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Modeling the progressive failure of scarf joints for wind turbine blade repair

机译:模拟风力涡轮机叶片修复围巾关节的逐步失效

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摘要

A continuum damage model for simulating propagation of debonding in joints, introducing a linear softening damage process for the adhesive agent, is used to predict failure of scarf joints. The proposed modeling procedure was applied to scarf joints of marine type with glass fiber reinforced polymer adherends, commonly encountered in wind turbine rotor blade repair. Tests on aviation type scarf joints with carbon fiber reinforced polymer adherends were also simulated. Stress analysis was performed using plane strain elements of a commercial finite element code allowing implementation of user-defined material behavior. Numerical results for different scarf angles were in good agreement with the experimental data. The proposed model has been utilized to design a repair patch on wind turbine rotor blade and the design has been validated by testing a full-scale subcomponent of the repaired blade.
机译:用于模拟关节中剥离传播的连续损伤模型,引入粘合剂的线性软化损伤工艺,用于预测围巾关节的失效。 拟议的建模程序应用于海洋型围巾关节,玻璃纤维增强聚合物粘附,通常遇到风力涡轮机转子叶片修复。 还模拟了碳纤维增强聚合物粘物的航空型围巾关节的试验。 使用商业有限元代码的平面应变元件进行应力分析,允许实现用户定义的材料行为。 不同围巾角度的数值结果与实验数据很好。 所提出的模型已经利用来设计风力涡轮机转子叶片上的修复贴片,并且通过测试修复刀片的全尺寸子组件来验证设计。

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