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    Inclusions and Service Induced Cracks in a Mature Population of Gas Turbine Engine Bearings

    Source: Journal of Tribology:;1982:;volume( 104 ):;issue: 003::page 300
    Author:
    J. R. Barton
    ,
    F. N. Kusenberger
    ,
    B. B. Baber
    DOI: 10.1115/1.3253202
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Comprehensive NDE data have been acquired on approximately 1000 main shaft ball bearings used in J57/TF33 gas turbine engines by processing through the Automated Bearing Inspection System, Mark I CIBLE. Bearing service hours ranged from zero (new) to approximately 13,000 hr; inclusions and service induced cracks were detected in a significant number of components. Endurance testing as well as metallurgical sectioning and scanning electron microscope investigations were used in correlation analyses. A linear extrapolation to the total service population of J57/TF33 #2 bearing position results in a forecast of over 200 cracked bearings in the fleet of B52, KC135, C141, and E3A aircraft that use these engines.
    keyword(s): Fracture (Materials) , Bearings , Gas turbines , Testing , Aircraft , Ball bearings , Scanning electron microscopes , Inspection , Engines AND Nondestructive evaluation ,
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      Inclusions and Service Induced Cracks in a Mature Population of Gas Turbine Engine Bearings

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/96458
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    • Journal of Tribology

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    contributor authorJ. R. Barton
    contributor authorF. N. Kusenberger
    contributor authorB. B. Baber
    date accessioned2017-05-08T23:14:26Z
    date available2017-05-08T23:14:26Z
    date copyrightJuly, 1982
    date issued1982
    identifier issn0742-4787
    identifier otherJOTRE9-28652#300_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/96458
    description abstractComprehensive NDE data have been acquired on approximately 1000 main shaft ball bearings used in J57/TF33 gas turbine engines by processing through the Automated Bearing Inspection System, Mark I CIBLE. Bearing service hours ranged from zero (new) to approximately 13,000 hr; inclusions and service induced cracks were detected in a significant number of components. Endurance testing as well as metallurgical sectioning and scanning electron microscope investigations were used in correlation analyses. A linear extrapolation to the total service population of J57/TF33 #2 bearing position results in a forecast of over 200 cracked bearings in the fleet of B52, KC135, C141, and E3A aircraft that use these engines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInclusions and Service Induced Cracks in a Mature Population of Gas Turbine Engine Bearings
    typeJournal Paper
    journal volume104
    journal issue3
    journal titleJournal of Tribology
    identifier doi10.1115/1.3253202
    journal fristpage300
    journal lastpage308
    identifier eissn1528-8897
    keywordsFracture (Materials)
    keywordsBearings
    keywordsGas turbines
    keywordsTesting
    keywordsAircraft
    keywordsBall bearings
    keywordsScanning electron microscopes
    keywordsInspection
    keywordsEngines AND Nondestructive evaluation
    treeJournal of Tribology:;1982:;volume( 104 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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