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涡轮轴低周疲劳寿命可靠性分析及优化设计方法研究
引用本文:陆艺鑫,吕震宙,冯凯旋,何良莉.涡轮轴低周疲劳寿命可靠性分析及优化设计方法研究[J].推进技术,2022,43(2):8-20.
作者姓名:陆艺鑫  吕震宙  冯凯旋  何良莉
作者单位:西北工业大学 航空学院,陕西 西安 710072
基金项目:国家自然科学基金(52075442);两机重大专项(2017-IV-0009-0046)。
摘    要:为保障涡轮轴在多种不确定性因素影响下的可靠性和寿命性能,建立了涡轮轴低周疲劳寿命可靠性分析与优化设计方法.搭建了涡轮轴结构分析、可靠性分析和可靠性优化设计的参数化平台,实现了设计参数的不同访问值处结构分析和可靠性分析的自主调用.提出了改进Monte Carlo结合自适应Kriging的算法(A-MCS-AK),通过多点...

关 键 词:涡轮轴  低周疲劳  结构分析  可靠性分析  优化设计  参数化平台
收稿时间:2021/7/29 0:00:00
修稿时间:2021/11/18 0:00:00

Probability Analysis and Reliability Based Design Optimization Methods for Low Cycle Fatigue Life of Turbine Shaft
LU Yi-xin,LYU Zhen-zhou,FENG Kai-xuan,HE Liang-li.Probability Analysis and Reliability Based Design Optimization Methods for Low Cycle Fatigue Life of Turbine Shaft[J].Journal of Propulsion Technology,2022,43(2):8-20.
Authors:LU Yi-xin  LYU Zhen-zhou  FENG Kai-xuan  HE Liang-li
Abstract:In order to ensure reliability and increase low cycle fatigue life (LCFL) of turbine shaft under various random uncertainties, the reliability analysis and reliability based design optimization (RBDO) were studied. A parameter platform is established for structure analysis, reliability analysis and RBDO of the LCFL of turbine shaft. Based on this platform, calling structure finite element software and reliability analysis can be automatically realized at different design parameters visited by RBDO iteration. For improving efficiency of reliability analysis greatly, an advanced Monte Carlo simulation combined with adaptive Kriging model (A-MCS-AK) is proposed by strategy of multi-training-point at one updating and candidate sample pool reduction. For two RBDO models of respectively maximizing expectation of LCFL and minimizing failure probability of LCFL of the turbine shaft, a quasi-sequential decoupling method is presented by combining cooperatively adaptive surrogate. The analysis results of the turbine shaft show that the parameterized platform completes the automatic and orderly transmission of data, and the proposed A-MCS-AK is more efficient than traditional adaptive Kriging combined with MCS (AK-MCS) for reliability analysis. The solutions of two RBDO models of the turbine shaft LCFL show that cooperatively adaptive surrogate strategy can improve the efficiency of solving RBDO under acceptable precision, and the average LCFL and the reliability can be improved simultaneously.
Keywords:Turbine shaft  Low cycle fatigue  Structure analysis  Reliability analysis  Optimal design  Parameterized platform
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