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    Analysis of Aerodynamic Journal Bearings With Small Number of Herringbone Grooves by Finite Element Method

    Source: Journal of Tribology:;1994:;volume( 116 ):;issue: 004::page 698
    Author:
    D. Bonneau
    ,
    J. Absi
    DOI: 10.1115/1.2927320
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A numerical study of gas herringbone grooved journal bearings is presented for small number of grooves. The compressible Reynolds equation is solved by use of the Finite Element Method. The nonlinearity of the discretized equations is treated with the Newton-Raphson procedure. A comparison of the results for a smooth bearing with previously published results is made and the domain of validity of the Narrow Groove Theory is analyzed. Load capacity, attitude angle, and stiffness coefficients are given for various configurations: groove angle and thickness of grooves, bearing number, and that for both smooth and grooved member rotating.
    keyword(s): Finite element methods , Journal bearings , Bearings , Equations , Stiffness , Thickness AND Stress ,
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      Analysis of Aerodynamic Journal Bearings With Small Number of Herringbone Grooves by Finite Element Method

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/114341
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    contributor authorD. Bonneau
    contributor authorJ. Absi
    date accessioned2017-05-08T23:45:32Z
    date available2017-05-08T23:45:32Z
    date copyrightOctober, 1994
    date issued1994
    identifier issn0742-4787
    identifier otherJOTRE9-28511#698_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/114341
    description abstractA numerical study of gas herringbone grooved journal bearings is presented for small number of grooves. The compressible Reynolds equation is solved by use of the Finite Element Method. The nonlinearity of the discretized equations is treated with the Newton-Raphson procedure. A comparison of the results for a smooth bearing with previously published results is made and the domain of validity of the Narrow Groove Theory is analyzed. Load capacity, attitude angle, and stiffness coefficients are given for various configurations: groove angle and thickness of grooves, bearing number, and that for both smooth and grooved member rotating.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAnalysis of Aerodynamic Journal Bearings With Small Number of Herringbone Grooves by Finite Element Method
    typeJournal Paper
    journal volume116
    journal issue4
    journal titleJournal of Tribology
    identifier doi10.1115/1.2927320
    journal fristpage698
    journal lastpage704
    identifier eissn1528-8897
    keywordsFinite element methods
    keywordsJournal bearings
    keywordsBearings
    keywordsEquations
    keywordsStiffness
    keywordsThickness AND Stress
    treeJournal of Tribology:;1994:;volume( 116 ):;issue: 004
    contenttypeFulltext
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