Počet záznamů: 1  

High-temperature low-cycle fatigue and fatigue–creep behaviour of Inconel 718 superalloy: Damage and deformation mechanisms

  1. 1.
    SYSNO ASEP0586291
    Druh ASEPJ - Článek v odborném periodiku
    Zařazení RIVJ - Článek v odborném periodiku
    Poddruh JČlánek ve WOS
    NázevHigh-temperature low-cycle fatigue and fatigue–creep behaviour of Inconel 718 superalloy: Damage and deformation mechanisms
    Tvůrce(i) Bartošák, M. (CZ)
    Horváth, J. (CZ)
    Gálíková, Markéta (UFM-A)
    Slaný, M. (CZ)
    Šulák, Ivo (UFM-A) ORCID
    Celkový počet autorů5
    Číslo článku108369
    Zdroj.dok.International Journal of Fatigue. - : Elsevier - ISSN 0142-1123
    Roč. 186, SEP (2024)
    Poč.str.17 s.
    Jazyk dok.eng - angličtina
    Země vyd.GB - Velká Británie
    Klíč. slovaLow-cycle fatigue ; Fatigue–creep ; Inconel 718 superalloy ; Damage mechanisms ; Microstructure
    Vědní obor RIVJG - Hutnictví, kovové materiály
    Obor OECDMaterials engineering
    CEPEH22_008/0004634 GA MŠMT - Ministerstvo školství, mládeže a tělovýchovy
    Způsob publikováníOpen access
    Institucionální podporaUFM-A - RVO:68081723
    UT WOS001249227100001
    EID SCOPUS85194333802
    DOI https://doi.org/10.1016/j.ijfatigue.2024.108369
    AnotaceIn this article, strain-controlled Low-Cycle Fatigue (LCF) and fatigue–creep tests were performed on Inconel
    718 nickel-based superalloy at temperatures of 650 ◦C and 730 ◦C. LCF tests at elevated temperatures were
    performed with a mechanical strain rate of 1 × 10−3/s, while fatigue–creep tests involved either tensile or
    compressive strain dwell. Both the LCF and fatigue–creep tests revealed cyclic softening, with the mean stress
    evolving oppositely to the applied strain dwell in the fatigue–creep tests. Investigations into the damage
    mechanisms identified intergranular cracking as the predominant failure mode. Fatigue–creep loading with
    a compressive dwell resulted in multiple crack initiations from transgranular oxide intrusions, along with
    multiple creep cavities during loading at 730 ◦C. Deformation features such as persistent slip bands and
    deformation nanotwins were observed during cycling at 650 ◦C. In addition, fatigue–creep tests at 730 ◦C
    exhibited 𝛿 phase precipitation and a coarsening of strengthening precipitates, contributing to additional
    softening that increased over prolonged test durations. Finally, the observed lifetime during LCF tests decreased
    with increasing temperatures, and fatigue–creep loading was observed to be more damaging than LCF. On the
    other hand, fatigue–creep loading with a tensile strain dwell demonstrated a higher lifetime compared to LCF
    at 730 ◦C.
    PracovištěÚstav fyziky materiálu
    KontaktYvonna Šrámková, sramkova@ipm.cz, Tel.: 532 290 485
    Rok sběru2025
    Elektronická adresahttps://www.sciencedirect.com/science/article/pii/S0142112324002275?via%3Dihub
Počet záznamů: 1  

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