大型复合材料筒形结构自动铺带技术
DOI:
作者:
作者单位:

航天材料及工艺研究所

作者简介:

通讯作者:

中图分类号:

基金项目:


Automated Tape Placement in Large Composite Cylinder Structure
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    采用国产T300/605 热熔法预浸料,对大型复合材料筒形结构自动铺带技术进行了研究。通过对
    自动铺带角度的工艺优化,铺带角度进行微调,实现了复合材料筒形结构的满覆盖铺放。在此基础上进行了大
    型复合材料筒形结构的自动铺带工艺试验,对自动铺带工艺试验件进行无损检测及取样性能测试。结果表明:
    预浸料铺覆性良好,自动铺带成型的预浸带间隙或重叠臆1 mm,铺带角度与理论铺带角度偏差臆0. 2毅。试验
    件成型质量良好,自动铺带技术可以满足大型复合材料结构高质量成型需求。

    Abstract:

    Automated tape placement in large cylinder structure was studied with domestic T300/605 melting prepared prepreg. The ply angle was optimized to achieve the full scale laying in large cylinder structure,which would avoid the gap oroverlaps. On the basis of the optimization, the process experiment of large cylinder structure with automated tape placement was carried out and the result indicated that the adhesion of the prepreg tape was fit for automated tape placement.The gap or overlap between the tapes were less than 1mm and the error of ply angle was less than 0.2毅. Nondestructive testing of the composite
    cylinder and test of mechanical and physical performance was carried out.The result showed that the property of the composite cylinder was eligible,which indicated that automated tape placement satisfied the moulding of the large cylinder structure.

    参考文献
    相似文献
    引证文献
引用本文

张蕾 王俊锋 刘伟 熊艳丽 范佳.大型复合材料筒形结构自动铺带技术[J].宇航材料工艺,2011,41(3).

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2016-11-28
  • 出版日期: