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    DRONE-BASED ACTIVE PROTECTION SYSTEM
    191.
    发明公开
    DRONE-BASED ACTIVE PROTECTION SYSTEM 审中-公开

    公开(公告)号：EP3410057A1

    公开(公告)日：2018-12-05

    申请号：EP18174698.3

    申请日：2018-05-29

    Applicant: Plasan Sasa Ltd.

    Inventor： YESHURUN, Yehoshua

    IPC: F41H11/00

    CPC classification number: G05D1/0094 ,  B64C39/024 ,  B64C2201/121 ,  B64C2201/141 ,  F41H11/00 ,  F41H13/005 ,  F41H13/0093 ,  F42B12/70 ,  G01S5/0072 ,  G01S7/38 ,  G05D1/0088 ,  G05D1/12

    Abstract: According to one aspect of the presently disclosed subject matter, there is provided a system for facilitating active protection of a target from a threat, the system comprising:
    • one or more platforms configured for directing operation of the system; and
    • one or more unmanned aerial vehicles (UAV's) configured to operate in the
    vicinity of the target, and to facilitate detection and/or neutralizing of the threat, wherein the platform is configured for autonomously detecting and providing instructions for neutralizing the threat, and wherein each of the unmanned aerial vehicles is configured for communicating (e.g., directly, without relying on any system external thereto and/or to the target) with the platform (e.g., the platform being configured to issue instructions to the UAV's).

    INTERCEPTION MISSILE AND WARHEAD THEREFOR
    194.
    发明公开
    INTERCEPTION MISSILE AND WARHEAD THEREFOR 审中-公开
    ABFANGRAKETE UND GEFECHTSKOPFDAFÜR

    公开(公告)号：EP3071925A1

    公开(公告)日：2016-09-28

    申请号：EP15733090.3

    申请日：2015-01-01

    Applicant: Israel Aerospace Industries Ltd.

    Inventor： ROVINSKY, Jacob

    IPC: F42B12/22 ,  F42B12/00

    CPC classification number: F42B12/22 ,  B64C39/024 ,  B64C2201/121 ,  F41G7/001 ,  F41G7/20 ,  F42B10/26 ,  F42B12/202 ,  F42B12/32 ,  F42C19/095

    Abstract: A fragmentation warhead is provided, capable of being mounted in a carrier vehicle, the warhead having a longitudinal axis. In at least one example the warhead includes a shell that extends along the longitudinal axis. The shell includes a fixed shell portion and a fragmentation portion, and defines therebetween a cavity for accommodating therein an explosive charge. The fragmentation portion includes at least one set of serially adjacent fragments in correspondingly serially contiguous relationship in the fragmentation portion and in generally helical relationship with respect to the longitudinal axis. A corresponding carrier vehicle and a corresponding missile are also provided.

    Abstract translation: 提供了能够安装在载体车辆中的分裂弹头，该弹头具有纵向轴线。 在至少一个示例中，弹头包括沿着纵向轴线延伸的壳体。 壳体包括固定壳体部分和碎裂部分，并且在其间限定用于在其中容纳炸药的空腔。 碎裂部分包括在碎裂部分中以相应的串联连续关系的至少一组串联相邻碎片，并且相对于纵向轴线呈大致螺旋关系。 还提供了相应的运载工具和相应的导弹。

    Payload delivery
    196.
    发明公开
    Payload delivery 审中-公开
    Nutzlastanlieferung

    公开(公告)号：EP2881698A1

    公开(公告)日：2015-06-10

    申请号：EP13275298.1

    申请日：2013-12-06

    Applicant: BAE Systems PLC

    Inventor： The designation of the inventor has not yet been filed

    IPC: F41G3/22 ,  F41G7/00 ,  F41G9/00 ,  G05D1/10 ,  G08G5/00

    CPC classification number: F41G9/002 ,  B64C2201/121 ,  B64C2201/128 ,  B64C2201/141 ,  B64C2201/145 ,  F41G3/22 ,  F41G7/007 ,  G05D1/0094 ,  G08G5/0069

    Abstract: Disclosed is a method for delivering a load (19) onboard an aircraft (2) to a target. The method comprises: acquiring a position of the target; acquiring parameter values relating to aircraft manoeuvrability; acquiring load properties; acquiring parameter values relating to environmental conditions; using the acquired information, determining a position and a velocity value; performing, by the aircraft (2), the procedure; and, at a point in the procedure that the aircraft (2) has the determined position and its travelling at a velocity equal to the determined velocity value, releasing the load (19). The determined position and velocity value are such that, were the aircraft (2) to release the load (19) whilst having the determined position and velocity, the load (19) would travel to be within a predetermined distance of the target. The procedure is such that the aircraft (2) would have the determined position and velocity at some time-step.

    Abstract translation: 公开了一种用于将飞机（2）上的载荷（19）输送到目标的方法。 该方法包括：获取目标的位置; 获取与飞机机动性有关的参数值; 获取负载特性; 获取与环境条件有关的参数值; 使用所获取的信息，确定位置和速度值; 由飞机（2）执行程序; 并且在飞行器（2）具有确定的位置并且以等于所确定的速度值的速度行进的过程中，释放负载（19）。 确定的位置和速度值使得在具有确定的位置和速度的情况下，飞行器（2）是释放负载（19），负载（19）将行进在目标的预定距离内。 该程序使得飞机（2）将在某个时间步长具有确定的位置和速度。

    Drohne
    200.
    发明公开
    Drohne 有权

    公开(公告)号：EP1674819A1

    公开(公告)日：2006-06-28

    申请号：EP05026655.0

    申请日：2005-12-07

    Applicant: LFK-Lenkflugkörpersysteme GmbH

    Inventor： Gleich, Peter ,  Maier, Franz

    IPC: F42B15/00 ,  B64C39/02 ,  B64C27/26 ,  B64C27/28

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/102 ,  B64C2201/121 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  F42B15/105

    Abstract: Es wird ein Kleinflugkörper mit einem Rumpf (Airframe), Mitteln zur Steuerung und einem Antrieb vorgeschlagen, bei dem im Rumpf ein Propeller-Elektroantrieb, eine Energieversorgung, eine TV-Kamera, eine Datenübertragungs- und Lenkelektronik sowie ein Gefechtskopf bzw. ein Wirksystem integriert und am Rumpf klapp-bzw. faltbare Flügel, Ruder und Propeller angeordnet sind.
    Der Kleinflugkörper kann für die Bekämpfung unterschiedlicher Ziele oder für unterschiedliche Missionen mit verschiedenen Wirksystemen bestückt werden.

    Abstract translation: 小飞机（无人机），机身，控制装置和推进电驱动。 机身包括推进电驱动，能量供应，电视摄像机，数据传输和指导电子，综合作战头和操作系统以及机身铰链翼型。

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