宇航材料工艺2011，Vol.41Issue(3)：31-33,37,4.
大型复合材料筒形结构自动铺带技术
Automated Tape Placement in Large Composite Cylinder Structure
张蕾 1王俊锋 1刘伟 1熊艳丽 1范佳1
作者信息
- 1. 航天材料及工艺研究所,北京,100076
- 折叠
摘要
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 or ovedaps. 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°. NondesUuctive testing of the composite cylinder and test of mechanical and physical perfonnance 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.关键词
自动铺带/筒形结构/复合材料Key words
Automated tape placement/ Cylinder structure / Composite引用本文复制引用
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):31-33,37,4.
