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contributor authorOscar C. De Santiago
contributor authorLuis San Andrés
date accessioned2017-05-09T00:23:50Z
date available2017-05-09T00:23:50Z
date copyrightJanuary, 2007
date issued2007
identifier issn1528-8919
identifier otherJETPEZ-26935#205_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135788
description abstractA simple procedure, with the potential as a field resource, for identification of a bearing support parameter from recorded transient rotor responses due to impact loads follows. The method is applied to a test rotor supported on a pair of mechanically complex bearing supports, each comprising a tilting pad bearing in series with an integral squeeze film damper. Identification of frequency dependent bearing force coefficients is good at a rotor speed of 2000 rpm. Stiffness coefficients are best identified in the low frequency range (below 25 Hz) while damping coefficients are best identified in the vicinity of the first natural frequency (48 Hz) of the rotor bearing system. The procedure shows that using multiple-impact frequency averaged rotor responses reduces the variability in the identified parameters. The identification of frequency-dependent force coefficients at a constant rotor speed is useful to assess rotor-bearing system stability.
publisherThe American Society of Mechanical Engineers (ASME)
titleField Methods for Identification of Bearng Support Parameters—Part I: Identification From Transient Rotor Dynamic Response due to Impacts
typeJournal Paper
journal volume129
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2227033
journal fristpage205
journal lastpage212
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001
contenttypeFulltext


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