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1. 发明授权

EP3601939B1 IMPROVED BULLET 有权转让
公开(公告)号：EP3601939B1
公开(公告)日：2024-05-29
申请号：EP18777451.8
申请日：2018-03-29
IPC分类号： F42B30/02 , F42B10/00 , F42B10/38 , F42B33/00 , F42B5/10 , F42B10/40
CPC分类号： F42B10/38 , F42B10/40 , F42B30/02

2. 发明公开

EP3222962A1 NON LETHAL RIFLE GRENADE PROVIDED WITH A BOOSTER 审中-公开
标题翻译：非狂躁的GR GR提供了一个助推器
公开(公告)号：EP3222962A1
公开(公告)日：2017-09-27
申请号：EP17165107.8
申请日：2013-10-22
申请人： Rayner, William, V.S.
发明人： Rayner, William, V.S.
IPC分类号： F42B30/04 , F41C27/06 , F41A21/32 , F42B10/40 , F42B12/50 , F41G1/35 , F41H13/00
CPC分类号： F41A21/32 , F41C27/06 , F41G1/35 , F41H13/0031 , F42B10/40 , F42B12/50 , F42B30/04 , F42B30/06
摘要： A duplex weapon system that is capable of firing a high-mass/low-velocity ("HMLV") projectile followed by a conventional projectile such as a bullet. A barrel adapter is aligned with the bore of the barrel of a conventional firearm. The barrel adapter includes an adapter bore running completely through its length, with the adapter bore terminating in an exit in the forward portion of the barrel adapter. The HMLV projectile is slidably attached to the exterior of the barrel adapter. The HMLV projectile includes a launch tube that covers the exit of the barrel adapter. When a first cartridge is fired by the firearm, expanding propellant gas rushes down the adapter bore and out the exit. The expanding gas forces the launch tube and the attached HMLV projectile away from the barrel adapter. The HMLV projectile then flies toward a target.
摘要翻译：双能武器系统，能够发射高质量/低速（“HMLV”）弹丸，随后是常规弹丸，如子弹。枪管适配器与传统枪支枪管的孔对准。枪管适配器包括一个完全贯穿其长度的适配器孔，适配器孔终止于枪管适配器前部的出口。 HMLV射弹可滑动地连接到枪管适配器的外部。 HMLV射弹包括一个覆盖枪管适配器出口的发射管。当第一个墨盒被枪支发射时，膨胀的推进剂气体冲下适配器孔并从出口排出。膨胀的气体迫使发射管和连接的HMLV抛射体远离筒适配器。 HMLV弹丸然后飞向目标。

3. 发明公开

EP2242691A1 DISPOSITIF DE REDUCTION DE TRAINEE AERODYNAMIQUE 有权转让
标题翻译： VORRICHTUNG ZUM VERRINGERN DES AERODYNAMISCHEN WIDERSTANDES
公开(公告)号：EP2242691A1
公开(公告)日：2010-10-27
申请号：EP08853244.5
申请日：2008-11-21
申请人： Astrium SAS
发明人： RAYMOND, Gérald , BOURDIEU, Philippe
IPC分类号： B64G1/00 , B64G1/14
CPC分类号： B64G1/14 , B64D27/023 , B64D29/04 , B64G1/002 , F42B10/40 , F42B15/00 , Y02T50/44
摘要： The invention relates to a device for reducing the aerodynamic drag of a vehicle (1) provided with at least one engine (2) including a gas ejection nozzle (3) protruding from the rear of the vehicle fuselage (4) and flaring away from the rear of the vehicle fuselage, characterised in that it comprises at least one member (5) for masking at least a portion of the nozzle, made of a resorptive material (6) that can be eliminated in the nozzle flow once the engine is operating. The invention also relates to a spacecraft including the same.
摘要翻译：用于减少车辆的空气动力学阻力的装置包括用于车辆发动机的喷嘴的至少一部分的至少一个掩蔽元件，所述掩蔽元件具有可再吸收的材料，其被设计成在发动机点燃时在喷嘴的流动中被消除。航天飞船包括附在飞船机身上的喷嘴。

