The elucidation of creep-fatigue damage mechanisms is still controversial for high-
temperature structures after surface strengthening treatments, which serves as a critical …

Aiming at the creep-fatigue interaction damage failure problem of turbine blades in
aeronautical engineering, firstly, based on the modified Kachanov-Rabotnov-Chaboche …

In this study, the microstructural evolutions are systematically investigated in the IN718 alloy
that has been in-service for eight years. Correspondingly, the effect of in-service process on …

For nuclear power generation as a carbon‐neutral energy source, in‐vessel retention (IVR)
must be implemented to maintain the structural integrity of nuclear reactor pressure vessel …

Abstract The AlCoCrFeNi 2.1 eutectic high-entropy alloy (EHEA) is regarded as a promising
candidate for structural materials in high-temperature equipment, which may experience the …

High-performance joining especially brazing has been highly expected in the manufacture
or maintenance of single crystal blades. In this paper, a Ni-40Cr-10Ta (at.%) alloy was …

A peridynamic creep–fatigue model is proposed to study creep–fatigue mechanical
responses and damage behaviors. A non-unified constitutive model is reformulated in a …

Nickel-based single crystal superalloys CMSX-4 have been widely used to manufacture
aeroengine turbine blades because of their excellent high-temperature comprehensive …

The background of deep peak-shaving poses demanding requirements for the performance
of metal components in thermal power plants. The cracking of the connecting fins on the side …

Epitaxial growth of titanium carbide (TiC) layer is vital for single-crystalline diamond (SCD) to
ensure wettability when brazed with metals, however, how TiC grain size affects the …