Identification and Estimation of Damage Severity in a Turbine Blade Packet Using Inverse Eigen-Value Analysis—A Numerical Study

IF 2 Q2 ENGINEERING, MULTIDISCIPLINARY
Animesh Chatterjee
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引用次数: 1

Abstract

Turbine blades are critical machine components in power plants and aerospace turbo engines. Failure of these blades in operation leads to catastrophic damages as well as high cost of maintenance and repair. Blades are often assembled in packets with lacing wire or shroud ring interconnections. Natural frequencies of the bladed packets are designed in a specific range to avoid possible resonant stresses. However, frequent damages during operation alter the stiffness of the blade-packet assembly and change the eigen-spectrum. A numerical study is presented in this work, where it is demonstrated that characteristic changes in eigen-spectrum can identify both severity and location of such damages. The work employs matrix perturbation theory on the eigen-value problem, formulated from the lumped-parameter modeling of the blade packet. Damage is considered as a perturbation in the stiffness matrix with damage severity acting as the perturbation parameter. First, a graphical pattern recognition method, and then, a damage proximity index evaluation method is suggested for damage identification. Further, an estimation algorithm for damage severity is presented with numerically simulated computations, which demonstrates that the methods can exactly identify the damage location and, with very little error, can estimate the damage severity.
基于逆特征值分析的涡轮叶片包损伤程度识别与估计数值研究
涡轮叶片是发电厂和航空涡轮发动机的关键部件。这些叶片在运行中出现故障会导致灾难性的损坏以及高昂的维护和维修成本。叶片通常用带线或护罩环连接在一起组装成包。叶片包的固有频率被设计在一个特定的范围内,以避免可能的谐振应力。然而,在运行过程中,频繁的损伤会改变叶片包组件的刚度,并改变特征谱。在这项工作中提出了一项数值研究,其中证明了特征谱的特征变化可以识别这种损伤的严重程度和位置。本文将矩阵摄动理论应用于特征值问题,该问题由叶片包的集总参数建模得到。将损伤视为刚度矩阵中的扰动,损伤程度作为扰动参数。首先提出了一种图形模式识别方法,然后提出了损伤接近度评价方法进行损伤识别。通过数值模拟计算,提出了一种损伤严重程度的估计算法,结果表明,该方法能准确识别损伤位置,并能以很小的误差估计损伤严重程度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
3.80
自引率
9.10%
发文量
25
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