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    • 71. 发明申请
    • Antenna apparatus
    • 天线装置
    • US20020140620A1
    • 2002-10-03
    • US09986291
    • 2001-11-08
    • MITSUBISHI DENKI KABUSHIKI KAISHA
    • Hidetaka YamauchiIchiro ShirokawaTomoaki Fukushima
    • H01Q003/02H01Q001/12
    • H01Q3/02H01Q3/08
    • There is disclosed an antenna apparatus used for satellite communication or the like and including an antenna rotating in an azimuth angle direction and an elevation angle direction, which can be miniaturized without using a slip ring for ensuring electrical connection between a stationary portion and a movable portion. A rotary member 3 is rotated by rotation of a motor 5 to rotate an antenna 11 about an azimuth axis. On the other hand, a motor 9 is rotated to rotate a rotary member 7, and a relative rotary shaft 14 is rotated by relative rotation between the rotary member 3 and the rotary member 7. The rotation of the relative rotary shaft 14 rotates the antenna 11 about an elevation angle axis by rotation transmission through a bevel gear 18 and a bevel gear 19.
    • 公开了一种用于卫星通信等的天线装置,并且包括在方位角方向和仰角方向上旋转的天线,其可以在不使用用于确保静止部分和可动部分之间的电连接的滑环的情况下小型化 。 旋转构件3通过马达5的旋转而旋转,以使天线11绕方位角旋转。 另一方面,马达9旋转以旋转旋转构件7,并且相对旋转轴14通过旋转构件3和旋转构件7之间的相对旋转而旋转。相对旋转轴14的旋转使天线 11通过锥齿轮18和锥齿轮19的旋转传递关于仰角轴。
    • 72. 发明授权
    • Reconfigurable antenna system
    • 可重构天线系统
    • US06456251B1
    • 2002-09-24
    • US09859546
    • 2001-05-17
    • Sudhakar Rao
    • Sudhakar Rao
    • H01Q128
    • H01Q19/12H01Q1/288H01Q3/02H01Q3/20H04B7/18515
    • A two-step method is used to reconfigure beams among different orbital slots for a satellite system. The satellite is biased at one or more orbital slots for a back-up mission, while it looks at the sub-satellite point for the primary mission. Body steering is achieved using pitch and roll biases. The main reflector of the antenna is gimballed in order to steer the beams to different locations for the back-up mission. Beam size is controlled through the use of different sized reflectors and by varying the feed size. Different sized beams are interleaved among multiple reflectors.
    • 使用两步法重新配置卫星系统的不同轨道时隙之间的波束。 卫星偏向于一个或多个轨道槽,用于后勤任务,同时它观察主要任务的副卫星点。 使用俯仰和倾斜偏压实现车身转向。 天线的主要反射器是gimballed,以便将梁转向不同的位置进行后备任务。 通过使用不同尺寸的反射器和改变进料尺寸来控制光束尺寸。 不同尺寸的光束在多个反射器之间交错。
    • 73. 发明授权
    • Loop antenna assembly
    • 环形天线组件
    • US06342861B1
    • 2002-01-29
    • US08931902
    • 1997-06-03
    • Daniel A. Packard
    • Daniel A. Packard
    • H01Q116
    • H01Q7/00H01Q1/16H01Q3/02H01Q3/12
    • A full-wave loop antenna assembly having unique mechanical stability and electromagnetic characteristics is disclosed. The antenna assembly is suitable for use in the High frequency and Very high frequency portions of the electromagnetic spectrum and is capable of supporting multiple driven and parasitic elements in a variety of configurations for multi-band operation. The assembly includes an upper load-bearing boom and a lower boom which may be load bearing, between which at least a part of the weight loads created by the driven and parasitic elements may be distributed. The assembly may also include a parasitic element, tuned as a reflector, which is considerably longer than other parasitic reflectors which are used with antennas of this type, thereby providing the desired directional characteristics over a wider range of frequencies than are obtained by other antennas of its type.
