Vibration mode shape extraction of bladed disk

0555035 - ÚT 2023 CZ eng C - Konferenční příspěvek (zahraniční konf.)
Mekhalfia, Mohammed Lamine - Procházka, Pavel - Tchawou Tchuisseu, Eder Batista - Maturkanič, Dušan - Hodboď, Robert
Vibration mode shape extraction of bladed disk.
Dynamics of Machines and Mechanical Systems with Interactions, DYMAMESI 2022. Prague: Institute of Thermomechanics Academy of Sciences of the Czech Republic, v. v. i., 2022 - (Zolotarev, I.; Pešek, L.; Kozień, M.), s. 39-42. ISBN 978-80-87012-78-9.
[International colloquium DYMAMESI 2022. Prague (CZ), 01.03.2022-02.03.2022]
Grant CEP: GA MŠMT(CZ) EF15_003/0000493
Grant ostatní: H2020(XE) 862034; AV ČR(CZ) StrategieAV21/3
Program: BATISTA; StrategieAV
Institucionální podpora: RVO:61388998
Klíčová slova: blade disk * mode shapes * laser doppler vibrometer
Obor OECD: Applied mechanics

This research paper deals with the experimental protocol followed to visualize the vibration mode shape of an aero-engine bladed disk. This study is based on a comparison between the numerical results obtained through Finite element methods (FEM) using ANSYS software and experimentally using the laser Doppler vibrometer. Therefore the bladed disk was transformed into a 3D virtual environment and structural analysis was performed. The results demonstrate a match between the numerical and the experimental one, this match offers the possibility for using the model for future studies.
Trvalý link: http://hdl.handle.net/11104/0331678