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    On the Effect of Thermal Energy Transport to the Performance of (Semi) Floating Ring Bearing Systems for Automotive Turbochargers

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 010::page 102507
    Author:
    Luis San Andrés
    ,
    Vince Barbarie
    ,
    Kostandin Gjika
    ,
    Avijit Bhattacharya
    DOI: 10.1115/1.4007059
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Bearing systems in engine-oil lubricated turbochargers (TCs) must operate reliably over a wide range of shaft speeds and withstand severe axial and radial thermal gradients. An engineered thermal management of the energy flows into and out of the bearing system is paramount in order to ensure the component’s mechanical integrity and the robustness of the bearing system. The bearings, radial and thrust type, act both as a load bearing and low friction support with the lubricant carrying away a large fraction of the thermal energy generated by rotational drag and the heat flow disposed from a hot shaft. The paper introduces a thermohydrodynamic analysis for the prediction of the pressure and temperature fields in a (semi) floating ring bearing (S)FRB system. The analysis simultaneously solves the Reynolds equation with variable oil viscosity and the thermal energy transport equation in the inner and outer films of the bearing system. Flow conditions in both films are coupled to the temperature distribution and heat flow through the (semi) floating ring. Other constraints include calculating the fluid films’ forces reacting to the externally applied load and to determine the operating journal and ring eccentricities. The predictions of performance for a unique realistic (S)FRB configuration at typical TC operating conditions reveal a distinct knowledge: (a) the heat flow from the shaft into the inner film is overwhelming, in particular, at the inlet lubricant plane where the temperature difference with the cold oil is largest; (b) the inner film temperature quickly increases as soon as the (cold) lubricant enters the film and is due to the large amount of energy generated by shear drag and the heat transfer from the shaft; (c) a floating ring develops a significant radial temperature gradient; (d) at all shaft speeds, low and high, the thermal energy carried away by the lubricant streams is no less than 70% of the total energy input; the rest is conducted through the TC casing. To warrant this thermal energy distribution, enough lubricant flow must be supplied to the bearing system. The efficient computational model offers a distinct advantage over existing lumped parameters thermal models and there is no penalty in the execution time.
    keyword(s): Pressure , Flow (Dynamics) , Heat , Temperature , Bearings , Thermal energy transport , Equations , Lubricants , Turbochargers , Drag (Fluid dynamics) , Stress AND Fluid films ,
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      On the Effect of Thermal Energy Transport to the Performance of (Semi) Floating Ring Bearing Systems for Automotive Turbochargers

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/148736
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorLuis San Andrés
    contributor authorVince Barbarie
    contributor authorKostandin Gjika
    contributor authorAvijit Bhattacharya
    date accessioned2017-05-09T00:49:59Z
    date available2017-05-09T00:49:59Z
    date copyrightOctober, 2012
    date issued2012
    identifier issn1528-8919
    identifier otherJETPEZ-926032#102507_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148736
    description abstractBearing systems in engine-oil lubricated turbochargers (TCs) must operate reliably over a wide range of shaft speeds and withstand severe axial and radial thermal gradients. An engineered thermal management of the energy flows into and out of the bearing system is paramount in order to ensure the component’s mechanical integrity and the robustness of the bearing system. The bearings, radial and thrust type, act both as a load bearing and low friction support with the lubricant carrying away a large fraction of the thermal energy generated by rotational drag and the heat flow disposed from a hot shaft. The paper introduces a thermohydrodynamic analysis for the prediction of the pressure and temperature fields in a (semi) floating ring bearing (S)FRB system. The analysis simultaneously solves the Reynolds equation with variable oil viscosity and the thermal energy transport equation in the inner and outer films of the bearing system. Flow conditions in both films are coupled to the temperature distribution and heat flow through the (semi) floating ring. Other constraints include calculating the fluid films’ forces reacting to the externally applied load and to determine the operating journal and ring eccentricities. The predictions of performance for a unique realistic (S)FRB configuration at typical TC operating conditions reveal a distinct knowledge: (a) the heat flow from the shaft into the inner film is overwhelming, in particular, at the inlet lubricant plane where the temperature difference with the cold oil is largest; (b) the inner film temperature quickly increases as soon as the (cold) lubricant enters the film and is due to the large amount of energy generated by shear drag and the heat transfer from the shaft; (c) a floating ring develops a significant radial temperature gradient; (d) at all shaft speeds, low and high, the thermal energy carried away by the lubricant streams is no less than 70% of the total energy input; the rest is conducted through the TC casing. To warrant this thermal energy distribution, enough lubricant flow must be supplied to the bearing system. The efficient computational model offers a distinct advantage over existing lumped parameters thermal models and there is no penalty in the execution time.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Effect of Thermal Energy Transport to the Performance of (Semi) Floating Ring Bearing Systems for Automotive Turbochargers
    typeJournal Paper
    journal volume134
    journal issue10
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4007059
    journal fristpage102507
    identifier eissn0742-4795
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsHeat
    keywordsTemperature
    keywordsBearings
    keywordsThermal energy transport
    keywordsEquations
    keywordsLubricants
    keywordsTurbochargers
    keywordsDrag (Fluid dynamics)
    keywordsStress AND Fluid films
    treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 010
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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