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High Cycle Fatigue Data Transferability of MAR-M 247 Superalloy from Separately Cast Specimens to Real Gas Turbine Blade

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    SYSNO ASEP0534779
    Document TypeJ - Journal Article
    R&D Document TypeJournal Article
    Subsidiary JČlánek ve WOS
    TitleHigh Cycle Fatigue Data Transferability of MAR-M 247 Superalloy from Separately Cast Specimens to Real Gas Turbine Blade
    Author(s) Šmíd, Miroslav (UFM-A) RID, ORCID
    Horník, Vít (UFM-A)
    Kunz, Ludvík (UFM-A) RID, ORCID
    Hrbáček, Karel (UFM-A)
    Hutař, Pavel (UFM-A) RID, ORCID
    Number of authors5
    Article number1460
    Source TitleMetals. - : MDPI
    Roč. 10, č. 11 (2020)
    Number of pages16 s.
    Languageeng - English
    CountryCH - Switzerland
    Keywordshigh-temperature fatigue ; nickel-based superalloy ; investment casting ; metallography ; turbine blade
    Subject RIVJL - Materials Fatigue, Friction Mechanics
    OECD categoryMechanical engineering
    R&D ProjectsLQ1601 GA MŠMT - Ministry of Education, Youth and Sports (MEYS)
    LM2015069 GA MŠMT - Ministry of Education, Youth and Sports (MEYS)
    EG15_019/0004399 GA MPO - Ministry of Industry and Trade (MPO)
    Research InfrastructureIPMINFRA - 90069 - Ústav fyziky materiálů AV ČR, v. v. i.
    Method of publishingOpen access
    Institutional supportUFM-A - RVO:68081723
    UT WOS000593263400001
    EID SCOPUS85094857586
    DOI10.3390/met10111460
    AnnotationCast polycrystalline superalloys are widely used for critical components in aerospace and
    automotive industries, such as turbine blades or turbocharges. Therefore, their fatigue endurance
    belongs to one of the most essential mechanical characteristics. Full-scale testing of such components
    involves great technical difficulties and requires significant experimental effort. The present study
    evaluates the effects of microstructural parameters with respect to representative fatigue testing of a
    cast turbine blade by separately cast specimens. For that purpose, the cast polycrystalline MAR-M 247
    Ni-based superalloy was investigated in the following conditions: (i) specimens extracted from a real
    gas turbine blade, specimens separately cast into the mould with (ii) top or (iii) bottom filling systems.
    Obtained diverse microstructures allowed us to assess the effect of grain size, porosity, and texture on
    fatigue performance. The tests were held at a symmetrical loading regime at temperature 800 °C
    in laboratory air. The results indicate that the level of porosity is a dominant structural parameter
    determining the fatigue endurance, while grain size and texture effects were of minor importance
    contributing mainly to fatigue life scatter.
    WorkplaceInstitute of Physics of Materials
    ContactYvonna Šrámková, sramkova@ipm.cz, Tel.: 532 290 485
    Year of Publishing2021
    Electronic addresshttps://www.mdpi.com/2075-4701/10/11/1460
Number of the records: 1  

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