摘要
对高熔点聚碳硅烷的合成反应条件进行了较为详细的研究,并通过改变化学反应的温度、压力和反应时间制备出了熔点高达380 ℃、数均分子量Mn > 3 000 、陶瓷收率达79 % ( 质量分数) 以上的陶瓷先驱体聚合物。该先驱体溶解性能好,并具有良好的纺丝性能。文中还利用IR、TG—DTA 等手段对该先驱体的热解机理进行了初步探讨。
A high melting point polycarbosilane was prepared by changing synthetic time, pressure and temperature. Its melting point of the polycarbosilane obtained is more than 380℃, its average molecular weight is more than 3 000,and its ceramic yield can reach 79% by weight. The polycarbosilane precursor can dissolve in solvents such as xylene and tuloene, and its solution has a good spinnality. The primary pyrolysis mechanism of the polycarbosilane was explored by IR and TG-DTA technique.
出处
《宇航材料工艺》
CAS
CSCD
北大核心
1999年第5期23-29,共7页
Aerospace Materials & Technology
关键词
高熔点
聚碳硅烷
热裂解机理
High melting point, Polycarbosilane ,Synthesis, Mechanism