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Fatigue Life Prediction in Composite Wind Turbine Blades: Effects of Variable Wind Load and Nonproportional Multi-axial Stress States

机译:复合风力涡轮机叶片中的疲劳寿命预测:可变风荷载与非贮值多轴应力状态的影响

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Conventional fatigue analysis of composite wind turbine blades has applied a fixed wind load distribution that does not fully capture the effect of variable wind load on fatigue life prediction. Another simplification in the conventional fatigue analysis is that the blades are often treated as a typical beam-like structure in which fatigue life calculation is limited in considering the normal stress component in the beam axis direction. Consequently, the effect of non-proportional multi-axial complex stress states on blade fatigue life prediction has been ignored. In order to study the fatigue effects of variable wind load and non-proportional multi-axial stress states, a comprehensive fatigue analysis that includes variable wind load, wind field simulation and aerodynamic analysis, stress analysis by finite element analysis, and fatigue damage evaluation based on tested fatigue data has been developed for composite wind turbine blades. The variable wind load is represented by a joint distribution of 10-minute mean wind speed and 10-minute turbulence intensity. The non-proportional multi-axial complex stress states are involved when calculating 10-minute fatigue damage of section points through laminate thickness. The annual fatigue damage is calculated based on the 10-minute fatigue damage and the joint distribution. Consequently, the blade fatigue effects due to both the variable wind load in a large spatiotemporal range and the non-proportional multi-axial complex stress states can be investigated. The case study reveals that the variable wind load has a significant influence on the fatigue life of composite wind turbine blades. It is also shown that neglecting transverse normal and shear stresses in the blade fatigue analysis could lead to substantially overestimated blade fatigue life.
机译:复合风力涡轮机叶片的传统疲劳分析施加了固定的风力载荷分布,该固定风力载荷分布不会完全捕捉变量风荷对疲劳寿命预测的影响。传统疲劳分析中的另一种简化是叶片通常被视为典型的光束状结构,其中疲劳寿命计算在考虑梁轴方向上的正常应力分量时受到限制。因此,忽略了非比例多轴复合应力状态对叶片疲劳寿命预测的影响。为了研究可变风荷载和非比例多轴应力状态的疲劳效应,综合疲劳分析包括可变风力荷载,风电场模拟和空气动力学分析,有限元分析的应力分析,以及基于疲劳损伤评估已经开发了测试疲劳数据,用于复合风力涡轮机叶片。变量风荷载是由10分钟的平均风速和10分钟湍流强度的接头分布表示。当通过层压厚度计算截面点的10分钟疲劳损坏时,涉及非比例多轴复合应力状态。年疲劳损坏是根据10分钟的疲劳损坏和关节分布计算的。因此,可以研究由于大的时空范围和非比例多轴复合应力状态的可变风荷载引起的叶片疲劳效应。案例研究表明,变量风荷对复合风力涡轮机叶片的疲劳寿命具有显着影响。还表明,忽略叶片疲劳分析中的横向正常和剪切应力可能导致基本上高估的叶片疲劳寿命。

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