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    Rotordynamic Optimization of Fixed Pad Journal Bearings Using Response Surface Design of Experiments

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 012::page 122502
    Author:
    Urbiola
    ,
    Santibaأ±ez
    ,
    Lأ³pez
    ,
    Ramأ­rez
    ,
    Yaأ±ez
    DOI: 10.1115/1.4034066
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The design process of journal bearings of turbomachines is complex and timeconsuming due to the many geometric and physical variables involved. This paper reports on the design of experiments (DOE) and the response surface design of experiments (RSDOE) methods employed on the design of the driveend and freeend threelobe journal bearings supporting a centrifugal compressor rotor. The suitability of each technique is discussed. The bearing design variables employed are bearing slenderness ratio, radial clearance, preload, and lubricant inlet temperature. The rotordynamic response variables selected were the critical speed location, the vibrations at critical speed and operating speed for both bearings, and the threshold speed of instability. The use of a nonlinear (quadratic) RSDOE model is justified. An optimization approach combining an SRDOE and rotordynamic finite element modeling is presented. This method leads to arrive to a multivariate model for multiobjective optimization with very few computations. Identification of the dominant design variables and their effects on several response variables allows establishing engineering feasible solutions with focus on manufacturing versus operating conditions tradeoff.
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      Rotordynamic Optimization of Fixed Pad Journal Bearings Using Response Surface Design of Experiments

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    http://yetl.yabesh.ir/yetl1/handle/yetl/161231
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorUrbiola
    contributor authorSantibaأ±ez
    contributor authorLأ³pez
    contributor authorRamأ­rez
    contributor authorYaأ±ez
    date accessioned2017-05-09T01:29:01Z
    date available2017-05-09T01:29:01Z
    date issued2016
    identifier issn1528-8919
    identifier othergtp_138_12_122502.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161231
    description abstractThe design process of journal bearings of turbomachines is complex and timeconsuming due to the many geometric and physical variables involved. This paper reports on the design of experiments (DOE) and the response surface design of experiments (RSDOE) methods employed on the design of the driveend and freeend threelobe journal bearings supporting a centrifugal compressor rotor. The suitability of each technique is discussed. The bearing design variables employed are bearing slenderness ratio, radial clearance, preload, and lubricant inlet temperature. The rotordynamic response variables selected were the critical speed location, the vibrations at critical speed and operating speed for both bearings, and the threshold speed of instability. The use of a nonlinear (quadratic) RSDOE model is justified. An optimization approach combining an SRDOE and rotordynamic finite element modeling is presented. This method leads to arrive to a multivariate model for multiobjective optimization with very few computations. Identification of the dominant design variables and their effects on several response variables allows establishing engineering feasible solutions with focus on manufacturing versus operating conditions tradeoff.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRotordynamic Optimization of Fixed Pad Journal Bearings Using Response Surface Design of Experiments
    typeJournal Paper
    journal volume138
    journal issue12
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4034066
    journal fristpage122502
    journal lastpage122502
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 012
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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