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    HYBRID OPTICAL AND MICROWAVE IMAGING SATELLITE
    23.
    发明申请
    HYBRID OPTICAL AND MICROWAVE IMAGING SATELLITE 有权
    混合光学和微波成像卫星

    公开(公告)号：US20140327596A1

    公开(公告)日：2014-11-06

    申请号：US13800243

    申请日：2013-03-13

    Applicant: ALLIANT TECHSYSTEMS INC.

    Inventor： Dilip K. Darooka

    IPC: H01Q19/12 ,  H01Q15/00

    CPC classification number: H01Q15/0033 ,  H01Q5/22 ,  H01Q19/191

    Abstract: A hybrid image gathering and data transmission system is provided. The system includes at least one parabolic reflector to gather, disseminate and direct electromagnetic radiation. A beam splitter using Fresnel Zone Plate Array (FZPA) is configured and arranged to receive and or transmit the electromagnetic radiation from or to the at least one parabolic reflector and separately focus microwave radiation and visual radiation. The beam splitter provides a gain in the microwave radiation and visual radiation. A Radio Frequency (RF) receiver/transmitter receives and transmits the microwave radiation from or to the beam splitter and a Focal Plane Array (FPA) receives the visible radiation from the beam splitter. A processor is in communication with the RF receiver and the FPA. The processor processes signals received by the RF receiver and the FPA and provide processed data to be transmitted to a remote location.

    Abstract translation: 提供了一种混合图像采集和数据传输系统。 该系统包括至少一个抛物面反射器，以收集，传播和引导电磁辐射。 使用菲涅耳区板阵列（FZPA）的分束器被配置和布置成接收和/或传送来自至少一个抛物面反射器的电磁辐射，并且分别聚焦微波辐射和视觉辐射。 分束器在微波辐射和视觉辐射方面提供增益。 射频（RF）接收器/发射器接收并发射来自分束器的微波辐射，并且焦平面阵列（FPA）接收来自分束器的可见光。 处理器与RF接收器和FPA通信。 处理器处理由RF接收机和FPA接收的信号，并提供要传输到远程位置的处理数据。

    ANNEALING SYSTEM FOR CARTRIDGE CASINGS
    24.
    发明申请
    ANNEALING SYSTEM FOR CARTRIDGE CASINGS 有权
    用于盒子的退火系统

    公开(公告)号：US20140318351A1

    公开(公告)日：2014-10-30

    申请号：US14265015

    申请日：2014-04-29

    Applicant: ALLIANT TECHSYSTEMS, INC.

    Inventor： James Eveland

    IPC: B23P15/22 ,  F42B33/14 ,  C21D9/00

    CPC classification number: B23P15/22 ,  C21D1/34 ,  C21D1/42 ,  C21D1/70 ,  C21D8/10 ,  C21D9/0006 ,  C21D9/12 ,  C21D9/16 ,  F42B33/14 ,  Y02P10/253

    Abstract: A portion of a work-hardened essentially tubular work piece such as a metallic firearm cartridge case is annealed by contact with solid or granular tooling material which has been heated to a temperature approximately that of the appropriate annealing temperature, thereby reducing the possibility of overheating the work piece, and also thereby permitting the annealing of only that portion of the work piece contacted or in close proximity to the point(s) of contact.

    Abstract translation: 通过与已经被加热到适当退火温度的温度的固体或颗粒工具材料的接触而将诸如金属火器盒壳体的加工硬化的基本上管状的工件的一部分退火，从而减少过热的可能性 工件，并且还允许只有接触的工件的那部分或接近点的退火。

    SOLAR ARRAYS, DEPLOYMENT MECHANISMS THEREFOR, AND RELATED METHODS
    25.
    发明申请
    SOLAR ARRAYS, DEPLOYMENT MECHANISMS THEREFOR, AND RELATED METHODS 有权
    太阳能阵列，其部署机制及相关方法

    公开(公告)号：US20140263847A1

    公开(公告)日：2014-09-18

    申请号：US13804331

    申请日：2013-03-14

    Applicant: ALLIANT TECHSYSTEMS INC.

    Inventor： Michael I. Eskenazi ,  Nicholas C. Wilder ,  David M. Murphy

    IPC: B64G1/22 ,  B64G1/44

    CPC classification number: B64G1/222 ,  B64G1/44 ,  H02S20/00 ,  H02S30/20 ,  Y02E10/50

    Abstract: Mechanisms for deploying a solar array include an elongated deployment member routed along a first panel, along an extension, and at least partially along a second panel. The elongated deployment member is configured to, upon retraction of the elongated deployment member by the deployment motor, move the extension into an extended position and rotate the second panel about a hub located at a distal end of the extension. Solar array assemblies include such a mechanism. Methods of deploying a solar array include retracting an elongated deployment member to rotate an extension into an extended position and further retracting the elongated deployment member to rotate a panel coupled to the extension approximately 360° about a hub of the extension.

