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Structural optimisation of composite wind turbine blade structures with variations of internal geometry configuration

机译:具有内部几何形状变化的复合风力涡轮机叶片结构的结构优化

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Structural optimisation techniques are frequently used as part of the design process for composite wind turbine blades. Most commonly this is achieved by modifying material placement within a standard structural design; less attention has been paid to the possibility of varying internal geometry to create novel structural configurations. In this work, a series of wind turbine blade designs with differing structural configurations have been created and compared to investigate the effect of allowing various aspects of the internal structural geometry to be varied. The geometry of the structural spar is thoroughly investigated by modifying the width of the spar caps, and the number and location of shear webs including the spanwise starting and ending locations. The location and extent of a trailing edge reinforcement are also considered, along with the material thickness distribution of the spar and trailing edge reinforcement. A series of five parametric 2D finite element models with geometry and materials placement variables were created and incorporated into a genetic optimisation algorithm. This method allows the optimisation process sufficient freedom to generate designs without being constrained by preconceived ideas of how the internal geometry should be configured. The optimum designs had mass reduced relative to the baseline by 3.5-7.4%. Structural analysis of the optimum designs revealed that the active constraint varied greatly between the different designs, and it is therefore recommended that a wider range of loading cases and constraints needs to be accounted for in optimisations that allow the structural geometry to vary compared to those that use a standard geometry. (C) 2016 Elsevier Ltd. All rights reserved.
机译:结构优化技术经常用作复合风力涡轮机叶片设计过程的一部分。通常,这是通过修改标准结构设计中的材料放置来实现的。人们很少关注改变内部几何形状以创建新颖的结构构造的可能性。在这项工作中,已经创建了一系列具有不同结构配置的风力涡轮机叶片设计,并进行了比较,以研究允许内部结构几何形状的各个方面发生变化的效果。通过修改翼梁帽的宽度以及剪切腹板的数量和位置(包括翼展方向的起始和结束位置)来彻底研究结构翼梁的几何形状。还要考虑后缘钢筋的位置和范围,以及翼梁和后缘钢筋的材料厚度分布。创建了一系列具有几何形状和材料放置变量的五个参数化2D有限元模型,并将其合并到遗传优化算法中。这种方法使优化过程有足够的自由来生成设计,而不受内部几何结构应如何配置的先入为主的思想的束缚。最佳设计的质量相对于基线降低了3.5-7.4%。最佳设计的结构分析显示,不同设计之间的有效约束差异很大,因此建议在优化中考虑更大范围的载荷工况和约束,以使结构几何形状与使用标准几何体。 (C)2016 Elsevier Ltd.保留所有权利。

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