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Decomposed Collaborative Modeling Approach for Probabilistic Fatigue Life Evaluation of Turbine Rotor

机译:汽轮机转子概率疲劳寿命评价分解的协作建模方法

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摘要

To improve simulation accuracy and efficiency of probabilistic fatigue life evaluation for turbine rotor, a decomposed collaborative modeling approach is presented. In this approach, the intelligent Kriging modeling (IKM) is firstly proposed by combining the Kriging model (KM) and an intelligent algorithm (named as dynamic multi-island genetic algorithm), to tackle the multi-modality issues for obtaining optimal Kriging parameters. Then, the decomposed collaborative IKM (DCIKM) comes up by fusing the IKM into decomposed collaborative (DC) strategy, to address the high-nonlinearity problems for accelerating simulation efficiency. Moreover, the DCIKM-based probabilistic fatigue life evaluation theory is introduced. The probabilistic fatigue life evaluation of turbine rotor is regarded as case study to verify the presented approach; the evaluation results reveal that the probabilistic fatigue life of turbine rotor is 3296 cycles. The plastic strain range ∆ and fatigue strength coefficient ′ are the main affecting factors to fatigue life, whose effect probability are 28% and 22%, respectively. By comparing with direct Monte Carlo method, KM method, IKM method and DC response surface method, the presented DCIKM is validated to hold high efficiency and accuracy in probabilistic fatigue life evaluation.
机译:提高涡轮机转子概率疲劳寿命评估的仿真精度和效率,提出了一种分解的协作建模方法。在这种方法中,首先通过将Kriging模型(KM)和智能算法(命名为动态多岛遗传算法)组合来提出智能Kriging建模(IKM),以解决用于获得最佳Kriging参数的多模态问题。然后,通过将IKM融入分解的协作(DC)策略来解决分解的协作IKM(DCIKM),以解决加速模拟效率的高非线性问题。此外,介绍了基于DCIKM的概率疲劳寿命评估理论。涡轮机转子的概率疲劳寿命评估被认为是验证所提出的方法的情况;评估结果表明,涡轮机转子的概率疲劳寿命为3296循环。塑料应变范围δ和疲劳强度系数'是疲劳寿命的主要影响因素,其效果概率分别为28%和22%。通过与直接蒙特卡罗方法,KM方法,IKM方法和直流响应表面方法进行比较,验证所呈现的DCICKM以保持概率疲劳寿命评估的高效率和准确性。

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