会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 1. 发明申请
    • PORTABLE SATELLITE DISH ANTENNA SYSTEM
    • 便携式卫星天线系统
    • US20110090132A1
    • 2011-04-21
    • US12906714
    • 2010-10-18
    • Timothy John Conrad
    • Timothy John Conrad
    • H01Q19/12
    • H01Q1/08H01Q19/12
    • A lightweight, portable satellite dish antenna system having base and lid portions which can be configured relative to each other in carrying and deployed positions. The base and lid portions are substantially the same size and shape and have respective interior and exterior sides with the satellite dish antenna of the system pivotally mounted to the interior side of the lid portion. In the carrying position, the satellite dish antenna is retracted to align with the interior side of the lid portion and the lid and base portions are secured together with the interior sides thereof facing and abutting each other. In the deployed or operating position, the lid portion is inverted and placed atop the base portion with the exterior side of the lid portion and the interior side of the base portion facing and abutting one another on mating bearing surfaces extending about a central, vertical axis.
    • 一种轻质便携式卫星天线系统,其具有基座和盖部分,其可以相对于彼此配置在携带和展开位置。 基部和盖部分具有大致相同的尺寸和形状,并且具有相应的内侧和外侧,系统的卫星天线可枢转地安装在盖部分的内侧。 在携带位置,卫星天线收回以与盖部分的内侧对准,并且盖和基部固定在一起,其内侧面对并彼此邻接。 在部署或操作位置中,盖部分被倒置并放置在基部的顶部,盖部分的外侧和基部的内侧面对并相互邻接,所述配合的轴承表面围绕中心的垂直轴线 。
    • 3. 发明申请
    • STABILIZING MECHANISM FOR A DEPLOYED REFLECTOR ANTENNA IN A MOBILE SATELLITE ANTENNA SYSTEM AND METHOD
    • 移动卫星天线系统和方法中的部署反射器天线的稳定机制
    • US20090085826A1
    • 2009-04-02
    • US11863570
    • 2007-09-28
    • Timothy John Conrad
    • Timothy John Conrad
    • H01Q3/02H01Q1/08
    • H01Q1/08H01Q1/3216H01Q1/3275H01Q19/13
    • A stabilizing mechanism and method for a deployed reflector antenna in a mobile satellite system. The stabilizing mechanism has a pair of stabilizing devices with a first end of each stabilizing device connected on a rear support of the reflector antenna. The first ends are positioned on opposite sides of the rear support. A second end of each stabilizing device is connected to a tilt mechanism in the mobile satellite system. The pair of stabilizing devices forms a support angle about the centerline of the reflector antenna and with the tilt mechanism. The pair of stabilizer devices pushes against the opposite sides with a pre-load force when the reflector antenna is deployed to minimize deflection of the reflector antenna due to environmental forces.
    • 一种在移动卫星系统中部署的反射天线的稳定机构和方法。 稳定机构具有一对稳定装置,每个稳定装置的第一端连接在反射器天线的后支撑上。 第一端位于后支撑件的相对侧上。 每个稳定装置的第二端连接到移动卫星系统中的倾斜机构。 该对稳定装置形成围绕反射器天线的中心线和倾斜机构的支撑角。 当反射器天线被展开以使由于环境力的反射器天线的偏转最小化时,该对稳定器装置以预加载力推动相对侧。
    • 4. 发明申请
    • FOLDING FEED MECHANISM AND METHOD FOR A MOBILE SATTELITE SYSTEM
    • 折叠进料机构和移动智能系统的方法
    • US20090085825A1
    • 2009-04-02
    • US11863812
    • 2007-09-28
    • Timothy John Conrad
    • Timothy John Conrad
    • H01Q1/08H01Q1/12
    • H01Q1/3216H01Q1/08H01Q1/3275H01Q19/13
    • A folding feed for a mobile satellite system having a reflector antenna, a feed, and a feed arm. The feed arm carries the feed at its distal end. A pivot is provided between the distal end and the feed. A feed stop block, connected at the distal end, has first and second surfaces. When the mobile satellite system stows the antenna, the feed pivots to abut the first surface against the feed to hold the feed at a first set angle. When said mobile satellite system deploys the antenna, the feed pivots to abut the second surface against the feed to hold the feed at the second set angle. A spring connected between the feed arm and feed holds the second surface against the feed. The first angle is greater than the second angle to provide a low profile to the stowed antenna.
    • 用于具有反射器天线,馈送和馈送臂的移动卫星系统的折叠馈送。 进料臂在其远端承载进料。 在远端和进料之间提供枢轴。 在远端连接的进料止动块具有第一和第二表面。 当移动卫星系统收起天线时,进给器枢转以使第一表面抵靠进给以将进给保持在第一设定角度。 当所述移动卫星系统部署天线时,进给器枢转以使第二表面抵靠进给件邻接,以将进给保持在第二设定角度。 连接在进料臂和进料之间的弹簧使第二表面抵靠进料。 第一角度大于第二角度,以向收起的天线提供低轮廓。
    • 8. 发明授权
    • Stabilizing mechanism for a deployed reflector antenna in a mobile satellite antenna system and method
    • 移动卫星天线系统中部署的反射天线的稳定机制及方法
    • US07518569B1
    • 2009-04-14
    • US11863570
    • 2007-09-28
    • Timothy John Conrad
    • Timothy John Conrad
    • H01Q3/02H01Q1/08
    • H01Q1/08H01Q1/3216H01Q1/3275H01Q19/13
    • A stabilizing mechanism and method for a deployed reflector antenna in a mobile satellite system. The stabilizing mechanism has a pair of stabilizing devices with a first end of each stabilizing device connected on a rear support of the reflector antenna. The first ends are positioned on opposite sides of the rear support. A second end of each stabilizing device is connected to a tilt mechanism in the mobile satellite system. The pair of stabilizing devices forms a support angle about the centerline of the reflector antenna and with the tilt mechanism. The pair of stabilizer devices pushes against the opposite sides with a pre-load force when the reflector antenna is deployed to minimize deflection of the reflector antenna due to environmental forces.
    • 一种在移动卫星系统中部署的反射天线的稳定机构和方法。 稳定机构具有一对稳定装置,每个稳定装置的第一端连接在反射器天线的后支撑上。 第一端位于后支撑件的相对侧上。 每个稳定装置的第二端连接到移动卫星系统中的倾斜机构。 该对稳定装置形成围绕反射器天线的中心线和倾斜机构的支撑角。 当反射器天线被展开以使由于环境力的反射器天线的偏转最小化时,该对稳定器装置以预加载力推动相对侧。