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    A Field Balancing Technique Based on Virtual Trial Weights Method for a Magnetically Levitated Flexible Rotor

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 009::page 92502
    Author:
    Wang, Yingguang
    ,
    Fang, Jiancheng
    ,
    Zheng, Shiqiang
    DOI: 10.1115/1.4027214
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: For 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.
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      A Field Balancing Technique Based on Virtual Trial Weights Method for a Magnetically Levitated Flexible Rotor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/154798
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    • Journal of Engineering for Gas Turbines and Power

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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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