Numerical and experimental damping prediction of a nonlinearly coupled low pressure steam turbine blading

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Autorschaft

  • Christian Siewert
  • Lars Panning
  • Christoph Gerber
  • Pierre Alain Masserey

Externe Organisationen

  • Alstom
Forschungs-netzwerk anzeigen

Details

OriginalspracheEnglisch
Titel des Sammelwerks2008 Proceedings of the ASME Turbo Expo
UntertitelPower for Land, Sea, and Air
Seiten531-542
Seitenumfang12
AuflagePART A
PublikationsstatusVeröffentlicht - Juni 2008
Veranstaltung2008 ASME Turbo Expo - Berlin, Deutschland
Dauer: 9 Juni 200813 Juni 2008

Publikationsreihe

NameProceedings of the ASME Turbo Expo
NummerPART A
Band5

Abstract

In this paper, a method for the dynamic analysis of a turbine blading coupled by shrouds and snubbers has been presented. In order to reduce the size of the problem, the modal description has been used in combination with the HBM resulting in a EQM formulated in the modal domain. The revealed system of nonlinear equations is solved in order to obtain the nonlinear frequency response of the blading coupled by shrouds and snubbers. To quantify the amount of damping in the system, the energy dissipation ratio R and the loss factor T||0SS have been defined. To compute these quantities, the energy applied to the blading per cycle, the dissipated energy per cycle and the maximum of the potential energy during a vibration cycle have to be computed. The influence of parameters like the coefficient of friction, the surface roughness or the stimulus on the loss factor have been evaluated numerically for the a real steam turbine blading (ND45A LP LSMB). For the analyzed steam turbine blading, the loss factor determined experimentally and the loss factor determined numerically have been compared. The calculated loss factors are in general in a good agreement to the experimentally determined loss factors. Especially the dependency of the loss factor on the nodal diameter is nearly identical in the numerical and experimental results.

ASJC Scopus Sachgebiete

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Numerical and experimental damping prediction of a nonlinearly coupled low pressure steam turbine blading. / Siewert, Christian; Panning, Lars; Gerber, Christoph et al.
2008 Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air. PART A. Aufl. 2008. S. 531-542 (Proceedings of the ASME Turbo Expo; Band 5, Nr. PART A).

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Siewert, C, Panning, L, Gerber, C & Masserey, PA 2008, Numerical and experimental damping prediction of a nonlinearly coupled low pressure steam turbine blading. in 2008 Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air. PART A Aufl., Proceedings of the ASME Turbo Expo, Nr. PART A, Bd. 5, S. 531-542, 2008 ASME Turbo Expo, Berlin, Deutschland, 9 Juni 2008. https://doi.org/10.1115/GT2008-51073
Siewert, C., Panning, L., Gerber, C., & Masserey, P. A. (2008). Numerical and experimental damping prediction of a nonlinearly coupled low pressure steam turbine blading. In 2008 Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air (PART A Aufl., S. 531-542). (Proceedings of the ASME Turbo Expo; Band 5, Nr. PART A). https://doi.org/10.1115/GT2008-51073
Siewert C, Panning L, Gerber C, Masserey PA. Numerical and experimental damping prediction of a nonlinearly coupled low pressure steam turbine blading. in 2008 Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air. PART A Aufl. 2008. S. 531-542. (Proceedings of the ASME Turbo Expo; PART A). doi: 10.1115/GT2008-51073
Siewert, Christian ; Panning, Lars ; Gerber, Christoph et al. / Numerical and experimental damping prediction of a nonlinearly coupled low pressure steam turbine blading. 2008 Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air. PART A. Aufl. 2008. S. 531-542 (Proceedings of the ASME Turbo Expo; PART A).
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abstract = "In this paper, a method for the dynamic analysis of a turbine blading coupled by shrouds and snubbers has been presented. In order to reduce the size of the problem, the modal description has been used in combination with the HBM resulting in a EQM formulated in the modal domain. The revealed system of nonlinear equations is solved in order to obtain the nonlinear frequency response of the blading coupled by shrouds and snubbers. To quantify the amount of damping in the system, the energy dissipation ratio R and the loss factor T||0SS have been defined. To compute these quantities, the energy applied to the blading per cycle, the dissipated energy per cycle and the maximum of the potential energy during a vibration cycle have to be computed. The influence of parameters like the coefficient of friction, the surface roughness or the stimulus on the loss factor have been evaluated numerically for the a real steam turbine blading (ND45A LP LSMB). For the analyzed steam turbine blading, the loss factor determined experimentally and the loss factor determined numerically have been compared. The calculated loss factors are in general in a good agreement to the experimentally determined loss factors. Especially the dependency of the loss factor on the nodal diameter is nearly identical in the numerical and experimental results.",
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AB - In this paper, a method for the dynamic analysis of a turbine blading coupled by shrouds and snubbers has been presented. In order to reduce the size of the problem, the modal description has been used in combination with the HBM resulting in a EQM formulated in the modal domain. The revealed system of nonlinear equations is solved in order to obtain the nonlinear frequency response of the blading coupled by shrouds and snubbers. To quantify the amount of damping in the system, the energy dissipation ratio R and the loss factor T||0SS have been defined. To compute these quantities, the energy applied to the blading per cycle, the dissipated energy per cycle and the maximum of the potential energy during a vibration cycle have to be computed. The influence of parameters like the coefficient of friction, the surface roughness or the stimulus on the loss factor have been evaluated numerically for the a real steam turbine blading (ND45A LP LSMB). For the analyzed steam turbine blading, the loss factor determined experimentally and the loss factor determined numerically have been compared. The calculated loss factors are in general in a good agreement to the experimentally determined loss factors. Especially the dependency of the loss factor on the nodal diameter is nearly identical in the numerical and experimental results.

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