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    Significance of Disk Flexing in Viscous-Damped Jet Engine Dynamics

    Source: Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 004::page 647
    Author:
    N. Klompas
    DOI: 10.1115/1.3446413
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new method of analyzing multishaft jet engine critical speeds and unbalance response is derived to account for flexible bladed disks, asymmetric mounting, and squeeze film bearing damping. The resulting elliptical shaft whirling drives traveling waves in disks at speeds equal to the sum and the difference of the rotating speed and the whirling speed. To illustrate a possible problem that cannot be predicted by current methods, a sample calculation shows a simplified model representing possible engine parameters tuned so that a critical speed associated with backward whirling is lowered into the operating range by reduction in disk stiffness. In contradiction to the current literature, the rotor is shown highly responsive to unbalance at this critical speed.
    keyword(s): Dynamics (Mechanics) , Disks , Jet engines , Whirls , Stiffness , Travel , Engines , Waves , Bearings , Damping AND Rotors ,
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      Significance of Disk Flexing in Viscous-Damped Jet Engine Dynamics

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/90959
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorN. Klompas
    date accessioned2017-05-08T23:04:40Z
    date available2017-05-08T23:04:40Z
    date copyrightOctober, 1978
    date issued1978
    identifier issn1528-8919
    identifier otherJETPEZ-26743#647_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/90959
    description abstractA new method of analyzing multishaft jet engine critical speeds and unbalance response is derived to account for flexible bladed disks, asymmetric mounting, and squeeze film bearing damping. The resulting elliptical shaft whirling drives traveling waves in disks at speeds equal to the sum and the difference of the rotating speed and the whirling speed. To illustrate a possible problem that cannot be predicted by current methods, a sample calculation shows a simplified model representing possible engine parameters tuned so that a critical speed associated with backward whirling is lowered into the operating range by reduction in disk stiffness. In contradiction to the current literature, the rotor is shown highly responsive to unbalance at this critical speed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSignificance of Disk Flexing in Viscous-Damped Jet Engine Dynamics
    typeJournal Paper
    journal volume100
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3446413
    journal fristpage647
    journal lastpage654
    identifier eissn0742-4795
    keywordsDynamics (Mechanics)
    keywordsDisks
    keywordsJet engines
    keywordsWhirls
    keywordsStiffness
    keywordsTravel
    keywordsEngines
    keywordsWaves
    keywordsBearings
    keywordsDamping AND Rotors
    treeJournal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 004
    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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