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    • 84. 发明申请
    • Tactical surveillance sensor projectile system
    • 战术监视传感器射弹系统
    • US20040075585A1
    • 2004-04-22
    • US10272894
    • 2002-10-17
    • Kenneth W. KaiserRobert L. FaizSean George
    • F41G007/00F42B015/04
    • F41F3/045F42B12/365F42B15/04
    • A tactical surveillance sensor projectile system includes a propellant and primer chamber, a firing device, a sensor device, a signal processor, and a fiber optic cable; the firing device fires the primer and propellant to establish a powered phase of flight followed by a ballistic phase of flight to clear an obstacle; the sensor device generates surveillance signals representative of ambient characteristics beyond the obstacle at least during the ballistic phase of flight; the signal processor is responsive to the sensor device for converting the signals representative of ambient conditions to an optical data stream; and the fiber optic cable delivers the optical data stream to a ground station at least during the ballistic phase of flight.
    • 一种战术监视传感器射出系统,包括推进剂和底漆室,点火装置,传感器装置,信号处理器和光纤电缆; 射击装置启动底漆和推进剂建立一个动力阶段的飞行,然后是飞行的弹道阶段,以清除障碍物; 传感器装置至少在飞行的弹道阶段产生代表超出障碍物的环境特性的监视信号; 所述信号处理器响应所述传感器装置将所述表示环境条件的信号转换成光数据流; 并且光纤电缆至少在飞行的弹道阶段将光数据流传送到地面站。
    • 85. 发明申请
    • STOWABLE INTEGRATED MOTOR PROPULSOR FINS
    • 可集成的电机推进器FINS
    • US20040065248A1
    • 2004-04-08
    • US10267100
    • 2002-10-08
    • Thomas J. Gieseke
    • B63G008/14
    • F42B19/12B63G8/18B63H5/14F42B12/36F42B12/365
    • A control surface system is particularly well suited to provide improved control for undersea vehicles having integrated motor propulsors (IMP). The control surface system is deployable beyond lateral peripheral dimensions of the IMP and undersea vehicle. A plurality of arc-shaped control elements is disposed in a stowed position in an annular intake recess inside of an annular duct on the undersea vehicle. Struts connect each of the control elements to the annular duct. A deployment device rotates each of the control elements and the struts radially outwardly beyond lateral peripheral dimensions of the vehicle to a fully deployed position. A latching mechanism selectively engages and disengages the struts to hold the control elements in the stowed position and the fully deployed position, respectively. Launch tubes sized for the undersea vehicles can launch undersea vehicles provided with control surface system.
    • 控制表面系统特别适合于为具有集成的马达推进器(IMP)的海底车辆提供改进的控制。 控制面系统可以超越IMP和海底车辆的外围尺寸。 多个弧形控制元件被设置在位于海底车辆上的环形管道内的环形进气口的收纳位置。 Struts将每个控制元件连接到环形管道。 部署装置将每个控制元件和支柱径向向外转动超过车辆的横向外围尺寸至完全展开位置。 闩锁机构选择性地接合和脱离支柱以将控制元件分别保持在收起位置和完全展开位置。 为海底车辆发射的发射管可以发射配备控制面系统的海底车辆。
    • 88. 发明授权
    • All-aspect bomb damage assessment system
    • 全方位炸弹伤害评估系统
    • US5537909A
    • 1996-07-23
    • US423391
    • 1995-04-17
    • Arthur J. SchneiderJames G. SmallDonald E. FrenchHenry August
    • Arthur J. SchneiderJames G. SmallDonald E. FrenchHenry August
    • F42B10/56B64D1/04F42B12/36F42B15/00G01S3/782G01S13/89
    • B64D1/04F42B12/365
    • A bomb damage assessment system that is carried by a weapon and released to provide imagery of a bombed area before and after bomb delivery. The system comprises a glider that is releasably secured to the weapon that includes tracking and guidance electronics for programmably controlling the flight thereof. An imaging system is disposed in the front end of the glider and a deployable ballute is disposed at the rear end thereof. A data link is provided for transmitting images to a command center for review. The system provides imagery of a target area before, during and after weapon impact. Television or infrared cameras may be used for day or night missions. As a target area is approached, the glider is released, is decelerated by the ballute, wings are unfolded, and the ballute is released, resulting in an aerodynamic vehicle that flies much slower than the weapon. The imaging system tracks the weapon to impact. The explosion of the weapon produces a hot spot that is tracked by the imaging system. The hot spot is tracked until a preselected depression angle is reached. The glider banks until the hot spot is at a predetermined angle relative to the centerline thereof. This results in a spiral glide path around the hot spot so that the target area is viewed from all aspects. The spiral path also results in a monotonically decreasing range to the hot spot. The glider may employ a GPS receiver, and the target location in GPS coordinates may be entered into the guidance and control system. The glider may be programmed to fly along a specific path or geometric surface in GPS coordinates toward the target. Using a fixed field of view imaging system, a large amount of background is seen from long range and better linear resolution is obtained at short range until the glider descends to the ground. Bomb damage assessment may be performed at the command center within minutes of weapon impact.
    • 炸弹损伤评估系统,由武器携带并被释放,以在炸弹传送前后提供轰炸区域的图像。 该系统包括可释放地固定到武器上的滑翔机,其包括用于可编程地控制其飞行的跟踪和引导电子装置。 成像系统设置在滑翔机的前端,并且可展开的小球在其后端设置。 提供数据链接用于将图像发送到指挥中心进行审查。 该系统在武器冲击之前,之中和之后提供目标区域的图像。 电视或红外摄像机可用于白天或夜间任务。 当接近目标区域时,滑翔机被释放,由球道减速,机翼展开,气球被释放,产生飞行比武器慢得多的空气动力学车辆。 成像系统跟踪武器的影响。 武器的爆炸产生了由成像系统跟踪的热点。 跟踪热点直到达到预选的俯角。 滑翔机直到热点相对于其中心线处于预定角度。 这导致围绕热点的螺旋滑动路径,使得从各个方面观察目标区域。 螺旋路径也导致热点单调减少的范围。 滑翔机可以使用GPS接收机,并且GPS坐标中的目标位置可以被输入到引导和控制系统中。 滑翔机可以被编程为沿GPS坐标向着目标的特定路径或几何表面飞行。 使用固定视野成像系统,从远距离看到大量的背景,并且在短距离内获得更好的线性分辨率,直到滑翔机下降到地面。 炸弹伤害评估可能在武器冲击的几分钟内在指挥中心进行。