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contributor authorM. S. Darlow
contributor authorA. G. Parkinson
contributor authorA. J. Smalley
date accessioned2017-05-08T23:11:10Z
date available2017-05-08T23:11:10Z
date copyrightJanuary, 1981
date issued1981
identifier issn1528-8919
identifier otherJETPEZ-26763#101_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94564
description abstractA flexible rotor balancing procedure, which incorporates the advantages and eliminates the disadvantages of the modal and influence coefficient procedures, has been developed and implemented. This new procedure, referred to as the Unified Balancing Approach, has been demonstrated on a supercritical power transmission shaft test rig. The test rig was successfully balanced through four flexural critical speeds with a substantial reduction in effort as compared with the effort required in modal and influence coefficient balancing procedures. A brief discussion of the Unified Balancing Approach and its relationship to the modal and influence coefficient methods is presented. A series of tests which were performed to evaluate the effectiveness of various balancing techniques are described. The results of the Unified Balancing Approach tests are presented and discussed. These results confirm the superiority of this balancing procedure for the supercritical shaft test rig in particular and for multiple-mode balancing in general.
publisherThe American Society of Mechanical Engineers (ASME)
titleDemonstration of a Unified Approach to the Balancing of Flexible Rotors
typeJournal Paper
journal volume103
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3230679
journal fristpage101
journal lastpage107
identifier eissn0742-4795
keywordsRotor balancing AND Rotors
treeJournal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 001
contenttypeFulltext


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