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    Load Support System Analysis-High Speed Input Pinion Configuration

    Source: Journal of Tribology:;1980:;volume( 102 ):;issue: 001::page 97
    Author:
    S. S. Gassel
    ,
    J. Pirvics
    DOI: 10.1115/1.3251447
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Structural assemblies which transmit power, helicopter gearboxes for example, require accurate evaluation of load and displacement distributions to ensure system design optimization. Particular performance parameters which depend on detailed understanding of the distributions are operating life and rigidity. The coupling complexity of system components; gears, shafts, bearings and the housing itself, prevents meaningful evaluation of performance from the study of isolated components. The entire load support system has to be examined in its interacting entirety. In this paper a theoretical study has been made to determine the performance of a load support system, consisting of a shaft and two taper roller bearings for the high-speed input pinion of an advanced helicopter transmission. SHABERTH, a computer program designed to perform thermo-mechanical analyses of arbitrarily configured rolling element bearing-shaft systems, was employed to analyze, both, a straddle arrangement where the spiral bevel pinion gear is located axially between the two bearings, and a cantilevered arrangement where the pinion is outboard of the bearings. The effects of preload, shaft wall thickness, bearing spacing and misalignment of bearing races were examined. Their influence on load distributions and bearing rating lives including simulation of bearing and shaft elastic deformations were evaluated for both support geometries. Additional effort was expended to detail the performance of the pinion designs over a range of shaft rotational speeds. Lubrication and friction effects were included. Particular attention was directed to local as well as global heat generation rates (HGR) to provide design information for proper lubrication of the bearings. The results provide guidance for improved design of transmissions and the load vector control within them. In particular, the relative merits of the straddle versus the cantilever design have been exposed so that their individual characteristics may be exploited to increase system survivability.
    keyword(s): Stress , Bearings , Design , Gears , Lubrication , Heat , Simulation , Service life (Equipment) , Deformation , Friction , Optimization , Cantilevers , Computer software , Displacement , Stiffness , Wall thickness AND Roller bearings ,
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      Load Support System Analysis-High Speed Input Pinion Configuration

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/93986
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    • Journal of Tribology

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    contributor authorS. S. Gassel
    contributor authorJ. Pirvics
    date accessioned2017-05-08T23:10:04Z
    date available2017-05-08T23:10:04Z
    date copyrightJanuary, 1980
    date issued1980
    identifier issn0742-4787
    identifier otherJOTRE9-28631#97_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93986
    description abstractStructural assemblies which transmit power, helicopter gearboxes for example, require accurate evaluation of load and displacement distributions to ensure system design optimization. Particular performance parameters which depend on detailed understanding of the distributions are operating life and rigidity. The coupling complexity of system components; gears, shafts, bearings and the housing itself, prevents meaningful evaluation of performance from the study of isolated components. The entire load support system has to be examined in its interacting entirety. In this paper a theoretical study has been made to determine the performance of a load support system, consisting of a shaft and two taper roller bearings for the high-speed input pinion of an advanced helicopter transmission. SHABERTH, a computer program designed to perform thermo-mechanical analyses of arbitrarily configured rolling element bearing-shaft systems, was employed to analyze, both, a straddle arrangement where the spiral bevel pinion gear is located axially between the two bearings, and a cantilevered arrangement where the pinion is outboard of the bearings. The effects of preload, shaft wall thickness, bearing spacing and misalignment of bearing races were examined. Their influence on load distributions and bearing rating lives including simulation of bearing and shaft elastic deformations were evaluated for both support geometries. Additional effort was expended to detail the performance of the pinion designs over a range of shaft rotational speeds. Lubrication and friction effects were included. Particular attention was directed to local as well as global heat generation rates (HGR) to provide design information for proper lubrication of the bearings. The results provide guidance for improved design of transmissions and the load vector control within them. In particular, the relative merits of the straddle versus the cantilever design have been exposed so that their individual characteristics may be exploited to increase system survivability.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLoad Support System Analysis-High Speed Input Pinion Configuration
    typeJournal Paper
    journal volume102
    journal issue1
    journal titleJournal of Tribology
    identifier doi10.1115/1.3251447
    journal fristpage97
    journal lastpage106
    identifier eissn1528-8897
    keywordsStress
    keywordsBearings
    keywordsDesign
    keywordsGears
    keywordsLubrication
    keywordsHeat
    keywordsSimulation
    keywordsService life (Equipment)
    keywordsDeformation
    keywordsFriction
    keywordsOptimization
    keywordsCantilevers
    keywordsComputer software
    keywordsDisplacement
    keywordsStiffness
    keywordsWall thickness AND Roller bearings
    treeJournal of Tribology:;1980:;volume( 102 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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