摘要
选用几种使纤维表面富碳的聚合物先驱体制做涂层纤维和陶瓷试件,测试其拉伸强度和弯曲强度,从而可以选择能使陶瓷材料增强的富碳界面原料体系,再通过正交实验优化出增强体、富碳界面、基体三者性能相匹配的陶瓷材料。为碳纤维增强陶瓷基复合材料性能优化做了有益的探索。
Polymer percursor the coated fibers with rich - carbon interphase were optimizde by means of tensile andfiexure test for the coated fibers and reinforced composites. A high performance ceramic composites was developed inwhich fibers, rich-carbon interphase and matrixs match .
出处
《宇航材料工艺》
CAS
CSCD
北大核心
1998年第3期36-39,共4页
Aerospace Materials & Technology