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1. 发明申请

US20140361938A1 MULTI-ELEVATIONAL ANTENNA SYSTEMS AND METHODS OF USE 有权
标题翻译：多功能天线系统及其使用方法
公开(公告)号：US20140361938A1
公开(公告)日：2014-12-11
申请号：US13915418
申请日：2013-06-11
申请人： Elwha, LLC
发明人： William D. Duncan , Roderick A. Hyde , Jordin T. Kare , Lowell L. Wood, JR.
IPC分类号： H01Q1/30 , H01Q1/28
CPC分类号： H01Q1/30 , H01Q1/285
摘要： The present disclosure provides systems and methods associated with an antenna system comprising a tension member configured to be towed by an aerial platform. In some embodiments, a first end of the tension member may be secured to the aerial platform and the second end may extend unsecured from the aerial platform at a different elevation than the first end. A plurality of antenna assemblies, each comprising at least one antenna, may be secured to and spaced along the length of the tension member. Each of the plurality of antennas may be adapted for use with a particular frequency or frequency bandwidth. For example, each of the plurality of antennas may be adapted or tuned for one or more frequencies useful for synthetic aperture radar (SAR). In some embodiments, a receiving system, a communication link, and/or an antenna location system may be utilized.
摘要翻译：本公开提供了与天线系统相关联的系统和方法，该天线系统包括构造成被空中平台牵引的张紧构件。在一些实施例中，张紧构件的第一端可以固定到空中平台，并且第二端可以以不同于第一端的高度从空中平台延伸出来。每个包括至少一个天线的多个天线组件可以固定到张力构件的长度上并与之隔开。多个天线中的每一个可以适于与特定频率或频率带宽一起使用。例如，可以针对用于合成孔径雷达（SAR）的一个或多个频率来适配或调整多个天线中的每一个。在一些实施例中，可以使用接收系统，通信链路和/或天线定位系统。

2. 发明申请

US20110162573A1 TOWED ANTENNA SYSTEM AND METHOD 有权
标题翻译：天线系统和方法
公开(公告)号：US20110162573A1
公开(公告)日：2011-07-07
申请号：US12797545
申请日：2010-06-09
申请人： Roger E. Race , Jacob C. Piskura , Davis S. Sanford
发明人： Roger E. Race , Jacob C. Piskura , Davis S. Sanford
IPC分类号： B63G8/00 , B63G8/42 , B63B21/66 , H01Q1/34
CPC分类号： H01Q1/04 , B63B2203/00 , B63G8/38 , H01Q1/30 , H01Q1/34
摘要： A towable antenna system is deployable and retrievable from and tetherable to an underwater vehicle while the underwater vehicle is submerged under water. An underwater vehicle having a towable antenna system is capable of communicating with one or more remote communication systems, the towable antenna system acting as an intermediary for communications between a submerged underwater vehicle and the one or more remote communication systems.
摘要翻译：一种可拖曳的天线系统是可展开的，并且可以从水下航行器收拢并连接到水下航行器，同时水下航行器淹没在水下。具有可拖曳天线系统的水下航行器能够与一个或多个远程通信系统进行通信，所述可拖曳天线系统充当淹没水下航行器与一个或多个远程通信系统之间的通信的中介。

3. 发明授权

US07830150B2 Helicopter electromagnetic prospecting system 有权
标题翻译：直升机电磁勘探系统
公开(公告)号：US07830150B2
公开(公告)日：2010-11-09
申请号：US11587887
申请日：2005-04-19
申请人： Philip Samuel Klinkert
发明人： Philip Samuel Klinkert
IPC分类号： G01V3/16 , H01Q1/30
CPC分类号： H01Q1/28 , H01Q1/30
摘要： An airborne electromagnetic prospecting system (10) is disclosed. The system (10) comprises a transmitter loop structure (12) hat is attached to, and arranged to be towed by, a helicopter (14). A transmitter (22) is fitted to the transmitter loop structure (12) for transmitting a primary electromagnetic field. A high drag bird (26) is attached to, and arranged to be towed by, the transmitter loop structure (12). A receiver (38) is fitted to the high drag bird (26) for receiving a primary and secondary resulting electromagnetic field, the secondary field arising from the interaction of the primary field with ground conductors that are traversed by the helicopter (14). Significantly, the high drag bird (26) is also attached to, and arranged to be towed by, the helicopter (14), so as to keep the position of the receiver (38) relative to the transmitter (22) substantially constant.
摘要翻译：公开了一种机载电磁勘探系统（10）。系统（10）包括发射机环路结构（12），帽子附接到并被安排成由直升机（14）拖曳。发射机（22）被安装到发射机环路结构（12）上，用于发射主电磁场。高阻力鸟（26）附接到发射机环路结构（12）并被布置成被发射机环路结构（12）拖曳。接收器（38）装配到高阻力鸟（26），用于接收主要和次要产生的电磁场，所述次级场是由直升机（14）穿过的主场与接地导体的相互作用产生的。重要的是，高拖曳鸟（26）也附接到并被布置成被直升机（14）拖曳，以便使接收器（38）相对于发射器（22）的位置基本上恒定。

