高韧性高性能QY9511双马来酰亚胺树脂(Ⅱ)

1.北京航空工艺研究所,100024

2.北京航空工艺研究所,100024

HIGH TOUGHNESS AND HIGH PERFORMANCE QY9511 BISMALEIMIDE RESIN(Ⅱ)

本文详细地论述了QY9511双马来酰亚胺的增韧改性原理、浇铸体性能、复合材料性能以及结果评价.

[1]	赵渠森.先进复合材料树脂体系648环氧[M].London,1986
[2]	赵渠森;李玉华;曹正华;孙冬生.QY8911双马来酰亚胺树脂[A].,1989
[3]	Jeon JY.;Tak TM. .SYNTHESIS AND CHARACTERIZATION OF POLYIMIDE DERIVATIVES PREPARED BY DIFFERENT ONE-STEP METHODS[J].Journal of Applied Polymer Science,1996(2):371-382.
[4]	日本东丽公司碳纤维资料[Z].,1998.
[5]	赵渠森;王京城.QY8911-Ⅲ韧性双马来酰亚胺树脂[J].航空工艺技术,1997(01)
[6]	Jack Boyd.New Generation Bismaleimide for aircraft primary structure[A].,1995
[7]	BrianP. Rice.Fracture Characterization of toughened Bismaleimide/ Graphite composites[A].,1990
[8]	Jack D. Boyed.Bismaleimide composites advanced high- temperature applications[A].,1993

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