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    A Thermohydrodynamic Sparse Mesh Model of Bump Type Foil Bearings

    Source: Journal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 002::page 22501
    Author:
    Feng, Kai
    ,
    Kaneko, Shigehiko
    DOI: 10.1115/1.4007728
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A numerical model for 3D thermohydrodynamic analysis of bumptype foil bearings with a sparse mesh across the air film is described. The model accounts for heat convection into cooling air, thermal expansion of the bearing components, and material property variations due to temperature rise. Deflection of the compliant foil strip, described as a linkspring structure, is coupled to the solution of the generalized Reynolds equation and the energy equation to account for the effect of foil deformation on the film thickness. The variation in bump stiffness with the thermal growth of bumps is also considered in the model. The unique airflow in foil bearings created by the top foil detachment in the subambient region is analyzed for use in modifying the thermal boundary condition. The Lobatto point quadrature algorithm is used to represent the model on a sparse mesh and thereby reduce the computational effort. The calculated bearing temperatures are in remarkable agreement with both the published test data with the use of cooling air and that without the use of cooling air. The change of bearing radial clearance due to thermal growth of the bearing components was found to significantly affect the bearing load and to be a likely cause of the obvious drop in load capacity with a rise in ambient temperature.
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      A Thermohydrodynamic Sparse Mesh Model of Bump Type Foil Bearings

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/151557
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorFeng, Kai
    contributor authorKaneko, Shigehiko
    date accessioned2017-05-09T00:58:03Z
    date available2017-05-09T00:58:03Z
    date issued2013
    identifier issn1528-8919
    identifier othergtp_135_2_022501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151557
    description abstractA numerical model for 3D thermohydrodynamic analysis of bumptype foil bearings with a sparse mesh across the air film is described. The model accounts for heat convection into cooling air, thermal expansion of the bearing components, and material property variations due to temperature rise. Deflection of the compliant foil strip, described as a linkspring structure, is coupled to the solution of the generalized Reynolds equation and the energy equation to account for the effect of foil deformation on the film thickness. The variation in bump stiffness with the thermal growth of bumps is also considered in the model. The unique airflow in foil bearings created by the top foil detachment in the subambient region is analyzed for use in modifying the thermal boundary condition. The Lobatto point quadrature algorithm is used to represent the model on a sparse mesh and thereby reduce the computational effort. The calculated bearing temperatures are in remarkable agreement with both the published test data with the use of cooling air and that without the use of cooling air. The change of bearing radial clearance due to thermal growth of the bearing components was found to significantly affect the bearing load and to be a likely cause of the obvious drop in load capacity with a rise in ambient temperature.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Thermohydrodynamic Sparse Mesh Model of Bump Type Foil Bearings
    typeJournal Paper
    journal volume135
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4007728
    journal fristpage22501
    journal lastpage22501
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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