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1. 发明公开

EP4394307A3 WEAPON TARGETING TRAINING SYSTEM AND METHOD THEREFOR 审中-实审
公开(公告)号：EP4394307A3
公开(公告)日：2024-09-18
申请号：EP24170846.0
申请日：2020-02-17
申请人： Sinab Technologies Pty Ltd
发明人： LANDERS, Anthony James
IPC分类号： F41J5/00 , F41A33/00 , F41G3/26 , B64D1/02 , B64D7/00 , B64D1/04 , B64D10/00 , B64D43/00 , F41G3/22 , F41G7/00 , F41G7/22
CPC分类号： B64D1/02 , B64D7/00 , F41G3/225 , F41G7/006 , F41G7/226 , F41G7/2293 , F41G7/2253 , B64D1/04 , B64D10/00 , B64D43/00
摘要： The present invention relates to a training system for training of a forward controller. The training system utilises a pod housing that can be attached to a hardpoint under an aircraft wing. The pod is configured to receive communications from the forward controller on the ground (or in another aircraft) and communicate wirelessly with an HMD and/or electronic device in the cockpit of the aircraft. This allows cheaper, less expensive aircraft to be used for training purposes.

2. 发明公开

EP4361223A1 COATING MATERIAL FOR A SURFACE OF AN AIRCRAFT WITH LIGHTNING PROTECTION 审中-公开
公开(公告)号：EP4361223A1
公开(公告)日：2024-05-01
申请号：EP23206435.2
申请日：2023-10-27
申请人： Airbus Defence and Space GmbH
发明人： DITTRICH, Kay Werner , KARCH, Christian , BLECKMANN, Matthias , SCHUSTER, Thomas
IPC分类号： C09D5/30 , C09D5/32 , C09D7/40 , C09D7/61 , B64D7/00 , B64D45/02
CPC分类号： C09D7/61 , C09D7/70 , C09D5/30 , C09D5/32 , B64D7/00 , B64D45/02 , C08K7/02 , C08K3/10
摘要： A coating material for a surface of an aircraft is proposed, having a polymer- or rubber-based dielectric matrix material, and first flakes of a metallic and/or soft-magnetic, electrically conductive material that are embedded into the matrix material, wherein the first flakes are geometrically two-dimensional and have a ratio of thickness to average diameter of 1:3 or less, and wherein the first flakes are separated from one another in the matrix material and/or have an electrically non-conductive coating.

3. 发明公开

EP3310657A1 AIRCRAFT STORES TRANSPORT SYSTEM 有权
标题翻译：飞机商店运输系统
公开(公告)号：EP3310657A1
公开(公告)日：2018-04-25
申请号：EP16741374.9
申请日：2016-06-21
申请人： BAE Systems PLC
发明人： WHITE, Andrew, Charles
IPC分类号： B64D1/10 , B64D7/00 , F41H3/00
CPC分类号： B64D1/10 , B64D7/00 , F41H3/00 , H01Q17/008
摘要： A system comprising: a low observable aircraft (2) having its external surfaces oriented at a limited number of directions; a device (12) mounted to the aircraft (2) outside the external surfaces of the aircraft (2); and a fairing (10) located outside the external surfaces of the aircraft (2), the fairing (10) being releasably coupled to the one or more external surfaces of the aircraft (2), at least part of the fairing (10) being spaced apart from one or more of the external surfaces of the aircraft (2) so as to define a chamber between the fairing (10) and that one or more external surfaces of the aircraft (2). The device (12) is wholly located within the chamber. One or more external surfaces of the fairing (10) are oriented in the same direction as at least one external surface of the aircraft (2).

4. 发明授权

EP2780659B1 PROTECTIVE MATERIAL ARRANGEMENT 有权转让
标题翻译：防护材料安排
公开(公告)号：EP2780659B1
公开(公告)日：2018-01-03
申请号：EP12787840.3
申请日：2012-11-06
申请人： BAE Systems PLC
发明人： DUNLEAVY, Michael , HAQ, Sajad , MORLEY, Caroline, Joleen
IPC分类号： F41H7/00 , F41H1/02 , F41H5/04
CPC分类号： B29C70/021 , B64D7/00 , F41H1/02 , F41H5/0478 , F41H5/0485 , F41H7/00
摘要： According to the invention there is provided an arrangement of protective material for dissipating the kinetic energy of a moving object including one or more layers of fibrous armour material encased within a sealed encasement, in which the sealed encasement is formed from a textile armour material which is impregnated with a polymeric substance.

