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  4. 航空级复合材料层板的定域相变控制与增韧研究进展

中国材料进展, 2009, 28(6): 13-18.

航空级复合材料层板的定域相变控制与增韧研究进展

张明 1, , 安学锋 2, , 刘立朋 3, , 益小苏 4,

1.中航工业北京航空材料研究院,先进复合材料国家重点实验室,北京,100095

2.中航工业北京航空材料研究院,先进复合材料国家重点实验室,北京,100095

3.中航工业北京航空材料研究院,先进复合材料国家重点实验室,北京,100095

4.中航工业北京航空材料研究院,先进复合材料国家重点实验室,北京,100095

基金项目:   国家重点基础研究发展规划(973计划)(2003CB615604)   国家自然科学基金重大项目(10590356)   中航一集团公司创新基金(HZ-KJ2006005)  

关键词： 复合材料层压板 , 层间增韧 , 相结构控制

Research and Development of Phase Control and Toughening at the Interphase of Aeronautical Polymer Matrix Composites

航空飞行器要求损伤容限设计,因此要求其复合材料具有高的韧性.与目前国内外广泛采用的整体增韧树脂基体或插层改性所进行的研究不同,主要介绍了在"离位"增韧的概念下,以时间-温度-转变(Time Temperature Transition,TTT)图为手段开展的复合材料层板层间定域相结构控制和增韧研究进展,给出了典型"离位"增韧复合材料的层板的层间相结构和韧性性能,证明了"离位"增韧可普适地将各种树脂基体的航空级复合材料层板层间定域的相形貌调控为相反转、双连续的相结构,从而达到大幅提高复合材料韧性的目的.

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