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    ROCKET PROPELLED BARRIER DEFENSE SYSTEM
    41.
    发明申请
    ROCKET PROPELLED BARRIER DEFENSE SYSTEM 有权
    ROCKET PROPELLED BARRIER防御系统

    公开(公告)号：US20120011996A1

    公开(公告)日：2012-01-19

    申请号：US12165759

    申请日：2008-07-01

    申请人： Richard Glasson

    发明人： Richard Glasson

    IPC分类号： F41H5/007 ,  F41H11/00 ,  F41H5/06

    CPC分类号： F41H11/04 ,  F41H13/0006

    摘要： A system providing a physical-barrier defense against rocket-propelled grenades (RPGs) that is suitable for use on aircraft, ground vehicles and ships. The system includes a propulsion device (for example, a rocket) and a barrier that is attached to the propulsion device by one or more tethers. The barrier includes an inflatable frame. When the propulsion device is launched, an inflator inflates the frame to assume an open state, and the propulsion device pulls the tether and the barrier along a trajectory for intercepting an RPG.

    摘要翻译： 一种适用于飞机，地面车辆和船只的火箭推进榴弹（RPG）的物理障碍防御系统。 该系统包括推进装置（例如，火箭）和通过一个或多个系绳附接到推进装置的障碍物。 屏障包括一个充气框架。 当推进装置被启动时，充气机使框架膨胀以呈现打开状态，并且推进装置沿着用于拦截RPG的轨迹拉动系绳和屏障。

    Ballistic and Impact Protective Visor System for Military Helmet Assembly
    42.
    发明申请
    Ballistic and Impact Protective Visor System for Military Helmet Assembly 有权
    军用头盔装配弹道防撞护角系统

    公开(公告)号：US20110307990A1

    公开(公告)日：2011-12-22

    申请号：US12875111

    申请日：2010-09-02

    申请人： Dominique Croteau ,  Stéphane Lebel

    发明人： Dominique Croteau ,  Stéphane Lebel

    IPC分类号： A41D13/11

    CPC分类号： A42B3/04 ,  A42B3/221 ,  A42B3/326 ,  F41H1/04 ,  F41H11/04 ,  G02C3/02 ,  G02C7/022 ,  G02C2202/04

    摘要： A visor for a helmet includes a lens having a top edge that slopes downward from a top center point to first right and left curve points, at the first curve points the top edge begins to slope more aggressively toward second right and left curve points, and more aggressively toward right and left side edge points. A plane of sight along the vertical extent of the lens is displaced above the plane intersecting the side edge points. The lens has a thickness defined between an inner concave surface and an outer convex surface; the inner and outer surfaces having different radii of curvatures. The lens tapers from the center toward the outer edges.

    摘要翻译： 用于头盔的面罩包括具有从顶部中心点向第一右侧和左侧弯曲点向下倾斜的顶部边缘的透镜，在第一曲线点，顶部边缘开始朝向第二左右曲线点更积极地倾斜，以及 更积极地朝向左右边缘点。 沿着透镜的垂直范围的视线在与边缘点相交的平面上移动。 透镜具有限定在内凹表面和外凸表面之间的厚度; 内表面和外表面具有不同的曲率半径。 透镜从中心向外边缘逐渐变细。

    MISSILE INTERCEPTOR WITH NET BODY
    44.
    发明申请
    MISSILE INTERCEPTOR WITH NET BODY 失效
    网络身心障碍者

    公开(公告)号：US20100102166A1

    公开(公告)日：2010-04-29

    申请号：US12134168

    申请日：2008-06-05

    申请人： Alexandr KONSTANTINOVSKIY

    发明人： Alexandr KONSTANTINOVSKIY

    IPC分类号： B64F1/02

    CPC分类号： F41H11/04 ,  F41H11/02

    摘要： The invention describes and claims an apparatus and method of missile interception. The missile interceptor comprises a net body with a plurality of sections and at least one missile trajectory effector. In the preferred variant, the missile trajectory effector is embodied as an exploding ring. A missile, passing through the net body, picks up a ring, which explodes once the missile passes a sufficient distance away from the missile interceptor. Preferred embodiments of the missile interceptor further comprise one or more vertically-positioned poles. Claimed method involves the use of such interceptor and positioning the interceptor on the likely trajectory of incoming missiles.

    摘要翻译： 本发明描述并要求一种导弹拦截的装置和方法。 导弹拦截器包括具有多个部分和至少一个导弹轨迹执行器的网体。 在优选的变型中，导弹轨迹执行器被实施为爆炸环。 一枚导弹穿过网身，拾起一个环，一旦导弹离导弹拦截距离足够远，就会爆炸。 导弹拦截器的优选实施例还包括一个或多个垂直定位的杆。 所声称的方法涉及使用这种拦截器并将拦截器定位在入射导弹的可能轨迹上。

    Vulnerable target protection system
    46.
    发明申请
    Vulnerable target protection system 有权
    弱势目标保护体系

    公开(公告)号：US20030127636A1

    公开(公告)日：2003-07-10

    申请号：US10277839

    申请日：2002-10-23

    申请人： Innofocus Consultants Limited

    发明人： Ludwig A. Piron

    IPC分类号： A01K003/00

    CPC分类号： F41H11/04 ,  F41H5/026 ,  F41H11/02

    摘要： A defense barrier for protecting a target from critical damage from the impact of a predetermined group of aircraft comprises: a plurality of towers spaced from the target, each tower being spaced from a neighbouring tower by a distance less than the wingspan of an aircraft in the predetermined group of aircraft having the smallest wingspan in the group; each tower being spaced from the target at least a distance d given by the formula: dnullh/tan(theta) where h is the height of the tower and theta is the smallest vertical approach angle of any aircraft from the predetermined group of aircraft sufficient to inflict critical damage to the target.

    摘要翻译： 用于保护目标免受来自预定组飞机的冲击的关键损伤的防御屏障包括：与目标间隔开的多个塔架，每个塔架与邻近的塔架间隔一定距离小于飞机的翼展距离 组中具有最小翼展的预定组的飞机; 每个塔与目标距离至少一定距离d，由公式给出：d = h / tan（θ）其中h是塔的高度，θ是来自预定飞机组的任何飞机的最小垂直进近角 足以对目标造成严重伤害。