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    On the Vibration Isolation of Flexible Structures

    Source: Journal of Applied Mechanics:;2007:;volume( 074 ):;issue: 003::page 415
    Author:
    Y. Q. Tu
    ,
    G. T. Zheng
    DOI: 10.1115/1.2201882
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Although the study of vibration isolation has a very long history, when an isolated structure is so flexible that it cannot be properly approximated with a rigid body or a single-degree-of-freedom model, its vibration isolation brings about some new questions and problems. By transforming the dynamic equation of motion of the coupled structure formed by the isolator and the isolated structure into the modal space and following the tradition of studying features of the vibration transmissibility across the isolator, questions and problems associated with the flexible structure vibration isolation are studied. It is found from the study that a lower isolation frequency and a higher damping level can both increase the isolation effectiveness, the isolated structure is a vibration absorber to the isolator, and a combination of the vibration isolation and the vibration attenuation can be more effective in mitigating the vibration. A numerical example of the whole spacecraft vibration isolation has proved the above conclusions.
    keyword(s): Equations of motion , Vibration isolation , Flexible structures , Frequency , Resonance , Plasticity , Damping , Equations , Space vehicles , Vibration absorbers AND Vibration ,
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      On the Vibration Isolation of Flexible Structures

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    contributor authorY. Q. Tu
    contributor authorG. T. Zheng
    date accessioned2017-05-09T00:22:30Z
    date available2017-05-09T00:22:30Z
    date copyrightMay, 2007
    date issued2007
    identifier issn0021-8936
    identifier otherJAMCAV-26636#415_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135111
    description abstractAlthough the study of vibration isolation has a very long history, when an isolated structure is so flexible that it cannot be properly approximated with a rigid body or a single-degree-of-freedom model, its vibration isolation brings about some new questions and problems. By transforming the dynamic equation of motion of the coupled structure formed by the isolator and the isolated structure into the modal space and following the tradition of studying features of the vibration transmissibility across the isolator, questions and problems associated with the flexible structure vibration isolation are studied. It is found from the study that a lower isolation frequency and a higher damping level can both increase the isolation effectiveness, the isolated structure is a vibration absorber to the isolator, and a combination of the vibration isolation and the vibration attenuation can be more effective in mitigating the vibration. A numerical example of the whole spacecraft vibration isolation has proved the above conclusions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Vibration Isolation of Flexible Structures
    typeJournal Paper
    journal volume74
    journal issue3
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2201882
    journal fristpage415
    journal lastpage420
    identifier eissn1528-9036
    keywordsEquations of motion
    keywordsVibration isolation
    keywordsFlexible structures
    keywordsFrequency
    keywordsResonance
    keywordsPlasticity
    keywordsDamping
    keywordsEquations
    keywordsSpace vehicles
    keywordsVibration absorbers AND Vibration
    treeJournal of Applied Mechanics:;2007:;volume( 074 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian