摘要
用简单的ｎ级动力学反应模型模拟高性能湿法成型用的环氧树脂配方的固化反应，并且利用ＤＳＣ技术检测了其整个固化反应的实际状态，比较了相应的理论预测与实验结果，实验证明采用优化固化温度和操作条件时其树脂力学性能得到明显的提高。
Curing reaction of high performance epoxy formula for wet filament winding is simulated basing on simple n stage model of dynamics, and differential scanning calorimetry (DSC) technique is used to monitor its whole curing process. Experimental results showed that mechanical properties of this resin system cured at the optimized curing temperature and operation condition are obviously improved.
出处
《固体火箭技术》
EI
CAS
CSCD
1998年第3期64-67,共4页
Journal of Solid Rocket Technology
关键词
环氧树脂
固化
缠绕结构
航空
复合材料
航天
Epoxy resin Curing Differential thermal analysis Winding structure technology