4. 发明公开

EP1320717A1 PENETRATOR ARROW PROJECTILE 审中-公开
公开(公告)号：EP1320717A1
公开(公告)日：2003-06-25
申请号：EP01972820.3
申请日：2001-09-28
申请人： Nammo Raufoss AS
发明人： FOSSUMSTUEN, Kai , ORBEKK, Erland
IPC分类号： F42B10/40
CPC分类号： F42B10/40
摘要： A penetrator arrow projectile for launching by use of a launcher projectile which comprises a propellant charge and which may be separated from the arrow projectile in the trajectory. A 'base-bleed' charge (2) is situated rearwardmost on the arrow projectile (1), in order to be ignited by means of an igniter device (3) in connection with the separation from the launcher projectile, which may comprise a forward igniter device for igniting the 'base-bleed' charge (2). The launcher projectile may also comprise a mechanism for retaining the arrow projectile (1) on the forward end and for releasing the arrow projectile in the trajectory.
摘要翻译：一种穿甲弹射弹，用于通过使用发射弹射弹发射，弹射弹包括推进剂弹药并且可以在弹道上与箭射弹分开。在箭头射弹（1）后面的最后端设有一个“漏斗”装药（2），以便借助于与发射器射弹分离有关的点火器装置（3）点燃，其可包括向前（2）点火装置。发射器射弹还可以包括用于将箭头射弹（1）保持在前端并且用于释放弹道中的箭射弹的机构。

5. 发明公开

EP1309831A1 GUIDED ARTILLERY MISSILE WITH EXTREMELY LONG RANGE 有权
标题翻译：导弹炮射程极长
公开(公告)号：EP1309831A1
公开(公告)日：2003-05-14
申请号：EP01938950.1
申请日：2001-06-13
申请人： Bofors Defence AB
发明人： HELLMAN, Ulf
IPC分类号： F42B10/38
CPC分类号： F42B10/14 , F42B10/40 , F42B15/105
摘要： The present invention relates to an artillery missile (1) intended for firing on a ballistic trajectory, with gliding characteristics which can be put into effect, after it has reached the summit of this trajectory, to increase the maximum range of the missile. In order to obtain these gliding characteristics, the missile is provided with extendable aerodynamic bearing surfaces divided into firstly canard fins (5-8), which are retracted in the front part of the missile body and can be extended after the summit of trajectory, secondly main bearing surfaces (9, 10) made of resilient material, which, likewise during launching, are curved in against and around the central part (3) of the missile body in shallow recesses adapted thereto in the outer casing of the missile and which, after the summit of trajectory and being extended, form the wings (9, 10) of the missile, and thirdly stern fins, which, durign at least launching, are covered i the retracted position by a protective cover (14) in the rear part (4) of the missile.
摘要翻译：本发明涉及一种炮弹导弹（1），用于在弹道上发射，具有滑行特性，在其达到该弹道的顶点之后可以起作用以增加导弹的最大射程。为了获得这些滑翔特性，导弹配备有可延伸的气动轴承表面，该表面被分成第一鸭鳍（5-8），它们缩回到弹体的前部并可在弹道顶点后延伸，其次由弹性材料制成的主轴承表面9,10同样在发射期间在导弹主体的中心部分3中与导弹主体的中心部分3在导弹的外壳中适配于其中的浅凹陷中弯曲，在弹道顶部并延伸之后，形成导弹的翼（9,10），并且第三尾翼至少在发射时通过后部的保护罩（14）覆盖在缩回位置（4）导弹。

