Number of the records: 1  

High cycle fatigue of nickel-based superalloy MAR-M 247 at high temperatures

  1. 1.
    SYSNO ASEP0435146
    Document TypeC - Proceedings Paper (int. conf.)
    R&D Document TypeConference Paper
    TitleHigh cycle fatigue of nickel-based superalloy MAR-M 247 at high temperatures
    Author(s) Šmíd, Miroslav (UFM-A) RID, ORCID
    Kunz, Ludvík (UFM-A) RID, ORCID
    Hutař, Pavel (UFM-A) RID, ORCID
    Hrbáček, K. (CZ)
    Number of authors4
    Source TitleXVII International Colloquium on Mechanical Fatigue of Metals (ICMFM17). - Amsterdam : Elsevier, 2014 / Gulagliano M. ; Vergani L. - ISSN 1877-7058
    Pagess. 329-332
    Number of pages4 s.
    Publication formOnline - E
    ActionICMFM 2014 International Colloquium on Mechanical Fatigue of Metals /17./
    Event date25.06.2014-27.06.2014
    VEvent locationVerbania
    CountryIT - Italy
    Event typeWRD
    Languageeng - English
    CountryNL - Netherlands
    KeywordsHigh cycle fatigue ; Superalloy ; MAR-M 247 ; High temperature ; Fracture surface ; S-N curve
    Subject RIVJL - Materials Fatigue, Friction Mechanics
    R&D ProjectsFR-TI4/030 GA MPO - Ministry of Industry and Trade (MPO)
    EE2.3.20.0214 GA MŠMT - Ministry of Education, Youth and Sports (MEYS)
    Institutional supportUFM-A - RVO:68081723
    UT WOS000396733300060
    EID SCOPUS84904421075
    DOI10.1016/j.proeng.2014.06.273
    AnnotationThe nickel-based superalloy MAR-M 247 was experimentally studied in the area of high-cycle fatigue at temperatures 650, 800 and 900 °C. The alloy, a cast polycrystalline material processed by hot isostatic pressing (HIP), was subjected to symmetrical cyclic loading. The fracture surfaces of specimens were studied by scanning electron microscopy from the perspective of the influence of temperature on the fatigue damage mechanism and fatigue crack initiation. The extent of Stage I of crystallographic fatigue crack propagation and non-crystallographic Stage II differs with various test temperatures. Fatigue crack initiation sites were predominantly shrinkage pores inherited from casting. The general description of governing mechanisms of the fatigue crack initiation and the crack propagation are proposed.
    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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