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11. 发明授权

EP1167915B1 Optronische Zündeinrichtung für einen Flugkörper 有权
标题翻译：对于导弹光电点火装置
公开(公告)号：EP1167915B1
公开(公告)日：2008-02-13
申请号：EP01115256.8
申请日：2001-06-23
申请人： Diehl BGT Defence GmbH & Co.KG
发明人： Ganghofer, Andreas
IPC分类号： F42C19/02
CPC分类号： F42C13/02 , F42B30/006 , F42C19/02

12. 发明公开

EP1167915A3 Optronische Zündeinrichtung für einen Flugkörper 有权
标题翻译：对于导弹光电点火装置
公开(公告)号：EP1167915A3
公开(公告)日：2003-12-03
申请号：EP01115256.8
申请日：2001-06-23
申请人： Diehl Munitionssysteme GmbH & Co. KG
发明人： Ganghofer, Andreas
IPC分类号： F42C19/02
CPC分类号： F42C13/02 , F42B30/006 , F42C19/02
摘要： Es wird eine optronische Zündeinrichtung (10) für einen Flugkörper wie eine Drohne, eine Rakete oder ein Flugzeug beschrieben, mit einem für seine Optikeinrichtung (12) vorgesehenen Sensorfenster (14), dem eine Luftablenkeinrichtung (16) zugeordnet ist, um die Luftströmung des fliegenden Flugkörpers vom Sensorfenster (14) fernzuhalten und am Sensorfenster (14) vorbeizulenken und auf diese Weise ein Verschmutzen und/oder Vereisen des Sensorfensters während der Mission des Flugkörpers zu verhindern.

13. 发明公开

EP0538215A1 A flip-out mechanism for target trackers 失效
标题翻译： AusklappmechanismusfürZielsuchgeräte。
公开(公告)号：EP0538215A1
公开(公告)日：1993-04-21
申请号：EP92850203.8
申请日：1992-08-27
申请人： Bofors AB
发明人： Vesa, Reijo
IPC分类号： F42B10/50 , F42B12/58
CPC分类号： F42B30/006
摘要： The present invention relates to a flip-out mechanism for target trackers (5) for sub-combat units (1) of the type intended to be transported by a carrier body to a target area where it is dropped for scanning the area under braked fall with its target tracker (5) and for combatting targets possibly identified there. The problem solved by the present invention is that of retarding, in a gentle and efficient manner, the flip-out of the target tracker (5) and thereafter of locking it in the flipped-out position.
摘要翻译：本发明涉及一种用于目标跟踪器（5）的翻转机构，该目标跟踪器（5）用于将由承载体运送到其下落的目标区域的类型的副作战装置（1），用于扫描制动坠落的区域其目标跟踪器（5）和用于对准可能在那里识别的目标。通过本发明解决的问题是以平缓和有效的方式延迟目标跟踪器（5）的翻转，然后将其锁定在翻转位置。

14. 发明公开

EP0424336A2 Subwarhead 失效
标题翻译： Subgefechtskopf。
公开(公告)号：EP0424336A2
公开(公告)日：1991-04-24
申请号：EP90850324.6
申请日：1990-10-03
申请人： Aktiebolaget Bofors
发明人： Axinger, Jan
IPC分类号： F42B10/50 , F42B12/04 , F42B12/58
CPC分类号： F42B30/006 , F42B10/50
摘要： The invention relates to a subwarhead which is arranged to be separated from a missile, for example a carrier shell or the like, over a target area. The subwarhead comprises an active part, a target detector (2) and an aerofoil (3), both the target detector (2) and the aerofoil (3) each being pivotably arranged on its own bearing shaft (4, 5) parallel with the line of symmetry of the active part in order to allow pivoting out of target detector (2) and aerofoil (3) from a folded-in position to a folded-out position at the side of the active part in order to allow a controlled movement of scanning of the target area. The target detector (2) and/or the aerofoil (3) are/is provided with one or more displaceably arranged extra aerofoils (7, 8, 9, 10, 13, 14) for the purpose of increasing the braking area of the subwarhead.
摘要翻译：本发明涉及一种子导弹，其被布置成在目标区域上与导弹（例如载体壳体等）分离。副标题包括活动部分，目标检测器（2）和机翼（3），目标检测器（2）和机翼（3）均可枢转地布置在其自身的轴承轴（4,5）上，平行于有源部分的对称线，以便允许从目标检测器（2）和机翼（3）从折叠位置枢转到活动部分侧面的折叠位置，以允许受控的移动扫描目标区域。目标检测器（2）和/或机翼（3）设置有一个或多个可置换排列的额外机翼（7,8,9,10,13,14），以增加副驾驶的制动面积。

15. 发明公开

EP0252036A3 Homing submunition 失效
标题翻译：喜欢的SUBMUNITION
公开(公告)号：EP0252036A3
公开(公告)日：1988-02-17
申请号：EP87850087
申请日：1987-03-17
申请人： Aktiebolaget Bofors
发明人： Persson, Per-Olof , Albrektsson, Kjell , Axinger, Jan , Fixell, Jan-Olof , Hyvärinen, Jari
IPC分类号： F42B13/50 , F41G07/22
CPC分类号： F42B30/006 , F42B10/50 , F42C13/006
摘要： The disclosure relates to a submunition disposed to be separated from an aeronautical body, for example a shell carrier canister or the like above a target area, the submunition essentially including a warhead (5), a target detector (6) and a device which imparts to the submunition rotation for scanning the target area in a helical pattern (4) during the fall of the submunition towards the target area. The target detector (6) is pivotally disposed on a carrying shaft (12a) parallel to the line of symmetry (5a) of the warhead in order to permit outward activation of the target detector (6) from a collapsed position where the optical axis of the target detector coincides with the line of symmetry (5a) of the warhead to an activated position where the optical axis of the target detector is parallel with the line of symmetry (5a) of the warhead, so as to permit free scanning vision for the target detector (6) beside the warhead (5).

16. 发明授权

EP0131744B1 Abwerfbarer Geschosskopf mit Annäherungszünder 失效
标题翻译：可靠的战争头与邻近的FUZE
公开(公告)号：EP0131744B1
公开(公告)日：1987-01-21
申请号：EP84106598.0
申请日：1984-06-08
申请人： Rheinmetall GmbH
发明人： Vavra, Norbert , Seidensticker, Jens, Dr.
IPC分类号： F42C19/06 , F42C13/00 , F42B13/04 , H01Q1/28
CPC分类号： F42B12/10 , F42B10/56 , F42B30/006 , F42C13/006 , F42C19/06

17. 发明公开

EP2852816A1 AUTONOMOUS MEASUREMENT OF THE INITIAL VELOCITY OF AN OBJECT THAT CAN BE FIRED 审中-公开
标题翻译：独立的测量点的最高时速被解雇
公开(公告)号：EP2852816A1
公开(公告)日：2015-04-01
申请号：EP13793422.0
申请日：2013-05-15
申请人： BAE Systems Bofors AB
发明人： FOHRMAN, Erik , HOLM, Tony
IPC分类号： G01C21/10 , F41G7/36 , F42B15/01 , G01P15/12
CPC分类号： G01P3/665 , F41A21/32 , F41G3/12 , F42B30/006 , G01P3/44 , G01P7/00 , G01P15/0888 , G01P15/12
摘要： The invention concerns a process for measuring the initial velocity V
0 of an object that can be fired such as a shell or projectile that exits a barrel, said measurement being based on measurement of the force exerted on a sensor device (100) configured inside the object that can be fired, characterized in that the force is measured autonomously inside the object by detection of changes in shape of the sensor device (100) during movement of said object inside the barrel prior to its exit. The invention also concerns a device for measuring the initial velocity V
0 of an object that can be fired such as a shell or projectile that exits the barrel of a firing device such as an artillery piece, comprising a force-detecting sensor device (100) configured inside the object that can be fired, characterized in that the force-detecting sensor device (100) is configured so as to detect changes in shape of said sensor device (100) during movement of said object inside the barrel prior to its exit, and in that an included signal-processing unit calculates and determines the initial velocity V
0 based on the detected changes in shape. The invention also concerns a device and process for measuring the acceleration forces acting on an object that can be fired during movement of said object inside the barrel prior to its exit.

