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41. 发明授权

US06720936B1 Adaptive antenna system 有权
标题翻译：自适应天线系统
公开(公告)号：US06720936B1
公开(公告)日：2004-04-13
申请号：US10142315
申请日：2002-05-09
申请人： Richard M. Koolish , Brig Barnum Elliott
发明人： Richard M. Koolish , Brig Barnum Elliott
IPC分类号： H01Q1502
CPC分类号： H01Q3/01 , H01Q15/147 , H01Q19/065
摘要： An adaptive antenna system (20) includes a programmable reflection surface (22), a controller (24) in communication wit the programmable reflection surface (22), and a feeder element (26) outwardly spaced from a receiving side (28) of the programmable reflection surface (22). The controller (24) is operable to write a pattern (34) of reflective (36) and absorptive (42) regions into the programmable reflection surface (22) in accordance with a frequency and a direction of a received or transmitted electromagnetic wave (32). The controller (24) is further operable to write patterns (68, 80) into the programmable reflection surface (22) to dynamically adjust adaptive antenna system (20) to changing frequencies and directions of transmitted and received electromagnetic waves.
摘要翻译：自适应天线系统（20）包括可编程反射表面（22），与可编程反射表面（22）通信的控制器（24）以及与所述可编程反射表面（22）的接收侧（28）向外间隔开的馈送元件可编程反射面（22）。控制器（24）可操作以根据接收或发射的电磁波的频率和方向（32）将反射（36）和吸收（42）区域的图案（34）写入可编程反射表面（22））。控制器（24）还可操作以将图案（68,80）写入可编程反射表面（22）以动态地调节自适应天线系统（20）以改变发射和接收的电磁波的频率和方向。

42. 发明申请

US20040004725A1 Measurement system for electromagnetic radiation structure 失效
标题翻译：电磁辐射结构测量系统
公开(公告)号：US20040004725A1
公开(公告)日：2004-01-08
申请号：US10401659
申请日：2003-03-28
发明人： Dimitry Gorinevsky , Tristram T. Hyde
IPC分类号： G01B009/02
CPC分类号： G01B11/24 , G02B26/06 , G02B26/0825 , H01Q3/01 , H01Q15/147 , H01Q19/00
摘要： A measurement system is provided that facilitates the measuring of a shape of a flexible electromagnetic radiation structure. The measurement system includes a plurality of local sensors, a central sensor and a measurement processor. Each of the plurality of local sensors is configured to sense the position of a portion of the flexible electromagnetic radiation structure. The central sensor is configured to determine an overall shape of the flexible electromagnetic radiation structure. The measurement processor provides the ability to combine sensor data from the local sensors and sensor data from the central sensor to provide an accurate measurement of the shape of the flexible electromagnetic radiation structure.
摘要翻译：提供了一种有助于测量柔性电磁辐射结构的形状的测量系统。测量系统包括多个本地传感器，中央传感器和测量处理器。多个本地传感器中的每一个被配置为感测柔性电磁辐射结构的一部分的位置。中央传感器被配置为确定柔性电磁辐射结构的整体形状。测量处理器提供将来自本地传感器的传感器数据和来自中央传感器的传感器数据组合以提供对柔性电磁辐射结构的形状的精确测量的能力。

43. 发明申请

US20030112201A1 Mirror surface accuracy measuring device and mirror surface control system of reflector antenna 失效
标题翻译：镜面精度测量装置和反射镜天线的镜面控制系统
公开(公告)号：US20030112201A1
公开(公告)日：2003-06-19
申请号：US10167417
申请日：2002-06-13
申请人： MITSUBISHI DENKI KABUSHIKI KAISHA
发明人： Tomohiro Mizuno
IPC分类号： H01Q001/42
CPC分类号： H01Q15/14 , H01Q15/141 , H01Q15/147 , H01Q19/30 , H01Q21/28
摘要： Radiation field distributions of all mirror panels composing a main reflector are measured and held in advance, radiation field distributions of a reflector antenna having the main reflector are measured by transmitting a radio wave from a collimation antenna arranged at a prescribed distance from the reflector antenna to the reflector antenna while changing an attitude of the reflector antenna, complex excitation coefficients of each mirror panel are calculated from the radiation field distributions of the mirror panels, the radiation field distributions of the reflector antenna and the attitudes of the reflector antenna, and mirror surface accuracy of the main reflector is calculated from the complex excitation coefficients of the mirror panels.
摘要翻译：测量并保持构成主反射器的所有镜面板的辐射场分布，具有主反射器的反射器天线的辐射场分布通过从布置在距反射器天线一定距离的准直天线发射无线电波来测量，反射器天线在改变反射器天线的姿态的同时，根据反射板的辐射场分布，反射天线的辐射场分布和反射器天线的态度以及镜面主反射器的精度由镜面板的复数激励系数计算。

