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    Characteristics of a Spherical Seat TPJB With Four Methods of Directed Lubrication—Part II: Rotordynamic Performance

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 012::page 122503
    Author:
    Coghlan, David M.
    ,
    Childs, Dara W.
    DOI: 10.1115/1.4036970
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measured and predicted rotordynamic characteristics are presented for a four-pad, spherical-seat, tilting-pad journal bearing (TPJB) with 0.5 pivot offset, 0.6 L/D, 101.6 mm nominal diameter, and 0.3 preload in the load-between-pivots orientation. One bearing is tested four separate times in the following four different lubrication configurations: (1) flooded single-orifice (SO) at the bearing shell, (2) evacuated leading edge groove (LEG), (3) evacuated spray-bar blocker (SBB), and (4) evacuated spray-bar (SB). The same set of pads is used for every test to maintain clearance and preload; each method of lubrication is added as an assembly to the bearing. Test conditions include surface speeds and unit loads up to 85 m/s and 2.9 MPa, respectively. Dynamic data includes four sets (one set for each bearing configuration) of direct and cross-coupled rotordynamic coefficients derived from measurements and fit to a frequency-independent stiffness-damping-mass (KCM) matrix model. The pivot stiffness (pad and pivot in series) is measured and incorporated into predictions.
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      Characteristics of a Spherical Seat TPJB With Four Methods of Directed Lubrication—Part II: Rotordynamic Performance

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4233854
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorCoghlan, David M.
    contributor authorChilds, Dara W.
    date accessioned2017-11-25T07:16:10Z
    date available2017-11-25T07:16:10Z
    date copyright2017/23/8
    date issued2017
    identifier issn0742-4795
    identifier othergtp_139_12_122503.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4233854
    description abstractMeasured and predicted rotordynamic characteristics are presented for a four-pad, spherical-seat, tilting-pad journal bearing (TPJB) with 0.5 pivot offset, 0.6 L/D, 101.6 mm nominal diameter, and 0.3 preload in the load-between-pivots orientation. One bearing is tested four separate times in the following four different lubrication configurations: (1) flooded single-orifice (SO) at the bearing shell, (2) evacuated leading edge groove (LEG), (3) evacuated spray-bar blocker (SBB), and (4) evacuated spray-bar (SB). The same set of pads is used for every test to maintain clearance and preload; each method of lubrication is added as an assembly to the bearing. Test conditions include surface speeds and unit loads up to 85 m/s and 2.9 MPa, respectively. Dynamic data includes four sets (one set for each bearing configuration) of direct and cross-coupled rotordynamic coefficients derived from measurements and fit to a frequency-independent stiffness-damping-mass (KCM) matrix model. The pivot stiffness (pad and pivot in series) is measured and incorporated into predictions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCharacteristics of a Spherical Seat TPJB With Four Methods of Directed Lubrication—Part II: Rotordynamic Performance
    typeJournal Paper
    journal volume139
    journal issue12
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4036970
    journal fristpage122503
    journal lastpage122503-13
    treeJournal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 012
    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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