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Frame of Space Deployable Antenna Reflector

机译:空间可展开天线反射器框架

摘要

1. Technical Result Reducing mass of reflector frame, increase in radiophysical indices, safety of deployment and rigidity. 2. Essence A reflector frame comprises deployment elements 2 joined to the central unit 1, which consist of two interconnected portions 3 and 4. The portion 3 being located from the side of reflector 5 is made in the form of sheet rib and presents the form making portion, whereas the power portion 4 located from the back surface has the form of sheet rib or cable ties. The edge 9 of the working profile of the form making portion is reinforced or made in the form of flexible rod; the periphery ends 10 are also reinforced or made in the form of the rod. 3. Field of Application Radio engineering.
机译:1.技术成果减轻了反射镜架的重量,提高了放射性指标,部署的安全性和刚性。 2.本质反射器框架包括连接到中央单元1的展开元件2,其由两个相互连接的部分3和4组成。部分3从反射器5的侧面定位为片状肋,并呈现为形成部分,而从背面定位的电源部分4具有片状肋或束线带的形式。成型部分的工作轮廓的边缘9被增强或制成柔性杆的形式;外围端10也被加强或制成杆的形式。 3.应用领域无线电工程。

著录项

  • 公开/公告号GEP20022732B

    专利类型

  • 公开/公告日2002-03-11

    原文格式PDF

  • 申请/专利权人

    申请/专利号GE1999AP03701

  • 发明设计人 MEDZMARIASHVILI ELGUDJA;DATASHVILI LERI;

    申请日1999-10-25

  • 分类号H01Q15/20;

  • 国家 GE

  • 入库时间 2022-08-22 00:45:21

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