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作 者:张旭辉 谢英姿[2] 张泽旭[1,2] 张灵玉 胡振英 侯卫权 ZHANG Xu-hui;XIE Ying-zi;ZHANG Ze-xu;ZHANG Ling-yu;HU Zhen-ying;HOU Wei-quan(Xi'an Chaoma Technology Co.,Ltd.,Xi'an 710025,China;Xi'an Aerospace Composite Materials Research Institute,Xi'an 710089,China)
机构地区:[1]西安超码科技有限公司,西安710025 [2]西安航天复合材料研究所,西安710089
出 处:《炭素》2018年第4期12-16,41,共6页Carbon
摘 要:以高温炉用料架研制为目标,设计并制备了炭/炭复合材料料架。产品采用针刺炭布、网胎交替叠层的预制体,优化组合预制体中结构单元,经气相、液相相结合的致密方法增密后,再经高温处理、机械加工后得到炭/炭复合材料料架。本文对炭/炭复合材料料架的微观形貌、热学性能和力学性能进行了分析,并对料架的载荷进行了核定。该料架可与产品一起经历惰性气氛2000℃以上高温处理过程,解决目前无适宜高温炉用料架的现状。The carbon-carbon frame used for high temperature furnace was prepared by processing a needle-punched carbon fiber preform which was stacked by non-weave yarn cloth and felt, and deposited in a chemical vapor deposition and resin impregnation process. The carbon-carbon composites frame was heat-treated in the high temperature furnace and then machined. The SEM images,thermal properties and mechanics properties of carbon-carbon composite frame were studied.The results show that the carboncarbon composite frame can bear over 2000℃ high temperature with products.This C/C frame solved the loading problem for the products which must be treated in high temperature furnace.
分 类 号:TQ165[化学工程—高温制品工业]
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