首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Blade Arrangement Optimization for Mistimed Bladed Disk Based on Gaussian Process Regression and Genetic Algorithm
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Blade Arrangement Optimization for Mistimed Bladed Disk Based on Gaussian Process Regression and Genetic Algorithm

机译:基于高斯过程回归和遗传算法的错时刀片磁盘刀片优化

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摘要

Mistiuning phenomena exist in the bladed disk due to the inevitable deviations among blades' properties, e.g., stiffness, mass, geometry, etc., leading to localization and response amplification. The dynamic performance of mistuned bladed disk is sensitive to the arrangement of blades. The blade arrangement optimization aims to obtain the optimal arrangement that minimizes the influence of mistuning. In this paper, a framework of high efficiency is raised to deal with the challenge of high computational cost this optimization. It comprehensively utilizes mixed-dimensional finite element model (MDFEM), Gaussian process (GP) regression, and genetic algorithm (GA). The MDFEM can perform mistimed modal analysis efficiently and provides the training set of GP regression rapidly. The GP model, as a surrogate model, predicts the desired dynamic performance directly without calculating the numerical model and can function as fitness function in optimization. GA has the capability to deal with combinatorial problems and is a good option for problems with large search domains and several local maxima/minima. The techniques and processes of three methods are illustrated in detail. Case studies, based on a real turbine, are concretely presented in a gradually progressive manner to test and verify the effectiveness, accuracy, and efficiency of methods and entire framework step by step. The results show the satisfactory optimal arrangement for a randomly chosen set of mistuned blades, and the influence of mistuning is reduced indeed. The time cost of the optimization has been reduced several orders of magnitude. This framework can be a promising approach for the blade arrangement optimization problem.
机译:由于叶片特性(例如,刚度,质量,几何形状等)之间不可避免的偏差,导致叶片盘中存在令人震惊的现象,从而导致定位和响应放大。雾化刀片式磁盘的动态性能对刀片的布置很敏感。叶片布置优化旨在获得使雾化影响最小的最佳布置。在本文中,提出了一个高效的框架来应对这种优化带来的高计算量的挑战。它综合利用了混合维有限元模型(MDFEM),高斯过程(GP)回归和遗传算法(GA)。 MDFEM可以有效地执行错误时态的模态分析,并迅速提供GP回归的训练集。 GP模型作为替代模型,可以直接预测所需的动态性能,而无需计算数值模型,并且可以在优化中用作适应度函数。 GA具有处理组合问题的能力,对于具有较大搜索域和多个局部最大值/最小值的问题是一个很好的选择。详细说明了三种方法的技术和过程。以逐步发展的方式具体介绍了基于真实涡轮机的案例研究,以逐步检验和验证方法和整个框架的有效性,准确性和效率。结果表明,对于一组随机选择的雾化叶片,其满意的最佳布置,确实减少了雾化的影响。优化的时间成本已减少了几个数量级。该框架可以是解决叶片布置优化问题的有前途的方法。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2020年第2期|021008.1-021008.12|共12页
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    Department of Aeronautics and Astronautics Fudan University Shanghai 200433 China Aerospace System Engineering Shanghai Shanghai 201109 China;

    Department of Aeronautics and Astronautics Fudan University Shanghai 200433 China;

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