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contributor authorS. H. Loewenthal
contributor authorD. W. Moyer
date accessioned2017-05-08T23:07:40Z
date available2017-05-08T23:07:40Z
date copyrightApril, 1979
date issued1979
identifier issn0742-4787
identifier otherJOTRE9-28624#171_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92696
description abstractBall bearings were fatigue tested with a noncontaminated MIL-L-23699 lubricant and with a contaminated MIL-L-23699 lubricant under four levels of filtration. The test filters had absolute particle removal ratings of 3, 30, 49, and 105 microns. Aircraft turbine engine contaminants were injected into the filter’s supply line at a constant rate of 125 milligrams per bearing hour. Bearing life and running track condition generally improved with finer filtration. The experimental lives of 3- and 30-micron filter bearings were statistically equivalent, approaching those obtained with the noncontaminated lubricant bearings. Compared to these bearings, the lives of the 49-micron bearings were statistically lower. The 105-micron bearings experienced gross wear. The degree of surface distress, weight loss, and probable failure mode were dependent on filtration level, with finer filtration being clearly beneficial.
publisherThe American Society of Mechanical Engineers (ASME)
titleFiltration Effects on Ball Bearing Life and Condition in a Contaminated Lubricant
typeJournal Paper
journal volume101
journal issue2
journal titleJournal of Tribology
identifier doi10.1115/1.3453307
journal fristpage171
journal lastpage176
identifier eissn1528-8897
keywordsFiltration
keywordsLubricants
keywordsBall bearings
keywordsBearings
keywordsFilters
keywordsFailure
keywordsGas turbines
keywordsAircraft
keywordsParticulate matter
keywordsWeight (Mass)
keywordsFatigue AND Wear
treeJournal of Tribology:;1979:;volume( 101 ):;issue: 002
contenttypeFulltext


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