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contributor authorT. M. Cameron
contributor authorR. E. Kielb
contributor authorT. M. Hoosac
contributor authorJ. H. Griffin
date accessioned2017-05-08T23:34:16Z
date available2017-05-08T23:34:16Z
date copyrightApril, 1990
date issued1990
identifier issn1048-9002
identifier otherJVACEK-28791#175_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107852
description abstractA procedure is outlined for determining the optimal design of friction dampers for high-speed turbomachinery blading. The procedure includes: An integration of bench test results with finite-element analysis and a single-mode blade model to ensure accuracy of the analytical model and improve reliability of the friction damper design; an extension of the single-mode blade model to predict the engine behavior of friction dampers; and a new way of viewing analytical and experimental results in terms of a damper performance curve to determine optimal design parameters, when the levels of excitation and damping in the system are unknown. Unique experiments are performed on a test disk in order to demonstrate and verify the accuracy of the design procedure.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Integrated Approach for Friction Damper Design
typeJournal Paper
journal volume112
journal issue2
journal titleJournal of Vibration and Acoustics
identifier doi10.1115/1.2930110
journal fristpage175
journal lastpage182
identifier eissn1528-8927
keywordsFriction
keywordsDampers
keywordsDesign
keywordsBlades
keywordsTurbomachinery
keywordsFinite element analysis
keywordsDisks
keywordsDamping
keywordsEngines AND Reliability
treeJournal of Vibration and Acoustics:;1990:;volume( 112 ):;issue: 002
contenttypeFulltext


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