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    Anti-ship cruise missile barrier
    3.
    发明授权
    Anti-ship cruise missile barrier 有权
    反舰巡航导弹屏障

    公开(公告)号：US09228807B1

    公开(公告)日：2016-01-05

    申请号：US13763954

    申请日：2013-02-11

    申请人： Lockheed Martin Corporation

    发明人： Kenneth M. Adams

    IPC分类号： F41H11/04 ,  B64B1/44 ,  G05D1/00

    CPC分类号： F41H11/04 ,  B64B1/44 ,  G05D1/0011

    摘要： A barrier for providing defense against attack from airborne cruise missiles includes a buoyant lighter than air structure. A curtain is suspended from structure and depends from the structure to a level approximately even with the surface. The barrier is deployed across a path identified as a potential attack path for an incoming threat. An incoming missile strikes the curtain which is adapted such that at least a portion of the curtain separates from the barrier and envelopes or entangles the incoming missile. The portion of the curtain covers the flight control planes of the missile and deprives the missile of lift. The missile falls to the surface short of its intended target. The intended target may be a ship which may deploy the barrier at a selected distance from the ship along a determined path of attack.

    摘要翻译： 提供防空袭巡航导弹袭击的障碍包括比空中结构更轻的轻型飞机。 窗帘从结构上悬挂下来，从结构到大致均匀的表面。 屏障部署在被识别为传入威胁的潜在攻击路径的路径上。 进入的导弹撞击窗帘，其适于使得至少一部分窗帘与屏障分开并包围或缠绕进入的导弹。 窗帘的一部分覆盖了导弹的飞行控制飞机，并剥夺了导弹的电梯。 导弹落在与目的不符的地面上。 预期的目标可以是可以沿着确定的攻击路径沿着选定的距离从船舶部署障碍物的船。

    Kinetic energy rod warhead deployment system
    5.
    发明申请
    Kinetic energy rod warhead deployment system 审中-公开
    动能棒弹头部署系统

    公开(公告)号：US20040055498A1

    公开(公告)日：2004-03-25

    申请号：US10370892

    申请日：2003-02-20

    发明人： Richard M. Lloyd

    IPC分类号： F42B012/58

    CPC分类号： F42B12/205 ,  F41H11/04 ,  F41H13/0006 ,  F42B12/22 ,  F42B12/32 ,  F42B12/58 ,  F42B12/60 ,  F42B12/64

    摘要： A kinetic energy rod warhead deployment system and method featuring jettison housings each including a plurality of lengthy individual projectiles therein and a navigatable carrier for the jettison housings. The jettison housings are ejected in the vicinity of targets whereupon the individual projectiles are deployed in the trajectory path of each target.

    摘要翻译： 一种动能棒弹头部署系统和方法，其特征在于，其中包括多个长度独立的射弹以及用于射出壳体的可导航载体。 抛射壳体在目标附近弹出，因此各个射弹部署在每个目标的轨迹路径上。

    Projectile deployed cable weapons system
    6.
    发明授权
    Projectile deployed cable weapons system 失效
    弹药部署有线武器系统

    公开(公告)号：US4327644A

    公开(公告)日：1982-05-04

    申请号：US123955

    申请日：1980-02-25

    申请人： Charles M. Stancil

    发明人： Charles M. Stancil

    IPC分类号： F41H11/02 ,  F42B12/68 ,  F42B13/56

    CPC分类号： F41H11/04 ,  F41H11/02 ,  F41H13/0006 ,  F42B12/68

    摘要： A projectile deployed cable weapons system for defeating helicopter rotor systems is disclosed. The deployed cable is intended to settle on the target helicopter from above, and damage is inflicted on the main rotor blade or tail rotor blade of the helicopter by sudden stoppage or castastrophic failure of the contacted rotor system.A particularly advantageous assemblage for deploying an amount of cable to defeat helicopter rotor systems is also disclosed. The weapons assemblage includes a first cavity for receiving a projectile, a second cavity containing an amount of cable, and a snaring means attached to the first cable and situated with respect to the first cavity so as to intercept the projectile when projected. Most advantageously the assemblage consists of a field container containing both the projectile and cable as a single operating unit to be attached to the muzzle of a mortar cannon of conventional design.In another embodiment a projectile such as a rocket or shell contains the cable and a submunition. After the projectile is aloft the submunition is fired to carry the cable from submunition in strand form.

    摘要翻译： 公开了一种用于击倒直升机转子系统的弹丸部署电缆武器系统。 部署的电缆旨在从上方安置在目标直升机上，并且由于接触的转子系统的突然停止或霰弹性故障对直升机的主转子叶片或尾部转子叶片造成损坏。 还公开了用于部署一定数量的电缆以击败直升机转子系统的特别有利的组合。 武器组合包括用于接收射弹的第一腔，包含一定数量的电缆的第二空腔，以及连接到第一电缆并且相对于第一空腔定位的卡环装置，以便在投射时拦截射弹。 最有利的是，组合件包括容纳抛射体和电缆的现场容器，作为单个操作单元，以连接到常规设计的砂浆炮的枪口。 在另一个实施例中，诸如火箭或壳的射弹包含电缆和子弹药。 射弹高空后，子弹被射击，以电子束弹药的形式携带电缆。

    INTERDICTION SYSTEM AND METHOD OF OPERATION
    7.
    发明申请
    INTERDICTION SYSTEM AND METHOD OF OPERATION 审中-公开

    公开(公告)号：US20180245888A1

    公开(公告)日：2018-08-30

    申请号：US15250794

    申请日：2016-08-29

    申请人： Airspace Systems Inc.

    发明人： Jasminder Banga ,  Earl Stirling ,  Noah Moore

    IPC分类号： F41H11/02 ,  F42B15/10

    CPC分类号： F41H11/02 ,  B64C39/024 ,  B64C2201/182 ,  F41H11/04 ,  F42B10/56 ,  F42B15/10

    摘要： A system for arresting and capturing airborne targets comprising: a projectile comprising an airframe which houses a means for entanglement, a means for propulsion, and a means for producing drag, wherein the means for entanglement is tethered to the airframe, a launcher capable of launching the projectile to within a close distance of an airborne target, wherein as the projectile approaches the airborne target the projectile is first slowed down by the means for producing drag, and second, as the projectile slows down the means for propulsion causes the means for entanglement to be projected towards the airborne target, wherein the means for entanglement arrests and captures the airborne target, thus tethering it to the projectile, and wherein the means for producing drag slows down the speed at which the projectile and tethered airborne target descend to the ground.

    Missile interceptor with net body
    10.
    发明授权
    Missile interceptor with net body 失效
    导弹拦截器与网体

    公开(公告)号：US08056855B2

    公开(公告)日：2011-11-15

    申请号：US12134168

    申请日：2008-06-05

    申请人： Alexandr Konstantinovskiy

    发明人： Alexandr Konstantinovskiy

    IPC分类号： F41H11/04 ,  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。