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    Experimental Load Capacity and Power Loss of Herringbone Grooved Gas Lubricated Journal Bearings

    Source: Journal of Tribology:;1971:;volume( 093 ):;issue: 003::page 415
    Author:
    R. E. Cunningham
    ,
    D. P. Fleming
    ,
    W. J. Anderson
    DOI: 10.1115/1.3451610
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Load capacity, attitude angle, and power loss were determined for 1 1/2-in-dia herringbone grooved journal bearings operating in air to speeds of 60,000 rpm. Results showed that groove-to-ridge-clearance ratios of 2.0 to 2.4 give a greater load capacity than do ratios outside this optimum range. Agreement with a small-eccentricity pressure perturbation theory was good for groove-to-ridge-clearance ratios in the optimum range. Power loss, relative to that calculated for a plain bearing of the same dimensions, did not vary widely for the range of geometric variables used. Relative power loss generally increased with speed and was generally comparable to that for a plain bearing.
    keyword(s): Stress , Journal bearings , Plain bearings , Clearances (Engineering) , Perturbation theory , Pressure AND Dimensions ,
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      Experimental Load Capacity and Power Loss of Herringbone Grooved Gas Lubricated Journal Bearings

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/155612
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    • Journal of Tribology

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    contributor authorR. E. Cunningham
    contributor authorD. P. Fleming
    contributor authorW. J. Anderson
    date accessioned2017-05-09T01:10:29Z
    date available2017-05-09T01:10:29Z
    date copyrightJuly, 1971
    date issued1971
    identifier issn0742-4787
    identifier otherJOTRE9-28563#415_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/155612
    description abstractLoad capacity, attitude angle, and power loss were determined for 1 1/2-in-dia herringbone grooved journal bearings operating in air to speeds of 60,000 rpm. Results showed that groove-to-ridge-clearance ratios of 2.0 to 2.4 give a greater load capacity than do ratios outside this optimum range. Agreement with a small-eccentricity pressure perturbation theory was good for groove-to-ridge-clearance ratios in the optimum range. Power loss, relative to that calculated for a plain bearing of the same dimensions, did not vary widely for the range of geometric variables used. Relative power loss generally increased with speed and was generally comparable to that for a plain bearing.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental Load Capacity and Power Loss of Herringbone Grooved Gas Lubricated Journal Bearings
    typeJournal Paper
    journal volume93
    journal issue3
    journal titleJournal of Tribology
    identifier doi10.1115/1.3451610
    journal fristpage415
    journal lastpage422
    identifier eissn1528-8897
    keywordsStress
    keywordsJournal bearings
    keywordsPlain bearings
    keywordsClearances (Engineering)
    keywordsPerturbation theory
    keywordsPressure AND Dimensions
    treeJournal of Tribology:;1971:;volume( 093 ):;issue: 003
    contenttypeFulltext
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