Effect of Aluminide Coating Thickness on High-Temperature Fatigue Response of MAR-M247 Nickel-Based Superalloy
Abstract
:1. Introduction
2. Materials and Methods
2.1. Material and Coating Deposition
2.2. Experimental Testing
3. Results and Discussion
3.1. Microstructural Characterization of the As-Received Material and Deposited Aluminide Coatings
3.2. High-Temperature Fatigue Testing
3.3. Fractographic Observations
4. Conclusions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Acknowledgments
Conflicts of Interest
References
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C | Cr | Mn | Si | W | Co | Al | Ni |
---|---|---|---|---|---|---|---|
0.09 | 8.80 | 0.10 | 0.25 | 9.70 | 9.50 | 5.70 | Bal. |
Coating Thickness | Deposition Time | Deposition Temperature | Internal Pressure | Protective Atmosphere |
---|---|---|---|---|
20 µm | 4 h | 1040 °C | 150 mbar | Hydrogen |
40 µm | 12 h |
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Kopec, M. Effect of Aluminide Coating Thickness on High-Temperature Fatigue Response of MAR-M247 Nickel-Based Superalloy. Coatings 2024, 14, 1072. https://doi.org/10.3390/coatings14081072
Kopec M. Effect of Aluminide Coating Thickness on High-Temperature Fatigue Response of MAR-M247 Nickel-Based Superalloy. Coatings. 2024; 14(8):1072. https://doi.org/10.3390/coatings14081072
Chicago/Turabian StyleKopec, Mateusz. 2024. "Effect of Aluminide Coating Thickness on High-Temperature Fatigue Response of MAR-M247 Nickel-Based Superalloy" Coatings 14, no. 8: 1072. https://doi.org/10.3390/coatings14081072