首页|期刊导航|复合材料科学与工程|碳纤维复合材料预湿热条件下疲劳寿命退化规律

碳纤维复合材料预湿热条件下疲劳寿命退化规律OA

Fatigue life degradation law of carbon fiber composites under pre-hygrothermal conditions

中文摘要英文摘要

本研究旨在揭示碳纤维复合材料在预湿热环境中的疲劳寿命退化机制,探究了复合材料在饱和吸湿量的 0%、40%、70%和 100%四种条件下的静拉伸强度及疲劳寿命,其中静拉伸破坏应力呈现波动特征,而疲劳寿命随吸湿量增加呈现单调递减.采用对数正态分布和二参数 Weibull 分布理论,分析层合板在各应力水平下的疲劳寿命分布规律,两种概率模型均展现优异拟合度;基于对数正态分布分析可靠性寿命规律,可靠性寿命随着可靠度的增加而减小,并随应力水平的减小而增大;预湿热疲劳破坏模式表现为覆盖整个工作段的纤维束断裂与分层多重损伤.这些发现为湿热环境复合材料工程应用提供了理论支撑.

This study aims to reveal the fatigue life degradation mechanisms of carbon fiber reinforced polymer(CFRP)composites under pre-hygrothermal environments.The static tensile strength and fatigue life of composites were investigated under four moisture absorption conditions(0%,40%,70%,and 100%of saturated moisture con-tent).The static tensile failure stress exhibited fluctuating characteristics,while the fatigue life showed a monotonic decreasing trend with increasing moisture absorption.The fatigue life distribution patterns of laminates under different stress levels were analyzed using log-normal distribution and two-parameter Weibull distribution theories,both demonstrating excellent fitting accuracy.Based on log-normal distribution analysis,the reliability life decreased with increasing reliability levels and increased with decreasing stress levels.The hygrothermal fatigue failure modes manifested as multiple damage mechanisms involving fiber bundle fracture spanning the entire working section and delamination damage.These findings provide theoretical support for the engineering application of composites in hy-grothermal environments.

张泽林;李哲;冯宇;王卓健;张鹏飞;尹生

空军工程大学 航空工程学院,西安 710038空军工程大学 航空工程学院,西安 710038空军工程大学 航空工程学院,西安 710038空军工程大学 航空工程学院,西安 710038中国人民解放军 95903 部队,北京 100070中国人民解放军94686 部队,北京 100070

通用工业技术

复合材料预湿热静拉伸强度可靠性寿命破坏模式

compositespre-hygrothermalstatic tensile strengthreliability lifefailure mode

《复合材料科学与工程》 2026 (3)

28-37,10

国家自然科学基金(52472465)陕西省创新能力支撑计划研究项目(2024ZC-KJXX-102)

10.19936/j.cnki.2096-8000.20260328.004

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