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    • 21. 发明申请
    • Orientation adjusting apparatus for a satellite antenna set with fine tuning units
    • 具有微调单元的卫星天线组的定向调整装置
    • US20050264467A1
    • 2005-12-01
    • US11114329
    • 2005-04-26
    • Hung-Yuan LinSan-Yi Kuo
    • Hung-Yuan LinSan-Yi Kuo
    • H01Q1/00H01Q1/08H01Q1/12H01Q3/02H01Q3/08
    • H01Q3/08H01Q1/125
    • An orientation adjusting apparatus includes a support base plate set rotatable relative to a mast about a first vertical axis. An azimuth bracket is rotatable relative to the top plate of support base plate set about a second vertical axis. An elevation bracket is rotatable relative to an elevation fine tune bracket about a first horizontal axis. The elevation fine tune bracket is rotatable relative to the azimuth bracket about a second horizontal axis. An azimuth angle fine tuning unit is operable to rotate the azimuth bracket relative to the top plate of support base plate set about the second vertical axis. An elevation angle fine tuning unit is operable to rotate the elevation fine tune bracket relative to the azimuth bracket about the second horizontal axis.
    • 一种定向调节装置,包括:一个相对于桅杆围绕第一垂直轴线旋转的支撑基板组件。 方位支架可相对于围绕第二垂直轴线设置的支撑基板的顶板旋转。 高度支架相对于围绕第一水平轴线的高度微调支架可旋转。 高度微调支架相对于方位角支架围绕第二水平轴线是可旋转的。 方位角微调单元可操作以使方位支架相对于围绕第二垂直轴线的支撑基板的顶板旋转。 仰角微调单元可操作以围绕第二水平轴相对于方位支架旋转升高微调支架。
    • 23. 发明授权
    • Orientation adjusting device for a satellite antenna
    • 卫星天线方位调整装置
    • US07164391B2
    • 2007-01-16
    • US11170231
    • 2005-06-28
    • Hung-Yuan LinSan-Yi Kuo
    • Hung-Yuan LinSan-Yi Kuo
    • H01Q3/02
    • H01Q1/125
    • An orientation adjusting device includes a base unit, a bracket unit, and an angle-adjusting mechanism. The bracket unit is coupled pivotally to the base unit. The angle-adjusting mechanism includes first and second rotatable units and first and second pivot joints. The first pivot joint interconnects the bracket unit and the first rotatable unit so as to permit rotation of the first rotatable unit relative to the bracket unit about a first horizontal axis. The second pivot joint interconnects the base unit and the second rotatable unit so as to permit rotation of the second rotatable unit relative to the base unit about a second horizontal axis parallel to the first horizontal axis. The telescopic unit interconnects the first and second rotatable units, and is operable so as to vary the distance between the first and second horizontal axes.
    • 定向调节装置包括基座单元,支架单元和角度调节机构。 支架单元枢转地联接到基座单元。 角度调节机构包括第一和第二可旋转单元以及第一和第二枢转接头。 第一枢转关节使托架单元和第一可旋转单元相互连接,以允许第一可旋转单元相对于托架单元围绕第一水平轴线旋转。 第二枢转关节使基部单元和第二可旋转单元相互连接,以允许第二可旋转单元相对于基部单元围绕平行于第一水平轴线的第二水平轴线旋转。 伸缩单元将第一和第二可旋转单元互连,并且可操作以改变第一和第二水平轴之间的距离。
    • 24. 发明申请
    • Orientation adjusting device for a satellite antenna
    • 卫星天线方位调整装置
    • US20060181477A1
    • 2006-08-17
    • US11170231
    • 2005-06-28
    • Hung-Yuan LinSan-Yi Kuo
    • Hung-Yuan LinSan-Yi Kuo
    • H01Q1/08
    • H01Q1/125
    • An orientation adjusting device includes a base unit, a bracket unit, and an angle-adjusting mechanism. The bracket unit is coupled pivotally to the base unit. The angle-adjusting mechanism includes first and second rotatable units and first and second pivot joints. The first pivot joint interconnects the bracket unit and the first rotatable unit so as to permit rotation of the first rotatable unit relative to the bracket unit about a first horizontal axis. The second pivot joint interconnects the base unit and the second rotatable unit so as to permit rotation of the second rotatable unit relative to the base unit about a second horizontal axis parallel to the first horizontal axis. The telescopic unit interconnects the first and second rotatable units, and is operable so as to vary the distance between the first and second horizontal axes.
