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contributor authorN. Klompas
date accessioned2017-05-08T23:15:38Z
date available2017-05-08T23:15:38Z
date copyrightJanuary, 1983
date issued1983
identifier issn1528-8919
identifier otherJETPEZ-26779#184_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97143
description abstractA new method is derived to calculate unbalance response of a complete turbomachine, including mount asymmetry, disk flexibility, and fluid-film bearing anisotropy by utilizing conventionally obtained stiffness coefficients for the rotor and stator. Formulation through the coordinates whirl and whip is in real variables with only eight equations per bearing. Whereas the stator is usually ignored, sample analysis illustrates possible strong influence of casing flexibility. Coordinate transformations to enhance visualization and verification of the solution are shown.
publisherThe American Society of Mechanical Engineers (ASME)
titleUnbalance Response Analysis of a Complete Turbomachine
typeJournal Paper
journal volume105
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3227385
journal fristpage184
journal lastpage191
identifier eissn0742-4795
keywordsTurbomachinery
keywordsBearings
keywordsPlasticity
keywordsStators
keywordsStiffness
keywordsAnisotropy
keywordsRotors
keywordsVisualization
keywordsDisks
keywordsEquations
keywordsFluid films AND Whirls
treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001
contenttypeFulltext


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