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尺寸高稳定性复合材料桁架结构的研制

马立 杨凤龙 陈维强 齐卫红 李艳辉

航天器环境工程2016,Vol.33Issue(3):229-234,6.
航天器环境工程2016,Vol.33Issue(3):229-234,6.DOI:10.3969/j.issn.1673-1379.2016.03.001

尺寸高稳定性复合材料桁架结构的研制

Development of a high dimensional stable composite truss

马立 1杨凤龙 1陈维强 1齐卫红 2李艳辉2

作者信息

  • 1. 北京卫星制造厂
  • 2. 航天东方红卫星有限公司 北京 100094
  • 折叠

摘要

Abstract

A high dimensional stable composite truss used for a certain satellite is discussed in this paper. Through the material selection, the ply design, and the CTE test & analysis, a high precision composite truss is manufactured, and the thermal deformation of the truss is measured. It is shown that the high dimensional stable structure made of high modulus CFRP with micrometer level accuracy can be obtained through an appropriate ply design. Some suggestions are made for reducing the thermal deformation and improving the dimensional stability & measurement accuracy. It is the first successful practice of the high dimensional stable composite structure being used for the ultra-stable satellite platform.

关键词

尺寸高稳定性/复合材料/桁架/热膨胀系数/微变形测量

Key words

high dimensional stability/composite materials/truss/coefficient of thermal expansion(CTE)/micro- deformation measurement

分类

通用工业技术

引用本文复制引用

马立,杨凤龙,陈维强,齐卫红,李艳辉..尺寸高稳定性复合材料桁架结构的研制[J].航天器环境工程,2016,33(3):229-234,6.

基金项目

国家自然科学基金项目 ()

航天器环境工程

OACSTPCD

1673-1379

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