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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:复合材料风力涡轮机叶片的疲劳寿命预测:可变风载荷和非比例多轴应力状态的影响

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摘要

Conventional fatigue analysis of composite wind turbine blades has applied a fixedrnwind load distribution that does not fully capture the effect of variable wind load onrnfatigue life prediction. Another simplification in the conventional fatigue analysis isrnthat the blades are often treated as a typical beam-like structure in which fatigue liferncalculation is limited in considering the normal stress component in the beam axisrndirection. Consequently, the effect of non-proportional multi-axial complex stressrnstates on blade fatigue life prediction has been ignored. In order to study the fatiguerneffects of variable wind load and non-proportional multi-axial stress states, arncomprehensive fatigue analysis that includes variable wind load, wind field simulationrnand aerodynamic analysis, stress analysis by finite element analysis, and fatiguerndamage evaluation based on tested fatigue data has been developed for compositernwind turbine blades. The variable wind load is represented by a joint distribution ofrn10-minute mean wind speed and 10-minute turbulence intensity. The non-proportionalrnmulti-axial complex stress states are involved when calculating 10-minute fatiguerndamage of section points through laminate thickness. The annual fatigue damage isrncalculated based on the 10-minute fatigue damage and the joint distribution.rnConsequently, the blade fatigue effects due to both the variable wind load in a largernspatiotemporal range and the non-proportional multi-axial complex stress states can berninvestigated. The case study reveals that the variable wind load has a significantrninfluence on the fatigue life of composite wind turbine blades. It is also shown thatrnneglecting transverse normal and shear stresses in the blade fatigue analysis could leadrnto substantially overestimated blade fatigue life.
机译:复合材料风力涡轮机叶片的常规疲劳分析已应用了固定的风载荷分布,该分布不能完全捕获可变风载荷对疲劳寿命预测的影响。传统疲劳分析的另一个简化之处是,叶片通常被视为典型的梁状结构,在考虑梁轴向上的法向应力分量时,疲劳寿命的计算受到限制。因此,非比例多轴复应力状态对叶片疲劳寿命预测的影响已被忽略。为了研究可变风荷载和非比例多轴应力状态的疲劳效应,进行了包括可变风荷载的综合疲劳分析,风场模拟和空气动力学分析,有限元分析应力分析以及基于测试疲劳数据的疲劳损伤评估已为复合材料风力涡轮机叶片开发。 10分钟平均风速和10分钟湍流强度的联合分布代表了可变风荷载。计算通过层压板厚度的截面点的10分钟疲劳损伤时,会涉及非比例的多轴复合应力状态。根据10分钟的疲劳损伤和接头分布来计算年疲劳损伤。因此,可以研究由于风载荷在较大的时空范围内变化以及非比例多轴复合应力状态引起的叶片疲劳效应。案例研究表明,可变风载荷对复合材料风力涡轮机叶片的疲劳寿命有重要影响。还显示出在叶片疲劳分析中忽略横向法向应力和剪切应力会导致大大高估叶片疲劳寿命。

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  • 来源
    《》|2015年|1-13|共13页
  • 会议地点 East Lansing MI(US)
  • 作者单位

    Department of Mechanical and Industrial Engineering, The University ofIowa, Iowa City, IA 52242, U.S.A. E-mail: olesya-zhupanska@uiowa.edu;

    Department of Mechanical and Industrial Engineering, The University of Iowa, IowaCity, IA 52242, U.S.A. E-mail: kyung-choi@uiowa.edu;

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  • 正文语种 eng
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