Fatigue Behavior of Open-Holed CFRP Laminates with Initially Cut Fibers

S. Sudarsono, K. Ogi
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引用次数: 13

Abstract

Carbon fiber-reinforced plastic (CFRP) laminates with initially cut fibers (ICFs) have good formability without large degradation of static strength; however, their fatigue behavior has not been investigated thus far. In this paper, we investigated fatigue behavior and damage progress of open-holed CFRP laminates with ICFs having interlayers. Three types of CFRP laminates were employed: a laminate without ICF fabricated using an autoclave (Continuous-A), a laminate with ICF fabricated using an autoclave (ICF-A) and a laminate with ICF fabricated using press molding (ICF-P). First, fatigue test was conducted to obtain S (maximum stress)-N (the number of cycles to failure) curves in order to reveal fatigue strength. The fatigue tests for several specimens were interrupted at three prescribed numbers of cycles to observe damage progress. It is found that the Continuous-A laminate shows little strength degradation in the S-N curve while fatigue strength in both ICF laminates is decreased by approximately 30% at N of 106. In contrast, the damage progress of the ICF-P laminate is the least among the three laminates while the delamination progress at both edges and around the hole in the Continuous-A laminate is the most prominent.
纤维初切开孔CFRP层合板的疲劳性能
初切纤维碳纤维增强塑料(CFRP)层压板具有良好的成形性,静强度下降不大;然而,迄今为止对其疲劳行为尚未进行研究。本文研究了含夹层碳纤维纤维的CFRP开孔复合材料层合板的疲劳性能和损伤过程。采用三种类型的CFRP层压板:使用高压灭菌器(Continuous-A)制造的不含ICF的层压板,使用高压灭菌器制造的ICF层压板(ICF- a)和使用压制成型制造的ICF层压板(ICF- p)。首先进行疲劳试验,得到S(最大应力)-N(循环失效次数)曲线,以揭示疲劳强度。在规定的三个循环次数下,对几个试件进行了疲劳试验,以观察损伤的进展。结果表明,在S-N曲线上,连续- a复合材料的强度衰减很小,而在N = 106时,两种ICF复合材料的疲劳强度均下降了约30%。相比之下,ICF-P层合板的损伤过程最小,而Continuous-A层合板的边缘和孔周围的分层过程最为突出。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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