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    Autonomous stratospheric unmanned airship
    261.
    发明授权
    Autonomous stratospheric unmanned airship 有权
    自主平流层无人飞艇

    公开(公告)号：US09004397B2

    公开(公告)日：2015-04-14

    申请号：US13817891

    申请日：2011-08-19

    Applicant: Bojan Pecnik

    Inventor： Bojan Pecnik

    IPC: B64B1/06 ,  B64B1/08 ,  B64B1/30 ,  B64B1/58

    CPC classification number: B64B1/08 ,  B64B1/06 ,  B64B1/30 ,  B64B1/58 ,  B64C2201/022 ,  B64C2201/122 ,  B64C2201/127

    Abstract: An autonomous stratospheric unmanned airship with an operating altitude from 5-22 km and with a multi-month operational cycle. Spheroid rigid geodesic frame of constant volume formed by a multitude of struts, with an outer envelope enclosing the frame defining the eigenfrequency spectrum of the airship above 20 Hz, with vibrational amplitudes between 0.1 and 1 cm. Independently controllable electrical propulsion units, attached to the frame in the horizontal plane passing through the center of mass, can change the direction and value of the thrust vector. Buoyancy is controlled with a system integrated inside the geodesic frame including buoyant fluid pressurized tanks, valves for the release of the buoyant fluid through the buoyant fluid conduit into the buoyant gas cell which fills the geodesic frame. Valves at the subsystem support platform enable ambient atmosphere to fill the internal volume of the frame not occupied by the buoyant gas cell.

    Abstract translation: 自主的平流层无人飞艇，运行高度为5-22公里，并具有多个月的运行周期。 具有恒定体积的球体刚性测地框架由多个支柱形成，外围包围框架，其限定了20Hz以上的飞艇的本征频谱，震动振幅在0.1和1cm之间。 独立可控的电动推进装置可以改变推力矢量的方向和值。 浮力由集成在测地框架内的系统控制，包括浮力流体加压罐，用于通过浮力流体导管将浮力流体释放到填充测地框架的浮力气室中的阀。 在子系统支撑平台上的阀门能够使环境气氛填充未被浮力气体池占据的框架的内部体积。

    High Altitude, Long Endurance, Unmanned Aircraft and Methods of Operation Thereof
    264.
    发明申请
    High Altitude, Long Endurance, Unmanned Aircraft and Methods of Operation Thereof 有权
    高海拔，长寿命，无人驾驶飞机及其操作方法

    公开(公告)号：US20140195150A1

    公开(公告)日：2014-07-10

    申请号：US13525045

    申请日：2012-06-15

    Applicant: Edward Oscar Rios

    Inventor： Edward Oscar Rios

    IPC: G01C21/00 ,  B64D43/00

    CPC classification number: B64C39/024 ,  B64C2201/122 ,  B64C2201/145 ,  B64D43/00 ,  B64D47/00 ,  G01C21/00 ,  G01S19/11 ,  G01S19/21 ,  G05D1/0022 ,  G05D1/0027 ,  G05D1/104 ,  H04B7/18504

    Abstract: Embodiments include one or more high altitude, long endurance (HALE) unmanned aircraft (110) capable of persistent station-keeping having one or more electromagnetic (IR/Visual/RF) sensor elements or suites (112, 337) for purposes of survey and/or signal gathering. Embodiments include one or more high altitude, long endurance (HALE) unmanned aircraft (110) capable of persistent station-keeping having a directable laser (331). Embodiments include a group of four or more high altitude, long endurance (HALE) unmanned aircraft (611-614) configured as GPS repeaters.

    Abstract translation: 实施例包括一个或多个能够持续驻留的具有一个或多个电磁（IR / Visual / RF）传感器元件或套件（112,337）的高空，长寿命（HALE）无人驾驶飞机（110），用于测量和 /或信号收集。 实施例包括能够持续驻留具有可定向激光（331）的一个或多个高空，长寿命（HALE）无人飞行器（110）。 实施例包括配置为GPS中继器的一组四个或更多的高空，长寿命（HALE）无人飞行器（611-614）。

    Unmanned aerial vehicle based sonar buoy
    265.
    发明授权
    Unmanned aerial vehicle based sonar buoy 有权
    无人机基于声纳浮标

    公开(公告)号：US08492692B2

    公开(公告)日：2013-07-23

    申请号：US13097394

    申请日：2011-04-29

    Applicant: Jeremy F. Fisher

    Inventor： Jeremy F. Fisher

    IPC: F42B12/56 ,  F42B15/01 ,  F42B15/08 ,  H04B1/59 ,  F42B15/00 ,  H04B1/00

    CPC classification number: F42B15/10 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/122 ,  B64C2201/165 ,  B64C2201/167 ,  B64C2201/201 ,  B64C2201/205 ,  F41F1/08 ,  F41F3/042

    Abstract: A sonar buoy includes a fuselage having a tube-like shape, one or more wings coupled to the fuselage, an engine coupled to the fuselage and operable to propel the sonar buoy through flight, and a guidance computer operable to direct the sonar buoy to a predetermined location. The sonar buoy further includes a sonar detachably coupled to the fuselage and forming at least a part of the fuselage, and a rocket motor detachably coupled to the fuselage. The one or more wings are operable to be folded into a position to allow the sonar buoy to be disposed within a launch tube coupled to a vehicle and to automatically deploy to an appropriate position for flight after the sonar buoy is launched from the launch tube. The rocket motor propels the sonar buoy from the launch tube and detaches from the fuselage after launch.

    Abstract translation: 声纳浮标包括具有管状形状的机身，耦合到机身的一个或多个翼，耦合到机身的发动机，并且可操作以通过飞行推进声纳浮标;以及引导计算机，其可操作以将声纳浮标引导到 预定位置。 声纳浮标还包括可拆卸地联接到机身并形成机身的至少一部分的声纳和可拆卸地联接到机身的火箭发动机。 一个或多个翼可操作以折叠到允许声纳浮标布置在联接到车辆的发射管内并且在从发射管发射声纳浮标之后自动部署到适当位置用于飞行的位置。 火箭发动机从发射管推进声纳浮标，并在发射后从机身分离。

    Remotely-guided vertical take-off system and method for delivering an ordnance to a target
    266.
    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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