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Structural reliability analysis of rotor blades in ultimate loading

机译:终极加载中转子叶片的结构可靠性分析

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The objective of the present work is the assessment of the reliability level of an already designed blade according to IEC 61400-1 ed3 implementing two different probabilistic approaches: the Edgeworth Expansion (EDW) and the Response Surface Method combined with Monte Carlo (RSM/MC). An existing probabilistic tool for the reliability analysis of rotor blades based on the EDW method has been further improved and enhanced by implementing also the RSM/MC approach. The analysis is performed at the ply level where material properties are also certified. Stress analysis is implemented using THIN, a numerical tool based on thin wall multi-cellular -beam sections. Material properties and extreme loads (stress resultants acting on the blade section) are considered as stochastic variables. The stochastic nature of all six stress resultants is taken into account and is estimated through available aero-elastic calculations. Correlations among the stress resultants are considered. Due to the high speed stress analysis of THIN, a straightforward comparison of the methods is performed with direct Monte Carlo simulation.
机译:本作工作的目的是评估根据IEC 61400-1 ED3实施两种不同的概率方法的IEC 61400-1 ED3的可靠性水平:EdgeWorth膨胀(EDW)和响应表面方法与蒙特卡罗(RSM / MC)相结合(RSM / MC )。基于EDW方法的转子叶片可靠性分析的现有概率工具进一步提高和增强了RSM / MC方法。该分析是在层次的水平上进行的,其中材料特性也认证。使用薄的基于薄壁多蜂窝 - 光部分的薄的数值工具来实现应力分析。材料性质和极端载荷(在刀片部分上作用的应力结果)被认为是随机变量。考虑所有六种应力结果的随机性质,并通过可用的航空弹性计算估计。考虑应力结果之间的相关性。由于薄的高速应力分析,通过直接蒙特卡罗模拟进行了对方法的直接比较。

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