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contributor authorB.-K. Choi
contributor authorJ. Lentz
contributor authorA. J. Rivas-Guerra
contributor authorM. P. Mignolet
date accessioned2017-05-09T00:10:17Z
date available2017-05-09T00:10:17Z
date copyrightJanuary, 2003
date issued2003
identifier issn1528-8919
identifier otherJETPEZ-26819#131_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/128422
description abstractThe focus of the present investigation is on the use of intentional mistuning of bladed disks to reduce their sensitivity to unintentional random mistuning. The class of intentionally mistuned disks considered here is limited, for cost reasons, to arrangements of two types of blades (A and B, say). A two-step procedure is then described to optimize the arrangement of these blades around the disk to reduce the effects of unintentional mistuning. First, a pure optimization effort is undertaken to obtain the pattern(s) of the A and B blades that yields small/the smallest value of the largest amplitude of response to a given excitation in the absence of unintentional mistuning. Then, in the second step, a pattern screening technique based on a recently introduced measure of localization is used to determine which of the patterns does have a large/small sensitivity to random unintentional mistuning. In this manner, expensive Monte Carlo simulations can be eliminated. Examples of application involving both simple bladed disk models and a 17-blade industrial rotor clearly demonstrate the significant benefits of using this class of intentionally mistuned disks.
publisherThe American Society of Mechanical Engineers (ASME)
titleOptimization of Intentional Mistuning Patterns for the Reduction of the Forced Response Effects of Unintentional Mistuning: Formulation and Assessment
typeJournal Paper
journal volume125
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1498270
journal fristpage131
journal lastpage140
identifier eissn0742-4795
keywordsOptimization
keywordsDisks
keywordsBlades AND Rotors
treeJournal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 001
contenttypeFulltext


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