Influence of Microstructural Change on Crack Growth in Thermal Barrier Coating Subjected to Thermal Cycling under Temperature Gradient

Author:

Kitazawa Rumi,Okada Mitsutoshi,Ozeki Takayuki

Publisher

Gas Turbine Society of Japan

Subject

Mechanical Engineering

Reference33 articles.

1. Kuwabara, M., and Hada, S., 2015, “Progress of Higher Temperature and Efficiency of Large Scale Gas Turbine and Future Prospects,” Journal of the Gas Turbine Society of Japan, Vol. 43, pp.308-313.

2. Kojima, Y., 2010, “Latest Technological Trends in Gas Turbine Heat Resistant Coating Development,” Journal of the Gas Turbine Society of Japan, Vol. 38, pp.85-90.

3. Okada, M., Ohtani, R., Kojima, Y., and Arikawa, H., 2005, “Development of Evaluation Method for Resistance to Thermal Cycling of Thermal Barrier Coatings for Gas Turbine -Damage Process of TBC and Improvement of Resistance to Thermal Cycling-,” Central Research Institute of Electric Power Industry Research Report, Q04017.

4. Okada, M., Hisamatsu, T., Yuri, I., Arikawa, H., and Kojima, Y., 2010, “Development of an Evaluation Method for Resistance to Thermal Cycling of TBC -Difference in Degradation and Damage between Thermal Cycling Tests under Isothermal State and under Temperature Gradient-,” Central Research Institute of Electric Power Industry Research Report, M10001.

5. Okada, M., Kitazawa, R., Takahashi, T., and Ozeki, T., 2021, “Delamination Conditions of Thermal Barrier Coating Subject to Thermal Cycling under Temperature Gradient,” Proceedings of the 49th Annual Conference of the Gas Turbine Society of Japan, A-21.

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