提高海流涡轮叶片夹层复合材料的粘结断裂韧性

Alexander Gonzalez, H. Mahfuz, Morteza Sabet
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引用次数: 5

摘要

对海流涡轮叶片夹层复合材料进行了研究。夹层与复合面板和聚合物泡沫芯是特别感兴趣的。泡沫作为芯材可以为叶片提供高的刚度和屈曲强度,而水下的密度是空气的800倍。除了刚度和强度,制造简单,自浮力和优异的疲劳性能是夹层复合材料的其他优点。而在夹层复合材料中,两种失效模式占主导地位;一种是岩心剪切,另一种是岩心面剥离。为了评估这种脱粘,我们确定了i型断裂韧性,也称为脱粘断裂韧性。该夹层复合材料由碳/环氧复合材料表面和聚氨酯泡沫芯组成。为了提高断裂韧性,在面芯界面处插入短切链垫(CSM)。采用ASTM D5528-01试验方法在单悬臂梁(SCB)配置下测定断裂韧性。复合材料的平均剥离韧性分别为177 J/m2和175 J/m2。在界面处加入CSM后,两种材料的韧性均提高了约14%。本文详细介绍了夹层结构的结构、特点和提高断裂韧性的来源。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Enhancing Debond Fracture Toughness of Sandwich Composites for Marine Current Turbine Blades
Sandwich composites for marine current turbine blades were investigated. Sandwich with composite face-sheet and polymeric foam core is of particular interest. Foam as core materials can provide high stiffness and buckling strength to the blade which is required under water where the density is 800 times higher than air. In addition to stiffness and strength, simplicity in manufacturing, self-buoyancy, and superior fatigue performance of sandwich composites are other advantages. However, in sandwich composites, two failure modes are dominant; one is core shear, and the other is face-core debonding. To assess this debonding, mode-I fracture toughness, also known as debond-fracture toughness was determined. The sandwich composite was made of carbon/epoxy face sheet with syntactic and polyurethane foam cores. In order to improve upon the fracture toughness, chopped strand mat (CSM) were inserted at the face-core interface. ASTM D5528-01 test method was used in single cantilever beam (SCB) configuration to determine the fracture toughness. Sandwich composites with a syntactic and polyurethane foam core were found to have an average debond toughness of 177 J/m2 and 175 J/m2, respectively. After CSM was introduced at the interface, toughness increased by about 14% in both cases. Details of sandwich construction, their characterization, and source of improvement in fracture toughness is described in the paper.
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