天线反射器复合材料轻量化研究
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TB3

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国家863高科技发展计划(2015AA03A201);上海市经信委产学研(沪CXY-2013-8)


Reduction of Weight of Antenna Reflector Using Lightweight Composite
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    摘要:

    采用树脂基复合材料代替铝合金材料研制反射器满足天线反射器减重要求,并建立反射器3D模型,通过有限元软件分别对铝合金以及复合材料反射器的模态进行分析。结果表明:在保持相同体积的条件下,复合材料反射器基频比铝合金反射器高出35.23%,减轻41.2%;为了保证星载反射器在服役环境中的精度,对两种材料反射器在-180~+80℃的热变形进行仿真。结果显示:采用[0/45/-45/90]2S铺层设计的反射器热变形量比铝合金反射器低94.25%;采用模压工艺研制的复合材料反射器型面精度为0.027 mm,满足使用要求,并且在服役环境下,复合材料型面精度稳定性优于铝合金反射器。

    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.

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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.

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  • 收稿日期:2017-05-11
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  • 在线发布日期: 2017-08-03
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