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contributor authorM. Botman
date accessioned2017-05-08T23:00:35Z
date available2017-05-08T23:00:35Z
date copyrightJuly, 1976
date issued1976
identifier issn1528-8919
identifier otherJETPEZ-26726#393_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88571
description abstractOil-film dampers are used in turbomachinery to suppress undesirable shaft dynamic responses. They are located at the nonrotating outer race of selected main bearings. A rig is described that was designed to evaluate the effect of damper geometry on the rotor responses. Typical test results are shown which indicate that cavitation limits the maximum speed at which dampers should be used. Below cavitation speed the effect of the damper appears predictable with existing theory. More tests are required to substantiate this. At high speeds the damper generates nonsynchronous motion. The damper may have a significant effect on the stiffness of the support felt by the rotor.
publisherThe American Society of Mechanical Engineers (ASME)
titleExperiments on Oil-Film Dampers for Turbomachinery
typeJournal Paper
journal volume98
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3446195
journal fristpage393
journal lastpage399
identifier eissn0742-4795
keywordsDampers
keywordsTurbomachinery
keywordsRotors
keywordsCavitation
keywordsBearings
keywordsMotion
keywordsFelts
keywordsDynamic response
keywordsGeometry AND Stiffness
treeJournal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 003
contenttypeFulltext


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