航空材料学报2012，Vol.32Issue(6)：1-13,13.DOI:10.3969/j.issn.1005-5053.2012.6.001
发动机用耐高温聚酰亚胺树脂基复合材料的研究进展
Advance in High Temperature Polyimide Resin Matrix Composites for Aeroengine
包建文 1陈祥宝1
作者信息
- 1. 北京航空材料研究院先进复合材料重点实验室,北京100095
- 折叠
摘要
Abstract
Advance in thermosetting polyimide and its composites were reviewed. In the last forty years, many kinds of endcap reagent were fund to synthesis polyimide resin matrix for composites, and most of polyimide was endcaped by Nadic anhydride or PEPA anhydride. Many series of polyimide resin were developed to the service in 280-450℃ for aeroengine. Low-cost polyimide, high toughness polyimide and organic/inorganic hybrid polyimide will be the main directions of polyimide study in the future.关键词
发动机/热固性聚酰亚胺/碳纤维/复合材料Key words
aeroengine/thermosetting polyimide/carbon fiber/composites分类
航空航天引用本文复制引用
包建文,陈祥宝..发动机用耐高温聚酰亚胺树脂基复合材料的研究进展[J].航空材料学报,2012,32(6):1-13,13.
