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    • 2. 发明申请
    • WIDE AREA NEUTRALIZER
    • 宽边中线
    • WO2013008138A1
    • 2013-01-17
    • PCT/IB2012/053399
    • 2012-07-04
    • ORLEV, NahumORLEV, Alon
    • ORLEV, NahumORLEV, Alon
    • F42B23/16F42C15/42
    • F41H11/00F41G9/00F42B12/202F42B12/22F42B12/60F42B23/16
    • A weapon system includes a number of WAN components, each WAN component includes a warhead, a launch mechanism for launching the warhead, an aiming mechanism for aiming the launch mechanism to launch the warhead in a desired direction, and a controller that, upon receipt of a command to aim and launch the warhead, operates the aiming mechanism to aim the warhead in the desired direction and then operates the launch mechanism to launch the warhead. The weapon system also includes a WAN component deployment mechanism for deploying the plurality of WAN components in a defended area; and a command center for instructing the controller of one or more of the WAN components to aim and launch the warhead of the each WAN component at a target that has been detected in the defended area.
    • 武器系统包括多个WAN组件,每个WAN组件包括弹头,用于发射弹头的发射机构,用于瞄准发射机构以期望的方向发射弹头的瞄准机构,以及控制器,在接收到 瞄准和发射弹头的指挥,实施瞄准机制,将弹头瞄准所需方向,然后运行发射机制发射弹头。 武器系统还包括用于在防御区域中部署多个WAN组件的WAN组件部署机制; 以及命令中心,用于指示所述WAN组件中的一个或多个的控制器在所述被防御区域中检测到的目标上瞄准并发射所述每个WAN组件的所述弹头。
    • 3. 发明申请
    • PYROPHORIC ARROWS
    • WO2009104134A3
    • 2009-11-26
    • PCT/IB2009050646
    • 2009-02-17
    • RAFAEL ADVANCED DEFENSE SYSORLEV NAHUMWEITZ AMIR
    • ORLEV NAHUMWEITZ AMIR
    • F42B12/44F42B6/00F42B10/08
    • F42B10/04F42B10/08F42B10/14F42B12/08F42B12/44F42B12/46F42B15/00
    • An arrow-type warhead (100,200,300,400,500,600,700) comprises an envelope (102,202), a filling (108), a hardened head section (104) to promote penetration of the target and a stabilizing mechanism (106,210,302,402,502,602) to stabilize the warhead in flight, hi some embodiments the filling (108) is pyrophoric and undergoes an exothermic reaction with the envelope upon impact. In other embodiments the filling is incendiary and undergoes reaction with the envelope upon impact in an oxygen rich-environment. In yet other embodiments, the filling is explosive. In all embodiments, the warhead may be equipped with a mini-rocket propulsion mechanism (802) for propelling the warhead to the target.
    • 箭头型弹头(100,200,300,400,500,600,700)包括一个信封(102,202),一个填充物(108),一个硬化头部分(104),以促进目标的穿透,以及一个稳定机构(106,210,302,402,502,602)以使飞行中的弹头稳定。 实施例中,填充物(108)是自燃的,并且在碰撞时与包壳发生放热反应。 在其它实施方案中,填充物是燃烧的,并且在富氧环境中冲击时与包络体发生反应。 在其他实施例中,填充物是爆炸性的。 在所有实施例中,弹头可以配备有用于将弹头推进到目标的微型火箭推进机构(802)。