Damage morphology of C/C-SiC composites under impact tests

V. Srivastava
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引用次数: 1

Abstract

C/C-SiC composite is a fibre composite made of carbon fibre and a brittle ceramic matrix. This has the advantage to combine monolithic ceramic with a higher tolerance of damage and lower specific stress. Characteristically states of defects already arise during the production process, such as crack pattern, fable fibres / matrix bond, delamination and high porosity. Some of the defects are favoured in view of the damage tolerance necessary for the technical use, but make it difficult to evaluate the damage condition. The main advantage of carbon fibre reinforced silicon carbide (C/C-SiC) is the damage tolerant mechanical behaviour compared to monolithic ceramics. Fracture mechanics test were carried out on chevron notched bend specimens. The present study is aimed to qualitatively examine the damage surface of C/C-SiC composites by the use of Scanning Electron Microscope (SEM) with the change of impact load. For quality assurance reasons the development of micro crack pattern under different loading conditions was investigated. Low and high impact tests were performed on C/C-SiC composites before and after the conditioning at 1600°C temperature.
C/C- sic复合材料冲击损伤形貌
C/C- sic复合材料是由碳纤维和脆性陶瓷基体制成的纤维复合材料。它的优点是将单片陶瓷与更高的损伤容忍度和更低的比应力相结合。典型的缺陷状态在生产过程中已经出现,如裂纹模式、纤维/基体粘结、分层和高孔隙率。考虑到技术使用所必需的损伤容限,有些缺陷是有利的,但却给损伤状况的评估带来了困难。与单片陶瓷相比,碳纤维增强碳化硅(C/C- sic)的主要优点是具有损伤容忍度。对字形缺口弯曲试件进行了断裂力学试验。利用扫描电子显微镜(SEM)对C/C- sic复合材料的损伤表面随冲击载荷的变化进行定性研究。为了保证质量,研究了不同加载条件下微裂纹模式的发展情况。在1600℃温度下,对C/C- sic复合材料进行了预处理前后的低冲击和高冲击试验。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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