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    LENS ANTENNA SYSTEM
    3.
    发明公开
    LENS ANTENNA SYSTEM 有权
    LINSENANTENNENSYSTEM

    公开(公告)号：EP1589611A4

    公开(公告)日：2006-03-22

    申请号：EP03703100

    申请日：2003-01-30

    申请人： SUMITOMO ELECTRIC INDUSTRIES ,  TOSHIBA CARRIER CORP

    发明人： KURODA MASATOSHI ,  KISHIMOTO TETSUO ,  OGAWA TAKAYA

    IPC分类号： H01Q1/42 ,  H01Q3/08 ,  H01Q3/14 ,  H01Q3/16 ,  H01Q15/08 ,  H01Q15/14 ,  H01Q19/06 ,  H01Q19/10

    CPC分类号： H01Q1/42 ,  H01Q3/08 ,  H01Q3/14 ,  H01Q3/16 ,  H01Q15/08 ,  H01Q15/14 ,  H01Q19/062 ,  H01Q19/104

    摘要： A small and compact lens antenna system in which a radio wave having a large incident angle from a circulating satellite as well as a geostationary satellite can be received without reducing the gain by combining a hemispherical lens and a reflector as one kind of Luneberg type antenna so that a radiator receives radio wave while converging. The lens antenna system comprises a lens antenna body (10) including a reflector (13) and a hemispherical lens (14) composed of a laminate of dielectric material mounted rotatably on a base plate (11) while being protected entirely with a radome (17) and radiators (16a, 16b) movable to an arbitrary position along a guide rail (15), and a reflector supporting means (20) capable of inclining the reflector (13) in an arbitrary direction on a base (21), wherein the incident angle of radio wave from a satellite can be adjusted to a desired range by inclining the reflector (13).

    摘要翻译： 一种紧凑型透镜天线组件A，其是包含半球形透镜和反射板的Luneberg透镜天线，以便将进入的无线电波会聚在馈电上，并且可以从不仅地球静止卫星或具有高增益的轨道卫星接收无线电波 即使进入的无线电波的入射角大也包括透镜天线体10，其包括基板11，反射板13和通过层叠电介质材料制成的半球透镜14。 板13和透镜14可旋转地安装在基板11上。天线体还包括可沿着导轨15移动到期望位置的馈送器16a和16b。天线组件还包括安装在反射板支撑装置20上的反射板支撑装置20 在基座21上并且能够使反射板13沿期望的方向倾斜。 通过倾斜反射板13，来自卫星的无线电波的入射角度可调整到预定范围内的值。

    SCANNING DIRECTIONAL ANTENNA WITH LENS AND REFLECTOR ASSEMBLY
    4.
    发明公开
    SCANNING DIRECTIONAL ANTENNA WITH LENS AND REFLECTOR ASSEMBLY 审中-公开
    SCANNING-RICHTANTENNE MIT LINSE UND REFLEKTORBAUGRUPPE

    公开(公告)号：EP1509970A4

    公开(公告)日：2005-09-21

    申请号：EP02807452

    申请日：2002-05-16

    申请人： EMS TECHNOLOGIES INC

    发明人： ZIMMERMAN KURT ALAN ,  WANN JOHN ELLIOTT ,  FREEMAN ROBERT ALLEN ,  BLACK DONALD NELSON JR ,  MARSIK JAMES CHARLES

    IPC分类号： H01Q17/00 ,  H01Q3/14 ,  H01Q3/16 ,  H01Q3/20 ,  H01Q19/06 ,  H01Q19/10

    摘要： An antenna comprising a feed (42) for delivering electromagnetic energy to a rotatable combination of a dielectric lens (44) and a reflective surface (46). The combination of the dielectric lens and the reflective surface is placed proximate to and in front of an energy feed, such as a horn (42), to support the scanning of an antenna beam in response to rotation of the lens/reflective surface assembly. The lens typically comprises a dielectric material and the reflective surface can comprise a thin layer of material operable to reflect electromagnetic energy. For example, the lens can comprise a half-cylinder shape of dielectric material and the reflective surface can be applied to the flat portion of the half-cylindrical lens. Alternatively, the antenna can comprise two or more electromagnetic feeds (72a, 72b, 72c, 72d) and a cylindrical lens of dielectric material including a centrally embedded, two-sided reflective surface. A positioning system can be used to rotate the combination of the lens and the reflective material proximate to and in front of the electromagnetic feed(s).

