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contributor authorWang, Yingguang
contributor authorFang, Jiancheng
contributor authorZheng, Shiqiang
date accessioned2017-05-09T01:07:55Z
date available2017-05-09T01:07:55Z
date issued2014
identifier issn1528-8919
identifier othergtp_136_09_092502.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154798
description abstractFor a magnetically levitated flexible rotor (MLFR), the amount of residual imbalance not only generates undesired vibrations, but also results in excessive bending, which may cause it hit to the auxiliary bearings. Thus, balancing below the critical speed is essential for the MLFR to prevent the impact. This paper proposes a balancing method of high precision and high efficiency, basing on virtual trialweights. First, to reduce the computed error of rotor's mode shapes, a synchronous notch filter is inserted into the active magnetic bearing (AMB) controller, achieving a free support status. Then, AMBs provide the rotor with the synchronous electromagnetic forces (SEFs) to simulate the trialweights. The SEFs with the initial angles varying from 0 deg to 360 deg in the rotational frame system result in continuous changes in the MLFR's deflection. Last, correction masses are calculated according to the changes. Compared to the trailweights method, the new method needs not testruns, which improves the balancing efficiency. Compared to the no trailweights method, the new method does not require a precise model of the rotorbearing system, which is difficult to acquire in the real system. Experiment results show that the novel method can reduce the residual imbalance effectively and accurately.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Field Balancing Technique Based on Virtual Trial Weights Method for a Magnetically Levitated Flexible Rotor
typeJournal Paper
journal volume136
journal issue9
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4027214
journal fristpage92502
journal lastpage92502
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 009
contenttypeFulltext


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