5. 发明授权

EP3025960B1 ARRANGEMENT AND METHOD FOR LAUNCHING COUNTER-MEASURES 有权
标题翻译：安排和发射反措施的方法
公开(公告)号：EP3025960B1
公开(公告)日：2017-11-15
申请号：EP15158853.0
申请日：2008-05-30
申请人： SAAB AB
发明人： Zachrisson, Björn
IPC分类号： B64D1/02 , F42B5/15 , F41F7/00 , F42B5/145 , B64D7/00
CPC分类号： B64D7/00 , F41F7/00 , F42B5/15
摘要： The invention relates to a method for launching counter-measures (5), such as flares and chaff, from a launch opening (14) of a dispenser (2) mounted on an aeroplane (1). The counter-measures (5) are launched in a direction obliquely forwards and downwards relative to the aeroplane, and in order to facilitate launching of counter-measures (5), a low dynamic pressure is created permanently across the launch opening (14) of the dispenser (2) by means of fixed means (24) acting on the air stream. The invention also relates to an arrangement for storing and launching counter-measures (5), such as flares and chaff, comprising an elongate body (8) provided with at least one launch opening (14) used for storing the counter-measures (5) in compartments (11.1,1 1.2,...,11-n), the arrangement being designed to be mounted on an aeroplane (1), with the longitudinal direction of the elongate body (8) essentially coinciding with the flight direction of the aeroplane (1), and the counter-measures (5) being connected to a firing control unit for feeding firing signals to the counter-measures. The arrangement is designed to be mounted under the aeroplane (1), and in that the compartments (11.1,11.2,...,11-n) are provided with openings (18.1,18.2,...,18.n) and are intended for launching the counter-measures (5) in a direction obliquely forwards and downwards relative to the aeroplane (1).

6. 发明授权

EP2969769B1 LIGHTNING PROTECTION FOR VEHICLES 有权
标题翻译：车辆防雷保护
公开(公告)号：EP2969769B1
公开(公告)日：2017-10-11
申请号：EP14711570.3
申请日：2014-03-13
申请人： BAE Systems PLC
发明人： JONES, Christopher, Charles, Rawlinson
IPC分类号： B64D45/02
CPC分类号： B64D45/02 , B64D7/00 , H05F3/04
摘要： A vehicle (2) comprising a vehicle part (4), the vehicle part (4) comprising: an electrically conductive core (6); a non-electrically conductive outer skin (8) made of a radar-absorbent material which surrounds, at least to some extent, the core (6) such that the core (6) is not visible from outside the vehicle (2); and one or more electrically conductive members (10) electrically connected to the core (6); each of the one or more members (10) is a tapered member having a relatively large cross sectional area where that member (10) is electrically connected to the core (6), and tapers from its end that is connected to the core (6) to a point; and the point of each member (10) is located at an outer surface of the external skin (8) such that the point of each of the members (10) is exposed.

