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contributor authorH. D. Nelson
contributor authorW. L. Meacham
contributor authorD. P. Fleming
contributor authorA. F. Kascak
date accessioned2017-05-08T23:15:28Z
date available2017-05-08T23:15:28Z
date copyrightJuly, 1983
date issued1983
identifier issn1528-8919
identifier otherJETPEZ-26783#606_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97074
description abstractThe method of component mode synthesis is developed to determine the forced response of nonlinear, multishaft, rotor-bearing systems. The formulation allows for simulation of system response due to blade loss, distributed unbalance, base shock, maneuver loads, and specified fixed frame forces. The motion of each rotating component of the system is described by superposing constraint modes associated with boundary coordinates and constrained precessional modes associated with internal coordinates. The precessional modes are truncated for each component and the reduced component equations are assembled with the nonlinear supports and interconnections to form a set of nonlinear system equations of reduced order. These equations are then numerically integrated to obtain the system response. A computer program, which is presently restricted to single shaft systems has been written and results are presented for transient system response associated with blade loss dynamics, with squeeze film dampers, and with interference rubs.
publisherThe American Society of Mechanical Engineers (ASME)
titleNonlinear Analysis of Rotor-Bearing Systems Using Component Mode Synthesis
typeJournal Paper
journal volume105
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3227460
journal fristpage606
journal lastpage614
identifier eissn0742-4795
keywordsBearings
keywordsRotors
keywordsEquations
keywordsBlades
keywordsComputer software
keywordsDampers
keywordsNonlinear systems
keywordsDynamics (Mechanics)
keywordsForce
keywordsMotion
keywordsSimulation
keywordsStress
keywordsStructural frames AND Shock (Mechanics)
treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003
contenttypeFulltext


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