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    The Impact of Pad Flexibility on the Rotordynamic Coefficients of Tilting Pad Journal Bearings

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 008::page 82501
    Author:
    Gaines, Jennifer E.
    ,
    Childs, Dara W.
    DOI: 10.1115/1.4032334
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Static and dynamic load tests were performed on a threepad, rockerpivot, tiltingpad journal bearing (TPJB) with three interchangeable pad configurations, each with measurably different pad flexibilities. Measured dynamicstiffness data for the bearing were readily fitted by a frequencyindependent, constantcoefficient [K][C][M] model. The testbearing had a 101.74 mm diameter with L/D = 0.6. Tests were conducted over the speed range of 6–12 krpm, with unit loads varying from 0.172 to 1.724 MPa. An ISO VG 46 lubricant was used as the test fluid. Pad flexibility was characterized as the change in the pad's bending stiffness or the change in pad thickness. A finiteelement model (FEM) was created to predict the structural bending stiffness of each pad configuration, showing a significant pad flexibility increase as pad thickness decreased. To examine the effect of pad flexibility on the rotordynamic coefficients, the measured results were compared across pad configurations and showed that the pad flexibility increase reduced the direct damping coefficients by 12–20%. As pad flexibility increased, the directstiffness coefficients could increase or decrease, depending on the unit load. They varied from an increase of 12% at low unit loads to a decrease of 3% at high unit loads. Results show that the pad's structural bending stiffness or flexibility is important when predicting the bearing’s dynamic performance. Damping is consistently overpredicted when neglecting pad flexibility. A nondimensional pad flexibility parameter خ±flex was developed. It related the average deflection across the pad surface to the pad's arc length and was to relate the pad flexibility of multiple bearings of different sizes. A bearing code was used to predict the percent change in direct damping coefficients for rigidpad/flexiblepivot and flexiblepad/flexiblepivot models for a surface speed of 54 m/s and a unit load of 783 kPa for the threepad configuration tested here plus five additional tested bearings from the literature. For the minimum pad thickness configuration tested here, the code predicted a 20% drop in predicted Cxx (offload axis direct damping) when comparing a model that included pad flexibility with a model that neglected pad flexibility. In terms of خ±flex, the two thinnest pad configurations tested here are quite flexible compared to both TPJB's pads used in industry and previously tested TPJB pads.
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      The Impact of Pad Flexibility on the Rotordynamic Coefficients of Tilting Pad Journal Bearings

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    https://yetl.yabesh.ir/yetl1/handle/yetl/161125
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorGaines, Jennifer E.
    contributor authorChilds, Dara W.
    date accessioned2017-05-09T01:28:35Z
    date available2017-05-09T01:28:35Z
    date issued2016
    identifier issn1528-8919
    identifier othergtp_138_08_082501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161125
    description abstractStatic and dynamic load tests were performed on a threepad, rockerpivot, tiltingpad journal bearing (TPJB) with three interchangeable pad configurations, each with measurably different pad flexibilities. Measured dynamicstiffness data for the bearing were readily fitted by a frequencyindependent, constantcoefficient [K][C][M] model. The testbearing had a 101.74 mm diameter with L/D = 0.6. Tests were conducted over the speed range of 6–12 krpm, with unit loads varying from 0.172 to 1.724 MPa. An ISO VG 46 lubricant was used as the test fluid. Pad flexibility was characterized as the change in the pad's bending stiffness or the change in pad thickness. A finiteelement model (FEM) was created to predict the structural bending stiffness of each pad configuration, showing a significant pad flexibility increase as pad thickness decreased. To examine the effect of pad flexibility on the rotordynamic coefficients, the measured results were compared across pad configurations and showed that the pad flexibility increase reduced the direct damping coefficients by 12–20%. As pad flexibility increased, the directstiffness coefficients could increase or decrease, depending on the unit load. They varied from an increase of 12% at low unit loads to a decrease of 3% at high unit loads. Results show that the pad's structural bending stiffness or flexibility is important when predicting the bearing’s dynamic performance. Damping is consistently overpredicted when neglecting pad flexibility. A nondimensional pad flexibility parameter خ±flex was developed. It related the average deflection across the pad surface to the pad's arc length and was to relate the pad flexibility of multiple bearings of different sizes. A bearing code was used to predict the percent change in direct damping coefficients for rigidpad/flexiblepivot and flexiblepad/flexiblepivot models for a surface speed of 54 m/s and a unit load of 783 kPa for the threepad configuration tested here plus five additional tested bearings from the literature. For the minimum pad thickness configuration tested here, the code predicted a 20% drop in predicted Cxx (offload axis direct damping) when comparing a model that included pad flexibility with a model that neglected pad flexibility. In terms of خ±flex, the two thinnest pad configurations tested here are quite flexible compared to both TPJB's pads used in industry and previously tested TPJB pads.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Impact of Pad Flexibility on the Rotordynamic Coefficients of Tilting Pad Journal Bearings
    typeJournal Paper
    journal volume138
    journal issue8
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4032334
    journal fristpage82501
    journal lastpage82501
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 008
    contenttypeFulltext
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