常幅疲劳加载下CFRP-钢界面黏结性能研究

EXPERIMENTAL STUDY ON INTERFACIAL BOND BEHAVIOR BETWEEN CFRP AND STEEL UNDER CONSTANT AMPLITUDE FATIGUE LOADING

  • 摘要: 为研究碳纤维增强复合材料(CFRP)-钢界面黏结性能及其在常幅疲劳加载下的损伤发展,采用非线性结构黏胶Araldite 2015制作了14个CFRP-钢单剪试件,并进行静力拉伸试验和不同荷载比(0.3~0.8静力极限承载力)条件下的疲劳拉伸试验。分析了常幅疲劳加载下荷载比对试件破坏模式、疲劳寿命及黏结性能的影响,揭示了疲劳加载下界面的损伤演化机理。研究结果表明:静力加载和常幅疲劳加载下,CFRP-钢单剪试件均发生胶层内失效。随着荷载比减小,钢板表面残留的结构黏胶减少。界面的疲劳寿命随荷载比的增大而减小,且疲劳寿命与荷载比呈幂函数关系。在常幅疲劳加载下,试件加载端的刚度随疲劳荷载循环次数增加逐渐退化,高荷载比下单次疲劳加载导致的界面刚度退化更为迅速。CFRP应变和界面剪应力分布表明:疲劳荷载下的界面失效是损伤累积发展的过程,界面失效先从加载端开始,其后逐步扩展到自由端。随着荷载比的增加,界面失效时CFRP板的峰值应变逐渐增长,但始终低于静力加载下的峰值应变。界面峰值剪应力随荷载比的提高呈现先增后降的趋势;荷载比≥0.7时,界面峰值剪应力略高于静力加载下的值。当荷载比从0.3增加到0.8时,界面黏结-滑移关系包络线由近似双线性转变为三线性,且荷载比为0.8时的平台段分布比荷载比为0.7时更广。通过单次疲劳加载下界面刚度退化表征界面损伤,发现距加载端67.5 mm以内的界面损伤累积速率低于67.5 mm以外的区域,且在超过67.5 mm的区域内,损伤累积速率基本一致。该研究系统分析了不同荷载比对CFRP-钢界面黏结性能的影响,为CFRP加固钢结构疲劳性能研究提供参考。

     

    Abstract: To explore the bond performance and damage progression at the interface between carbon fiber-reinforced polymer (CFRP) and steel under constant amplitude fatigue loading, fourteen CFRP-to-steel single-lap shear joints, fabricated using the nonlinear structural adhesive Araldite 2015, were tested under both monotonic and fatigue loadings. The influence of load ratio on failure mode, fatigue life, and bond performance was examined, shedding light on the damage evolution at the CFRP-steel interface under fatigue. Under monotonic loading and constant amplitude fatigue loading, CFRP-steel single-lap shear specimens all experienced failure within the adhesive layer. As the load ratio decreased, the residual adhesive on the steel surface decreased. The fatigue life of the interfaces decreases with the increased load ratio, with a power-law relationship observed between fatigue life and load ratio. During fatigue loading, the stiffness at the loading end of the specimen progressively degraded with fatigue cycles, particularly noticeable at higher load ratios. Analysis of CFRP strain distribution and interfacial shear stress suggested that the cohesive failure under fatigue loading initiated at the loading end and propagated towards the free end as a result of damage accumulation. An increase in the load ratio resulted in higher peak strain at the CFRP laminate at failure, although the value remained lower than that under monotonic loading. The peak shear stress first increased and then decreased with the increasing of load ratio. At high load ratios (≥0.7), the peak shear stress exceeded that under monotonic loading. The bond-slip response evolved from approximately bilinear at the load ratio of 0.3 to trilinear at the load ratio of 0.8, with the latter showing a more extended plateau than that at the load ratio of 0.7. Stiffness degradation under a single cycle of fatigue loading indicated varying damage accumulation rates. Within 67.5 mm from the loading end, the rate was lower compared with regions beyond 67.5 mm, where the rates were approximately the same. This study analyzed the influence of load ratios on the bond performance of CFRP-steel interface under fatigue loading, providing valuable insights for research on the fatigue behavior of CFRP-strengthened steel structures.

     

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