2021
DOI: 10.1016/j.matdes.2021.109561
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Quantitative mapping of service process-microstructural degradation-property deterioration for a Ni-based superalloy based on chord length distribution imaging process

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Cited by 29 publications
(9 citation statements)
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“…However, researchers have focused on developing physical models for establishing quantitative relationships between the states of microstructures, aging or service processes, and the corresponding phases of physical properties. A data-driven model for small data can be an alternative to developing quantitative relationships beyond the conventional method [8].…”
Section: Yearmentioning
confidence: 99%
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“…However, researchers have focused on developing physical models for establishing quantitative relationships between the states of microstructures, aging or service processes, and the corresponding phases of physical properties. A data-driven model for small data can be an alternative to developing quantitative relationships beyond the conventional method [8].…”
Section: Yearmentioning
confidence: 99%
“…However, researchers have focused on developing physical model quantitative relationships between the states of microstructures, agin cesses, and the corresponding phases of physical properties. A data-d small data can be an alternative to developing quantitative relationships ventional method [8]. The gas path analysis (GPA) method is traditionally used for gas t This is a method of calculating component characteristic parameters su and turbine efficiency, heat of combustion of fuel, and unmeasured v temperature and pressure from measured data [9].…”
Section: Yearmentioning
confidence: 99%
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“…Nickel-based superalloys (Ni 0.25 Al 0.75 , NiAl, Ni 0.75 Al 0.25 , etc.) are key materials in the manufacture of advanced aero engines because of their excellent properties, such as resistance to high-temperature deformation, oxidation and corrosion, especially their ability to work at temperatures as high as 85% to 90% of the melting point [ 1 , 2 , 3 , 4 ]. Ni 3 Al superalloy has a melting point temperature as high as 1395 °C and excellent yield properties in the middle-temperature range of 600–800 °C due to its new two-phase (γ′-γ) microstructure; therefore, it has received significant research attention and has become one of the most promising candidate materials for blades and impellers of the new-generation aero engine [ 5 , 6 ].…”
Section: Introductionmentioning
confidence: 99%