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contributor authorAnoop K. Dhingra
contributor authorJuan I. Hidalgo
date accessioned2017-05-09T00:27:50Z
date available2017-05-09T00:27:50Z
date copyrightSeptember, 2008
date issued2008
identifier issn1528-8919
identifier otherJETPEZ-27035#054503_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137887
description abstractTurbosets used in power generation industry are frequently placed on flexible foundations, which significantly influence the overall dynamics. Establishment of structural models that capture the rotor and foundation effects reliably using finite element modeling or modal analysis is difficult because of model complexity and/or costs involved. This paper presents a method to extract modal parameter information of a turboset using frequency response function data recorded during high speed balancing. The main advantage of the present method over the others is the low cost and small effort involved, so that it is of practical use in an industrial setting. A real life example dealing with parameter extraction for a large generator rotor is presented to demonstrate its implementation.
publisherThe American Society of Mechanical Engineers (ASME)
titleModal Parameter Extraction of a Turboset From High Speed Balance Data
typeJournal Paper
journal volume130
journal issue5
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2938275
journal fristpage54503
identifier eissn0742-4795
keywordsTransfer functions
keywordsBearings
keywordsRotors
keywordsGenerators
keywordsPolynomials AND Vibration
treeJournal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 005
contenttypeFulltext


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