GUIDED WEAPON WITH IN-FLIGHT-SWITCHABLE MULTIPLE FUZE MODES
    1.
    发明申请
    GUIDED WEAPON WITH IN-FLIGHT-SWITCHABLE MULTIPLE FUZE MODES 有权
    带有飞行可切换多种燃料模式的指导武器

    公开(公告)号:US20110041720A1

    公开(公告)日:2011-02-24

    申请号:US12918327

    申请日:2009-02-12

    IPC分类号: F42B15/01

    摘要: A method for operating a guided munition with a switchable fuse arrangement includes launching the guided munition towards a target. During flight of the guided munition, images are provided to a remote operator, who supplies a switching input. Responsive to said switching input, the fuze arrangement is switched to either of at least two of the following states: a delayed detonation state in which detonation of the explosive charge is delayed by a time delay after impact of the guided munition, an impact detonation state in which detonation of the explosive charge occurs on impact of the guided munition, a proximity detonation state in which detonation of the explosive charge is triggered by a proximity sensing arrangement, and a disabled state in which the guided munition functions as a guided kinetic shell without detonation of the explosive charge.

    摘要翻译: 用可切换的保险丝装置来操作制导弹药的方法包括朝向目标发射导弹。 在飞行中的导弹弹药中,图像提供给遥控操作员,他们提供切换输入。 响应于所述切换输入,引信布置被切换到以下状态中的至少两个状态:延迟爆炸状态,其中爆炸装置的爆炸在受到导弹的冲击之后延迟时间延迟,撞击爆炸状态 其中爆炸装药的爆炸是在制导弹药的冲击下发生的,爆炸装置的爆炸引爆的邻近的爆炸状态是由接近感应装置引起的,而在这种情况下,被引导的弹药作为引导的动力弹壳起作用, 引爆炸药。

    Guided weapon with in-flight-switchable multiple fuze modes
    2.
    发明授权
    Guided weapon with in-flight-switchable multiple fuze modes 有权
    具有飞行中可切换多重引信模式的导弹武器

    公开(公告)号:US08689692B2

    公开(公告)日:2014-04-08

    申请号:US12918327

    申请日:2009-02-12

    IPC分类号: F42C9/14

    摘要: A method for operating a guided munition with a switchable fuze arrangement includes launching the guided munition towards a target. During flight of the guided munition, images are provided to a remote operator, who supplies a switching input. Responsive to said switching input, the fuze arrangement is switched to either of at least two of the following states: a delayed detonation state in which detonation of the explosive charge is delayed by a time delay after impact of the guided munition, an impact detonation state in which detonation of the explosive charge occurs on impact of the guided munition, a proximity detonation state in which detonation of the explosive charge is triggered by a proximity sensing arrangement, and a disabled state in which the guided munition functions as a guided kinetic shell without detonation of the explosive charge.

    摘要翻译: 用可切换的引信装置操作制导弹药的方法包括向目标发射导弹。 在飞行中的导弹弹药中,图像提供给遥控操作员,他们提供切换输入。 响应于所述切换输入,引信布置被切换到以下状态中的至少两个状态:延迟爆炸状态,其中爆炸装置的爆炸在受到导弹的冲击之后延迟时间延迟,撞击爆炸状态 其中爆炸装药的爆炸是在制导弹药的冲击下发生的,爆炸装置的爆炸引爆的邻近的爆炸状态是由接近感应装置引起的,而在这种情况下,被引导的弹药作为引导的动力弹壳起作用, 引爆炸药。