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Forced response of mistuned bladed disks: Identification and prediction.

机译:雾状刀片盘的强制响应:识别和预测。

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摘要

The present investigation focuses on the dynamic analysis of randomly mistuned bladed disks. In particular, various techniques are employed to obtain reliable estimates of the probability density function of the amplitude of blade response corresponding to a harmonic excitation. First, the applicability of the combined Closed Form-Perturbation (CFP) method is demonstrated for both stiffness and damping mistuning under resonant excitation. To this end, a new numerical algorithm is presented that permits a computationally efficient evaluation of the linearized probability density function of the amplitude of blade vibration. The results of the damping mistuning analysis demonstrate in particular the potentially damaging effects of blade-to-blade changes in damping coefficients and emphasize the need to model such variations.; Next, an adaptive perturbation scheme is introduced for the determination of the forced vibration response of mistuned bladed disks. The versatility of the proposed approach not only guarantees the reliability of the computed response but also leads to an excellent compromise between accuracy and computational effort. The limiting case of a disk supporting an infinite number of blades is considered next to yield the corresponding limit distribution of the amplitude of blade response. This exact asymptotic result can be used in connection with a small size Monte Carlo simulation to produce extremely accurate estimates of the probability density function of blade amplitude in a computationally efficient way.; Finally, the estimation of the parameters of a structural model to represent "at best" a set of measurements of the steady state response of a mistuned bladed disk is achieved by relying on a new technique that combines the advantages of the least squares and maximum likelihood identification methods.
机译:本研究侧重于随机雾化的叶片盘的动态分析。特别地,采用各种技术来获得与谐波激励相对应的叶片响应的振幅的概率密度函数的可靠估计。首先,证明了组合式闭合形式扰动(CFP)方法在共振激励下对于刚度和阻尼微扰的适用性。为此,提出了一种新的数值算法,该算法允许对叶片振动幅度的线性化概率密度函数进行有效的计算评估。阻尼失谐分析的结果特别表明了叶片间的阻尼系数变化的潜在破坏作用,并强调了对这种变化建模的需求。接下来,介绍了一种自适应摄动方案,用于确定雾化叶片盘的强制振动响应。所提出方法的多功能性不仅保证了所计算响应的可靠性,而且导致了准确性与计算工作之间的极佳折衷。接下来考虑支持无限数量的叶片的盘的极限情况,以产生叶片响应幅度的相应极限分布。该精确的渐近结果可以与小尺寸的蒙特卡洛模拟结合使用,以高效计算的方式对叶片振幅的概率密度函数进行极精确的估计。最后,依靠一种结合了最小二乘和最大似然性优点的新技术,可以估算结构模型的参数,以“最好”地表示一组雾化刀片式磁盘的稳态响应测量值。识别方法。

著录项

  • 作者

    Lin, Chung-Chih.;

  • 作者单位

    Arizona State University.;

  • 授予单位 Arizona State University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1994
  • 页码 182 p.
  • 总页数 182
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业 ;
  • 关键词

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