首页> 外国专利> REFLECTOR ASSEMBLY FOR A SATELLITE ANTENNA CAPABLE OF IMPROVING THE EFFECTIVENESS AND PRODUCTIVITY OF A MANUFACTURING PROCESS BY INCREASING THE RIGIDITY OF A REFLECTOR AND A MANUFACTURING METHOD THEREOF

REFLECTOR ASSEMBLY FOR A SATELLITE ANTENNA CAPABLE OF IMPROVING THE EFFECTIVENESS AND PRODUCTIVITY OF A MANUFACTURING PROCESS BY INCREASING THE RIGIDITY OF A REFLECTOR AND A MANUFACTURING METHOD THEREOF

机译:卫星天线的反射器组件,可通过增加反射器的刚度和制造方法来提高制造过程的效率和生产率

摘要

PURPOSE: A reflector assembly for a satellite antenna and a manufacturing method thereof are provided to increase the rigidity of a reflector without increasing a dead load by combining a stiffening member with the edge of the reflector along the circumferential direction of the reflector.;CONSTITUTION: A reflector assembly(100) for a satellite antennas includes a reflector(110) and a stiffening member(120) with a parabola shape. The stiffening member is combined with the reflector in order to increase the rigidity of the reflector to stress which is added through an external shock. The reflector is formed into a parabola reflector used for a conventional satellite antenna. The reflector includes a bent part(115) in which an insertion space is formed. The bent part is formed in the edge of the reflector along the circumferential direction of the reflector. The bent part is combined with the stiffening member to increase the rigidity of the reflector.;COPYRIGHT KIPO 2012
机译:目的:提供一种用于卫星天线的反射器组件及其制造方法,以通过在反射器的圆周方向上结合加强构件和反射器的边缘来增加反射器的刚度而不增加静载荷。用于卫星天线的反射器组件(100)包括反射器(110)和具有抛物线形状的加强构件(120)。加强构件与反射器结合,以增加反射器对因外部冲击而增加的应力的刚度。该反射器形成为用于常规卫星天线的抛物线反射器。反射器包括在其中形成插入空间的弯曲部分(115)。弯曲部分沿着反射器的圆周方向形成在反射器的边缘中。弯曲部分与加强构件结合在一起,以提高反射镜的刚性。; COPYRIGHT KIPO 2012

著录项

  • 公开/公告号KR20110136357A

    专利类型

  • 公开/公告日2011-12-21

    原文格式PDF

  • 申请/专利权人 INTELLIAN TECHNOLOGIES INC.;

    申请/专利号KR20100056297

  • 发明设计人 SON MIN SON;

    申请日2010-06-15

  • 分类号H01Q15/16;H01Q1/28;

  • 国家 KR

  • 入库时间 2022-08-21 17:11:20

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