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高精度碳纤维复合材料副反射面天线制备工艺

张娟娟 李宗周 沈辉 刘图远 朱荣峰

宇航材料工艺2018,Vol.48Issue(3):47-50,4.
宇航材料工艺2018,Vol.48Issue(3):47-50,4.DOI:10.12044/j.issn.1007-2330.2018.03.010

高精度碳纤维复合材料副反射面天线制备工艺

Preparationof High Precision Carbon Fiber Composite (CFC)Secondary Reflector Antenna

张娟娟 1李宗周 2沈辉 3刘图远 3朱荣峰3

作者信息

  • 1. 上海复合材料科技有限公司,上海201112
  • 2. 上海航天树脂基复合材料工程技术研究中心,上海201112
  • 折叠

摘要

Abstract

The effects of selection of mold materials,processing of assembly and machining on the manufacturing of high precision CFC-made secondary reflector antenna were analyzed through researching the key assembly techniques,compared mold material,optimized assembly process and machining verification experiment.The results show that invar is an ideal mold material for the manufacturing of high precision CFC-made secondary reflector antenna.When the sandwich structure is assembled,adopting the in situ assembly technique for the external covering and individual adoption of the cellular around transitional region of the antenna covering can effectively avoid the poor surface accuracy of the antenna.A comprehensive application of an auxiliary mould for the machining and the 3D image measurement system can effectively ensure the high positional accuracy of the assembly reference point and significantly shorten the manufacturing period of the antenna.

关键词

高精度/副反射面天线/碳纤维复合材料/模具材料/原位装配/三维摄影测量

Key words

High precision/Secondary reflector antenna/Carbon fibre composites/In situ assembling/3D image measurement system

分类

通用工业技术

引用本文复制引用

张娟娟,李宗周,沈辉,刘图远,朱荣峰..高精度碳纤维复合材料副反射面天线制备工艺[J].宇航材料工艺,2018,48(3):47-50,4.

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

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