Number of the records: 1  

In-situ Study of the Mechanisms of High Temperature Damage

  1. 1.
    SYSNO ASEP0435392
    Document TypeC - Proceedings Paper (int. conf.)
    R&D Document TypeConference Paper
    TitleIn-situ Study of the Mechanisms of High Temperature Damage
    Author(s) Petrenec, M. (CZ)
    Polák, Jaroslav (UFM-A) RID, ORCID
    Šamořil, T. (CZ)
    Dluhoš, J. (CZ)
    Obrtlík, Karel (UFM-A) RID, ORCID
    Number of authors5
    Source Title11th International Fatigue Congress. - Zurich : Trans Tech Publications, 2014 / Clark G. ; Wang Ch. - ISSN 1022-6680 - ISBN 978-3-03835-008-8
    Pagess. 891-892
    Number of pages6 s.
    Publication formPrint - P
    ActionFatigue 2014 - International Fatigue Congress /11./
    Event date02.03.2014-07.03.2014
    VEvent locationMelbourne
    CountryAU - Australia
    Event typeWRD
    Languageeng - English
    CountryCH - Switzerland
    Keywordsfatigue damage ; high temperature ; nickel superalloy ; TEM lamella
    Subject RIVJL - Materials Fatigue, Friction Mechanics
    R&D ProjectsGA13-23652S GA ČR - Czech Science Foundation (CSF)
    Institutional supportUFM-A - RVO:68081723
    UT WOS000337767700083
    EID SCOPUS84898881690
    DOI10.4028/www.scientific.net/AMR.891-892.530
    AnnotationIn-situ Low Cycle Fatigue test (LCF) at temperature 635 °C have been performed in SEM on flat specimen of cast Inconel 713LC superalloy. The aim of the investigation was to study mechanisms of the fatigue damage during elastic-plastic cycling by the observations of the characteristic surface relief evolution and the accompanying internal dislocation structures. The selected locations on the surface were systematically studied in-situ and documented by SEM and using AFM. The surface relief in the first tensile half-cycle was formed by numerous slip steps on the primary slip planes (111). In the following compression half-cycle additional opposite slip were formed. The relief was modified in the next cycles but without forming additionally new slip traces in the primary system. The reorientation of two grains in the gauge area was measured using EBSD. At the end of cyclic loading the relation between surface persistent slip markings and persistent slip bands in the interior of the material was documented by TEM on lamella prepared by FIB. The early stages of extrusion and intrusion formation were documented. The damage mechanism evolution is closely connected with the cyclic strain localization to the persistent slip bands that are also places of fatigue crack initiation.
    WorkplaceInstitute of Physics of Materials
    ContactYvonna Šrámková, sramkova@ipm.cz, Tel.: 532 290 485
    Year of Publishing2015
Number of the records: 1  

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