44. 发明授权

US06255997B1 Antenna reflector having a configured surface with separated focuses for covering identical surface areas and method for ascertaining the configured surface 有权
标题翻译：具有配置表面的天线反射器，具有用于覆盖相同表面区域的分离焦点和用于确定配置表面的方法
公开(公告)号：US06255997B1
公开(公告)日：2001-07-03
申请号：US09455189
申请日：1999-12-06
申请人： Norbert Ratkorn , Michael Truemper , Christian Hunscher , Robert Sekora
发明人： Norbert Ratkorn , Michael Truemper , Christian Hunscher , Robert Sekora
IPC分类号： H01Q1910
CPC分类号： H01Q25/007 , H01Q15/147 , H01Q19/17 , H01Q19/195
摘要： A reflector for reflecting electromagnetic waves has a configured surface for these waves whereby localized deformations or configurations such as bumps (B) and dents (D) of the reflector (1) are so constructed that the reflector cooperates with several focuses (10A, 10B; 110A, 110B) which are spatially separated from the reflector proper. These focuses are so arranged that the electromagnetic beams emanating from the respective radiators (4A, 4B; 40A, 40B) and are directed onto the reflector can be directed through the reflector onto a common region (3A, 3B) to be illuminated, whereby particularly the beams may be tuned to different frequencies or for operation in different frequency bands. Such reflectors are particularly useful in antenna systems for communications such as satellite communications.
摘要翻译：用于反射电磁波的反射器具有用于这些波的配置表面，由此反射器（1）的局部变形或构造（例如凸块（B）和凹陷（D））被构造成使得反射器与多个焦点（10A，10B; 110A，110B），其与反射器本体在空间上分离。这些焦点被布置成使得从相应的辐射器（4A，4B; 40A，40B）发射并被引导到反射器上的电磁波束可以被引导通过反射器到公共区域（3A，3B）上以被照亮，波束可以调谐到不同的频率或在不同的频带中操作。这种反射器在诸如卫星通信的通信的天线系统中特别有用。

45. 发明授权

US6052095A Dual gridded reflector antenna 有权
标题翻译：双网格反射天线
公开(公告)号：US6052095A
公开(公告)日：2000-04-18
申请号：US267097
申请日：1999-03-10
申请人： Parthasarathy Ramanujam , Philip H. Law , Nancy Garcia , Daniel A. White
发明人： Parthasarathy Ramanujam , Philip H. Law , Nancy Garcia , Daniel A. White
IPC分类号： H01Q1/28 , H01Q15/14 , H01Q15/22 , H01Q19/13 , H01Q21/28 , H01Q25/00 , H01Q19/14
CPC分类号： H01Q21/28 , H01Q1/288 , H01Q15/147 , H01Q15/22 , H01Q19/132 , H01Q25/001 , Y10S343/02
摘要： An improved dual gridded reflector antenna configuration which allows cross-polarization radiation to be scanned in any given direction. The dual-gridded reflector assembly includes a front parabolic reflector illuminated by a first source, and a second parabolic reflector illuminated by a second source. The second reflector is positioned adjacent to and behind the front reflector such that the center points of the reflectors align to define a center axis. Additionally, the first and second sources are positioned at different offsets with respect to the reflectors and have a respective rotated offset angle with respect to the center axis such that the sources define an antenna feed separation. By modifying the offsets and the rotated offset angles, the feed separation can be designed to have an inclination with respect to the north-south or east-west feed separation direction.
摘要翻译：改进的双网格反射器天线配置，允许在任何给定方向上扫描交叉极化辐射。双网格反射器组件包括由第一源照射的前抛物面反射器和由第二源照射的第二抛物面反射器。第二反射器定位成与前反射器相邻并在其后面，使得反射器的中心点对准以限定中心轴线。此外，第一和第二源相对于反射器定位在不同的偏移处，并且相对于中心轴线具有相应的旋转偏移角，使得源限定天线馈送间隔。通过改变偏移量和旋转的偏移角度，进给分离可以被设计成相对于南北或东西方的进给分离方向具有倾斜度。

