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    Spiral Vibration of a Turbogenerator Set: Case History, Stability Analysis, Measurements and Operational Experience

    Source: Journal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 001::page 12509
    Author:
    Lothar Eckert
    ,
    Joachim Schmied
    DOI: 10.1115/1.2747645
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A hydrogen-cooled turbogenerator operating at 3600 rpm showed the phenomenon of spiral vibration with a forward rotating unbalance vector. The relative shaft vibration measured at the non-driven end-bearing was close to the trip level. Spiral vibration is observed at various types of rotating machinery with both rotation directions of the unbalance vector, i.e., forward and backward. Spiral vibration is caused by a vibration-induced hot spot on the shaft surface generated by friction. The turbogenerator has three bearings: two main bearings and the brush gear bearing. The carbon brushes sliding on the slip rings were identified as the hot spot location. Potential modifications were studied using hot spot stability analyses with a rotor dynamic model of the generator rotor on three journal bearings. The applied method, introduced by Schmied (1987, “Spiral Vibrations of Rotors” Proc. 11th Biennial ASME Design Engineering Div. Conf., Vib. Noise, DE-Vol. 2, Rotating Machinery Dynamics, Boston, MA, ASME H0400B, pp. 449–456), allows the handling of general systems. The hot spot model is based on the theory of Kellenberger (1978, Ingenieur-Archiv, 47, pp. 223–229; 1980, Journal of Mechanical Design, 102, pp. 177–184) using a thermal equation between the shaft’s thermal deflection and the shaft displacement at the hot spot location. Three different relations between the heat input and the shaft vibration were modeled: heat input proportional to the shaft displacement, to the shaft velocity, and to the shaft acceleration. The model, in which the heat input is proportional to the velocity, is the most suitable variant for slip rings. This was confirmed by comparison with the measured vibration behavior. A modification of the shaft line was selected based on the calculation results and was successfully implemented. This generator and other generators with the same modified brush gear unit have been in operation for more than four years.
    keyword(s): Stability , Heat , Vibration , Displacement , Turbogenerators , Rotors AND Bearings ,
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      Spiral Vibration of a Turbogenerator Set: Case History, Stability Analysis, Measurements and Operational Experience

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    https://yetl.yabesh.ir/yetl1/handle/yetl/138035
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorLothar Eckert
    contributor authorJoachim Schmied
    date accessioned2017-05-09T00:28:08Z
    date available2017-05-09T00:28:08Z
    date copyrightJanuary, 2008
    date issued2008
    identifier issn1528-8919
    identifier otherJETPEZ-26984#012509_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/138035
    description abstractA hydrogen-cooled turbogenerator operating at 3600 rpm showed the phenomenon of spiral vibration with a forward rotating unbalance vector. The relative shaft vibration measured at the non-driven end-bearing was close to the trip level. Spiral vibration is observed at various types of rotating machinery with both rotation directions of the unbalance vector, i.e., forward and backward. Spiral vibration is caused by a vibration-induced hot spot on the shaft surface generated by friction. The turbogenerator has three bearings: two main bearings and the brush gear bearing. The carbon brushes sliding on the slip rings were identified as the hot spot location. Potential modifications were studied using hot spot stability analyses with a rotor dynamic model of the generator rotor on three journal bearings. The applied method, introduced by Schmied (1987, “Spiral Vibrations of Rotors” Proc. 11th Biennial ASME Design Engineering Div. Conf., Vib. Noise, DE-Vol. 2, Rotating Machinery Dynamics, Boston, MA, ASME H0400B, pp. 449–456), allows the handling of general systems. The hot spot model is based on the theory of Kellenberger (1978, Ingenieur-Archiv, 47, pp. 223–229; 1980, Journal of Mechanical Design, 102, pp. 177–184) using a thermal equation between the shaft’s thermal deflection and the shaft displacement at the hot spot location. Three different relations between the heat input and the shaft vibration were modeled: heat input proportional to the shaft displacement, to the shaft velocity, and to the shaft acceleration. The model, in which the heat input is proportional to the velocity, is the most suitable variant for slip rings. This was confirmed by comparison with the measured vibration behavior. A modification of the shaft line was selected based on the calculation results and was successfully implemented. This generator and other generators with the same modified brush gear unit have been in operation for more than four years.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSpiral Vibration of a Turbogenerator Set: Case History, Stability Analysis, Measurements and Operational Experience
    typeJournal Paper
    journal volume130
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2747645
    journal fristpage12509
    identifier eissn0742-4795
    keywordsStability
    keywordsHeat
    keywordsVibration
    keywordsDisplacement
    keywordsTurbogenerators
    keywordsRotors AND Bearings
    treeJournal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 001
    contenttypeFulltext
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