4. 发明授权

US06683555B2 Fast deploy, retrievable and reusable airborne counter-measure system 有权
标题翻译：快速部署，可检索和可重用的机载对抗系统
公开(公告)号：US06683555B2
公开(公告)日：2004-01-27
申请号：US10105716
申请日：2002-03-25
申请人： Mark A. Carlson , James J. Jordan , John Russotti
发明人： Mark A. Carlson , James J. Jordan , John Russotti
IPC分类号： H01Q1514
CPC分类号： B64D3/02 , F41J2/00 , F41J9/10 , G01S7/021 , H01Q1/30
摘要： A fast deployment and retrieval system permits the rapid deployment of a decoy in seconds in response to an incoming threat, thus eliminating the necessity of pre-deployment, with retrieval permitting reeling in and deployment of the decoy a number of times during a mission in response to threats, and a commensurate reduction in life cycle cost. Upon detection of an incoming threat by a warning receiver, a controller coupled to a transmission releases a brake that is utilized to control the speed of deployment, whereas upon retrieval, the transmission drives a motor for retrieval of the decoy. The system is thus reusable, fast reacting, and also minimizes range penalty considerations because the decoy is only deployed when needed. In one embodiment, the system accommodates both a towing cable and a fiber-optic signal cable in which apparatus for unwinding of the cables is mechanically ganged together so that the cables pay out at the same rate. This type of payout lowers the stress on the fragile fiber-optic cable making possible multiple deployments and retrievals in response to separate threats during a mission. In another embodiment, a single, structural member with embedded conductors is utilized to connect the towed device to the round assembly.
摘要翻译：快速的部署和检索系统允许在几秒钟内快速部署诱饵以响应传入的威胁，从而消除了预部署的必要性，通过检索允许在响应任务期间多次堕落和部署诱饵威胁，并相应降低生命周期成本。在通过警告接收器检测到进入的威胁时，耦合到传输器的控制器释放用于控制部署速度的制动器，而在检索时，变速器驱动用于检索诱饵的马达。因此，只有在需要的时候部署诱饵才能使系统重复使用，快速反应，同时也减小了距离惩罚的考虑。在一个实施例中，系统容纳牵引电缆和光纤信号电缆，其中用于电缆解开的装置机械地组合在一起，使得电缆以相同的速率支付。这种类型的支付降低了脆弱的光纤电缆的压力，从而可以在任务期间响应单独的威胁进行多次部署和检索。在另一个实施例中，使用具有嵌入导体的单个结构构件将拖曳装置连接到圆形组件。

5. 发明授权

US06348891B1 Far field monitor apparatus 有权
标题翻译：远场监视装置
公开(公告)号：US06348891B1
公开(公告)日：2002-02-19
申请号：US09630275
申请日：2000-08-01
申请人： Toshimi Uemura
发明人： Toshimi Uemura
IPC分类号： G01S116
CPC分类号： G01S1/16 , G01S1/024 , H01Q1/30 , H01Q3/34 , H01Q21/28
摘要： In a far field monitor apparatus, each of first and second ILS localizers includes a receiving antenna, a plurality of couplers, a combiner, a receiver, and a first detector. The receiving antenna is formed from a plurality of antenna elements symmetrically arranged in a direction perpendicular to the longitudinal direction of a runway. The receiving antennas of the first and second ILS localizers oppose each other. The couplers are arranged in units of antenna elements to pick up some of signals obtained by the antenna elements in a predetermined amplitude and phase. The combiner combines output signals from the couplers. The receiver receives a combined signal output from the combiner. The first detector detects, on the basis of a receiving signal output from the receiver, a predetermined monitor parameter representing the radiation state of a radio wave radiated from the opposing-side ILS localizer.
摘要翻译：在远场监视装置中，第一和第二ILS定位器中的每一个包括接收天线，多个耦合器，组合器，接收器和第一检测器。接收天线由沿着与跑道的纵向方向垂直的方向对称配置的多个天线元件形成。第一和第二ILS定位器的接收天线彼此相对。耦合器以天线元件为单位布置，以便以预定的幅度和相位拾取由天线元件获得的一些信号。组合器组合了耦合器的输出信号。接收器接收从组合器输出的组合信号。第一检测器基于从接收器输出的接收信号检测表示从相对侧ILS定位器辐射的无线电波的辐射状态的预定监视参数。

