Experimental and Numerical Analysis of Rotational Speed Influence on the Nonlinear Dynamics of Turbine Blades with Shroud Coupling

verfasst von: Florian Jäger, Lars Panning-Von Scheidt, Jörg Wallaschek
Abstract: The structural mechanical properties of blades in turbomachinery depend on the operating speed. In addition to effects such as stress stiffening and spin softening, the rotational speed influences the nonlinear contact properties in shroud-coupled turbine blades. A change in operating point consequently leads to changes in natural frequencies, vibration modes and effective damping. For the design of new turbine blades, the correct modeling of all combined speed-variable properties is necessary to protect the blades against high cycle fatigue failures at any operating point. A nonlinear computational model with a variable-speed formulation of the structural properties is developed and the dynamics of a medium-pressure turbine blading with shroud coupling is analyzed at several operating points. In a rotational test rig, the disk and blade assembly is excited with higher-harmonic excitation force components at different rotational speeds. The comparison of the amplitude responses shows the influence of the rotational speed on the damping and the resonant frequency and confirms the validity of the developed computational model.
Organisationseinheit(en): Institut für Dynamik und Schwingungen
Typ: Artikel
Journal: International Journal of Gas Turbine, Propulsion and Power Systems
Band: 15
Seiten: 18-26
Anzahl der Seiten: 9
Publikationsdatum: 05.2024
Publikationsstatus: Veröffentlicht
Peer-reviewed: Ja
ASJC Scopus Sachgebiete: Maschinenbau
Elektronische Version(en): https://doi.org/10.38036/jgpp.15.2_17 (Zugang: Offen)

BibTeX

@article{469e5dffd9bd40e5949f72045fdf2ced,
title = "Experimental and Numerical Analysis of Rotational Speed Influence on the Nonlinear Dynamics of Turbine Blades with Shroud Coupling",
abstract = "The structural mechanical properties of blades in turbomachinery depend on the operating speed. In addition to effects such as stress stiffening and spin softening, the rotational speed influences the nonlinear contact properties in shroud-coupled turbine blades. A change in operating point consequently leads to changes in natural frequencies, vibration modes and effective damping. For the design of new turbine blades, the correct modeling of all combined speed-variable properties is necessary to protect the blades against high cycle fatigue failures at any operating point. A nonlinear computational model with a variable-speed formulation of the structural properties is developed and the dynamics of a medium-pressure turbine blading with shroud coupling is analyzed at several operating points. In a rotational test rig, the disk and blade assembly is excited with higher-harmonic excitation force components at different rotational speeds. The comparison of the amplitude responses shows the influence of the rotational speed on the damping and the resonant frequency and confirms the validity of the developed computational model.",
author = "Florian J{\"a}ger and {Panning-Von Scheidt}, Lars and J{\"o}rg Wallaschek",
note = "Publisher Copyright: Copyright {\textcopyright}2024 Florian J{\"a}ger, Lars Panning-von Scheidt and J{\"o}rg Wallaschek.",
year = "2024",
month = may,
doi = "10.38036/jgpp.15.2_17",
language = "English",
volume = "15",
pages = "18--26",
journal = "International Journal of Gas Turbine, Propulsion and Power Systems",
issn = "1882-5079",
publisher = "Gas Turbine Society of Japan (GTSJ)",
number = "2",
}