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    Piston Ring Thermal Transient Effects on Lubricant Temperatures in Advanced Engines

    Source: Journal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 003::page 543
    Author:
    M. E. Boisclair
    ,
    D. P. Hoult
    ,
    V. W. Wong
    DOI: 10.1115/1.3240289
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: One class of advanced diesel engines operates with low heat rejection and high operating temperatures; piston-ring / liner lubrication is a major problem for these engines. This study attempts to illustrate the time-dependent thermal environment around the top piston ring and lubricant in these advanced engines. Particular emphasis will be placed on the maximum lubricant temperature. The analysis starts with a standard cycle simulation and a global finite-element analysis of the piston and liner in relative motion. A more detailed finite-element model, which considers variable oil film thickness on the liner, focuses on the top ring and lubricant and uses the groove and liner temperatures generated in the global analysis as boundary conditions. Results for different heat rejection engine configurations are presented. We observe that because of major transient effects, high lubricant temperature is experienced not only at top ring reversal but also down the liner to bottom ring reversal.
    keyword(s): Piston rings , Temperature , Engines , Lubricants , Heat , Lubrication , Motion , Simulation , Finite element analysis , Boundary-value problems , Cycles , Diesel engines , Film thickness , Finite element model , Pistons AND Operating temperature ,
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      Piston Ring Thermal Transient Effects on Lubricant Temperatures in Advanced Engines

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/105385
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. E. Boisclair
    contributor authorD. P. Hoult
    contributor authorV. W. Wong
    date accessioned2017-05-08T23:29:57Z
    date available2017-05-08T23:29:57Z
    date copyrightJuly, 1989
    date issued1989
    identifier issn1528-8919
    identifier otherJETPEZ-26669#543_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105385
    description abstractOne class of advanced diesel engines operates with low heat rejection and high operating temperatures; piston-ring / liner lubrication is a major problem for these engines. This study attempts to illustrate the time-dependent thermal environment around the top piston ring and lubricant in these advanced engines. Particular emphasis will be placed on the maximum lubricant temperature. The analysis starts with a standard cycle simulation and a global finite-element analysis of the piston and liner in relative motion. A more detailed finite-element model, which considers variable oil film thickness on the liner, focuses on the top ring and lubricant and uses the groove and liner temperatures generated in the global analysis as boundary conditions. Results for different heat rejection engine configurations are presented. We observe that because of major transient effects, high lubricant temperature is experienced not only at top ring reversal but also down the liner to bottom ring reversal.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePiston Ring Thermal Transient Effects on Lubricant Temperatures in Advanced Engines
    typeJournal Paper
    journal volume111
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3240289
    journal fristpage543
    journal lastpage552
    identifier eissn0742-4795
    keywordsPiston rings
    keywordsTemperature
    keywordsEngines
    keywordsLubricants
    keywordsHeat
    keywordsLubrication
    keywordsMotion
    keywordsSimulation
    keywordsFinite element analysis
    keywordsBoundary-value problems
    keywordsCycles
    keywordsDiesel engines
    keywordsFilm thickness
    keywordsFinite element model
    keywordsPistons AND Operating temperature
    treeJournal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 003
    contenttypeFulltext
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