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Reducing the number of load cases for fatigue damage assessment of offshore wind turbine support structures using a simple severity-based sampling method

机译:使用简单的基于严重性的采样方法减少海上风力涡轮机支撑结构的疲劳损伤评估数量

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摘要

The large amount of computational effort required for a full fatigueassessment of offshore wind turbine support structures under operationalconditions can make these analyses prohibitive, especially for applicationslike design optimization, for which the analysis would have to be repeated foreach iteration of the process. To combat this issue, we present a simpleprocedure for reducing the number of load cases required for an accuratefatigue assessment. After training on one full fatigue analysis of a basedesign, the method can be applied to establish a deterministic, reducedsampling set to be used for a family of related designs. The method is basedon sorting the load cases by their severity, measured as the product offatigue damage and probability of occurrence, and then calculating therelative error resulting from using only the most severe load cases toestimate the total fatigue damage. By assuming this error to be approximatelyconstant, one can then estimate the fatigue damage of other designs usingjust these load cases. The method yields a maximum error of about 6 %when using around 30 load cases (out of 3647) and, for most cases, errors ofless than 1 %–2 % can be expected for sample sizes in the range15–60. One of the main points in favor of the method is its simplicity whencompared to more advanced sampling-based approaches. Though there arepossibilities for further improvements, the presented version of the methodcan be used without further modifications and is especially useful for designoptimization and preliminary design. We end the paper by noting somepossibilities for future work that extend or improve upon the method.
机译:充满疲劳所需的大量计算工作近海风力涡轮机支撑结构的评估条件可以使这些分析禁止,特别是对于应用程序与设计优化一样,必须重复分析的分析每个过程的迭代。要打击这个问题,我们展示了一个简单的减少准确所需的负载箱数的步骤疲劳评估。培训基地的一个完整疲劳分析后设计,该方法可应用于确定确定性,减少采样集用于一系列相关设计。该方法是基于的通过严重性对负载案例进行排序,测量为产品疲劳损坏和发生概率,然后计算仅使用最严重的负载案例产生的相对错误估计总疲劳损坏。通过假设此错误约为常数,然后可以估计其他设计的疲劳损坏只是这些负载案例。该方法产生约6%的最大误差使用大约30个装载案例(在3647中),并且对于大多数情况而言,误差在范围内的样本尺寸可以预期小于1%-2%15-60。有利于该方法的主要点之一是其简单性与更先进的基于采样的方法相比。虽然有进一步改进的可能性,所呈现的方法版本可以在没有进一步的修改的情况下使用,并且对于设计特别有用优化与初步设计。我们通过注意到一些纸张结束了纸张未来工作的可能性,延伸或改进方法。

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