6. 发明授权

US5326040A Sphere and cable deployer 失效
标题翻译：球形和电缆部署器
公开(公告)号：US5326040A
公开(公告)日：1994-07-05
申请号：US51336
申请日：1993-04-23
申请人： Richard E. Kramer
发明人： Richard E. Kramer
IPC分类号： H01Q1/30 , B65H75/40
CPC分类号： H01Q1/30
摘要： A sphere and cable deployer apparatus for deploying a cable and associated sphere from a vehicle such as a satellite. The sphere and cable deployer apparatus has a drum for storing the cable that is driven by a drive shaft and gears form a drive motor to deploy the cable/sphere away. The drive motor also drives a drive roller through a series of gears and clutches that applies tension to the cable as it is being unwound from the drum. The sphere and cable deployer apparatus also has a sphere housing with two shell-like halves that pivot outward due to spring forces to release the sphere. The pivoting housing halves also provide a storage compartment for a short cable that is attached to the outer surface of the sphere. The pivoting housing halves are held in place by two cables that are under tension and associated pins that fit in holes in the housing halves and are released by cable cutters that cut the cables.
摘要翻译：用于从诸如卫星的车辆部署电缆和相关球体的球体和电缆部署器装置。球和电缆部署器设备具有用于存储由驱动轴驱动的电缆的鼓，齿轮形成驱动马达以将电缆/球体部署。驱动电机还通过一系列齿轮和离合器来驱动驱动辊，当从滚筒展开时，离合器对电缆施加张力。球和电缆部署器装置还具有球壳，其具有两个壳状半部，其由于弹力而向外枢转以释放球体。枢转壳体半部还提供用于连接到球体的外表面的短电缆的存储隔间。枢转壳体半部通过处于张力处的两根电缆和相关销钉保持在适当的位置，所述电缆适配于壳体半部中的孔中并且由切割电缆的电缆切割器释放。

7. 发明授权

US4743916A Method and apparatus for proportional RF radiation from surface wave transmission line 失效
标题翻译：来自地面波传输线的比例射频辐射的方法和装置
公开(公告)号：US4743916A
公开(公告)日：1988-05-10
申请号：US813049
申请日：1985-12-24
申请人： Greg A. Bengeult
发明人： Greg A. Bengeult
IPC分类号： H01Q1/30 , H01Q13/20 , H01Q13/00 , H01Q1/36
CPC分类号： H01Q13/20 , H01Q1/30
摘要： In a system for launching RF energy as a traveling surface wave onto a single wire transmission line and causing such energy to be radiated away from the line at a downstream location, a series of window radiators of annular shape are spaced along the line, coaxial therewith, each for radiating a portion of the surface wave energy. Each radiator has a conductive component that causes decoupling and radiation of a portion of the RF energy, and a dielectric window that allows the remaining portion of RF energy to pass therethrough and continue, as an attached surface wave, downstream to a succeeding, similarly formed radiator where the decoupling and partial radiation occurs again. Thus, from the same surface wave transmission line system, it is possible to radiate RF energy from two or more discrete locations along the line.
摘要翻译：在用于将射频能量作为行进表面波发射到单线传输线上并使得能量在下游位置从线路辐射的系统中，一系列环形的窗口辐射器沿着该线与其同轴地间隔开每个用于辐射表面波能量的一部分。每个散热器具有导致部分RF能量的去耦和辐射的导电部件，以及允许RF能量的剩余部分通过其中并作为附着表面波继续下游的介电窗口，其类似地形成散热器再次发生去耦和部分辐射。因此，从相同的表面波传输线系统，可以沿着线从两个或更多个离散位置辐射RF能量。

8. 发明授权

US4335469A Method and system for radiating RF power from a trailing wire antenna 失效
标题翻译：用于从拖尾天线辐射RF功率的方法和系统
公开(公告)号：US4335469A
公开(公告)日：1982-06-15
申请号：US160354
申请日：1980-06-18
申请人： Nelson B. Tharp , Harry F. Hartley
发明人： Nelson B. Tharp , Harry F. Hartley
IPC分类号： H01Q1/30
CPC分类号： H03H7/38 , H01Q1/30
摘要： A trailing wire antenna coupling and control method for providing maximum voltage limited power output from power amplifiers of a high power low frequency RF transmitter system while varying the inductance of the coupling circuit to present a high resistance load having practically zero reactance to the power amplifiers, all during extension and retraction of the antenna toward and from its optimum length, as well as at the optimum length.
摘要翻译：一种拖线式天线耦合和控制方法，用于在改变耦合电路的电感以提供对功率放大器具有几乎零电抗的高电阻负载的同时，提供从大功率低频RF发射机系统的功率放大器输出的最大电压限制功率，在天线向着和从其最佳长度延伸和缩回时以及在最佳长度处都是这样。

9. 发明授权

US3522609A Airborne antenna coupled to adjustable helical counterpoise 失效
标题翻译： AIRBORNE天线与可调节的螺旋式反应器相结合
公开(公告)号：US3522609A
公开(公告)日：1970-08-04
申请号：US3522609D
申请日：1968-07-23
申请人： ROBERT ELLIS
发明人： ELLIS ROBERT
IPC分类号： H01Q1/30
CPC分类号： H01Q1/30

10. 发明授权

US3487412A Trailing antenna for aircraft 失效
标题翻译：航空天线
公开(公告)号：US3487412A
公开(公告)日：1969-12-30
申请号：US3487412D
申请日：1966-09-15
申请人： ROGERS WILLIAM C
发明人： ROGERS WILLIAM C
IPC分类号： H01Q1/30
CPC分类号： H01Q1/30

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