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天线反射器复合材料轻量化研究

董晓阳 郭金海 吴文平 史文锋 陈浩然

宇航材料工艺2017,Vol.47Issue(4):37-41,5.
宇航材料工艺2017,Vol.47Issue(4):37-41,5.DOI:10.12044/j.issn.1007-2330.2017.04.008

天线反射器复合材料轻量化研究

Reduction of Weight of Antenna Reflector Using Lightweight Composite

董晓阳 1郭金海 1吴文平 1史文锋 1陈浩然2

作者信息

  • 1. 上海复合材料科技有限公司,上海201112
  • 2. 南京航空航天大学,南京210016
  • 折叠

摘要

Abstract

In order to reduce antenna reflector weight,the aluminum alloy is replaced by resin composite.The 3D model of antenna reflector was designed.The model of antenna reflector with two kinds of material were simulated by finite element software.The results show that the composite antenna reflector fundamental frequency is 35.23% higher than that of aluminum alloy at the same volume and the weight reduces 41.2%.The thermal deformation of antenna reflector with two kinds of material were simulated at the temperature between-180℃ and +80℃,the composite reflector thermal deformation is 94.25% less than aluminum alloy while the plies are [0/45/-45/90]2s to the composite reflector root mean square (RMS) is 0.027 mm,the RMS stabilization of composite reflector is superior to aluminum alloy in deep space.

关键词

天线/反射器/复合材料/有限元/轻量化

Key words

Antenna/Reflector/Composite/Finite element/Lightweight

分类

通用工业技术

引用本文复制引用

董晓阳,郭金海,吴文平,史文锋,陈浩然..天线反射器复合材料轻量化研究[J].宇航材料工艺,2017,47(4):37-41,5.

基金项目

国家863高科技发展计划(2015AA03A201) (2015AA03A201)

上海市经信委产学研(沪CXY-2013-8) (沪CXY-2013-8)

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

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