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    Resonance Suppression in Multi-Degree-of-Freedom Rotating Flexible Structures Using Order-Tuned Absorbers

    Source: Journal of Vibration and Acoustics:;2012:;volume( 134 ):;issue: 006::page 61016
    Author:
    Serif Gozen
    ,
    Brian J. Olson
    ,
    Steven W. Shaw
    ,
    Christophe Pierre
    DOI: 10.1115/1.4007564
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper considers the dynamic response and order-tuning of vibration absorbers fitted to a rotating flexible structure under traveling wave (TW) engine order excitation. Of specific interest is the extension of previous results on the so-called no-resonance zone, that is, a region in linear tuning parameter space in which the coupled structure/absorber system does not experience resonance over all rotation speeds. The no-resonance feature was shown to exist for cyclic rotating structures with one structural and one absorber degree of freedom (DOF) per sector. This work uses a higher-fidelity structural model to investigate the effects of higher modes on the cyclically-coupled system. It is shown that the no-resonance zone is replaced by a resonance-suppression zone in which one structural mode is suppressed, but higher-order resonances still exist with the addition of the absorbers. The results are general in the sense that one vibration mode can be eliminated using a set of identically-tuned absorbers on a rotating structure with arbitrarily many DOFs per sector.
    keyword(s): Resonance , Rotors , Disks , Blades , Flexible structures , Vibration , Vibration absorbers AND Rotation ,
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      Resonance Suppression in Multi-Degree-of-Freedom Rotating Flexible Structures Using Order-Tuned Absorbers

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    https://yetl.yabesh.ir/yetl1/handle/yetl/150599
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    contributor authorSerif Gozen
    contributor authorBrian J. Olson
    contributor authorSteven W. Shaw
    contributor authorChristophe Pierre
    date accessioned2017-05-09T00:55:29Z
    date available2017-05-09T00:55:29Z
    date copyright41244
    date issued2012
    identifier issn1048-9002
    identifier otherJVACEK-926529#vib_134_6_061016.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/150599
    description abstractThis paper considers the dynamic response and order-tuning of vibration absorbers fitted to a rotating flexible structure under traveling wave (TW) engine order excitation. Of specific interest is the extension of previous results on the so-called no-resonance zone, that is, a region in linear tuning parameter space in which the coupled structure/absorber system does not experience resonance over all rotation speeds. The no-resonance feature was shown to exist for cyclic rotating structures with one structural and one absorber degree of freedom (DOF) per sector. This work uses a higher-fidelity structural model to investigate the effects of higher modes on the cyclically-coupled system. It is shown that the no-resonance zone is replaced by a resonance-suppression zone in which one structural mode is suppressed, but higher-order resonances still exist with the addition of the absorbers. The results are general in the sense that one vibration mode can be eliminated using a set of identically-tuned absorbers on a rotating structure with arbitrarily many DOFs per sector.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleResonance Suppression in Multi-Degree-of-Freedom Rotating Flexible Structures Using Order-Tuned Absorbers
    typeJournal Paper
    journal volume134
    journal issue6
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.4007564
    journal fristpage61016
    identifier eissn1528-8927
    keywordsResonance
    keywordsRotors
    keywordsDisks
    keywordsBlades
    keywordsFlexible structures
    keywordsVibration
    keywordsVibration absorbers AND Rotation
    treeJournal of Vibration and Acoustics:;2012:;volume( 134 ):;issue: 006
    contenttypeFulltext
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