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contributor authorT. Berruti
contributor authorS. Salvano
contributor authorS. Filippi
contributor authorL. Goglio
contributor authorM. M. Gola
date accessioned2017-05-09T00:07:30Z
date available2017-05-09T00:07:30Z
date copyrightApril, 2002
date issued2002
identifier issn1528-8919
identifier otherJETPEZ-26812#388_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126791
description abstractThe paper describes the development of an instrumented test rig suitable to carry out vibration testing of the bladed segments of a turbine (belonging to a stator low pressure stage) in which the friction occurring at the contact of neighboring segments is used in service to damp the vibrations. The system is able to assign the desired preload to the segment and to measure the forces exerted in the contact and the relative displacements due to slipping. The main results that can be obtained concern the type of motion that takes place (stick/slip) and the effect of the interlocking on it, the friction coefficients, the contact tangential stiffness, and, more generally, the frequency response.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Test Rig for Frictionally Damped Bladed Segments
typeJournal Paper
journal volume124
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1419015
journal fristpage388
journal lastpage394
identifier eissn0742-4795
keywordsForce
keywordsFriction
keywordsCalibration
keywordsDisplacement
keywordsStiffness
keywordsVibration
keywordsMotion
keywordsSignals
keywordsStrain gages
keywordsStructural frames
keywordsTransducers AND Frequency response
treeJournal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 002
contenttypeFulltext


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