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contributor authorL. E. Barrett
contributor authorE. J. Gunter
contributor authorP. E. Allaire
date accessioned2017-05-08T23:04:46Z
date available2017-05-08T23:04:46Z
date copyrightJanuary, 1978
date issued1978
identifier issn1528-8919
identifier otherJETPEZ-26739#89_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/91029
description abstractThis paper presents a rapid approximate method for calculating the optimum bearing or support damping for multimass flexible rotors to minimize unbalance response and to maximize stability in the vicinity of the rotor first critical speed. A multimass rotor is represented by an equivalent single-mass model for purposes of the analysis. The optimum bearing damping is expressed as a function of the bearing stiffness and rotor modal stiffness at the rigid bearing critical speed. Stability limits for aerodynamic cross coupling and viscous internal rotor friction damping are also presented. Comparison of the optimum damping obtained by this approximate method with that obtained by full scale linearized transfer matrix methods for several rotor-bearing configurations shows good agreement. The method has the advantage of being quickly and easily applied and can reduce analysis time by eliminating a time consuming search for the approximate optimum damping using more exact methods.
publisherThe American Society of Mechanical Engineers (ASME)
titleOptimum Bearing and Support Damping for Unbalance Response and Stability of Rotating Machinery
typeJournal Paper
journal volume100
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3446331
journal fristpage89
journal lastpage94
identifier eissn0742-4795
keywordsMachinery
keywordsBearings
keywordsDamping
keywordsStability
keywordsRotors
keywordsStiffness AND Friction
treeJournal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 001
contenttypeFulltext


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