宇航材料工艺2012，Vol.42Issue(4)：55-57,3.
共固化复合材料/铝蜂窝夹层结构性能
Properties of Co-Curing Composite Panel/Aluminium Honeycomb Sandwich Structure
潘玲英 1孙宏杰 1尹亮 1林娜 1杨智勇1
作者信息
- 1. 航天材料及工艺研究所,北京 100076
- 折叠
摘要
Abstract
Composite panel/aluminium sandwich structure was fabricated by the co-curing process. The effect of processing pressure on the properties of composite panel was investigated to determine the co-curing pressure. The properties of aluminium honeycomb with different dimension parameter and their sandwich structures were also tested and analyzed. The results show that the processing pressure has little effect on the properties of thin composite panel. The sandwich structure fabricated by the aluminium honeycomb of 0. 04 mm×4 mm has high specific strength and modulus, and is easier to fabricate. Therefore, it has more widely potential applications.关键词
共固化/复合材料/铝蜂窝/夹层结构/性能Key words
Co-curing/ Composite/ Aluminium honeycomb/ Sandwich structure/ Property引用本文复制引用
潘玲英,孙宏杰,尹亮,林娜,杨智勇..共固化复合材料/铝蜂窝夹层结构性能[J].宇航材料工艺,2012,42(4):55-57,3.