    • 公开了具有独特机械稳定性和电磁特性的全波环形天线组件。 天线组件适用于电磁频谱的高频部分和极高频部分,并且能够支持用于多频带操作的各种配置中的多个驱动和寄生元件。 该组件包括上部承载起重臂和可以是负载承载的下部起重臂,在该起重臂之间可以分配由驱动和寄生元件产生的重量负载的至少一部分。 组件还可以包括调谐为反射器的寄生元件,其比与这种天线一起使用的其它寄生反射器相当长,从而在比其它天线获得的更宽的频率范围内提供期望的方向特性 它的类型。
    • 76. 发明授权
    • Microstrip wide band antenna and radome
    • 微带宽带天线和天线罩
    • US06246368B1
    • 2001-06-12
    • US09155831
    • 1998-12-16
    • Douglas R B DemingDax CraigRobert E MunsonJoseph T Negler
    • Douglas R B DemingDax CraigRobert E MunsonJoseph T Negler
    • H01Q138
    • H01Q9/0407H01Q1/42H01Q3/02H01Q9/0471
    • A Radio Frequency (RF) microstrip antenna employs a planar or curved radiator element that is mounted or supported in spaced relation to a planar or curved ground plane element A RF feed is attached near one edge of the radiator element for receiving and/or transmitting RF signals; in a lobe that is substantially perpendicular to the ground plane element. The radiator element and the ground plane element are maintained in a converging inclined or tilted physical relationship. When a coaxial cable is employed as the antenna feed, the cable's outer insulation is secured to the ground plane element, the cable's center conductor extends away from the ground plane element to provide a signal feed to the radiator element and to provide physical support for one edge of the radiator element, and two insulator posts extend away from the ground plane element to provide support for the opposite edge of the radiator element. A two-piece, snap-together, radome is provided, wherein a bottom half nonmovably supports the feed line and ground plane member and adjustably supports the inclined radiating element, wherein a top half snap-fits to the bottom half and wherein the top half includes internal extenting tabs that engage edge portions of the ground plane member.
    • 射频(RF)微带天线采用平面或弯曲的散热器元件,其以平面或弯曲的接地平面元件的间隔的关系安装或支撑.RF馈送被附接在散热器元件的一个边缘附近,用于接收和/或发射RF 信号; 在基本垂直于接地平面元件的叶片中。 散热器元件和接地平面元件保持在会聚倾斜或倾斜的物理关系。 当使用同轴电缆作为天线馈电时,电缆的外部绝缘体固定到接地平面元件,电缆的中心导体远离接地平面元件延伸,以向散热器元件提供信号馈送并为一个 散热器元件的边缘,并且两个绝缘体柱远离接地平面元件延伸以为散热器元件的相对边缘提供支撑。 提供两件式的卡扣式雷达罩,其中底部半部不可移动地支撑进给线和接地平面构件并且可调节地支撑倾斜的辐射元件,其中上半部卡扣配合到下半部,并且其中上半部 包括接合平面构件的边缘部分的内部扩展突片。
    • 77. 发明授权
    • Suspension device
    • 悬挂装置
    • US06236376B1
    • 2001-05-22
    • US09333883
    • 1999-06-15
    • Göran Ors
    • Göran Ors
    • H01Q302
    • H01Q3/02
    • A suspension device for rotatable appliances, such as antennas, of the type which for rotation is connectible with a frame-mounted shaft which extends through a power operated disk or a similar antenna mounting and which, beyond the antenna mounting, has a free end mounted in a stationary part, which is capable of limited motion generated rated by insufficient concentricity between the antenna mounting and the shaft. An angle-transducing device is provided for said shaft. A connector is arranged adjacent to or round the shaft and directs components of force on the stationary part which have arisen owing to sufficient concentricity to merely displacement in the X-Y direction in a plane perpendicular to the shaft, by the connector being displaceably fixed in the X direction to the stationary part and displaceably fixed in the Y direction to the frame, or by the connector being displaceably fixed in the X direction to the shaft and displaceably fixed in the Y direction to the antenna mounting.
