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contributor authorMartel, Carlos
contributor authorMartín, Juan A.
date accessioned2022-02-04T23:04:06Z
date available2022-02-04T23:04:06Z
date copyright1/1/2020 12:00:00 AM
date issued2020
identifier issn0742-4795
identifier othergtp_142_01_011022.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4276035
description abstractThe estimation of the final vibration amplitude of a turbomachinery bladed disk is of extreme practical importance; it is an essential information for the prediction of the level of high cycle fatigue of the blades and for the subsequent estimation of its operative life span. The forced response vibration is saturated by the nonlinear damping introduced by the friction forces at the interfaces between blade and disk (and/or at the included dampers). The computation of the final amplitude of the limit cycle oscillation requires to solve a quite complicated nonlinear problem. In the case of a tuned bladed disk, this problem can be reduced to a single sector calculation with phase lag boundary conditions. The solution of this one-sector problem requires to consider many harmonics in order to capture the details of the nonlinear time periodic oscillation that sets in. If the small unavoidable differences among blades (mistuning) are also taken into account, then the situation becomes even more complicated because the solution of the mistuned vibration problem requires to consider not only a single sector but also the complete bladed disk. The possibility of applying multiple scales techniques to drastically simplify this problem is explored in this paper. The idea is to exploit the fact that all relevant effects present (forcing, nonlinear friction, and mistuning) are, in most practical situations, small effects that develop in a time scale that is much longer than that associated with the natural elastic vibration frequency of the tuned system. A mass-spring model with microslip nonlinear friction is used to represent the forced bladed disk. The multiple scales method is used to asymptotically derive simplified models for both tuned and mistuned configurations. The results of the asymptotic model are compared with those from the mass-spring system and used to analyze the particular characteristics of the nonlinear friction effects on the final vibration states.
publisherThe American Society of Mechanical Engineers (ASME)
titleAsymptotic Description of Forced Response Vibration Saturation by Friction Forces
typeJournal Paper
journal volume142
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4044934
journal fristpage011022-1
journal lastpage011022-8
page8
treeJournal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 001
contenttypeFulltext


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