CHARGE CREUSE ET APPLICATION POUR LA SEPARATION DE DEUX ETAGES D'UN ENGIN AERONAUTIQUE OU SA NEUTRALISATION
    5.
    发明公开
    CHARGE CREUSE ET APPLICATION POUR LA SEPARATION DE DEUX ETAGES D'UN ENGIN AERONAUTIQUE OU SA NEUTRALISATION 审中-公开
    空心装药和使用分离两个航天飞行器的水平或为中和它

    公开(公告)号:EP3102906A1

    公开(公告)日:2016-12-14

    申请号:EP15704735.8

    申请日:2015-02-03

    摘要: The invention relates to a hollow charge which includes: a confinement casing (1); an explosive charge (2) placed in the confinement casing (1) and having a V-shaped surface (2A); a detonator (3) placed behind the explosive charge (2); and a spraying material layer (4) placed in front of the V-shaped surface (2A) of the explosive charge (2). A pyrogenic material layer (10) is used to heat the spray coating (4). Said pyrogenic material can also be mixed with the explosive charge (2). The invention is useful for separating two floors of an aeronautical vehicle or for neutralizing the latter.

    摘要翻译: 甲聚能射孔弹,其包括包壳,以爆炸的炸药在安全壳放置并具有V形表面,放在后面炸药的熔丝,和投射材料的层中的炸药的V形表面的前面放置 收费。 热解材料的层用于加热所述投影涂层。 这种热原材料因此可以与炸药混合。

    AUS EINEM DRALLSTABILISIERTEN TRÄGERGESCHOSS AUSSTOSSBARE SUBMUNITION, INSBESONDERE LEUCHTMUNITION
    7.
    发明公开
    AUS EINEM DRALLSTABILISIERTEN TRÄGERGESCHOSS AUSSTOSSBARE SUBMUNITION, INSBESONDERE LEUCHTMUNITION 有权
    澳大利亚金融监督管理局(TRAGERGESCHOSS)澳大利亚证券监督管理委员会(INSBESONDERE LEUCHEMUNITION)

    公开(公告)号:EP3017271A1

    公开(公告)日:2016-05-11

    申请号:EP14730896.9

    申请日:2014-06-17

    发明人: GUTH, Sven

    IPC分类号: F42B15/36 F42B12/62 F42B4/28

    摘要: The invention relates to a submunition (1), in particular luminous munition, that can be discharged from a spin-stabilized carrier projectile and has a submunition body (2) and a parachute housing (3) arranged on the rear side of the submunition body (2) with a main parachute located therein. To achieve the effect that the main parachute is activated when there is a predeterminable spin of the submunition (1), the invention proposes connecting the submunition body (2) and the parachute housing (3) releasably to one another by way of a centrifugal coupling (4) in such a way that the submunition body (2) and the parachute housing (3) are non-positively and/or positively connected to one another by the centrifugal coupling (4) as a result of the centrifugal force occurring when the carrier projectile is fired, and in such a way that the centrifugal coupling (4) releases the connection between the submunition body (2) and the parachute housing (3) after the centrifugal force has subsided to a predeterminable value.

    摘要翻译: 本发明涉及一种子弹药(1),特别是发射弹药,其可以从旋转稳定的载体射弹排出,并具有子弹体(2)和设置在子弹体背面的降落伞壳体(3) (2)位于其中的主降落伞。 为了实现当子弹药(1)存在可预定的旋转时主降落伞被激活的效果,本发明提出通过离心联轴器将子弹药体(2)和降落伞壳体(3)可释放地彼此连接 (4),使得子弹药体(2)和降落伞壳体(3)通过离心联轴器(4)彼此不正和/或正相关,这是由于当离心力联轴器 在离心力已经下降到可预定的值之后,离心联轴器(4)以离散联接器(4)释放子弹药体(2)和降落伞壳体(3)之间的连接的方式被发射。

    MISSILE POURVU D'UNE COIFFE DE PROTECTION SÉPARABLE
    8.
    发明公开
    MISSILE POURVU D'UNE COIFFE DE PROTECTION SÉPARABLE 有权
    IS配备可分对CAP导弹

    公开(公告)号:EP2960618A1

    公开(公告)日:2015-12-30

    申请号:EP15290152.6

    申请日:2015-06-10

    申请人: MBDA France

    IPC分类号: F42B10/46 F42B15/36

    CPC分类号: F42B10/46 F42B15/36

    摘要: - Le missile (1) comprend au moins un étage propulsif (5) séparable et un véhicule terminal (6) qui est agencé à l'avant de l'étage propulsif (5) séparable, ledit missile (1) étant pourvu à l'avant d'une coiffe de protection (2) séparable comprenant au moins deux coques individuelles (3, 4), et d'une pièce de liaison (10A) liée au missile (1), vers l'arrière au-delà de la position (P1) de l'extrémité arrière (11) du véhicule terminal (6), ladite coiffe de protection (2) étant configurée pour, lorsqu'elle est montée sur le missile (1), entourer tout ledit véhicule terminal (6) et étant liée par une extrémité arrière à la pièce de liaison (10A) par l'intermédiaire d'éléments de liaison articulés (7).

    DISTRIBUTED ORDNANCE SYSTEM, MULTIPLE STAGE ORDNANCE SYSTEM, AND RELATED METHODS
    9.
    发明公开
    DISTRIBUTED ORDNANCE SYSTEM, MULTIPLE STAGE ORDNANCE SYSTEM, AND RELATED METHODS 有权
    VERTEILTES MUNITIONSSYSTEM,MEHRSTUFIGES MUNITIONSSYSTEM UNDZUGEHÖRIGEVERFAHREN

    公开(公告)号:EP2893289A2

    公开(公告)日:2015-07-15

    申请号:EP13840177.3

    申请日:2013-09-10

    IPC分类号: F42B15/01 F42B15/12 F42B15/36

    摘要: A distributed ordnance system comprises a plurality of ordnance controllers and a plurality of firing units. Each ordnance controller of the plurality of ordnance controllers may be operably coupled with at least one firing unit of the plurality of firing units. Each ordnance controller may be configured to provide power signals to the at least one firing unit coupled therewith, and communicate with the at least one firing unit for initiation of an ordnance event. A multiple stage ordnance system may comprise a first stage and a second stage that each include an ordnance controller configured to control operation of an ordnance event, and at least one firing unit to initiate the ordnance event. Related methods for constructing a multiple stage ordnance control system and controlling initiation of an energetic material are also disclosed.

    摘要翻译: 分布式弹药系统包括多个弹药控制器和多个发射单元。 多个弹药控制器的每个弹药控制器可以与多个击发单元中的至少一个击发单元可操作地联接。 每个弹药控制器可以被配置为向与其耦合的至少一个击发单元提供功率信号,并且与至少一个击发单元通信以启动弹药事件。 多级武器系统可以包括第一级和第二级,每级包括被配置为控制弹药事件的操作的弹药控制器,以及至少一个起动单元以启动弹药事件。 还公开了用于构建多级弹道控制系统和控制高能材料的启动的相关方法。