宇航材料工艺2018，Vol.48Issue(1)：37-43,7.DOI:10.12044/j.issn.1007-2330.2018.01.007
共熔法制备超高温陶瓷基复合材料
Ultra-High Ceramic Matrix Composites Made by Eutectic Method
杨金华 1刘占军 2郭全贵3
作者信息
- 1. 中国航发北京航空材料研究院,先进复合材料国防科技重点实验室,北京100095
- 2. 中国航发北京航空材料研究院,航空材料先进腐蚀与防护航空科技重点实验室,北京100095
- 3. 中国科学院山西煤炭化学研究所,中国科学院炭材料重点实验室,太原030001
- 折叠
摘要
Abstract
Ultra-high temperature ceramic matrix composites were firstly made by eutectic method.The composites were made from ZrB2 and flake graphite,ZrB2,TaB2,SiC and flake graphite,or ZrB2,MoSi2 and flake graphite,respectively.Results shows that different phases distribute uniformly in these composites,and the graphite phases in the composites were highly ordered.The d002 values of the graphite in the composites were 0.335 4,0.335 9 and 0.337 7 nm,and the Lc values were 63.4,51.5 and 68.7 nm,respectively.Boron had already doped into the carbon net,as indicated by the Raman analysis,and some amount of pores existed in the composites.Also,thermal conductivity coefficient of the composites were not very high.Eutectic method could be a promising method for making ultra-high temperature ceramic matrix composites.关键词
二硼化锆/超高温陶瓷/陶瓷基复合材料/共熔Key words
ZrB2/Ultra-high ceramics/Ceramic matrix composites/Eutectic分类
通用工业技术引用本文复制引用
杨金华,刘占军,郭全贵..共熔法制备超高温陶瓷基复合材料[J].宇航材料工艺,2018,48(1):37-43,7.
