平纹编织复合材料层合板静态压缩与压-压疲劳性能

TB332; 采用电液伺服疲劳试验机开展玻璃纤维平纹编织复合材料层合板的静态压缩和压-压疲劳性能实验.应力比为R=10,拟合出S-N曲线,基于疲劳实验过程中的刚度退化、能量耗散、循环蠕变与循环软化来表征疲劳损伤演化,结合扫描电子显微镜对断口形貌进行观察.结果表明:试件的条件疲劳极限为静态压缩强度的66.3%;通过双加权最小二乘法拟合的S-N曲线具有较高可信度;随着循环次数的增加,试件刚度逐渐下降,各峰值载荷下的能量耗散逐渐增加;在循环加载初期,试件表现出强烈循环蠕变现象,高峰值载荷作用下的试件表现出强烈循环软化行为;试件经过循环加载抵抗变形能力得到增强;断口观察到了基体开裂、纤维/基体界面脱粘...

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Published in航空材料学报 Vol. 42; no. 2; pp. 64 - 72
Main Authors 张铁纯, 杨晨晨, 王轩, 周春苹
Format Journal Article
LanguageChinese
Published 中国民航大学 航空工程学院, 天津 300300%航空工业济南特种结构研究所 高性能电磁窗航空科技重点实验室, 济南250023 01.04.2022
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ISSN1005-5053
DOI10.11868/j.issn.1005-5053.2021.000106

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Abstract TB332; 采用电液伺服疲劳试验机开展玻璃纤维平纹编织复合材料层合板的静态压缩和压-压疲劳性能实验.应力比为R=10,拟合出S-N曲线,基于疲劳实验过程中的刚度退化、能量耗散、循环蠕变与循环软化来表征疲劳损伤演化,结合扫描电子显微镜对断口形貌进行观察.结果表明:试件的条件疲劳极限为静态压缩强度的66.3%;通过双加权最小二乘法拟合的S-N曲线具有较高可信度;随着循环次数的增加,试件刚度逐渐下降,各峰值载荷下的能量耗散逐渐增加;在循环加载初期,试件表现出强烈循环蠕变现象,高峰值载荷作用下的试件表现出强烈循环软化行为;试件经过循环加载抵抗变形能力得到增强;断口观察到了基体开裂、纤维/基体界面脱粘、纤维断裂和分层四种失效模式;与疲劳断口相比,静态压缩断口表现出较大的分层损伤.
AbstractList TB332; 采用电液伺服疲劳试验机开展玻璃纤维平纹编织复合材料层合板的静态压缩和压-压疲劳性能实验.应力比为R=10,拟合出S-N曲线,基于疲劳实验过程中的刚度退化、能量耗散、循环蠕变与循环软化来表征疲劳损伤演化,结合扫描电子显微镜对断口形貌进行观察.结果表明:试件的条件疲劳极限为静态压缩强度的66.3%;通过双加权最小二乘法拟合的S-N曲线具有较高可信度;随着循环次数的增加,试件刚度逐渐下降,各峰值载荷下的能量耗散逐渐增加;在循环加载初期,试件表现出强烈循环蠕变现象,高峰值载荷作用下的试件表现出强烈循环软化行为;试件经过循环加载抵抗变形能力得到增强;断口观察到了基体开裂、纤维/基体界面脱粘、纤维断裂和分层四种失效模式;与疲劳断口相比,静态压缩断口表现出较大的分层损伤.
Author 王轩
杨晨晨
张铁纯
周春苹
AuthorAffiliation 中国民航大学 航空工程学院, 天津 300300%航空工业济南特种结构研究所 高性能电磁窗航空科技重点实验室, 济南250023
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Author_FL YANG Chenchen
ZHANG Tiechun
ZHOU Chunping
WANG Xuan
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Keywords 复合材料;疲劳;S-N曲线;刚度退化;能量耗散;断口形貌
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Title 平纹编织复合材料层合板静态压缩与压-压疲劳性能
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