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Stress-Strain Response and Fatigue Lifetime of EEQ-111 Superalloy in Cyclic Loading at High Temperatures

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68081723%3A_____%2F24%3A00582280" target="_blank" >RIV/68081723:_____/24:00582280 - isvavai.cz</a>

  • Result on the web

    <a href="http://dx.doi.org/10.1016/j.prostr.2023.12.016" target="_blank" >http://dx.doi.org/10.1016/j.prostr.2023.12.016</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1016/j.prostr.2023.12.016" target="_blank" >10.1016/j.prostr.2023.12.016</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Stress-Strain Response and Fatigue Lifetime of EEQ-111 Superalloy in Cyclic Loading at High Temperatures

  • Original language description

    The material under investigation was polycrystalline Sulzer’s nickel-based superalloy EEQ-111 which is equivalent to the original nGTD-111 developed in the late 1970s. The EEQ-111 superalloy is typical with coarse polyhedral dendritic grains with an average ngrain size of (2.48 ± 0.87) mm. The microstructure consists of γ channels, a bimodal distribution of nano-sized coherent γ´ nprecipitates, γ/γ´ eutectic, and MC and M23C6 carbides. The proportion of casting defects in the material is minimal due to the napplication of hot isostatic pressing. Low cycle fatigue experiments were executed on solid cylindrical specimens with a gauge nlength and diameter of 15 mm and 6 mm, respectively. A symmetrical push-pull cycling under strain control mode was utilized at n800 °C and 900 °C using servo-hydraulic testing machine MTS 810. Hysteresis loops, fatigue hardening/softening curves, and nfatigue lifetime curves in Coffin-Manson, Basquin, and total strain amplitude representations were obtained. Analysis of fracture nsurfaces and secondary cracks from metallographic sections revealed the preferential initiation sites of fatigue cracks that are nindependent of temperature. In contrast, the fatigue crack propagation is purely transgranular at 800 °C, whereas a mix of ntransgranular and intergranular crack propagation can be found at 900 °C indicating grain boundary weakening.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20501 - Materials engineering

Result continuities

  • Project

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2024

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    Procedia Structural Intergrity

  • ISBN

  • ISSN

    2452-3216

  • e-ISSN

  • Number of pages

    11

  • Pages from-to

    154-164

  • Publisher name

    Elsevier

  • Place of publication

    Amsterdam

  • Event location

    London

  • Event date

    Sep 12, 2023

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article