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LOW CYCLE FATIGUE BEHAVIOR AND FATIGUE CRACK INITIATION IN MAR-M247 AT 700 °C
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SYSNO ASEP 0491917 Document Type C - Proceedings Paper (int. conf.) R&D Document Type Conference Paper Title LOW CYCLE FATIGUE BEHAVIOR AND FATIGUE CRACK INITIATION IN MAR-M247 AT 700 °C Author(s) Šulák, Ivo (UFM-A) ORCID
Obrtlík, Karel (UFM-A) RID, ORCID
Hrbáček, K. (CZ)Number of authors 3 Source Title METAL 2017 - 26th International Conference on Metallurgy and Materials, Conference Proceedings. - Ostrava : Tanger, 2017 - ISBN 978-80-87294-79-6 Pages s. 1580-1586 Number of pages 7 s. Publication form Medium - C Action METAL 2017: International Conference on Metallurgy and Materials /26./ Event date 24.05.2017 - 26.05.2017 VEvent location Brno Country CZ - Czech Republic Event type WRD Language eng - English Country CZ - Czech Republic Keywords Nickel-based superalloy ; cyclic stress-strain curve ; Fatigue life ; fatigue crack initiation ; focus ion beam Subject RIV JL - Materials Fatigue, Friction Mechanics OECD category Audio engineering, reliability analysis R&D Projects GA15-20991S GA ČR - Czech Science Foundation (CSF) TA04011525 GA TA ČR - Technology Agency of the Czech Republic (TA ČR) Institutional support UFM-A - RVO:68081723 UT WOS 000434346900255 EID SCOPUS 85043373713 Annotation The second generation nickel-based superalloy MAR-M247 offers a satisfying combination of fatigue and creep properties and oxidation and corrosion resistance that are required for application at elevated temperatures in hostile environments. The microstructure consists mainly of the face centred cubic γ matrix and ordered γ´ strengthening precipitates (L12 crystal structure). The present work focuses on low cycle fatigue (LCF) behaviour of polycrystalline nickel-based superalloy MAR-M247 at high temperature. LCF tests were conducted on cylindrical specimens in a symmetrical push-pull cycle under strain control with constant total strain amplitude and strain rate at 700 °C in ambient air. Cyclic stress-strain curves and fatigue life curves in the representation of plastic strain amplitude vs. stress amplitude and stress amplitude vs. the number of cycles to failure, respectively, were plotted and compared with data obtained on Inconel 713LC. Special attention was paid to the investigation of crack initiation in MAR-M247 during low cycle fatigue. Crack initiation sites were studied by means of scanning electron microscopy (SEM) in dual beam microscope TESCAN LYRA 3 XMU FESEM equipped with focus ion beam (FIB). Specimens’ surface observations revealed the formation of pronounced surface relief indicating localisation of plastic deformation. Observations in transmission electron microscope (TEM) confirmed localisation of cyclic plastic deformation in persistent slip bands along {111} slip planes. Fractographic analysis revealed fatigue crack initiation sites. Fatigue crack propagation in stage I was typical of smooth facets up to 500 μm long. Workplace Institute of Physics of Materials Contact Yvonna Šrámková, sramkova@ipm.cz, Tel.: 532 290 485 Year of Publishing 2020
Number of the records: 1