    摘要翻译： 一种包括馈送器（42）的天线，用于向电介质透镜（44）和反射表面（46）的可旋转组合传送电磁能。 介质透镜和反射表面的组合放置在能量馈源（例如喇叭（42））附近并位于其前面，以响应于透镜/反射表面组件的旋转而支持天线光束的扫描。 透镜通常包括电介质材料并且反射表面可以包括可操作以反射电磁能量的薄层材料。 例如，透镜可以包括半圆柱形状的介电材料，并且反射表面可以被应用于半圆柱形透镜的平坦部分。 或者，天线可以包括两个或更多个电磁馈电（72a，72b，72c，72d）以及包括中心嵌入的双面反射表面的介电材料的柱面透镜。 可以使用定位系统来旋转靠近电磁馈送器和电磁馈送器前方的透镜和反射材料的组合。

    FUNKGERÄT MIT BEWEGLICHER ANTENNE
    5.
    发明公开
    FUNKGERÄT MIT BEWEGLICHER ANTENNE 失效
    与手机天线RADIO

    公开(公告)号：EP0986835A1

    公开(公告)日：2000-03-22

    申请号：EP98933443.8

    申请日：1998-05-06

    申请人： ROBERT BOSCH GMBH

    发明人： HOFFMEISTER, Markus ,  GRUNEWALD, Jörg

    IPC分类号： H01Q1/24 ,  H04B1/38 ,  H04M1/02 ,  H01Q3/16 ,  H01Q3/18

    CPC分类号： H01Q1/24 ,  H01Q3/16 ,  H01Q3/18 ,  H04M1/0202

    摘要： The invention relates to a radio device (1) which allows for a more flexible antenna. The inventive radio device (1) comprises a housing (5) with a listening device (15) on a first side (10) and an antenna element (25) on a second side (20), said second side being opposite said first side (10). The antenna element (25) is positioned on the second side (20) of the housing (5) in such a way that it can move. Said antenna element (25) has a directional radiation characteristic in at least one first position (31, 32, 35, 36) and an omnidirectional radiation characteristic in at least one second position (33, 34, 37, 38).

    Tensioned cord attachement of antenna reflector to inflated support structure
    6.
    发明公开
    Tensioned cord attachement of antenna reflector to inflated support structure 失效
    Gespannte Seilbefestigung eines Antennenreflektors mit einer aufblasbaren Struktur

    公开(公告)号：EP0977308A1

    公开(公告)日：2000-02-02

    申请号：EP98305677.1

    申请日：1998-07-16

    申请人： HARRIS CORPORATION

    发明人： Bibb, Allen

    IPC分类号： H01Q15/16 ,  H01Q1/42 ,  H01Q3/16

    CPC分类号： H01Q15/163 ,  H01Q1/288

    摘要： The antenna has an inflatable support structure (80) to which a reflective material surface (60) is attached by a tensionable attachment arrangement allowing deployment of the reflector from, for example, a space vehicle (90). The reflective surface (60) is for energy incident from an antenna feed horn (65). Upon being inflated, the support structure places the attachment arrangement (70) in tension and causes the reflective surface (60) to acquire an intended reflective surface geometry, e.g. a parabolic mesh surface. The inflatable support structure (80) is transparant to energy and is formed either as a toroid (80) surrounding the reflective surface (60) or as an elliptical or spherical balloon (30) enveloping the reflective surface (10 in Fig.1). The antenna is used in airborne and spaceborne applications and has the advantage that the antenna reflector is insensitive to variations in pressure, the intended antenna profile does not change and the energy gathering and focussing properties are not impaired.

    摘要翻译： 天线具有可膨胀的支撑结构（80），反射材料表面（60）通过可张紧的附接布置附接到该支撑结构（80），从而允许来自例如空间飞行器（90）的反射器的展开。 反射表面（60）用于从天线馈电喇叭（65）入射的能量。 在充气时，支撑结构将附接装置（70）放置在张紧状态，并使反射表面（60）获得预期的反射表面几何形状，例如， 抛物面网格表面。 可膨胀支撑结构（80）透射能量并且形成为围绕反射表面（60）的环形（80）或形成为包围反射表面（图1中的10）的椭圆形或球形气球（30）。 该天线用于机载和空间应用中，并且具有天线反射器对压力变化不敏感的优点，预期的天线轮廓不改变，并且能量聚集和聚焦特性不受损害。