碳化硅/碳化硅复合材料的面内剪切破坏行为和机械性能

Tianshan Li, Guoqiang Yu, Shihao Zhou, Zhikang Zheng, Xiguang Gao, Yingdong Song
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引用次数: 0

摘要

纤维增强陶瓷基复合材料,特别是SiC/SiC复合材料,具有轻质、高强、耐高温等特点,是航空航天飞行器构件的理想结构候选材料,面内剪切性能是表征材料力学性能和构件评估的重要指标之一,本文设计加工了面内剪切试件和试验装置及方法,研究了SiC/SiC陶瓷基纤维束复合材料在剪切力学行为下的力学性能和失效行为。结果表明,基体开裂和纤维断裂是主要的失效模式,试样剪切力-位移曲线存在两个明显的阶段,纤维断裂是试样应变的主要原因。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
In-plane shear failure behavior and mechanical properties of SiC/SiC Composites
Fiber-reinforced ceramic matrix composites, especially SiC/SiC composites, have the characteristics of lightweight, high strength, high-temperature resistance, etc., which are ideal structural candidates for aerospace vehicle components, in-plane shear performance is one of the important indicators to characterize the mechanical properties of materials and component assessment, this paper designs and processes the in-plane shear test pieces and test devices and methods to study the shear mechanical behavior under the mechanical properties and failure behavior of SiC/SiC ceramic-based fiber bundle composites are studied under shear mechanical behavior. The results show that matrix cracking and fiber fracture are the main failure modes, and there are two obvious phases in the specimen shear force-displacement curves, and fiber fracture is the main cause of strain in the specimen.
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