Abstract
Nickel-based single-crystal superalloy turbine blades have been widely used in engines of aircrafts or power plants, but some defect grains are often found on the surface of the blade after full heat treatment or even after casting. Rhenium-rich particles, as well as an intermediate layer, were almost always detected along any defect grain boundary region, if it existed, from a low-angle grain boundary to a high-angle boundary. The particles were also found on the top surface of the base material. The composition and morphology of the particles were different from the most common topologically close packed phases or a fine particle with similar morphology detected at the boundary region between a recrystallized grain and a matrix grain. An additional heat treatment could completely dissolve the fine particles. Furthermore, any rhenium-rich particles were not reformed after achieving uniform distribution of the alloying elements.
Original language | English |
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Article number | 1201 |
Journal | Crystals |
Volume | 11 |
Issue number | 10 |
DOIs | |
Publication status | Published - 6 Oct 2021 |
Bibliographical note
Funding: This work was supported by the Engineering and Physical Sciences Research Council,grant number EP/T018518/1.
Acknowledgments: The financial support and provision of evaluation test pieces by Rolls-Royce plc is acknowledged.
Keywords
- Cross section
- Investment casting
- Oxidation
- Surface defect
- Turbine blade
ASJC Scopus subject areas
- General Chemical Engineering
- General Materials Science
- Condensed Matter Physics
- Inorganic Chemistry