IN-SITU HIGH TEMPERATURE LOW CYCLE FATIGUE STUDY OF SURFACE TOPOGRAPHY EVOLUTION IN NICKEL SUPERALLOY

1 PETRENEC Martin
Co-authors:
2 POLÁK Jaroslav 1,3 ŠAMOŘIL Tomáš 1 DLUHOŠ Jiří 4 OBRTLÍK Karel
Institutions:
1 TESCAN ORSAY HOLDING, a.s., Brno, Czech Republic, EU, martin.petrenec@tescan.cz, jiri.dluhos@tescan.cz
2 CEITEC IPM, Institute of Physics of Materials ASCR, Brno, Czech Republic, EU, polak@ipm.cz
3 CEITEC BUT, Brno University of Technology, Brno, Czech Republic, tomas.samoril@ceitec.vutbr.cz
4 Institute of Physics of Materials ASCR, Brno, Czech Republic, EU, obrtlik@ipm.cz
Conference:
23rd International Conference on Metallurgy and Materials, Hotel Voronez I, Brno, Czech Republic, EU, May 21 - 23, 2014
Proceedings:
Proceedings 23rd International Conference on Metallurgy and Materials
Pages:
1139-1144
ISBN:
978-80-87294-52-9
ISSN:
2694-9296
Published:
18th June 2014
Proceedings of the conference were published in Web of Science and Scopus.
Metrics:
273 views / 165 downloads
Abstract

In-situ Low Cycle Fatigue test (LCF) at temperature 635 °C have been performed in Scanning Electron Microscope (SEM) equipped with Electron Backscatter Diffraction analysis (EBSD) on a small dog-bone-shaped specimen of cast Inconel 713LC superalloy. The aim of the work was to study early stage fatigue damage at high temperature by the observations of the characteristic surface relief evolution and crystallographic characterization changes by EBSD together with post observation of internal dislocation structures on FIB prepared TEM lamella. The detail of slip bands shape was checked by FIB and AFM microscopes. The LCF test was conducted on GATAN stage with pre tilted position and constant stress amplitude of total cycle number of 20. The relief produced in the first cycle determines the other locations of the localized cyclic slip to the primary slip planes (111). The relief was modified in the next cycles but without forming additionally new slip traces in the primary system. Based on EBSD analysis before and after LCF, the orientation of two grains was changed which caused activation of second slip system. The damage mechanism evolution is closely connected with the cyclic strain localization to the persistent slip bands where the fatigue cracks were initiated.

Keywords: In-situ, SEM, high temperature, fatigue, superalloy

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