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contributor authorDavid P. Fleming
date accessioned2017-05-08T23:21:21Z
date available2017-05-08T23:21:21Z
date copyrightApril, 1985
date issued1985
identifier issn0742-4787
identifier otherJOTRE9-28443#274_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/100496
description abstractSqueeze film dampers are widely used to control vibrations in aircraft turbine engines and other rotating machinery. However, if shaft unbalance rises appreciably above the design value (e.g., due to a turbine blade loss), a conventional squeeze film will be overloaded, and will no longer be effective in controlling vibration amplitudes and bearing forces. This paper describes a new damper concept characterized by two oil films. Under normal conditions, only one low-clearance film is active, allowing precise location of the shaft centerline. Under high unbalance conditions, both films are active, controlling shaft vibration in a near-optimum manner, and allowing continued operation until a safe shutdown can be made.
publisherThe American Society of Mechanical Engineers (ASME)
titleDual Clearance Squeeze Film Damper for High Load Conditions
typeJournal Paper
journal volume107
journal issue2
journal titleJournal of Tribology
identifier doi10.1115/1.3261045
journal fristpage274
journal lastpage278
identifier eissn1528-8897
keywordsStress
keywordsClearances (Engineering)
keywordsDampers
keywordsVibration
keywordsAircraft
keywordsDesign
keywordsGas turbines
keywordsBearings
keywordsTurbine blades
keywordsForce AND Machinery
treeJournal of Tribology:;1985:;volume( 107 ):;issue: 002
contenttypeFulltext


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