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    A Chambered Porous Damper for Rotor Vibration Control: Part I—Concept Development

    Source: Journal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 002::page 360
    Author:
    J. Tecza
    ,
    J. Walton
    DOI: 10.1115/1.2906717
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper a novel, high-load chambered porous damper design, supporting analysis, and experimental results are presented. It was demonstrated that significant damping can be generated from the viscous discharge losses of capillary tubes arranged in chambered segments with large radial clearances and that the resulting damping is predictable and fairly constant with speed and eccentricity ratio. This design avoids the nonlinearities associated with high-eccentricity operation of conventional squeeze film dampers. Controlled orbit tests with a porous chambered configuration were completed and favorably compared with theoretical predictions. The ability to accommodate high steady-state and transient imbalance conditions makes this damper well suited to a wide range of rotating machinery, including aircraft gas turbine engines.
    keyword(s): Dampers , Rotor vibration , Damping , Design , Gas turbines , Aircraft , Steady state , Machinery AND Stress ,
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      A Chambered Porous Damper for Rotor Vibration Control: Part I—Concept Development

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/111941
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. Tecza
    contributor authorJ. Walton
    date accessioned2017-05-08T23:41:20Z
    date available2017-05-08T23:41:20Z
    date copyrightApril, 1993
    date issued1993
    identifier issn1528-8919
    identifier otherJETPEZ-26715#360_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111941
    description abstractIn this paper a novel, high-load chambered porous damper design, supporting analysis, and experimental results are presented. It was demonstrated that significant damping can be generated from the viscous discharge losses of capillary tubes arranged in chambered segments with large radial clearances and that the resulting damping is predictable and fairly constant with speed and eccentricity ratio. This design avoids the nonlinearities associated with high-eccentricity operation of conventional squeeze film dampers. Controlled orbit tests with a porous chambered configuration were completed and favorably compared with theoretical predictions. The ability to accommodate high steady-state and transient imbalance conditions makes this damper well suited to a wide range of rotating machinery, including aircraft gas turbine engines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Chambered Porous Damper for Rotor Vibration Control: Part I—Concept Development
    typeJournal Paper
    journal volume115
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906717
    journal fristpage360
    journal lastpage365
    identifier eissn0742-4795
    keywordsDampers
    keywordsRotor vibration
    keywordsDamping
    keywordsDesign
    keywordsGas turbines
    keywordsAircraft
    keywordsSteady state
    keywordsMachinery AND Stress
    treeJournal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 002
    contenttypeFulltext
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