6. 发明公开

EP0268566A2 Base bleed unit 失效
标题翻译：基础-Ausströmeinheit。
公开(公告)号：EP0268566A2
公开(公告)日：1988-05-25
申请号：EP87850268.1
申请日：1987-09-03
申请人： Andersson, Kurt Göran , Gunners, Nils-Erik , Nilsson, Yngve Lennart
发明人： Andersson, Kurt Göran , Gunners, Nils-Erik , Nilsson, Yngve Lennart
IPC分类号： F42B13/267
CPC分类号： F42B10/40
摘要： A base bleed unit arranged to increase the range of fire or to reduce the time of flight for shells and projectiles includes a housing (1) surrounding a fuel charge (6) and associated igniter (4), extending from the rear portion of a projectile body (2) and including at least one outlet nozzle (5, 5ʹ, 5ʺ) for combustion gases, which by means of a mass flow, and possibly combustion adjacent to the base plane, reduce existing base drag. According to an embodiment of the invention, the housing (1) comprises a caseshaped member 1 attachable against a projectile body (2), having at least one igniter (4) arranged adjacent to an internal plane of a restricting wall surface at the housing (1), located in an opposed relationship to the portion of the housing (1) attachable against a projectile body (2). The combustion flame of the igniter (4) is hereby maintained directed towards the fuel charge (6) and away from the outlet nozzle/nozzles (5, 5ʹ, 5ʺ). Advantageously, a number of outlet nozzles (5, 5ʹ, 5ʺ) are used, arranged spaced in an annular relationship to each other, and preferably inclined towards the outer peripheral portion of the restricting wall surface. A number of igniters (4) are advantageously used, located in recesses or blind holes taken up by the inside plane of the restricting wall surface. It is further advantageous to arrange the open portion of each igniter (4) partly covered by a covering means, thus accomplishing a reduced outlet area. According to a second embodiment, the housing (1) may also be formed by attachment of a bottom member to a projectile body (2) having a rearwardly open projectile extension, said bottom member including one or a number of igniters (4).
摘要翻译：布置成增加火焰范围或减少壳和射弹的飞行时间的基本放气单元包括围绕燃料喷射器（6）的围绕着喷射器的后部的相关联的点火器（4）的壳体（1）主体（2）并且包括用于燃烧气体的至少一个出口喷嘴（5,5'，5“），其通过质量流动和可能邻近基本平面的燃烧而减少现有的底部阻力。根据本发明的实施例，壳体（1）包括可抵靠射弹体（2）附接的壳体构件1，其具有邻近于壳体处的限制壁表面的内平面设置的至少一个点火器（4）位于与可抵靠射弹体（2）的壳体（1）的部分相对的关系中。因此，点火器（4）的燃烧火焰被保持指向燃料装料（6）并且远离出口喷嘴/喷嘴（5,5'，5“）。有利地，使用多个出口喷嘴（5,5'，5“），它们以彼此间隔开的环形关系布置，优选地朝向限制壁表面的外周部分倾斜。有利地使用多个点火器（4），位于由限制壁表面的内平面所牵引的凹陷或盲孔中。进一步有利的是将每个点火器（4）的开口部分部分地被覆盖装置覆盖，从而实现减小的出口面积。根据第二实施例，壳体（1）还可以通过将底部构件附接到具有向后开放的射出延伸部的射弹体（2）而形成，所述底部构件包括一个或多个点火器（4）。

7. 发明公开

EP3217138A1 NON LETHAL RIFLE GRENADE PROVIDED WITH A LASER SIGHT 审中-公开
标题翻译：提供激光瞄准器的非狂躁鞭炮
公开(公告)号：EP3217138A1
公开(公告)日：2017-09-13
申请号：EP17165099.7
申请日：2013-10-22
申请人： Rayner, William, V.S.
发明人： Rayner, William, V.S.
IPC分类号： F41A21/32 , F42B12/34 , F41C27/06 , F41G1/35 , F42B30/04 , F42B10/40 , F41H13/00 , F42B12/50
CPC分类号： F41A21/32 , F41C27/06 , F41G1/35 , F41H13/0031 , F42B10/40 , F42B12/50 , F42B30/04 , F42B30/06
摘要： A duplex weapon system that is capable of firing a high-mass/low-velocity ("HMLV") projectile followed by a conventional projectile such as a bullet. A barrel adapter is aligned with the bore of the barrel of a conventional firearm. The barrel adapter includes an adapter bore running completely through its length, with the adapter bore terminating in an exit in the forward portion of the barrel adapter. The HMLV projectile is slidably attached to the exterior of the barrel adapter. The HMLV projectile includes a launch tube that covers the exit of the barrel adapter. When a first cartridge is fired by the firearm, expanding propellant gas rushes down the adapter bore and out the exit. The expanding gas forces the launch tube and the attached HMLV projectile away from the barrel adapter. The HMLV projectile then flies toward a target.
摘要翻译：双能武器系统，能够发射高质量/低速（“HMLV”）弹丸，随后是常规弹丸，如子弹。枪管适配器与传统枪支枪管的孔对准。枪管适配器包括一个完全贯穿其长度的适配器孔，适配器孔终止于枪管适配器前部的出口。 HMLV射弹可滑动地连接到枪管适配器的外部。 HMLV射弹包括一个覆盖枪管适配器出口的发射管。当第一个墨盒被枪支发射时，膨胀的推进剂气体冲下适配器孔并从出口排出。膨胀的气体迫使发射管和连接的HMLV抛射体远离筒适配器。 HMLV弹丸然后飞向目标。

8. 发明授权

EP2242691B1 DISPOSITIF DE REDUCTION DE TRAINEE AERODYNAMIQUE 有权转让
标题翻译：装置以降低气动阻力
公开(公告)号：EP2242691B1
公开(公告)日：2017-03-01
申请号：EP08853244.5
申请日：2008-11-21
申请人： Airbus Defence and Space SAS
发明人： RAYMOND, Gérald , BOURDIEU, Philippe
IPC分类号： B64D27/02 , B64D29/04 , B64G1/14 , B64G1/00 , F42B10/40 , F42B15/00
CPC分类号： B64G1/14 , B64D27/023 , B64D29/04 , B64G1/002 , F42B10/40 , F42B15/00 , Y02T50/44

9. 发明公开

EP2909565A4 DUPLEX WEAPON SYSTEM 审中-公开
标题翻译：双面武器系统
公开(公告)号：EP2909565A4
公开(公告)日：2016-10-12
申请号：EP13873483
申请日：2013-10-22
申请人： RAYNER WILLIAM V S
发明人： RAYNER WILLIAM V S
IPC分类号： F41A21/32 , F41C27/06 , F41G1/00 , F41H13/00 , F42B12/34 , F42B12/36 , F42B12/46 , F42B12/50
CPC分类号： F41A21/32 , F41C27/06 , F41G1/35 , F41H13/0031 , F42B10/40 , F42B12/50 , F42B30/04 , F42B30/06
摘要： A duplex weapon system that is capable of firing a high-mass/low-velocity ("HMLV") projectile followed by a conventional projectile such as a bullet. A barrel adapter is aligned with the bore of the barrel of a conventional firearm. The barrel adapter includes an adapter bore running completely through its length, with the adapter bore terminating in an exit in the forward portion of the barrel adapter. The HMLV projectile is slidably attached to the exterior of the barrel adapter. The HMLV projectile includes a launch tube that covers the exit of the barrel adapter. When a first cartridge is fired by the firearm, expanding propellant gas rushes down the adapter bore and out the exit. The expanding gas forces the launch tube and the attached HMLV projectile away from the barrel adapter. The HMLV projectile then flies toward a target.

10. 发明公开

EP3004790A1 DRAG REDUCTION SYSTEM 审中-公开
标题翻译： WIDERSTANDSVERMINDERUNGSSYSTEM
公开(公告)号：EP3004790A1
公开(公告)日：2016-04-13
申请号：EP14728257.8
申请日：2014-05-30
申请人： BAE SYSTEMS plc
发明人： FLYNN, Dennis Joseph , LOCKING, Paul Martin , JOHNSON, Martin
IPC分类号： F42B10/40 , F42B10/66
CPC分类号： F42B10/40 , F42B10/66 , F42B10/666 , F42B10/668
摘要： The invention relates to a drag reduction system, more specifically a forward mounted drag reduction system for use on extended range artillery. There is provided a long range artillery projectile having forward end comprising a fuze, an aft located base unit and located therebetween a projectile body defining cavity which comprises a payload, a forwardly located gas generator capable of generating a gas flow, and an ignition device to ignite the gas generator; preferably at a predetermined time after the projectile is launched.
摘要翻译：减阻系统技术领域本发明涉及一种减阻系统，更具体地说涉及一种用于扩展射程火炮的前挂式减阻系统。提供了一种远距离炮弹，其前端包括一个引信，一个位于后部的基座单元，并位于此之间，具有一个定位腔体的射弹体，其包括有效载荷，一个能够产生气流的向前定位的气体发生器，以及点火装置点燃气体发生器; 优选在发射弹丸之后的预定时间。

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