Layered energetic material having multiple ignition points
    3.
    发明授权
    Layered energetic material having multiple ignition points 有权
    具有多个点火点的分层能量材料

    公开(公告)号:US09464874B1

    公开(公告)日:2016-10-11

    申请号:US14213750

    申请日:2014-03-14

    摘要: An energetic material having thin, alternating layers of metal oxide and reducing metal is provided. The energetic material may be provided in the form of a sheet, foil, cylinder, or other convenient structure. A method of making the energetic material resists the formation of oxide on the surface of the reducing metal, allowing the use of multiple thin layers of metal oxide and reducing metal for maximum contact between the reactants, without significant lost volume due to oxide formation. An ignition system for the energetic material includes multiple ignition points, as well as a means for controlling the timing and sequence of activation of the individual ignition points. The combination of the energetic material and ignition system provides a means of charge and blast shaping, ignition timing, pressure curve control and maximization, and safe neutralization of the energetic material.

    摘要翻译: 提供具有薄的交替层的金属氧化物和还原金属的高能材料。 能量材料可以以片材,箔,圆筒或其它方便的结构的形式提供。 使能量材料能够抵抗还原金属表面上形成氧化物的方法,允许使用金属氧化物和还原金属的多个薄层来最大程度地接触反应物,而不会由于形成氧化物而明显地损失体积。 用于能量材料的点火系统包括多个点火点,以及用于控制各点火点的启动的时序和顺序的装置。 高能材料和点火系统的组合提供了充电和鼓风成型,点火正时,压力曲线控制和最大化的手段,以及高能材料的安全中和。

    APPARATUS AND METHOD FOR PROGRAMMING A PROJECTILE
    4.
    发明申请
    APPARATUS AND METHOD FOR PROGRAMMING A PROJECTILE 审中-公开
    用于编程项目的装置和方法

    公开(公告)号:US20140060298A1

    公开(公告)日:2014-03-06

    申请号:US14059023

    申请日:2013-10-21

    IPC分类号: F42C11/00

    摘要: A measurement apparatus is provided, which is included on a measurement and programming basis for a projectile, which detects the fields and/or signals which emerge/originate from a programming coil, and is electrically connected to an evaluation device which itself evaluates these detected values. These values can then be taken into account for the programming of the projectile.

    摘要翻译: 提供了一种测量装置,其包括在用于射弹的测量和编程基础上,其用于检测从编程线圈出现/产生的场和/或信号,并且电连接到本身评估这些检测值的评估装置 。 然后可以将这些值考虑在射弹的编程中。

    METHOD AND DEVICE FOR PROGRAMMING A PROJECTILE
    5.
    发明申请
    METHOD AND DEVICE FOR PROGRAMMING A PROJECTILE 有权
    用于编程项目的方法和装置

    公开(公告)号:US20140007760A1

    公开(公告)日:2014-01-09

    申请号:US13563803

    申请日:2012-08-01

    申请人: Henry Roger FRICK

    发明人: Henry Roger FRICK

    IPC分类号: F42C11/06 F41G9/00

    摘要: An inductive or capacitative programming of a projectile is disclosed. A waveguide is used for the programming, the electromagnetic field being concentrated in the waveguide. The used programming unit includes at least one waveguide which is preferable located and/or integrated in the region of the muzzle, for example in front of the muzzle brake. A transmission coupler for the transmission is fed by a signal generator. The information relating to the projectile is modulated to the carrier frequency in the modulator. A reception coupler integrated on/in the projectile is electrically interconnected to a store or processor in the projectile. The reception coupler receives the modulated signal and transmits it to the processor which is where the eventual programming takes place.

    摘要翻译: 公开了一种对弹丸的感性或电容性编程。 波导用于编程,电磁场集中在波导中。 所使用的编程单元包括至少一个波导,其优选位于和/或集成在枪口的区域中,例如在枪口制动器的前面。 用于传输的传输耦合器由信号发生器馈送。 与射弹相关的信息调制到调制器的载波频率。 集成在射弹上的接收耦合器与射弹中的存储或处理器电互连。 接收耦合器接收调制信号并将其发送到最终编程发生的处理器。

    Rocket ejection delay apparatus and/or method
    6.
    发明授权
    Rocket ejection delay apparatus and/or method 有权
    火箭喷射延迟装置和/或方法

