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    INTERCEPTION MISSLE AND WARHEAD THEREFOR
    92.
    发明申请
    INTERCEPTION MISSLE AND WARHEAD THEREFOR 审中-公开
    拦截错误和WARHEAD

    公开(公告)号：US20160320165A1

    公开(公告)日：2016-11-03

    申请号：US15108656

    申请日：2015-01-01

    Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

    Inventor： Jacob Rovinsky

    IPC: F42B12/22 ,  F41G7/20 ,  F41G7/00 ,  B64C39/02

    CPC classification number: F42B12/22 ,  B64C39/024 ,  B64C2201/121 ,  F41G7/001 ,  F41G7/20 ,  F42B10/26 ,  F42B12/202 ,  F42B12/32 ,  F42C19/095

    Abstract: A fragmentation warhead is provided, capable of being mounted in a carrier vehicle, the warhead having a longitudinal axis. In at least one example the warhead includes a shell that extends along the longitudinal axis. The shell includes a fixed shell portion and a fragmentation portion, and defines therebetween a cavity for accommodating therein an explosive charge. The fragmentation portion includes at least one set of serially adjacent fragments in correspondingly serially contiguous relationship in the fragmentation portion and in generally helical relationship with respect to the longitudinal axis. A corresponding carrier vehicle and a corresponding missile are also provided.

    Abstract translation: 提供了能够安装在载体车辆中的分裂弹头，该弹头具有纵向轴线。 在至少一个示例中，弹头包括沿着纵向轴线延伸的壳体。 壳体包括固定壳体部分和碎裂部分，并且在其间限定用于在其中容纳炸药的空腔。 碎裂部分包括在碎裂部分中以相应的串联连续关系的至少一组串联相邻碎片，并且相对于纵向轴线呈大致螺旋关系。 还提供了相应的载体车辆和相应的导弹。

    TRAILER FOR AUTONOMOUS VEHICLE
    93.
    发明申请
    TRAILER FOR AUTONOMOUS VEHICLE 审中-公开
    自动车辆拖车

    公开(公告)号：US20160200235A1

    公开(公告)日：2016-07-14

    申请号：US14912474

    申请日：2014-09-11

    Applicant: SILICIS TECHNOLOGIES, INC.

    Inventor： Michael J. Stigler ,  Nicholas James Setar

    IPC: B60P3/11 ,  B64B1/66 ,  B64C39/02 ,  B60P7/06 ,  B60P7/08

    CPC classification number: B60P3/11 ,  B60P7/06 ,  B60P7/0876 ,  B64B1/10 ,  B64B1/50 ,  B64B1/58 ,  B64B1/66 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/06 ,  B64C2201/101 ,  B64C2201/12 ,  B64C2201/121 ,  B64C2201/125 ,  B64C2201/127 ,  B64C2201/148 ,  B64C2201/208 ,  B64F1/14 ,  B64F3/02 ,  G08C17/02

    Abstract: The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.

    Abstract translation: 所公开的实施例包括用于由命令和控制接口控制的自主车辆的拖车。 拖车包括拖车主体，其构造成将自主车辆保持在未部署的构造中。 拖车还以部署的配置锚定自主车辆。 提供了系绳，其具有联接到拖车主体的第一端和被配置为联接到自主车辆的第二端。 使用绞盘来调节系绳的长度以在未部署的配置和部署配置之间移动自主车辆。 此外，通信系统与命令和控制界面以及自主车辆进行通信，以控制自动车辆在未部署配置和部署配置之间的移动。

    Power Safety Instrument System
    95.
    发明申请
    Power Safety Instrument System 有权
    电力安全仪表系统

    公开(公告)号：US20150321769A1

    公开(公告)日：2015-11-12

    申请号：US14715236

    申请日：2015-05-18

    Applicant: James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

    Inventor： James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

    IPC: B64D45/00 ,  B64D43/00

    CPC classification number: G01C23/00 ,  B60Q1/00 ,  B64C27/00 ,  B64C27/006 ,  B64C27/04 ,  B64C27/52 ,  B64C29/00 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/121 ,  B64D43/00 ,  B64D45/00 ,  G01C21/00 ,  G01D7/02 ,  G05D17/02

    Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

    Abstract translation: 电力安全系统被配置为在飞行器中提供电力信息。 电力安全系统包括具有电力需求指示器和功率可用指示器的电力安全仪器，每个都位于显示器上。 所需电源指示灯和电源指示灯的位置表示执行悬停飞行操作所需的电力和功率。 电力安全系统可以在飞行计划模式或当前飞行模式下操作。 电力安全系统使用至少一个传感器来测量对所需功率和可用功率有影响的变量。

    Hovering Surveillance Air Vehicle
    97.
    发明申请
    Hovering Surveillance Air Vehicle 审中-公开
    悬停监控机动车

    公开(公告)号：US20140284422A1

    公开(公告)日：2014-09-25

    申请号：US13848443

    申请日：2013-03-21

    Applicant: Itzhak Sapir

    Inventor： Itzhak Sapir

    IPC: B64B1/00

    CPC classification number: B64B1/24 ,  B64B1/40 ,  B64B1/62 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/121 ,  B64C2201/123

    Abstract: A hovering surveillance device. An electronic imaging device is disposed on a housing having a primary lift element, at least one compressed lighter-than-air gas element, a pitch adjustment element, and, a steering element. The compressed lighter-than-air gas is channeled to the primary lift element and the pitch adjustment element to selectively vary the altitude and angle for the housing such that scene of interest may be imaged. The lighter-than-air gas may be selected from the group of helium, hydrogen, heated air, neon, ammonia, and methane.

    Abstract translation: 悬停监视装置。 电子成像装置设置在具有主提升元件的壳体上，至少一个压缩的轻质空气气体元件，俯仰调节元件和转向元件。 压缩的轻型空气气体被引导到主提升元件和俯仰调节元件以选择性地改变壳体的高度和角度，使得可以对感兴趣的场景进行成像。 轻于空气的气体可以选自氦气，氢气，加热空气，氖气，氨气和甲烷。

    Remotely-guided vertical take-off system and method for delivering an ordnance to a target
    99.
    发明授权
    Remotely-guided vertical take-off system and method for delivering an ordnance to a target 有权
    远程引导的垂直起飞系统和向目标传送弹药的方法

    公开(公告)号：US08314374B2

    公开(公告)日：2012-11-20

    申请号：US11455709

    申请日：2006-06-20

    Applicant: Burak Uzman

    Inventor： Burak Uzman

    IPC: F41G7/20 ,  F41G7/24 ,  F41G7/30

    CPC classification number: F42B12/365 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/122 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  F41G7/30 ,  F42B15/01 ,  F42B15/10 ,  G05D1/0038

    Abstract: A lightweight, man-portable weapon delivery system includes a fuselage, and first and second wings mounted to opposing sides of the fuselage. The system includes an electric motor for driving a propeller for providing thrust to propel the system. The electric motor is mounted to the fuselage, and configured to be remotely started by a user. The system includes an imaging device mounted to the system and configured to capture images of a theater of operations of the system. The system includes a communication circuit in communication with the imaging device and configured to transmit the images from the imaging device to the user for viewing the theater of operations of the system for remotely steering the system. The communication circuit is configured to receive commands from the user for steering the system into the target. The system includes a payload configured to store the ordnance.

    Abstract translation: 轻便的便携式武器传送系统包括机身，以及安装在机身相对两侧的第一和第二翼。 该系统包括用于驱动螺旋桨以提供推力以推动系统的电动马达。 电动机安装在机身上，并被配置为由用户远程启动。 该系统包括安装到系统并被配置为捕获系统的操作剧场的图像的成像装置。 该系统包括与成像装置通信的通信电路，并且被配置为将图像从成像装置传输到用户，以观看用于远程转向系统的系统的操作剧场。 通信电路被配置为从用户接收命令以将系统转向目标。 系统包括配置为存储军械的有效载荷。

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