46. 发明授权

US5524524A Integrated spacing and orientation control system 失效
标题翻译：集成间距和方向控制系统
公开(公告)号：US5524524A
公开(公告)日：1996-06-11
申请号：US328255
申请日：1994-10-24
申请人： Les H. Richards , David J. Schorr , Mark J. Kelley , Philip L. McDuffie , Edward R. Coleman
发明人： Les H. Richards , David J. Schorr , Mark J. Kelley , Philip L. McDuffie , Edward R. Coleman
IPC分类号： F21S2/00 , F41H11/12 , F41H11/14 , H01Q15/14 , H01Q15/20 , F42B22/24
CPC分类号： F41H11/12 , F21S2/00 , F41H11/14 , H01Q15/147 , H01Q15/20
摘要： An integrated spacing and orientation control system is provided for carrying an array of objects and maintaining a predetermined orientation of the objects and a predetermined spacing between objects. In a presently preferred application, the spacing and orientation system carries an array of anti-mine munitions for clearing a path through a minefield. The invention deploys the anti-mine munitions in a downwardly pointed orientation with proper spacing between munitions, even when the array of munitions is deployed using rocket motors.
摘要翻译：提供了一种集成的间隔和取向控制系统，用于承载物体阵列并保持物体的预定取向和物体之间的预定间隔。在目前优选的应用中，间距和取向系统携带一系列防雷弹药，用于清除通过雷区的路径。本发明以反弹的方式将弹药以适当的间距向下定位，即使使用火箭发动机部署弹药阵列也是如此。

47. 发明授权

US5440320A Antenna reflector reconfigurable in service 失效
标题翻译：天线反射镜可重新配置使用
公开(公告)号：US5440320A
公开(公告)日：1995-08-08
申请号：US292607
申请日：1994-08-18
申请人： Olivier Lach , Serge Schenck
发明人： Olivier Lach , Serge Schenck
IPC分类号： H01Q15/14 , H01Q15/20
CPC分类号： H01Q15/147
摘要： An in-service reconfigurable antenna reflector having a rigid support structure, a deformable reflective surface having radio reflection properties and actuators operating on the deformable reflective surface to deform it. The reflective surface is elastically deformable with stiffness in bending and the actuators operate at control points of the deformable reflective surface, transversely thereto.
摘要翻译：一种在役可重新配置的天线反射器，其具有刚性支撑结构，具有无线电反射特性的可变形反射表面和在可变形反射表面上操作以使其变形的致动器。反射表面可弯曲地具有刚度弹性变形，并且致动器在可变形反射表面的横向于其处的控制点处操作。

48. 发明授权

US4845510A Reflector surface adjustment structure 失效
标题翻译：反光镜表面调整结构
公开(公告)号：US4845510A
公开(公告)日：1989-07-04
申请号：US83489
申请日：1987-08-10
申请人： Stanley S. Chang , Amilcar B. Ybarra-Rojas , Hui Bau
发明人： Stanley S. Chang , Amilcar B. Ybarra-Rojas , Hui Bau
IPC分类号： H01Q15/14 , H01Q3/20 , H01Q15/16
CPC分类号： H01Q15/16 , H01Q15/147
摘要： Rear and forward reflector shells or dishes (36,38) are independently supported on a dynamically rigid truss structure (12) by means of separate studs extending from the forward nodes of the truss to the two shells. Forward node (22) carries adjustable rear shell stud (52) and independently carries adjustable forward shell stud (80). Both of the studs have flat portions oriented normal to the radius of the shell so that radial shell expansion due to temperature and temperature differential minimize shell distortion.
摘要翻译：后部和前部反射器壳体或盘（36,38）通过从桁架的前部节点延伸到两个壳体的单独的螺柱独立地支撑在动态刚性的桁架结构（12）上。正向节点（22）承载可调节的后壳螺柱（52），并且独立地承载可调节的前壳螺柱（80）。两个螺柱具有垂直于壳体半径的平坦部分，使得由于温度和温度差异引起的径向壳体膨胀使壳体变形最小化。

