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    On the Accuracy of Rolling Bearing Fatigue Life Prediction

    Source: Journal of Tribology:;1996:;volume( 118 ):;issue: 002::page 297
    Author:
    T. A. Harris
    ,
    J. I. McCool
    DOI: 10.1115/1.2831299
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Ball and roller bearings are designed to meet endurance requirements basically determined according to the Standard fatigue life calculation method. This method is based on the Lundberg-Palmgren fatigue life theory as modified by reliability, material, and lubrication factors. As application load and spied requirements have increased, the Lundberg-Palmgren method has resulted in bearings of increased size, adding unnecessarily to the size and weight of mechanisms. This is a critical design situation for weight and size-sensitive components such as aircraft gas turbine engines and helicopter power transmissions. The bearing life prediction method developed by Ioannides and Harris recognizes the existence of a fatigue limit stress. If the stresses an operating bearing experiences do not exceed the limit stress, the bearing can achieve infinite life. In any case, the method tends to predict longer lives than the Lundberg-Palmgren method. This paper evaluates the life prediction accuracies of the Lundberg-Palmgren and Ioannides-Harris methods by comparing lives calculated according to these methods and to those actually experienced in 62 different applications. As a result of the investigation, the Ioannides-Harris method is shown to more accurately predict bearing fatigue endurance.
    keyword(s): Fatigue life , Rolling bearings , Bearings , Stress , Weight (Mass) , Fatigue , Lubrication , Reliability , Design , Gas turbines , Aircraft , Roller bearings , Fatigue limit AND Mechanisms ,
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      On the Accuracy of Rolling Bearing Fatigue Life Prediction

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    http://yetl.yabesh.ir/yetl1/handle/yetl/117727
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    contributor authorT. A. Harris
    contributor authorJ. I. McCool
    date accessioned2017-05-08T23:51:44Z
    date available2017-05-08T23:51:44Z
    date copyrightApril, 1996
    date issued1996
    identifier issn0742-4787
    identifier otherJOTRE9-28519#297_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117727
    description abstractBall and roller bearings are designed to meet endurance requirements basically determined according to the Standard fatigue life calculation method. This method is based on the Lundberg-Palmgren fatigue life theory as modified by reliability, material, and lubrication factors. As application load and spied requirements have increased, the Lundberg-Palmgren method has resulted in bearings of increased size, adding unnecessarily to the size and weight of mechanisms. This is a critical design situation for weight and size-sensitive components such as aircraft gas turbine engines and helicopter power transmissions. The bearing life prediction method developed by Ioannides and Harris recognizes the existence of a fatigue limit stress. If the stresses an operating bearing experiences do not exceed the limit stress, the bearing can achieve infinite life. In any case, the method tends to predict longer lives than the Lundberg-Palmgren method. This paper evaluates the life prediction accuracies of the Lundberg-Palmgren and Ioannides-Harris methods by comparing lives calculated according to these methods and to those actually experienced in 62 different applications. As a result of the investigation, the Ioannides-Harris method is shown to more accurately predict bearing fatigue endurance.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Accuracy of Rolling Bearing Fatigue Life Prediction
    typeJournal Paper
    journal volume118
    journal issue2
    journal titleJournal of Tribology
    identifier doi10.1115/1.2831299
    journal fristpage297
    journal lastpage309
    identifier eissn1528-8897
    keywordsFatigue life
    keywordsRolling bearings
    keywordsBearings
    keywordsStress
    keywordsWeight (Mass)
    keywordsFatigue
    keywordsLubrication
    keywordsReliability
    keywordsDesign
    keywordsGas turbines
    keywordsAircraft
    keywordsRoller bearings
    keywordsFatigue limit AND Mechanisms
    treeJournal of Tribology:;1996:;volume( 118 ):;issue: 002
    contenttypeFulltext
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