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Fretting Fatigue Behaviour of Pin-Loaded Thermoset Carbon-Fibre-Reinforced Polymer (CFRP) Straps

机译:针状热固性碳纤维增强聚合物(CFRP)带的微动疲劳行为

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摘要

This paper focuses on the fretting fatigue behaviour of pin-loaded carbon-fibre-reinforced polymer (CFRP) straps studied as models for rigging systems in sailing yachts, for suspenders of arch bridges and for pendent cables in cranes. Eight straps were subjected to an ultimate tensile strength test. In total, 26 straps were subjected to a fretting fatigue test, of which ten did not fail. An S–N curve was generated for a load ratio R of 0.1 and a frequency f of 10 Hz, showing a fatigue limit stress of the straps around the matrix fatigue limit, corresponding to 46% of the straps’ ultimate tensile strength (σUTS). The fatigue limit was defined as 3 million load cycles (N = 3 × 106), but tests were even conducted up to N = 11.09 × 106. Catastrophic failure of the straps was initiated in their vertex areas. Investigations on the residual strength and stiffness properties of straps tested around the fatigue limit stress (for N ≥ 1 × 106) showed little influence of the fatigue loading on these properties. Quasi-static finite element analyses (FEA) were conducted. The results obtained from the FEA are in good agreement with the experiments and demonstrate a fibre parallel stress concentration in the vertex area of factor 1.3, under the realistic assumption of a coefficient of friction (cof) between pin and strap of 0.5.
机译:本文着重研究了销钉负载碳纤维增强聚合物(CFRP)皮带的微动疲劳行为,这些皮带被研究为帆船游艇的索具系统模型,拱桥悬挂器和吊车吊索的模型。八个带子经受极限拉伸强度测试。总共对26条皮带进行了微动疲劳测试,其中10条没有失效。载荷比R为0.1且频率f为10 Hz时,生成了一条S–N曲线,显示出条带的疲劳极限应力在基体疲劳极限附近,相当于条带极限抗拉强度(σUTS)的46% 。疲劳极限定义为3百万个负载循环(N = 3×10 6 ),但是甚至进行了高达N = 11.09×10 6 的测试。皮带的灾难性故障始于其顶点区域。对在疲劳极限应力(N≥1×10 6 )附近测试的带材的残余强度和刚度特性的研究表明,疲劳载荷对这些特性的影响很小。进行了准静态有限元分析(FEA)。从FEA获得的结果与实验非常吻合,并且在实际假设销与带之间的摩擦系数(cof)为0.5的情况下,纤维平行应力集中在顶点区域为1.3。

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