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单向碳/碳复合材料的蠕变内应力
引用本文:石英,李贺军.单向碳/碳复合材料的蠕变内应力[J].固体火箭技术,1995,18(4):59-62.
作者姓名:石英  李贺军
作者单位:西北工业大学碳/碳复合材料研究所
基金项目:国家自然科学基金,航空科学基金
摘    要:用应力降落法测定单向PAN基碳纤维T300增加热碳基复合材料在1900-2350℃蠕变内应力σ0,结果及分析表明,对单向C/C复合材料,σ0不是一个材料常数,而是温度T、初始力σs及结构因子S的函数,即σ0=σ0(t,σs,S)。

关 键 词:碳碳复合材料  蠕变  内应力  应力试验  航空材料

Creep Internal Stress of the Unidirection Carbon-Carbon Composite
Shi Rong, Li Hejun, Yang Zheng, Qiao Shengru, Liu Yinglou, Kang Mokuang.Creep Internal Stress of the Unidirection Carbon-Carbon Composite[J].Journal of Solid Rocket Technology,1995,18(4):59-62.
Authors:Shi Rong  Li Hejun  Yang Zheng  Qiao Shengru  Liu Yinglou  Kang Mokuang
Abstract:The creep internal stress ac of the unidirection C/C composite which consists of T300 carbon fiber (based on PAN precursor) as the reinforcement and pyrolytic carbon as the matrix is determinated by means of the stress drop method. Results and analysises show that o of the unidirection C/C composite isn't a constant but a function of the temperature T, start stress and structure factor S, i. e. o=o(T, o, S). For same type of meaterial with a same S and under constant start stress s, o=0. 086T+290. 6; and at a same temperature, o increases with increment of o. A viscoelasticity model based on the microstructure model of T300 carbon fiber/pyrolytic carbon unidirection composite is suggested and used for analyzing the physical nature of its creep internal stress. It is considered that o implicates that the interface takes a effect of impeding the creep and o is sensitive to the interface.
Keywords:Carbon carbon composite  Creep Internal stress  Stress testing Viscoelasticity  
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