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High-Temperature Fatigue Testing of Turbine Blades Cover

High-Temperature Fatigue Testing of Turbine Blades

Open Access
|Apr 2024

Abstract

This paper evaluates the efficacy of a patented grip for high-temperature fatigue testing by establishing the S-N curve for full-scale nickel-based turbine blades under simulated environmental conditions. Initially, a bending test assessed the stress-displacement characteristics of the component. This was followed by a series of fatigue tests at 950°C, using cyclic bending with force amplitudes from 5.2 kN to 6.6 kN and a constant frequency of 10 Hz. The setup, integrating the grip into a standard testing machine, proved effective for high-temperature tests and successfully determined the service life of full-scale components.

DOI: https://doi.org/10.2478/fas-2023-0002 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 22 - 27
Published on: Apr 29, 2024
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2024 Mateusz Kopec, Dominik Kukla, Mirosław Wyszkowski, Zbigniew L. Kowalewski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.