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contributor authorE. Capiez-Lernout
contributor authorJ.-P. Lombard
contributor authorE. Seinturier
contributor authorC. Dupont
contributor authorC. Soize
date accessioned2017-05-09T00:16:06Z
date available2017-05-09T00:16:06Z
date copyrightJuly, 2005
date issued2005
identifier issn1528-8919
identifier otherJETPEZ-26871#621_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131775
description abstractThis paper deals with the characterization of the blade manufacturing geometric tolerances in order to get a given level of amplification in the forced response of a mistuned bladed-disk. The theory is based on the use of a nonparametric probabilistic model of blade random uncertainties. The dispersion parameters controlling the nonparametric model are estimated as a function of the geometric tolerances. The industrial application is devoted to the mistuning analysis of a 22 blades wide chord fan stage. Centrifugal stiffening due to rotational effects is also included. The results obtained validate the efficiency and the reliability of the method on three-dimensional bladed disks.
publisherThe American Society of Mechanical Engineers (ASME)
titleBlade Manufacturing Tolerances Definition for a Mistuned Industrial Bladed Disk
typeJournal Paper
journal volume127
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1850497
journal fristpage621
journal lastpage628
identifier eissn0742-4795
keywordsManufacturing
keywordsDisks
keywordsBlades
keywordsProbability AND Geometry
treeJournal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 003
contenttypeFulltext


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