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Reliability-Based Low Fatigue Life Analysis of Turbine Blisk with Generalized Regression Extreme Neural Network Method

机译:基于可靠性的汽轮机叶盘低疲劳寿命的广义回归极限神经网络方法

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摘要

Turbine blisk low cycle fatigue (LCF) is affected by various factors such as heat load, structural load, operation parameters and material parameters; it seriously influences the reliability and performance of the blisk and aeroengine. To study the influence of thermal-structural coupling on the reliability of blisk LCF life, the generalized regression extreme neural network (GRENN) method was proposed by integrating the basic thoughts of generalized regression neural network (GRNN) and the extreme response surface method (ERSM). The mathematical model of the developed GRENN method was first established in respect of the LCF life model and the ERSM model. The method and procedure for reliability and sensitivity analysis based on the GRENN model were discussed. Next, the reliability and sensitivity analyses of blisk LCF life were performed utilizing the GRENN method under a thermal-structural interaction by regarding the randomness of gas temperature, rotation speed, material parameters, LCF performance parameters and the minimum fatigue life point of the objective of study. The analytical results reveal that the reliability degree was 0.99848 and the fatigue life is 9419 cycles for blisk LCF life when the allowable value is 6000 cycles so that the blisk has some life margin relative to 4500 cycles in the deterministic analysis. In comparison with ERSM, the computing time and precision of the proposed GRENN under 10,000 simulations is 1.311 s and 99.95%. This is improved by 15.18% in computational efficiency and 1.39% in accuracy, respectively. Moreover, high efficiency and high precision of the developed GRENN become more obvious with the increasing number of simulations. In light of the sensitivity analysis, the fatigue ductility index and temperature are the key factors of determining blisk LCF life because their effect probabilities reach 41% and 26%, respectively. Material density, rotor speed, the fatigue ductility coefficient, the fatigue strength coefficient and the fatigue ductility index are also significant parameters for LCF life. Poisson’s ratio and elastic modulus of materials have little effect. The efforts of this paper validate the feasibility and validity of GRENN in the reliability analysis of blisk LCF life and give the influence degrees of various random parameters on blisk LCF life, which are promising to provide useful insights for the probabilistic optimization of turbine blisk LCF life.
机译:涡轮叶轮低周疲劳(LCF)受各种因素影响,例如热负荷,结​​构负荷,运行参数和材料参数;它严重影响了叶轮和航空发动机的可靠性和性能。为了研究热-结构耦合对叶轮LCF寿命可靠性的影响,结合广义回归神经网络(GRNN)和极限响应面法(ERSM)的基本思想,提出了广义回归极端神经网络(GRENN)方法。 )。首先针对LCF寿命模型和ERSM模型建立了已开发GRENN方法的数学模型。讨论了基于GRENN模型的可靠性和灵敏度分析的方法和过程。接下来,在考虑气体温度,转速,材料参数,LCF性能参数和目标的最小疲劳寿命点的随机性的情况下,利用GRENN方法在热-结构相互作用下,对大盘LCF寿命进行可靠性和敏感性分析。研究。分析结果表明,当确定值为6000次循环时,叶轮LCF寿命的可靠性等级为0.99848,疲劳寿命为9419次循环,因此在确定性分析中,叶轮相对于4500次循环具有一定的寿命余量。与ERSM相比,建议的GRENN在10,000次仿真下的计算时间和精度为1.311 s和99.95%。计算效率分别提高了15.18%,准确度提高了1.39%。而且,随着仿真次数的增加,已开发的GRENN的高效率和高精度变得更加明显。根据敏感性分析,疲劳延展性指数和温度是确定叶型LCF寿命的关键因素,因为它们的作用概率分别达到41%和26%。材料密度,转子速度,疲劳延性系数,疲劳强度系数和疲劳延性指数也是LCF寿命的重要参数。材料的泊松比和弹性模量影响很小。本文的工作验证了GRENN在叶轮LCF寿命可靠性分析中的可行性和有效性,并给出了各种随机参数对叶轮LCF寿命的影响程度,有望为涡轮叶轮LCF寿命的概率优化提供有用的见解。 。

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