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Statistics of response of a mistuned and frictionally damped bladed disk assembly subjected to random excitation.

机译:受到随机激励的雾化且摩擦阻尼的叶片盘组件的响应统计。

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摘要

In this thesis, analytical techniques have been developed to efficiently compute the statistics of the response of a mistuned bladed disk assembly (with and without friction dampers) subjected to random excitation. The accuracy of these analytical techniques has been tested by the simple discrete model which represents the basic characteristics of the blade disk vibration. Considering the circumferential pressure field of a turbomachinery, three different types of excitation are considered: white noise excitation, narrow band random excitation and sinusoidal excitation with unknown amplitudes. The narrow band random excitation can be generated as an output of the band-pass filter with the white noise as an input and the sinusoidal excitation with unknown amplitude is considered as a sinusoidal functions where the amplitude and phase shift are time-invariant random variables. The sensitivities of the response to mistuning have been examined as a function of the frequency bandwidth of random excitation and the structural coupling stiffness. Furthermore, the effects of correlation of narrow band excitation on the response variance of mistuned system are investigated.; To investigate the effect of normal load on the performance of a friction damper, the equivalent linearization method (ELM) is used for white noise and narrow band random excitations and the harmonic balance method (HBM) is used for sinusoidal excitation with unknown amplitudes. To examine the accuracy of ELM, the analytical results for a tuned and a mistuned system with friction dampers are compared with those from the numerical integration of differential equations. Then, the analytical techniques are used to calculate the statistics of response variance of a frictionally damped and mistuned bladed disk assembly subjected to random excitation. The performance of both types of friction dampers, blade-to-blade and blade-to-ground dampers, are represented by a new set of nondimensionalized variables, so that the optimal normal loads can be obtained without any direct information about the external force.
机译:在本文中,已经开发了分析技术来有效地计算受到随机激励的雾化叶片盘组件(带和不带摩擦阻尼器)的响应统计量。这些分析技术的准确性已通过简单的离散模型进行了测试,该模型代表了叶片盘振动的基本特征。考虑到涡轮机械的圆周压力场,考虑了三种不同类型的激励:白噪声激励,窄带随机激励和振幅未知的正弦激励。窄带随机激励可以作为带通滤波器的输出生成,白噪声作为输入,振幅未知的正弦激励被视为正弦函数,其中振幅和相移是时不变的随机变量。根据随机激励的频率带宽和结构耦合刚度,已检查了对失谐响应的敏感性。此外,研究了窄带激励的相关性对失谐系统响应方差的影响。为了研究正常负载对摩擦阻尼器性能的影响,等效线性化方法(ELM)用于白噪声和窄带随机激励,谐波平衡方法(HBM)用于振幅未知的正弦激励。为了检查ELM的精度,将带有摩擦阻尼器的调谐和雾化系统的分析结果与微分方程数值积分的结果进行了比较。然后,使用分析技术来计算受到随机激励的摩擦阻尼和雾化叶片盘组件的响应方差统计量。一组新型的无量纲变量代表了两种类型的摩擦阻尼器的性能:叶片到叶片阻尼器和叶片到地面阻尼器,因此可以获得最佳法向载荷,而无需任何有关外力的直接信息。

著录项

  • 作者

    Cha, Douksoon.;

  • 作者单位

    The Pennsylvania State University.;

  • 授予单位 The Pennsylvania State University.;
  • 学科 Engineering Mechanical.; Applied Mechanics.
  • 学位 Ph.D.
  • 年度 1999
  • 页码 186 p.
  • 总页数 186
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;应用力学;
  • 关键词

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