玻璃钢/复合材料 ›› 2008, Vol. 203 ›› Issue (1): 21-24.

• 材料研究 • 上一篇    下一篇

RFI工艺成型碳NCF/环氧5228A复合材料研究

  

  • 出版日期:2008-01-28 发布日期:2008-01-25

STUDY ON CARBON FIBER NCF/EPOXY 5228A COMPOSITES FORMED BY RFI PROCESS

  • Online:2008-01-28 Published:2008-01-25

摘要:

借助流变仪和差示扫描量热仪分析5228A环氧树脂膜的性能,以此为参考制定树脂膜渗透成型工艺(RFI)的固化制度|制备并测试增强材料为T700-12k碳纤维无屈曲织物(NCF)、铺层方式为[(0,90)/(±45)]s的层合板力学性能,其层间剪切强度比相应的无纬布层合板高25.3%|在层合板研究的基础上成功研制了规格为1000×200×37mm的帽形梁|利用超声波无损检测和金相显微检查等手段检测帽形梁的质量,检测结果显示,帽形梁材质致密、内部无明显缺陷,将应用于某型号卫星主承力结构。研究表明,5228A环氧树脂膜具有良好的工艺性,RFI工艺能够应用于复合材料复杂结构件的制造。

关键词: 无屈曲织物, 树脂膜渗透成型工艺, 力学性能, 帽形梁

Abstract:

The properties of epoxy film 5228A are analyzed by using rheometer and differential scanning calorimetry(DSC).Curing system of resin film infusion is set,based on the results.Laminates are formed,which is reinforced by T700-12k carbon fiber non crimp fabric(NCF) and ply orientation is [(0,90)/(±45)]s.The mechanical properties of laminates are tested.The interlaminar shear strength is 25.3% higher than that of prepreg laminate.A hat-shape beam is successfully fabricated,which dimension is 1000×200×37mm.The quality of beam is inspected with ultrasonic non destructive test(NDT) and metalloscope.The results validate that the beam is compact and non-defective.It will be utilized in a primary structure of satellite.The research shows that epoxy film 5228A has a good processibility,and RFI is suitable for manufacturing complex composite material parts.

Key words: non crimp fabric(NCF), resin film infusion(RFI), mechanical properties, hat-shape beam