Manufacturing Technology 2019, 19(6):1067-1070 | DOI: 10.21062/ujep/419.2019/a/1213-2489/MT/19/6/1067
Numerical Modal Analysis of the Turbo-jet Engine Rotor Blades
- Faculty of Industrial Technologies in Púchov, Alexander Dubček University of Trenčín. I. Krásku 491/30, 020 01 Púchov. Slovac Republic
The given paper is closely connected with the numerical modal analysis of eigenfrequencies and eigenshapes for turbine blades of the turbojet engine with the help of the mathematic modelling. The mathematic model was created in Pro-Engineer program and it was subsequently created to the ANSYS program in order to apply finite element method. Distribution of the stress in the turbine blades is presented in [Pa]. The presented results of the eigenshapes and distribution of the stress are obtained in the graphic form.
Keywords: modal analysis, eigenfrequencies, eigenshapes, stress, finite element method
Grants and funding:
Slovak Grant Agency VEGA 1/0649/17, KEGA 007TnUAD-4/2017, and resulted from the project “Center for quality testing and diagnostics of materials”, ITMS code 26210120046 relating to the Operational Program Research and Development funded from European Fund of Regional Development.
Published: December 1, 2019 Show citation
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