    • 用于可旋转的装置的悬挂装置,例如用于旋转的类型的天线,可与通过动力操作的盘或类似的天线安装件延伸的框架安装的轴连接,并且超过天线安装件具有自由端安装 在静止部分中,其能够由天线安装件和轴之间的不足的同心度产生额定的运动。 为所述轴提供角度转换装置。 连接器布置成与轴相邻或圆周布置,并且在垂直于轴的平面中由于足够的同心度而仅在XY方向上的位移而引起固定部分上的力分量,该连接器可移动地固定在X 方向移动到固定部分并且沿Y方向可移动地固定到框架上,或者通过连接器沿X方向可移动地固定到轴上并且沿着Y方向可移动地固定到天线安装件。
    • 78. 发明授权
    • Method and apparatus for radio frequency beam pointing
    • 射频指向的方法和装置
    • US06184825B2
    • 2001-02-06
    • US09342369
    • 1999-06-29
    • James W. WehnerRichard B. SherwoodEdward J. Simmons, Jr.
    • James W. WehnerRichard B. SherwoodEdward J. Simmons, Jr.
    • H01Q300
    • H01Q3/02
    • An RF beam pointing apparatus (500, 600) compensates for the effects of settling errors on antenna pointing. The beam pointing apparatus includes an attitude reference system (502, 528, 530, 534) generating an antenna attitude output from the satellite attitude. Also included is attitude comparison circuitry (528, 530), coupled to the attitude reference system, that includes an antenna pointing error output. Control circuitry (528, 530) is coupled to the attitude reference system (502, 528, 530, 534) and the attitude comparison circuitry (528, 530). The control circuitry (528,530) directs the attitude comparison circuitry (528, 530) to generate control error output signals in response to dynamic settling antenna pointing errors induced by a mechanical slew on the satellite. An electronic beam pointing system (500, 600) is provided to steer the antenna (544) in response to the antenna pointing error signals to reduce the dynamic settling antenna pointing errors to within a predetermined pointing accuracy for nominal operation (202).
    • RF射线指向装置(500,600)补偿天线指向的稳定误差的影响。 光束指向装置包括产生从卫星姿态输出的天线姿态的姿态参考系统(502,528,532,534)。 还包括耦合到姿态参考系统的姿态比较电路(528,530),其包括天线指向误差输出。 控制电路(528,530)被耦合到姿态参考系(502,528,534,534)和姿态比较电路(528,530)。 控制电路(528,530)引导姿态比较电路(528,530)响应于由卫星上的机械摆动引起的动态稳定天线指向误差而产生控制误差输出信号。 提供电子束指向系统(500,600)以响应于天线指向误差信号来引导天线(544),以将动态稳定天线指向误差降低到用于标称操作的预定指向精度(202)内。
    • 79. 发明授权
    • RV mounting for a satellite dish
    • RV安装卫星天线
    • US6124836A
    • 2000-09-26
    • US290191
    • 1999-04-13
    • John Stephen Rogers
    • John Stephen Rogers
    • H01Q1/12H01Q3/02
    • H01Q1/125H01Q1/1214H01Q3/02
    • In a collapsible roof mounting for orienting a satellite dish system from below, an upper channel-shaped formation arranged to present a dish-shaped component adjacent one end and an arm formation for the feed horn intermediately thereof and nestable within and interconnected to a lower channel-shaped formation adjacent the other end for swinging movement thereabove, a tubular shaft formation supporting the lower channel-shaped formation centrally thereof from below for rotation about a substantially upright axis, a displaceable linkage including a worm gear interconnected to the upper channel-shaped formation and a worm extending axially of the tubular shaft formation for swinging the upper channel-shaped formation upwardly from the nested disposition and reversely, a handle formation for the tubular shaft formation below the roof for imparting rotation thereto and a crank for the worm located below the handle formation for imparting displacement to the worm and worm gear.
    • 在用于从下方定向卫星天线系统的可折叠屋顶安装件中,布置成呈现邻近一端的碟形部件的上通道形状的形成物,并且用于其中间的馈电喇叭的臂形成并且可嵌套在下通道内并且互连到下通道 形状相邻的另一端用于在其上方摆动运动,一个管状轴结构,从下方中心地支撑下部通道形状,用于围绕基本上直立的轴线旋转;可移动联动装置,包括互连到上部通道形状的蜗轮 以及从所述管状轴结构轴向延伸的蜗杆,用于使所述上通道形状的结构从所述嵌套的配置向上摆动,并且反向地形成用于在所述顶部下方进行旋转的用于所述管状轴形成的手柄结构,以及用于所述蜗杆的曲柄, 手柄形成用于向蜗轮和蜗轮传递位移。