Abstract
A turbine compressor package is used for pipeline gas transmission. When operating, compressor turbine blades develop vibration, which increases the number of dynamic stress cycles and results in the blade failure. The present study aims to determine the frequency of natural blade vibration and to consider it in the context of the blade repair process. In the first stage of the study, an oscillating contour is developed to generate standing oscillation wave which characteristics are used as experimental data. To process those data, a mathematical model is developed to calculate the blade resonant frequency. Finally, the boundaries of the assured quality area are determined. Blade operation capacity analysis method will allow us to reduce the number of environmentally dangerous experiments.
Cited by
3 articles.
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1. A novel method for the natural frequency estimation of the jet engine turbine blades based on its dimensions;Heliyon;2024-02
2. Laser cladding of the coating on the shroud flanges of the turbine blades;VII INTERNATIONAL CONFERENCE “SAFETY PROBLEMS OF CIVIL ENGINEERING CRITICAL INFRASTRUCTURES” (SPCECI2021);2023
3. Repair of bandage shelves of turbine blades;INTERNATIONAL SCIENTIFIC AND PRACTICAL CONFERENCE “ENERGY, ECOLOGY AND TECHNOLOGY IN AGRICULTURE” (EEA2022);2022