    • 定向调节装置包括基座单元,支架单元和角度调节机构。 支架单元枢转地联接到基座单元。 角度调节机构包括第一和第二可旋转单元以及第一和第二枢转接头。 第一枢转关节使托架单元和第一可旋转单元相互连接,以允许第一可旋转单元相对于托架单元围绕第一水平轴线旋转。 第二枢转关节使基部单元和第二可旋转单元相互连接,以允许第二可旋转单元相对于基部单元围绕平行于第一水平轴线的第二水平轴线旋转。 伸缩单元将第一和第二可旋转单元互连,并且可操作以改变第一和第二水平轴之间的距离。
    • 25. 发明授权
    • Housing of satellite receiver and method for forming the same
    • 卫星接收机的壳体及其形成方法
    • US07459994B2
    • 2008-12-02
    • US11307473
    • 2006-02-09
    • Yung-Chin ChenHung-Yuan LinSan-Yi Kuo
    • Yung-Chin ChenHung-Yuan LinSan-Yi Kuo
    • H01P5/12
    • H01Q13/0283
    • Since gaps generated when assembling a high-frequency satellite receiver interrupt reception of satellite signals, accurate assembly or reduction in number of parts for assembly reduces interruption of reception of satellite signals. A signal feeding portion, a circuit board containing portion, and a signal output portion of a high-frequency satellite receiver extend from a first side of a main body of the high-frequency satellite receiver, so that the main body, the signal feeding portion, the circuit board containing portion, and the signal output portion are monolithically formed together, thereby preventing gaps resulting from assembly from affecting the reception of satellite signals.
    • 由于在组装高频卫星接收机中断接收卫星信号时产生的间隙,用于组装的部件的精确组装或减少减少了卫星信号的接收中断。 高频卫星接收机的信号馈送部分,电路板容纳部分和信号输出部分从高频卫星接收机的主体的第一侧延伸,使得主体,信号馈送部分 ,电路板容纳部分和信号输出部分一体地形成在一起,从而防止组装所产生的间隙影响卫星信号的接收。
    • 26. 发明申请
    • HOUSING OF SATELLITE RECEIVER AND METHOD FOR FORMING THE SAME
    • 卫星接收机的壳体及其形成方法
    • US20070139136A1
    • 2007-06-21
    • US11307473
    • 2006-02-09
    • Yung-Chin ChenHung-Yuan LinSan-Yi Kuo
    • Yung-Chin ChenHung-Yuan LinSan-Yi Kuo
    • H01P5/12
    • H01Q13/0283
    • Since gaps generated when assembling a high-frequency satellite receiver interrupt reception of satellite signals, accurate assembly or reduction in number of parts for assembly reduces interruption of reception of satellite signals. A signal feeding portion, a circuit board containing portion, and a signal output portion of a high-frequency satellite receiver extend from a first side of a main body of the high-frequency satellite receiver, so that the main body, the signal feeding portion, the circuit board containing portion, and the signal output portion are monolithically formed together, thereby preventing gaps resulting from assembly from affecting the reception of satellite signals.
    • 由于在组装高频卫星接收机中断接收卫星信号时产生的间隙,用于组装的部件的精确组装或减少减少了卫星信号的接收中断。 高频卫星接收机的信号馈送部分,电路板容纳部分和信号输出部分从高频卫星接收机的主体的第一侧延伸,使得主体,信号馈送部分 ,电路板容纳部分和信号输出部分一体地形成在一起,从而防止组装所产生的间隙影响卫星信号的接收。