A model order reduction method based on the Component Mode Synthesis for mistunend bladed disks is introduced, with one component for the disk and one component for each blade. The interface between the components at the blade roots is reduced using the wave-based substructuring method, which employs tuned system modes. These system modes are calculated first, and used subsequently during the reduction of the individual components, which eliminates the need to build a partially reduced intermediate model with dense matrices. For the disk, a cyclic Craig-Bampton reduction is applied. The deviations of the stiffness and mass matrices of individual disk sectors are then projected into the cyclic basis of interior and interface modes of the disk substructure. Thereby it is possible to model small disk mistuning in addition to large mistuning of the blades.
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ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition
June 11–15, 2018
Oslo, Norway
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5115-9
PROCEEDINGS PAPER
Reduced-Order Modeling of Bladed Disks Considering Small Mistuning of the Disk Sectors
Lukas Schwerdt,
Lukas Schwerdt
Leibniz Universität Hannover, Hannover, Germany
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Sebastian Willeke,
Sebastian Willeke
Leibniz Universität Hannover, Hannover, Germany
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Lars Panning-von Scheidt,
Lars Panning-von Scheidt
Leibniz Universität Hannover, Hannover, Germany
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Jörg Wallaschek
Jörg Wallaschek
Leibniz Universität Hannover, Hannover, Germany
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Lukas Schwerdt
Leibniz Universität Hannover, Hannover, Germany
Sebastian Willeke
Leibniz Universität Hannover, Hannover, Germany
Lars Panning-von Scheidt
Leibniz Universität Hannover, Hannover, Germany
Jörg Wallaschek
Leibniz Universität Hannover, Hannover, Germany
Paper No:
GT2018-76610, V07CT35A033; 9 pages
Published Online:
August 30, 2018
Citation
Schwerdt, L, Willeke, S, Panning-von Scheidt, L, & Wallaschek, J. "Reduced-Order Modeling of Bladed Disks Considering Small Mistuning of the Disk Sectors." Proceedings of the ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. Volume 7C: Structures and Dynamics. Oslo, Norway. June 11–15, 2018. V07CT35A033. ASME. https://doi.org/10.1115/GT2018-76610
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