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    Recent Blade Vibration Techniques

    Source: Journal of Engineering for Gas Turbines and Power:;1967:;volume( 089 ):;issue: 003::page 437
    Author:
    E. K. Armstrong
    DOI: 10.1115/1.3616710
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The methods which have been used recently to predict the amplitudes of vibration of compressor blades are explained. Examples for resonances with maldistributions in the intake flow and downstream blockages are given. Two techniques of obtaining blade vibration data from the HP shaft of a two-shaft jet engine are described. By comparing the measured amplitudes with the fatigue properties of blading, a parameter has been established which is used in assessing the seriousness of a vibration when considering its service life.
    keyword(s): Vibration , Blades , Jet engines , Fatigue properties , Flow (Dynamics) , Compressors AND Service life (Equipment) ,
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      Recent Blade Vibration Techniques

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    http://yetl.yabesh.ir/yetl1/handle/yetl/118478
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    contributor authorE. K. Armstrong
    date accessioned2017-05-08T23:53:05Z
    date available2017-05-08T23:53:05Z
    date copyrightJuly, 1967
    date issued1967
    identifier issn1528-8919
    identifier otherJETPEZ-26661#437_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118478
    description abstractThe methods which have been used recently to predict the amplitudes of vibration of compressor blades are explained. Examples for resonances with maldistributions in the intake flow and downstream blockages are given. Two techniques of obtaining blade vibration data from the HP shaft of a two-shaft jet engine are described. By comparing the measured amplitudes with the fatigue properties of blading, a parameter has been established which is used in assessing the seriousness of a vibration when considering its service life.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRecent Blade Vibration Techniques
    typeJournal Paper
    journal volume89
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3616710
    journal fristpage437
    journal lastpage444
    identifier eissn0742-4795
    keywordsVibration
    keywordsBlades
    keywordsJet engines
    keywordsFatigue properties
    keywordsFlow (Dynamics)
    keywordsCompressors AND Service life (Equipment)
    treeJournal of Engineering for Gas Turbines and Power:;1967:;volume( 089 ):;issue: 003
    contenttypeFulltext
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