    Abstract translation: 用于部署太阳能阵列的机构包括沿着第一面板沿着延伸部沿着第二面板至少部分地布置的细长展开构件。 细长展开构件构造成在通过展开电机缩回细长展开构件时，将延伸部移动到延伸位置，并且使第二面板围绕位于延伸部的远端的毂旋转。 太阳能阵列组件包括这种机构。 部署太阳能阵列的方法包括缩回细长展开构件以将延伸部旋转到延伸位置，并且进一步缩回细长展开构件以使围绕延伸部的轮毂大约360°连接到延伸部的面板旋转。

    RELOADING KIT WITH LEAD FREE BULLET COMPOSITION
    26.
    发明申请
    RELOADING KIT WITH LEAD FREE BULLET COMPOSITION 有权
    使用无铅BULLET组合物重新装载

    公开(公告)号：US20140260926A1

    公开(公告)日：2014-09-18

    申请号：US14208271

    申请日：2014-03-13

    Applicant: Alliant Techsystems Inc.

    Inventor： Rochelle D. POORE ,  Daniel B. SHIPMAN

    IPC: F42B33/00

    CPC classification number: F42B12/745 ,  F42B30/02 ,  F42B33/001 ,  F42B33/002 ,  F42B33/0207 ,  F42B33/04 ,  F42B33/10

    Abstract: The present disclosure is directed to reloading kits containing a packaged high-density metal-filled polymer composition that is moldable and used in producing lead-free or “green” bullets for individual firearms. Such kits and compositions may be used by individuals in their reloading process.

    Abstract translation: 本公开涉及包含可包装的高密度金属填充聚合物组合物的重新装载试剂盒，其可模塑并用于生产单个火器的无铅或“绿色”子弹。 这些试剂盒和组合物可以由个体在其重新加载过程中使用。

    METHOD AND APPARATUS FOR BALLISTIC TAILORING OF PROPELLANT STRUCTURES AND OPERATION THEREOF FOR DOWNHOLE STIMULATION
    28.
    发明申请
    METHOD AND APPARATUS FOR BALLISTIC TAILORING OF PROPELLANT STRUCTURES AND OPERATION THEREOF FOR DOWNHOLE STIMULATION 有权
    用于推进式结构的弹丸定型的方法和装置以及用于下颌刺激的操作

    公开(公告)号：US20140238678A1

    公开(公告)日：2014-08-28

    申请号：US13781217

    申请日：2013-02-28

    Applicant: ALLIANT TECHSYSTEMS INC.

    Inventor： JOHN A. ARRELL, JR. ,  STEVEN E. MOORE

    IPC: E21B43/263 ,  C06B45/00

    CPC classification number: E21B43/263 ,  C06B45/00 ,  C06B45/10 ,  C06B45/105 ,  E21B33/124 ,  E21B43/247 ,  F42B1/00 ,  F42B1/04

    Abstract: Propellant structures and stimulation tools incorporating propellant structures may comprise composite propellant structures including two or more regions of propellant having different compositions, different grain structures, or both. An axially extending initiation bore containing a initiation element may extend through a center of the propellant structure, or may be laterally offset from the center. An offset initiation bore may be employed with a composite grain structure. Methods of tailoring ballistic characteristics of propellant burn to result in desired operational pressure pulse characteristics are also disclosed.

    Abstract translation: 包含推进剂结构的推进剂结构和刺激工具可以包括复合推进剂结构，包括具有不同组成，不同晶粒结构或两者的两个或更多个推进剂区域。 包含起始元件的轴向延伸的起始孔可以延伸穿过推进剂结构的中心，或者可以从中心横向偏移。 偏移引发孔可以与复合晶粒结构一起使用。 还公开了调整推进剂燃烧的弹道特性以产生期望的操作压力脉冲特性的方法。

    SHOTGUN SHELL WITH WEIGHTED WAD
    30.
    发明申请
    SHOTGUN SHELL WITH WEIGHTED WAD 审中-公开
    SHOTGUN壳与加重的WAD

    公开(公告)号：US20130228090A1

    公开(公告)日：2013-09-05

    申请号：US13683795

    申请日：2012-11-21

    Applicant: ALLIANT TECHSYSTEMS INC.

    Inventor： Chris L. Billings

    IPC: F42B7/08

    CPC classification number: F42B7/08 ,  F42B7/04 ,  F42B10/50

    Abstract: A shotgun cartridge having a weighted wad for controlling the separation point between the wad and the shot load. The wad having a tail portion and a nose portion with the nose portion shifting the center of gravity of the wad axially forward away from the center of pressure compared to where the center of gravity would be if the nose portion was not weighted thereby controlling the shot load separation and enhancing the shot pattern.

    Abstract translation: 霰弹枪筒具有用于控制焊盘和射击负载之间的分离点的加权焊盘。 具有尾部和鼻部的小篮部分，其鼻部部分使瓦the重心从压力中心轴向向前移动，相比之下，如果鼻部部分没有被称重，则重心将由此控制射击 负载分离和增强射击模式。

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