Cui Wenbin, Chen Xuan, Chen Chao, Cheng Li, Ding Junliang, Zhang Hui
Aeronautics Engineering College, Air Force Engineering University, Xi'an 710038, China.
Materials (Basel). 2020 Feb 18;13(4):908. doi: 10.3390/ma13040908.
A liquid nitrogen cooling system was developed to ensure the successful ultrasonic testing of composite materials to characterize the very High Cycle Fatigue (VHCF) of carbon fiber reinforced plastics (CFRP). The fatigue failure of CFRP occurs even in the very high cycle range and there is no traditional fatigue limit. The S-N curve of the CFRP presents a step whose characteristics appear in the transition between high cycle and very high cycle fatigue. The damage evolution of CFRP in the same field of view is investigated. The morphology of damaged CFRP composites under ultrasonic loading is described by three characteristics: matrix damage at the intersection of fiber bundles, near fiber bundle parallel section matrix cavity and matrix penetration. With the increasing of cycles, the damage process is also presented in turn according to these three characteristics. The post-fatigue bending modulus changed significantly from the pre-fatigue values, indicating that the VHCF had a considerable impact on the mechanical properties of the composite. An evolution threshold was introduced from the S-N curve to determine the fatigue evolution law from the high cycle regime to the very high cycle regime.
开发了一种液氮冷却系统,以确保对复合材料进行成功的超声检测,从而表征碳纤维增强塑料(CFRP)的超高周疲劳(VHCF)特性。CFRP的疲劳失效甚至在超高周范围内也会发生,并且不存在传统的疲劳极限。CFRP的S-N曲线呈现出一个台阶,其特征出现在高周疲劳和超高周疲劳的过渡阶段。研究了CFRP在同一视场中的损伤演变。超声加载下受损CFRP复合材料的形态由三个特征描述:纤维束交叉处的基体损伤、纤维束平行截面附近的基体空洞和基体贯穿。随着循环次数的增加,损伤过程也依次按照这三个特征呈现。疲劳后弯曲模量与疲劳前的值相比有显著变化,表明VHCF对复合材料的力学性能有相当大的影响。从S-N曲线引入了一个演变阈值,以确定从高周区域到超高周区域的疲劳演变规律。