7. 发明公开

EP3190378A1 MULTIFUNKTIONALE PRÜFVORRICHTUNG FÜR EINE BEWAFFNUNG 有权
标题翻译：多功能测试装置的武器
公开(公告)号：EP3190378A1
公开(公告)日：2017-07-12
申请号：EP17150302.2
申请日：2017-01-04
申请人： MBDA Deutschland GmbH
发明人： Grabmeier, Michael , Baier, Siegfried , Böhm, Alfred
IPC分类号： F42B35/00 , B64F5/60
CPC分类号： F42B35/00 , B64D7/00 , B64F5/60
摘要： Eine multifunktionale Prüfvorrichtung für eine Bewaffnung eines eine Waffenanlage (60) aufweisenden Bewaffnungsträgers (6), wobei die Bewaffnung zumindest eine am Bewaffnungsträger (6) anbringbare Waffenträgereinrichtung (7) für zumindest einen Flugkörper (80, 82, 84, 86) aufweist, zeichnet sich dadurch aus, dass die Prüfvorrichtung (1) versehen ist mit einer ersten Stimulations- und Prüfkomponente (2) für die Waffenanlage (60) des Bewaffnungsträgers (6), wobei die erste Stimulations- und Prüfkomponente (2) eine erste Prüfschnittstelle (20) aufweist, die mit einer Waffenanlagenschnittstelle 62() des Bewaffnungsträgers (6) verbindbar ist; einer zweiten Stimulations- und Prüfkomponente (3) für die Waffenträgereinrichtung (7), wobei die zweite Stimulations- und Prüfkomponente (3) eine zweite Prüfschnittstelle (30) aufweist, die mit einer Bewaffnungsträgerschnittstelle (70) der Waffenträgereinrichtung (7) verbindbar ist; einer dritten Stimulations- und Prüfkomponente (4) für die Waffenträgereinrichtung (7), wobei die dritte Stimulations- und Prüfkomponente (4) zumindest eine dritte Prüfschnittstelle (40, 42) aufweist, die mit einer Flugkörperschnittstelle (72) der Waffenträgereinrichtung (7) verbindbar ist, und einer vierten Stimulations- und Prüfkomponente (5) für den zumindest einen Flugkörper (80, 82, 84, 86), wobei die vierte Stimulations- und Prüfkomponente (5) zumindest eine vierte Prüfschnittstelle (50) aufweist, die mit einer Waffenträgerschnittstelle des zumindest einen Flugkörpers (80, 82, 84, 86) verbindbar ist.
摘要翻译：用于装备一种武器系统（60），其具有装备支承件（6），其中，所述武装对装备支撑的至少一个（6）附接武器载体装置（7）用于至少一个导弹（80，82，84，86），其特征在于一种多功能测试装置其特征在于，所述测试设备（1）设置有一个第一刺激和试验组分（2）的装备支承件（6），其中所述第一刺激和测试部件（2）包括第一测试接口的武器系统（60）（20）可连接到武器载体（6）的武器设备接口62（10）; 对于武器支撑装置的第二起搏和检查组件（3）（7），其中，所述第二起搏和检查组件（3）具有第二测试接口（30）与所述武器的载体装置（7）是可连接的装备车辆接口（70）; 第三刺激和检查组件（4），用于武器支撑装置（7），其中，所述第三刺激和检查组件（4）的至少一个第三测试接口（40，42），其与所述武器托架装置的一个导弹接口（72）（7）连接和第四刺激和检查组件（5），用于所述至少一个导弹（80，82，84，86），其中所述第四刺激和检查组件（5）包括至少一个第四测试接口（50）使用武器载体接口该至少一个导弹（80,82,84,86）是可连接的。

8. 发明授权

EP2382126B1 DISPENSER UNIT FOR COUNTERMEASURES 有权
标题翻译：分配器单元的对策
公开(公告)号：EP2382126B1
公开(公告)日：2017-05-17
申请号：EP09838488.6
申请日：2009-01-16
申请人： Saab AB
发明人： MELIN, Robert , ZACHRISSON, Björn , SJÖBECK, Benny
IPC分类号： B64D1/02 , F41H11/02 , B64D7/00 , F42B4/26 , F42B5/15 , F41F5/00 , F41F7/00
CPC分类号： B64D1/02 , B64D7/00 , F41F5/00 , F41F7/00 , F42B4/26 , F42B5/15

9. 发明授权

EP2676099B1 EQUIPMENT FOR THE REDUCTION OF THE RADAR MARKING FOR AIRCRAFTS 有权转让
标题翻译：减少飞机雷达标记的设备
公开(公告)号：EP2676099B1
公开(公告)日：2017-04-26
申请号：EP12711220.9
申请日：2012-02-13
申请人： LEONARDO S.P.A.
发明人： MERLO, Emanuele , BRENNA, Fabio
IPC分类号： F41H3/00 , B64D7/00
CPC分类号： H01Q17/00 , B63G8/34 , B64D7/00 , F28F27/00 , F41H3/00 , F41J2/00 , F41J2/02

10. 发明授权

EP2421754B1 Dispenser Unit with closable counter-measure compartments 有权
标题翻译：点火单元可锁定对策室
公开(公告)号：EP2421754B1
公开(公告)日：2016-10-19
申请号：EP09843741.1
申请日：2009-04-23
申请人： Saab AB
发明人： ZÄTTERQVIST, Christer
IPC分类号： B64D1/02 , F41H11/02 , F41J2/02 , F42B12/70 , F41F3/065 , B64D7/00
CPC分类号： B64D7/00 , F41F3/065 , F41J2/02 , F42B12/70

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