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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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