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contributor authorChaw-Wu Tseng
contributor authorMechanical Engineer
contributor authorJr-Yi Shen
contributor authorMechanical Engineer
contributor authorHyunchul Kim
contributor authorI. Y. Shen
date accessioned2017-05-09T00:18:23Z
date available2017-05-09T00:18:23Z
date copyrightApril, 2005
date issued2005
identifier issn1048-9002
identifier otherJVACEK-28873#125_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/132913
description abstractThis paper demonstrates a unified approach to analyze linear vibration of rotating machines with arbitrary geometry and complexity. In this formulation, the rotating machine consists of three components: a rotating part (rotor), a stationary part (stator or housing), and multiple bearings. The rotor is assumed axisymmetric and spinning at constant speed. Moreover, the rotor and the housing have arbitrary geometry and complexity. The bearings connecting the rotor and housing could be rolling-element bearings or hydrodynamic bearings. The paper consists of three major sections: mathematical modeling, integration with finite element analysis (FEA), and experimental verification. For the mathematical modeling, a stationary rotor with free boundary conditions is first discretized to obtain its normal vibration modes and modal parameters. In the meantime, the housing with its actual boundary conditions (but no bearings) is also discretized. The discretization can be achieved, for example, through FEA to accommodate arbitrary and complex geometry of the rotor and the housing. Because these vibration modes are complete, modal response of each mode can serve as a generalized coordinate to describe vibration of the actual spinning rotor and housing system. With these generalized coordinates, gyroscopic effects of the spinning rotor can be derived through material derivatives for a ground-based observer. As a result, application of Lagrange equation leads to a set of gyroscopic equations of motion with constant coefficients. These coefficients, however, contain complicated volume integrals of the mode shapes and their spatial derivatives. Therefore, algorithms are developed to calculate these coefficients explicitly from FEA. For the experimental verification, a ball-bearing spindle carrying a cylinder closed at one end is used to validate the mathematical model. Frequency response functions of the spindle/cylinder system are measured for spin speed ranging from 0 to 6000 rpm. Natural frequencies measured from the experiments agree very well with the theoretical predictions from the unified approach up to 2 kHz.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Unified Approach to Analyze Vibration of Axisymmetric Rotating Structures with Flexible Stationary Parts
typeJournal Paper
journal volume127
journal issue2
journal titleJournal of Vibration and Acoustics
identifier doi10.1115/1.1857917
journal fristpage125
journal lastpage138
identifier eissn1528-8927
keywordsForce
keywordsSpindles (Textile machinery)
keywordsBearings
keywordsFinite element analysis
keywordsRotors
keywordsVibration
keywordsFrequency
keywordsShapes
keywordsParticle spin
keywordsDeformation
keywordsEquations of motion
keywordsGeometry
keywordsMachinery
keywordsCylinders
keywordsBoundary-value problems AND Equations
treeJournal of Vibration and Acoustics:;2005:;volume( 127 ):;issue: 002
contenttypeFulltext


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