delivery devices (100). In one embodiment, the guidance system (102) comprises an interface (110) configured to attach to the ordnance delivery devices (100) in the suite, such, as via the fuze well. The guidance system (102) may further include a control system (112) adapted to attempt to establish communications with a subsystem of the ordnance delivery device (100) and operate the guidance system (102) as a standalone guidance system if the attempt fails. The guidance system (102) may further include a control surface (120) interchangeably attachable, for example via an interchangeable control surface module.

4. 发明授权

EP1366339B1 2-D PROJECTILE TRAJECTORY CORRECTOR 有权
标题翻译：二维弹道FLOOR校正装置
公开(公告)号：EP1366339B1
公开(公告)日：2009-07-29
申请号：EP02713500.3
申请日：2002-01-29
申请人： BAE Systems Land & Armaments L.P.
发明人： RUPERT, John, G. , SIEWART, Jeff
IPC分类号： F42B10/50 , F42B10/54 , F42B10/60
CPC分类号： F42B12/36 , F42B10/50 , F42B10/54 , F42B10/64
摘要： A device and method of adjusting a trajectory of a projectile (20) in flight including increasing projectile (20) drag to effect a downrange correction and altering the yaw of repose to effect a cross range correction. A method of a vernier correction to the trajectory is included.

5. 发明公开

EP1540264A1 BREMSEINRICHTUNG FÜR EIN BAHNKORRIGIERBARES DRALLSTABILISIERTES ARTILLERIEPROJEKTIL 有权转让
标题翻译：刹车装置FOR A BAHNKORRIGIERBARES DRALL稳定型炮弹
公开(公告)号：EP1540264A1
公开(公告)日：2005-06-15
申请号：EP03775150.0
申请日：2003-09-10
申请人： Diehl BGT Defence GmbH & Co.KG
发明人： BÄR, Klaus , KAUTZSCH, Karl
IPC分类号： F42B10/50
CPC分类号： F42B10/50
摘要： The aim of the invention is to rapidly bring a ring wheel-shaped textile braking element (16), which is radially deployed by a centrifugal force, into a dimensionally stable contour that is defined at all times even under conditions during which it is being flown against. To this end, a fabric (33) that is cut to size in the shape of a circular ring is provided with a reduced outer circumference (32) by means of radially extending tucks whereby restricting the spreading movement to the shape of a flat obtuse-angled hollow truncated cone, which is coupled to a retaining ring (15) at the inner circumference (31) by means of reinforcing strips (34) that are sewn along generators of the outer surface of the cone, and which is provided with an encircling mass accumulation part (29) along the outer circumference (32) while serving to increase the centrifugal deploying forces. In the front face area of the stowing space (14), the ring (15) is axially fixed in the contour of the detonator (11) while momentarily slipping through relative to the spin of the projectile.

6. 发明授权

EP0675334B1 Engin largable à stabilisation et freinage aérodynamique 失效
标题翻译：空气动力学稳定和脱落体制动装置
公开(公告)号：EP0675334B1
公开(公告)日：2000-04-12
申请号：EP95400414.9
申请日：1995-02-27
申请人： Matra Bae Dynamics France
发明人： Elmayan, Naîri , Seco, Manuel Henri , Beslier, Hugues , Audouin, Jean-Pierre
IPC分类号： F42B10/16 , F42B10/50
CPC分类号： F42B10/16 , F42B10/50

7. 发明公开

EP0907874A1 MEANS FOR INCREASING THE DRAG ON A MUNITION 失效
标题翻译： DEVICE FOR弹丸增加空气阻力
公开(公告)号：EP0907874A1
公开(公告)日：1999-04-14
申请号：EP97928379.0
申请日：1997-06-30
申请人： THE SECRETARY OF STATE FOR DEFENCE
发明人： SIDFORD, Rufus, William-Intellectual Property Dept
IPC分类号： F42B10
CPC分类号： F42B10/50
摘要： A means for increasing the drag of a munition to effect a course correction having coplanar interlocking pairs of drag plates (24, 26) being laterally extendable from an undeployed configuration, substantially contained within the munition, to a deployed configuration. The drag plates (101, 103) are provided with projections (34, 38) and slots (36, 40), the projections (34, 38) of one of a pair of drag plates being adapted to locate in the slots (34, 40) of the other drag plate in the undeployed configuration and being adapted such that they extend beyond halfway into the munition. A deployment means (60, 62, 70, 72) retains the drag plates in the undeployed configuration until receipt of a control signal and then effects deployment of the drag plates, the distance travelled between the deployed and undeployed configurations being determined by the extent of the projections (34, 38).

