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首页> 外文期刊>Journal of turbomachinery >A Reduced-Order Meshless Energy Model for the Vibrations of Mistimed Bladed Disks-Part Ⅰ: Theoretical Basis
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A Reduced-Order Meshless Energy Model for the Vibrations of Mistimed Bladed Disks-Part Ⅰ: Theoretical Basis

机译:错时叶片盘振动的降阶无网格能量模型-第一部分:理论基础

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摘要

In this paper, a reduced order model for the vibrations of bladed disk assemblies was achieved. The system studied was a 3D annulus of shroudless, "custom-tailored," mis-tuned blades attached to a flexible disk. Specifically, the annulus was modeled as a spectral-based "meshless" continuum structure utilizing only nodal data to describe the arbitrary volume in which the system's dynamical energy was minimized. An extended Ritz variational procedure was used to minimize this energy, subjected to constraints imposed by an assumed 3D displacement field of mathematically complete, orthonormal "blade-disk" polynomials multiplied by generalized coefficients. The coefficients were determined by constraining the polynomial series to satisfy the extended Ritz stationary equations and essential boundary conditions of the bladed disk. From this, the governing equations of motion were generated into their usual dynamical forms to calculate upper-bounds on the actual free and forced responses of bladed disks. No conventional finite elements and element connectivity or component substructuring data were needed. This paper, Part I, outlines the theoretical foundation of the present model, and through extensive Monte Carlo simulations, establishes the analytical basis, predictive accuracy, and re-analysis efficiency of the present technology in the prediction of 3D maximum response amplitude of mistuned bladed disks having increasing numbers of nodal diameter excitations. Further applications validating, the 3D approach against conventional finite element procedures of free and forced response prediction of a mistuned Integrally-Bladed Rotor used in practice is presented in a companion paper, Part Ⅱ (Fang, McGee, and El-Aini, 2013, "A Reduced-Order Meshless Energy Model for the Vibrations of Mistuned Bladed Disks-Part Ⅱ: Finite Element Benchmark Comparisons, ASME J. Turbom-ach., to be published.
机译:在本文中,获得了叶片盘组件振动的降阶模型。研究的系统是连接到软盘的3D无环,“定制化”,误调刀片的3D环。具体来说,环被建模为基于光谱的“无网格”连续体结构,仅使用节点数据来描述系统动能最小的任意体积。使用扩展的Ritz变分程序来使这种能量最小化,受到数学上完整的正交“叶片-磁盘”多项式的假定3D位移场乘以广义系数所施加的约束。通过约束多项式级数来满足这些系数,以满足扩展的Ritz平稳方程和叶片盘的基本边界条件。由此,将运动的控制方程式生成为它们通常的动力学形式,以计算叶片盘的实际自由响应和强制响应的上限。不需要常规的有限元和单元连接性或组件子结构数据。本文的第一部分概述了本模型的理论基础,并通过广泛的蒙特卡洛模拟,建立了本技术在预测雾化叶片的3D最大响应幅度方面的分析基础,预测精度和重新分析效率。节点直径激励次数不断增加的磁盘。进一步的应用程序验证,在附篇第二部分(Fang,McGee和El-Aini,2013年,“针对惯用的整体叶片转子的自由和强制响应预测的常规有限元程序的3D方法)在实践中进行了介绍”误调叶片磁盘振动的降阶无网格能量模型-第二部分:有限元基准比较,ASME J. Turbom-ach。将要出版。

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  • 来源
    《Journal of turbomachinery》 |2013年第6期|061001.1-061001.20|共20页
  • 作者单位

    Howard University, Washington, DC 20059;

    Postdoctoral Research Associate Howard University, Washington, DC 20059;

    Senior Fellow Pratt and Whitney Rocketdyne, West Palm Beach, FL 33401;

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