Repair of Ni-based single-crystal superalloys using vacuum plasma spray
Hot isostatic pressing
DOI:
10.1016/j.matdes.2019.107656
Publication Date:
2019-02-13T23:23:58Z
AUTHORS (11)
ABSTRACT
Turbine blades in aviation engines and land based gas-turbines are exposed to extreme environments. They suffer damage accumulation associated with creep, oxidation fatigue loading. Therefore, advanced repair methods of special interest for the gas-turbine industry. In this study, CMSX-4 powder is sprayed by Vacuum Plasma Spray (VPS) on single-crystalline substrates similar compositions. The influence substrate temperature investigated altering heating stage between 850 °C 1000 °C. Different spray parameters were explored identify their microstructure. Hot isostatic pressing (HIP) featuring fast quenching rates was used minimize porosity allow well-defined heat-treatments coatings. microstructure analysed orientation imaging scanning electron microscopy (SEM), using backscatter diffraction (EBSD). effects different processing regarding grain size. results show that optimized HIP can lead dense coatings optimum γ/γ′ interface coating oxide free shows good mechanical integrity. formation fine crystalline regions as a result cooling observed at single-crystal surface, which resulted growth during heat-treatment orientations determined crystallography substrate.
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