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Substructure-based distributed collaborative probabilistic analysis method for low-cycle fatigue damage assessment of turbine blade-disk

机译:涡轮叶片低周疲劳损伤评估的基于子结构的分布式协同概率分析方法

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摘要

A numerical simulation-based probabilistic analysis methodology, substructure-based distributed collaborative probabilistic analysis method (SDCPAM), is proposed for accurate and efficient fatigue prognosis based on distributed collaborative response surface method (DCRSM) and substructure analysis method. This paper focuses on the low-cycle fatigue (LCF) damage assessment for turbine blade–disk system. Based on the established probabilistic strain–life models and fatigue reliability model for tandem system, the LCF damage principle of turbine blade–disk system is proposed and integrated with SDCPAM. Following that, the LCF life prediction of the turbine blade–disk is completed, and probabilistic sensitivity analyses of blade and disk to the LCF life of the turbine blade–disk system are achieved. According to the above efforts, the feasibility and effectiveness of SDCPAM is verified. Finally, the LCF damage assessment for the blade–disk system is accomplished, and the influences of applied cycle and reliability level on the LCF damage are investigated. Through the comparisons of the proposed with traditional fatigue reliability model, it is illustrated that the proposed fatigue reliability model is reasonable. The results show that blade and disk almost have the same great influence on the blade–disk LCF life. In addition, applied cycles under normal and lognormal distributions produce the same LCF damage reliability that decreases with increasing applied cycle and reliability level. The efforts of this study indicate the reasonability of the proposed method and models in describing the LCF damage reliability of the blade–disk system, and enrich the reliability theory and method for the complex structure with multi-component and multi-failure mode.
机译:提出了一种基于数值模拟的概率分析方法,基于子结构的分布式协同概率分析方法(SDCPAM),用于基于分布式协同响应面方法(DCRSM)和子结构分析方法的准确,高效的疲劳预测。本文着重于涡轮叶片系统的低周疲劳(LCF)损伤评估。基于已建立的串列系统的概率应变寿命模型和疲劳可靠性模型,提出了涡轮叶片盘系统的LCF损伤原理,并与SDCPAM集成。随后,完成了涡轮叶片盘的LCF寿命预测,并完成了叶片和盘对涡轮叶片盘系统LCF寿命的概率敏感性分析。通过以上努力,验证了SDCPAM的可行性和有效性。最后,完成了对刀片磁盘系统的LCF损伤评估,并研究了应用周期和可靠性水平对LCF损伤的影响。通过与传统疲劳可靠性模型的比较,表明所提出的疲劳可靠性模型是合理的。结果表明,刀片和磁盘对刀片-磁盘LCF寿命的影响几乎相同。此外,在正态分布和对数正态分布下应用的循环会产生相同的LCF破坏可靠性,但随着应用循环和可靠性水平的提高而降低。这项研究的努力表明了所提出的方法和模型在描述叶片-磁盘系统的LCF损伤可靠性方面的合理性,并丰富了具有多成分和多失效模式的复杂结构的可靠性理论和方法。

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