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Toward composite wind turbine blade fatigue life assessment using ply scale damage model

机译:朝向复合风力涡轮机叶片疲劳寿命评估使用帘布层尺度损伤模型

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Fatigue design optimization of composite material structures is limited by the classical approaches used, derived from knowledge based on metal fatigue. Other approaches exist to describe damage mechanisms of composites but they cannot always be applied at the structure scale because of their complexity. However, assumptions can be made in the case of beam structures to reduce the structural investigation at the section scale. With these assumptions this paper proposes to compare a progressive fatigue damage model written at the ply scale to the normative approach for the assessment of wind turbine blade section design. It is shown that the normative approach is very conservative and the progressive fatigue damage model provides very useful information to understand damage propagation at the structure scale.
机译:复合材料结构的疲劳设计优化受到基于金属疲劳的知识的经典方法的限制。存在其他方法来描述复合材料的损伤机制,但由于它们的复杂性,它们不能总是在结构规模上应用。然而,在梁结构的情况下可以进行假设,以减少截面规模的结构调查。通过这些假设,本文建议比较普及规模写入的渐进疲劳损伤模型,以评估风力涡轮机叶片段设计的规范方法。结果表明,规范方法是非常保守的,并且渐进的疲劳损伤模型提供了理解结构规模损坏传播的非常有用的信息。

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