摘要
本文研究了适合大型飞机典型结构件生产用热塑性聚醚酰亚胺树脂增韧改性的高韧性QY95 11双马来酰亚胺树脂的合成工艺、树脂性能及其与碳纤维T30 0、T70 0S、T80 0H预浸料及复合材料的工艺规范和力学性能。简述了QY95
This paper studies the synthesizing process,properties of QY9511 high toughness BIM resin modified with thermoplastic PEI,and the process specification and mechanical property improvement of T300,T700S and T800H prepreg and composites with QY9511 as resin matrix,the characteristic and application of QY9511 are also briefly described.
出处
《纤维复合材料》
CAS
2001年第4期3-9,共7页
Fiber Composites
