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INVESTIGATION OF THE FATIGUE FAILURE MECHANISMS FOR STITCHED AND UNSTITCHED UNIDIRECTIONAL COMPOSITES

机译:缝合和非自行复合材料缝合和非自行复合材料的疲劳失效机制研究

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The traditional glass fabrics used in composite structures are usually in the form of two dimensional (2D) fibre architectures. They are relatively inexpensive and usually provide good in-plane mechanical properties. However, most of them have relatively poor through-thickness mechanical properties because the load applied the translaminar direction is predominately carried by the resin matrix. During last two decades, a considerable amount of research has been devoted to improving the through-thickness mechanical properties of composite laminate by developing the 3-D fibre architecture that includes braiding, knitting, weaving and stitching. The purpose of this study is to apply the stitching technologies into the composite materials in wind turbine blades that are designed to have fatigue life of 20 years and more.
机译:复合结构中使用的传统玻璃织物通常是二维(2D)纤维架构的形式。它们相对便宜,通常提供良好的面内机械性能。然而,大多数具有相对较差的贯穿厚度力学性能,因为施加旋转曲线素方向的负荷主要由树脂基质承载。在过去二十年中,通过开发包括编织,针织,编织和缝合的三维光纤架构来改善复合层压板的贯穿厚度力学性能。本研究的目的是将缝合技术应用于风力涡轮机叶片中的复合材料,这些材料被设计为具有20年和更多的疲劳寿命。

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