    公开(公告)号:US07918419B2

    公开(公告)日:2011-04-05

    申请号:US11488201

    申请日:2006-07-17

    IPC分类号: B64D17/72

    摘要: An ejection delay system, apparatus and/or method including an electronic ejection delay system having an ignition device; a power source connected to the ignition device; and, a flight parameter sensor switch electrically connected to the power source to initiate the provision of power from the power source to the ignition device; the electronic ejection delay system being disposed in some implementations in a housing system including a housing; a forward closure for closing the top end of the housing; and, an aft closure for closing the aft end of the housing. Also disclosed is a method for ejecting a rocket recovery system in flight; including sensing a parameter associated with flight; and, initiating deployment of a recovery system.

    摘要翻译: 一种喷射延迟系统,装置和/或方法,包括具有点火装置的电子喷射延迟系统; 连接到点火装置的电源; 以及飞行参数传感器开关,其电连接到所述电源以启动从所述电源向所述点火装置提供电力; 电子喷射延迟系统在一些实施方式中被布置在包括壳体的壳体系统中; 用于封闭壳体顶端的向前封闭件; 以及用于关闭壳体的后端的后盖。 还公开了一种在飞行中弹出火箭回收系统的方法; 包括感测与飞行有关的参数; 并启动部署恢复系统。

    GUIDED WEAPON WITH IN-FLIGHT-SWITCHABLE MULTIPLE FUZE MODES
    7.
    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。

    Synchronously timed fuse procedure or process
    8.
    发明授权
    Synchronously timed fuse procedure or process 有权
    同步定时保险丝程序或过程

    公开(公告)号:US07886647B2

    公开(公告)日:2011-02-15

    申请号:US11414194

    申请日:2006-05-01

    申请人: Craig L Holloway

    发明人: Craig L Holloway

    IPC分类号: B64D1/04

    CPC分类号: F42C11/065 F42C11/001

    摘要: A synchronously timed fused is installed into ordnance the ordnance is delivered to a target area, in a shaped charge formation and a simultaneous explosion event occurs.

    摘要翻译: 同步定时熔断器安装在弹药中,弹药以成形的电荷形成传送到目标区域,并发生同时爆炸事件。

    METHOD TO ENSURE PAYLOAD ACTIVATION OF ORDNANCE
    9.
    发明申请
    METHOD TO ENSURE PAYLOAD ACTIVATION OF ORDNANCE 失效
    确保荷载活动的方法

    公开(公告)号:US20100005995A1

    公开(公告)日:2010-01-14

    申请号:US11797496

    申请日:2007-05-03

    IPC分类号: F42C9/16

    CPC分类号: F42C15/40 F42C11/065

    摘要: A method to ensure payload activation of ordnance independently of a preset period of time including the steps of providing a power source to a clock, a detonator and a trigger circuit; the clock providing an initial count and a terminal count; the initial count providing a trigger signal to the trigger; the trigger circuit providing a terminal count signal to a self-destruct system if a malfunction results in no clock operation.

    摘要翻译: 一种确保与预设时间段无关地起作用的方法,包括向时钟,雷管和触发电路提供电源的步骤; 时钟提供初始计数和终端计数; 初始计数提供触发信号; 如果故障导致没有时钟操作,则触发电路向自毁系统提供终端计数信号。

    Projectile with variable target transition detection capability and method therefor
    10.
    发明授权
    Projectile with variable target transition detection capability and method therefor 失效
    具有可变目标转移检测能力的弹丸及其方法

    公开(公告)号:US06483323B1

    公开(公告)日:2002-11-19

    申请号:US08580116

    申请日:1996-01-16

    IPC分类号: G01R2708

    摘要: A projectile fuze detects transitions between target layers by an electronic antenna radiating laterally into the target material and coupled to a pullable oscillator whose frequency shifts as the target material changes while the projectile penetrates. A frequency shift threshold detector relates the observed frequency shifts to a stored target profile to detonate the projectile after the desired layer penetration.

    摘要翻译: 射弹引信通过横向辐射到目标材料中的电子天线来检测目标层之间的转换,并且耦合到可弹性振荡器,其随着目标材料随着射弹穿透而变化。 频移阈值检测器将观察到的频移与存储的目标轮廓相关联,以在期望的层穿透之后引爆射弹。