49. 发明授权

US4811033A Antenna surface contour control system 失效
标题翻译：天线表面轮廓控制系统
公开(公告)号：US4811033A
公开(公告)日：1989-03-07
申请号：US118995
申请日：1987-11-10
申请人： Elvin L. Ahl , James B. Miller
发明人： Elvin L. Ahl , James B. Miller
IPC分类号： H01Q15/14 , H01Q15/16 , H01Q9/34
CPC分类号： H01Q15/147 , H01Q15/161 , Y10S343/02
摘要： The invention is a system for automatically controlling the surface contour of a deployable and restowable antenna 11 having a mesh reflector surface 26 supported by a circular, folding hoop 12 affixed to a central, telescoping column 14. The antenna 11, when deployed, forms a quad-aperture reflector with each quadrant A-D of the mesh surface 26 shaped to provide an offset parabolic RF reflector.The hoop 12 is supported and positioned by quartz support cords 12 attached to the top 22 of column 14 and by lower graphite hoop control cords 23 that extend between the hoop 12 and base 24 of the column 14. The antenna 11, an RF reflective surface 26, is a gold plated molybdenum wire mesh supported on a graphite cord truss structure that includes the hoop control cords and a plurality of surface control cords 27 attached at selected points on the surface 26 and to the base 24 of column 14. The contour of the three-dimensional surface 26 of the antenna 11 is controlled by selectively adjusting the lengths of the surface control cords 27 and the graphite hoop control cords 23 by means of novel actuator assemblies 56 that automatically sense and change the lengths of the lower hoop control cords 23 and surface control cords 27 to control the contour of the surface 26 of the antenna 11.
摘要翻译：本发明是一种用于自动控制可部署和可再生天线11的表面轮廓的系统，其具有由固定到中心伸缩柱14上的圆形折叠环12支撑的网状反射器表面26.天线11在展开时形成四孔径反射器，其网形表面26的每个象限AD成形为提供偏移的抛物面RF反射器。环12由附接到塔14的顶部22的石英支撑绳12和在柱14的环12和底座24之间延伸的下部石墨箍控制帘线23支撑和定位。天线11，RF反射表面 26是支撑在石墨帘线桁架结构上的镀金钼丝网，其包括环控制绳索和附接在表面26上的选定点和柱14的基座24上的多个表面控制帘线27.轮廓天线11的三维表面26通过新颖的致动器组件56选择性地调节表面控制线27和石墨箍控制绳23的长度来控制，该致动器组件56自动地感测并改变下环控制绳的长度 23和表面控制线27，以控制天线11的表面26的轮廓。

50. 发明授权

US4578680A Feed displacement correction in a space fed lens antenna 失效
标题翻译：空间馈送镜头天线中的进给位移校正
公开(公告)号：US4578680A
公开(公告)日：1986-03-25
申请号：US606325
申请日：1984-05-02
申请人： Randy L. Haupt
发明人： Randy L. Haupt
IPC分类号： H01Q1/12 , H01Q3/26 , H01Q3/46 , H01Q15/14 , H01Q3/36
CPC分类号： H01Q1/1264 , H01Q15/147 , H01Q3/2658 , H01Q3/46
摘要： A space fed microwave lens antenna for deployment in outer space or other remote, hazardous or unattended location. Electronic means are provided for compensating for errors in the mechanical displacement of the phased array feed elements from the phased array lens elements.
摘要翻译：空间馈送微波透镜天线，用于外部空间或其他远程，危险或无人值守的位置。提供电子装置用于补偿相控阵进给元件与相控阵透镜元件的机械位移误差。

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