首页 | 本学科首页   官方微博 | 高级检索  
     检索      

热处理对C/ SiC 复合材料拉伸性能的影响
引用本文:王红琴 成来飞,梅 辉,张立同 方 鹏.热处理对C/ SiC 复合材料拉伸性能的影响[J].宇航材料工艺,2010,40(3).
作者姓名:王红琴 成来飞  梅 辉  张立同 方 鹏
作者单位:西北工业大学超高温结构复合材料国防科技重点实验室,西安,710072
基金项目:西北工业大学基础研究基金,国家自然科学基金国际合作项目 
摘    要:对等温化学气相渗透法(ICVI)制备的C/SiC复合材料进行热处理,利用声发射(AE)技术对热处理前后C/SiC试样拉伸过程声发射累积能量进行分析,通过SEM进行微结构观察。结果表明:界面层较薄的C/SiC试样经1 500℃热处理后拉伸强度与初始强度相近,经1 700和1 900℃热处理后拉伸强度显著提高,其断裂应变随着热处理温度升高而大幅提高,弹性模量却呈现下降趋势;界面层较厚的C/SiC试样经1 500和1 700℃热处理后拉伸强度变化不大,断裂应变显著提高,弹性模量逐渐降低,经1 900℃热处理后拉伸强度和断裂应变开始下降,而弹性模量变化较小。热处理可以显著提高C/SiC的韧性,在拉伸过程中的断裂功和声发射累积能量均显著增加。界面层较薄的C/SiC断裂模式从脆性逐渐向韧性转变,而界面层较厚的C/SiC热处理后韧性进一步提高。

关 键 词:C/SiC复合材料  热处理  拉伸性能  声发射

Effects of Heat Treatment on Tensile Properties of C/ SiC Composite
Wang Hongqin,Cheng Laifei,Mei Hui,Zhang Litong,Fang Peng.Effects of Heat Treatment on Tensile Properties of C/ SiC Composite[J].Aerospace Materials & Technology,2010,40(3).
Authors:Wang Hongqin  Cheng Laifei  Mei Hui  Zhang Litong  Fang Peng
Institution:National Key Laboratory of Thermostructure Composite Materials, Northwestern Polytechnical University
Abstract:C/ SiC composites fabricated by isothermal chemical vapor infiltration were heat treated. Acoustic emission (AE) was introduced to analyze the variations of AE accumulative energy during monotonic tensile test. The microstructures were examined by scanning electronic microscope (SEM). The results indicate that, for the thin interlayer C/SiC, its tensile strength is close to the initial one after heat treatment at 1 500 , but tensile strengths of the compositescan be increased after heat treatment at 1 700 and 1 900. With the increase of heat treatment temperature, tensile stresses increase significantly and modulus decrease gradually. For the thick interlayer C/ SiC, tensile strengths have little changes and tensile stresses increase obviously but modulus decrease gradually after heat treatment at 1 500 and 1 700, while tensile strength and strain begin to decrease but modulus has little change after the same heat treatment at 1 900. Heat treatment remarkably improves the toughness of C/ SiC composites. The fracture work and AE accumula tive energy increase obviously after heat treatment. For the composites with thin interlayer, the fracture mechanism varies from brittle mode to toughness one, and for the composites with thick interlayer, the toughness is further enhanced.
Keywords:C/ SiC composite  Heat treatment  Tensile properties  Acoustic emission
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《宇航材料工艺》浏览原始摘要信息
点击此处可从《宇航材料工艺》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号