8. 发明授权

EP0630465B1 DISPOSITIF DE POSITIONNEMENT POUR SOUS-MUNITION DISPERSABLE 失效
标题翻译：设备用于定位的集束弹药
公开(公告)号：EP0630465B1
公开(公告)日：1997-10-01
申请号：EP94900192.9
申请日：1993-11-16
申请人： GIAT Industries
发明人： DUSSOL, Jean-Pierre
IPC分类号： F42B23/24 , F42B10/50
CPC分类号： F42B23/24 , F42B10/50
摘要： The field of the present invention is that of devices for positioning dispersible sub-ammunition. The device for positioning sub-ammunition (1) according to the invention comprises a series of flexible tongues (16, 20, 22) regularly spaced about the sub-ammunition. The device is characterized in that the tongues are so arranged that the resultant of the aerodynamic forces acting on the sub-ammunition (1) is applied at a point to the rear of the latter's centre of gravity, and in that the tongues (22) secured to a surface (10) located in a rear part of the sub-ammunition in the direction of its path are so shaped that they undergo permanent deformation once the mine is released. Application to dispersible mines.

9. 发明公开

EP0675334A1 Engin largable à stabilisation et freinage aérodynamique 失效
标题翻译： Aerodynamische Stabilisier- und BremsvorrichtungfürAbwurfkörper。
公开(公告)号：EP0675334A1
公开(公告)日：1995-10-04
申请号：EP95400414.9
申请日：1995-02-27
申请人： MATRA DEFENSE
发明人： Elmayan, Naîri , Seco, Manuel Henri , Beslier, Hugues , Audouin, Jean-Pierre
IPC分类号： F42B10/16 , F42B10/50
CPC分类号： F42B10/16 , F42B10/50
摘要： L'engin largable est muni de moyens passifs de stabilisation aérodynamique et destiné à prendre une trajectoire initiale sensiblement parallèle à la vitesse de l'aéronef après largage. Il comporte, à l'arrière, des volets (17) déployables automatiquement après largage et constitués de façon que la pression dynamique qui s'exerce sur les volets modifie automatiquement la traînée supplémentaire donnée par les volets en fonction inverse de ladite pression dynamique.
摘要翻译：导弹配备被动稳定器，并设计成跟踪与发射飞机平行的初始轨迹。它具有灵活的后挡板（17），其在发射后自动部署，使得它们的部署速率随着释放时施加到其上的空气动力压力而变化。襟翼的前端固定在导弹（10）的主体上，并被一系列较短的叶片（20）加固。否则，襟翼可以是金属叶片的形式，其被枢转到导弹的后部并且通过空气的压力向外打开。他们的枢轴可以装备有在给定压力下缩回或断裂的止动件。

10. 发明公开

EP0540484A1 Improvements to sub-combat units 失效
标题翻译：对战斗单位的改进
公开(公告)号：EP0540484A1
公开(公告)日：1993-05-05
申请号：EP92850202.0
申请日：1992-08-27
申请人： Bofors AB
发明人： Axinger, Jan , Engman, Peter
IPC分类号： F42B12/58 , F42B10/50
CPC分类号： F42B10/50
摘要： The invention relates to a sub-combat unit which is arranged to be separated from a flying body, for example a carrier shell or the like, for example over a target area, the sub-combat unit including a warhead, a target detector and two diametrically disposed carrier surfaces (1, 2) which, via carrier arms (7, 8) are pivotally disposed each on its own shaft (4, 5) located in a plane which is normal to the line of symmetry of the warhead from a collapsed position in which the carrier arms and carrier surfaces connect to the circumferential surface of the sub-combat unit, and to a position opened at 90° at which both of the carrier surfaces form a retarding area for the fall velocity of the sub-combat unit and impart to the sub-combat unit a rotation for scanning the target area in a helical pattern during the fall of the sub-combat unit towards the target area. The sub-combat unit includes a wing flip-out mechanism with damping devices (9, 10) of rubber disposed on each carrier surface (1, 2), in connection with the casing of the sub-combat unit, the damping devices being compressed by the carrier arms (7, 8) during the flip-out movement, and return stops (11, 12) against which the carrier arms are operative to spring back.
摘要翻译：本发明涉及一种分战斗单元，该分战斗单元布置成例如在目标区域上与飞行体例如载体外壳等分离，该分战斗单元包括弹头，目标探测器和两个（1,2），其通过承载臂（7,8）分别枢转地设置在其自己的轴（4,5）上，所述轴（4,5）位于与战斗部的对称线垂直的平面上，所述平面与折叠其中载体臂和载体表面连接到分战斗单元的圆周表面的位置以及以90°打开的位置，在该位置两个载体表面形成用于次战斗单元的下降速度的减速区域并且在子战斗单元朝向目标区域坠落期间向副战斗单元施加用于以螺旋模式扫描目标区域的旋转。该次战斗单元包括机翼翻转机构，该机翼翻转机构具有设置在每个载体表面（1,2）上的橡胶缓冲装置（9,10），与该分战斗单元的外壳连接，该缓冲装置被压缩在翻转运动期间通过承载臂（7,8）以及返回止动件（11,12），承载臂可操作地抵靠止动件（11,12）弹回。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式