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    Novel Dynamic Rotor and Blade Deformation and Vibration Monitoring Technique

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 001::page 12504
    Author:
    Thorsten Pfister
    ,
    Philipp Günther
    ,
    Florian Dreier
    ,
    Jürgen Czarske
    DOI: 10.1115/1.4004160
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Monitoring rotor deformations and vibrations dynamically is an important task for improving both the safety and the lifetime as well as the energy efficiency of motors and turbo machines. However, due to the high rotor speed encountered in particular at turbo machines, this requires concurrently high measurement rate and high accuracy, which is hardly possible to achieve with currently available measurement techniques. To solve this problem, in this paper, we present a novel nonincremental interferometric optical sensor that measures simultaneously the in-plane velocity and the out-of-plane position of laterally moving objects with micrometer precision and concurrently with microsecond temporal resolution. It will be shown that this sensor exhibits the outstanding feature that its measurement uncertainty is generally independent of the object velocity, which enables precise deformation and vibration measurements also at high rotor speed. Moreover, this sensor does not require an in situ calibration and it allows a direct measurement of blade velocity variations in contrast to blade tip timing systems. For application under harsh environmental conditions such as high temperatures, a robust and miniaturized fiber-optic sensor setup was developed. To demonstrate the capability of this sensor, measurements of tip clearance changes and rotor blade vibrations at varying operating conditions of a transonic centrifugal compressor test rig at blade tip velocities up to 600 m/s are presented among others.
    keyword(s): Deformation , Measurement , Sensors , Rotors , Vibration , Blades , Clearances (Engineering) , Machinery AND Compressors ,
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      Novel Dynamic Rotor and Blade Deformation and Vibration Monitoring Technique

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    http://yetl.yabesh.ir/yetl1/handle/yetl/148950
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorThorsten Pfister
    contributor authorPhilipp Günther
    contributor authorFlorian Dreier
    contributor authorJürgen Czarske
    date accessioned2017-05-09T00:50:42Z
    date available2017-05-09T00:50:42Z
    date copyrightJanuary, 2012
    date issued2012
    identifier issn1528-8919
    identifier otherJETPEZ-27180#012504_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148950
    description abstractMonitoring rotor deformations and vibrations dynamically is an important task for improving both the safety and the lifetime as well as the energy efficiency of motors and turbo machines. However, due to the high rotor speed encountered in particular at turbo machines, this requires concurrently high measurement rate and high accuracy, which is hardly possible to achieve with currently available measurement techniques. To solve this problem, in this paper, we present a novel nonincremental interferometric optical sensor that measures simultaneously the in-plane velocity and the out-of-plane position of laterally moving objects with micrometer precision and concurrently with microsecond temporal resolution. It will be shown that this sensor exhibits the outstanding feature that its measurement uncertainty is generally independent of the object velocity, which enables precise deformation and vibration measurements also at high rotor speed. Moreover, this sensor does not require an in situ calibration and it allows a direct measurement of blade velocity variations in contrast to blade tip timing systems. For application under harsh environmental conditions such as high temperatures, a robust and miniaturized fiber-optic sensor setup was developed. To demonstrate the capability of this sensor, measurements of tip clearance changes and rotor blade vibrations at varying operating conditions of a transonic centrifugal compressor test rig at blade tip velocities up to 600 m/s are presented among others.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNovel Dynamic Rotor and Blade Deformation and Vibration Monitoring Technique
    typeJournal Paper
    journal volume134
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4004160
    journal fristpage12504
    identifier eissn0742-4795
    keywordsDeformation
    keywordsMeasurement
    keywordsSensors
    keywordsRotors
    keywordsVibration
    keywordsBlades
    keywordsClearances (Engineering)
    keywordsMachinery AND Compressors
    treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 001
    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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