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    Identification of Rotordynamic Force Coefficients of a Metal Mesh Foil Bearing Using Impact Load Excitations

    Source: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 011::page 112501
    Author:
    Luis San Andrés
    ,
    Thomas Abraham Chirathadam
    DOI: 10.1115/1.4002658
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Metal mesh foil bearings (MMFBs) are inexpensive compliant gas bearing type that aim to enable high speed, high temperature operation of small turbomachinery. A MMFB with an inner diameter of 28.00 mm and length of 28.05 mm is constructed with low cost and common materials. The bearing incorporates a copper mesh ring, 20% in compactness, and offering large material damping beneath a 0.127 mm thick preformed top foil. Prior experimentations (published papers) provide the bearing structure force coefficients and the break away torque for bearing lift off. Presently, the MMFB replaces a compressor in a small turbocharger driven test rig. Impact load tests aid to identify the direct and cross-coupled rotor dynamic force coefficients of the floating MMFB while operating at a speed of 50 krpm. Tests conducted with and without shaft rotation show the MMFB direct stiffness is less than its structural (static) stiffness, ∼25% lower at an excitation frequency of 200 Hz. The thin air film acting in series with the metal mesh support and separating the rotating shaft and the bearing inner surface while airborne reduces the bearing stiffness. The equivalent viscous damping is nearly identical with and without shaft rotation. The identified loss factor, best representing the hysteretic type damping from the metal mesh, is high at ∼0.50 in the frequency range 0–200 Hz. This magnitude reveals large mechanical energy dissipation ability from the MMFB. The measurements also show appreciable cross directional motions from the unidirectional impact loads, thus generating appreciable cross-coupled force coefficients. Rotor speed coast down measurements reveal pronounced subsynchronous whirl motion amplitudes locked at distinct frequencies. The MMFB stiffness hardening nonlinearity produces the rich frequency forced response. The synchronous as well as subsynchronous motions peak while the shaft traverses its critical speeds. The measurements establish reliable operation of the test MMFB while airborne.
    keyword(s): Force , Stress , Bearings , Rotors , Metals , Rotation , Damping , Stiffness AND Motion ,
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      Identification of Rotordynamic Force Coefficients of a Metal Mesh Foil Bearing Using Impact Load Excitations

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    http://yetl.yabesh.ir/yetl1/handle/yetl/145902
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorLuis San Andrés
    contributor authorThomas Abraham Chirathadam
    date accessioned2017-05-09T00:43:26Z
    date available2017-05-09T00:43:26Z
    date copyrightNovember, 2011
    date issued2011
    identifier issn1528-8919
    identifier otherJETPEZ-27176#112501_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/145902
    description abstractMetal mesh foil bearings (MMFBs) are inexpensive compliant gas bearing type that aim to enable high speed, high temperature operation of small turbomachinery. A MMFB with an inner diameter of 28.00 mm and length of 28.05 mm is constructed with low cost and common materials. The bearing incorporates a copper mesh ring, 20% in compactness, and offering large material damping beneath a 0.127 mm thick preformed top foil. Prior experimentations (published papers) provide the bearing structure force coefficients and the break away torque for bearing lift off. Presently, the MMFB replaces a compressor in a small turbocharger driven test rig. Impact load tests aid to identify the direct and cross-coupled rotor dynamic force coefficients of the floating MMFB while operating at a speed of 50 krpm. Tests conducted with and without shaft rotation show the MMFB direct stiffness is less than its structural (static) stiffness, ∼25% lower at an excitation frequency of 200 Hz. The thin air film acting in series with the metal mesh support and separating the rotating shaft and the bearing inner surface while airborne reduces the bearing stiffness. The equivalent viscous damping is nearly identical with and without shaft rotation. The identified loss factor, best representing the hysteretic type damping from the metal mesh, is high at ∼0.50 in the frequency range 0–200 Hz. This magnitude reveals large mechanical energy dissipation ability from the MMFB. The measurements also show appreciable cross directional motions from the unidirectional impact loads, thus generating appreciable cross-coupled force coefficients. Rotor speed coast down measurements reveal pronounced subsynchronous whirl motion amplitudes locked at distinct frequencies. The MMFB stiffness hardening nonlinearity produces the rich frequency forced response. The synchronous as well as subsynchronous motions peak while the shaft traverses its critical speeds. The measurements establish reliable operation of the test MMFB while airborne.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleIdentification of Rotordynamic Force Coefficients of a Metal Mesh Foil Bearing Using Impact Load Excitations
    typeJournal Paper
    journal volume133
    journal issue11
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4002658
    journal fristpage112501
    identifier eissn0742-4795
    keywordsForce
    keywordsStress
    keywordsBearings
    keywordsRotors
    keywordsMetals
    keywordsRotation
    keywordsDamping
    keywordsStiffness AND Motion
    treeJournal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 011
    contenttypeFulltext
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