18. 发明公开

EP2735838A1 Munition d'artillerie à structure coulissante 审中-公开
标题翻译： Artilleriemunition mit Schiebestruktur
公开(公告)号：EP2735838A1
公开(公告)日：2014-05-28
申请号：EP13194106.4
申请日：2013-11-22
申请人： TDA ARMEMENTS S.A.S.
发明人： Cohe, Patrick , Dubois, Bertrand , Moreau, Fabien
IPC分类号： F42B12/22 , F42B12/10 , F42B30/00 , F42B12/62
CPC分类号： F42B12/625 , F42B12/10 , F42B12/22 , F42B30/006
摘要： L'invention porte sur une munition d'artillerie comprenant un axe longitudinal, une partie avant (2) et une partie arrière (3), caractérisée en ce qu'elle comprend une structure coulissante comprenant d'une part une enveloppe structurale (5) fixée à la partie avant (2), et d'autre part un corps (6) fixé à la partie arrière (3) et comprenant un objet fonctionnel;
et en ce que le corps (6) peut coulisser dans l'enveloppe structurale (5) selon l'axe longitudinal (X) entre eux positions :
- une position repliée adaptée au tir de la munition, l'enveloppe structurale (5) étant placée en butée contre la partie arrière (3) de la munition ; l'objet fonctionnel du corps (6) étant protégé à l'intérieur de l'enveloppe structurale (5),
- une position déployée adaptée au fonctionnement de l'objet après le tir de la munition, l'objet fonctionnel étant découvert, entre l'enveloppe structurale (5) et la partie arrière (3) de la munition, par coulissement du corps (6) au moins partiellement hors de l'enveloppe structurale (5).
摘要翻译：该弹药具有包括固定在前部（2）上的结构壳体（5）和安装在后部（3）上的主体6的滑动结构。身体可以在结构外壳之间滑动，用于弹药的射击的缩回位置，以及在弹药射击之后功能对象即弹头的操作的延伸位置。滑动结构包括在壳体和主体之间的机械止动单元（15），用于在弹药射击期间支撑由前部在壳体上施加的纵向和角度的机械约束。

19. 发明公开

EP2433479A2 LOW COST, HIGH STRENGTH ELECTRONICS MODULE FOR AIRBORNE OBJECT 有权
标题翻译：低成本高强度电子模块飞行物体
公开(公告)号：EP2433479A2
公开(公告)日：2012-03-28
申请号：EP10784886.3
申请日：2010-05-11
申请人： Raytheon Company
发明人： GESWENDER, Chris, E.
IPC分类号： H05K7/14
CPC分类号： H05K1/144 , F42B15/08 , F42B30/006 , F42C19/06 , H05K7/1434 , H05K2201/09027 , H05K2201/10378 , H05K2201/2018
摘要： An electronics module is provided for utilization onboard an airborne object. In one embodiment, the electronics module includes a housing having a cavity therein, a first printed circuit board (PCB) disposed in the cavity, a second PCB disposed in the cavity above the first PCB, and a supportive interconnect structure. The supportive interconnect structure includes a substantially annular insulative body and a plurality of vias. The substantially annular insulative body extends around an inner circumferential portion of the housing between the first PCB and the second PCB to support the second PCB and to axially space the second PCB from the first PCB. The plurality of vias is formed through the substantially annular insulative body and electrically couples the first PCB to the second PCB.

20. 发明公开

EP1922665A2 METHOD AND APPARATUS FOR IMPACT DETECTION AND PRIORITIZATION OF IMPACT INFORMATION TRANSMITTED TO A RECEIVING STATION 有权
标题翻译：方法和装置碰撞检测和优先次序，以一台发送的影响的信息
公开(公告)号：EP1922665A2
公开(公告)日：2008-05-21
申请号：EP06851401.7
申请日：2006-06-09
申请人： ITT Manufacturing Enterprises, Inc.
发明人： PADEREWSKI, Gary , LESAGE, John
IPC分类号： G06F19/00
CPC分类号： F42B12/365 , F42B30/006
摘要： An impact detection system according to the present invention includes an impact sensor, damage sensors and an electronics package. The impact sensor includes a fiber optic grid preferably attached to a target object to detect impact locations on the target. The damage sensors measure damage sustained by the object, while the electronics package monitors the fiber optic grid, records the impact location and sends information pertaining to the impact location and target damage through a telemetry link with limited bandwidth to a receiving station. In order to ensure transmission of desired information, the electronics package allocates telemetry bandwidth to sensor information most relevant to impact location and target damage to enable transmission in the limited time interval available prior to target destruction or impact detection system disablement. This is accomplished by dynamically allocating reporting priority to different sensors during an impact.

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