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contributor authorCorso Padova
contributor authorSteve Manwaring
contributor authorMaurice Adams
contributor authorMichael Adams
contributor authorGamaliel Young
contributor authorJeffrey Barton
contributor authorMichael G. Dunn
date accessioned2017-05-09T00:18:05Z
date available2017-05-09T00:18:05Z
date copyrightOctober, 2005
date issued2005
identifier issn0889-504X
identifier otherJOTUEI-28723#726_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/132772
description abstractAn experimental capability using an in-ground spin-pit facility specifically designed to investigate aeromechanic phenomena for gas turbine engine hardware rotating at engine speed is demonstrated herein to obtain specific information related to prediction and modeling of blade-casing interactions. Experiments are designed to allow insertion of a segment of engine casing into the path of single-bladed or multiple-bladed disks. In the current facility configuration, a 90deg sector of a representative engine casing is forced to rub the tip of a single-bladed compressor disk for a selected number of rubs with predetermined blade incursion into the casing at rotational speeds in the vicinity of 20,000rpm.
publisherThe American Society of Mechanical Engineers (ASME)
titleDevelopment of an Experimental Capability to Produce Controlled Blade Tip∕Shroud Rubs at Engine Speed
typeJournal Paper
journal volume127
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1934429
journal fristpage726
journal lastpage735
identifier eissn1528-8900
keywordsEngines
keywordsBlades AND Stress
treeJournal of Turbomachinery:;2005:;volume( 127 ):;issue: 004
contenttypeFulltext


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