A Review of the Machining of the Film Cooling Holes with Thermal Barrier Coatings Through Non-traditional Machining Methods
Author:
Funder
Natural Science Foundation of Xinjiang Uygur Autonomous Region
Xinjiang Tianchi Doctoral Project
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s12541-024-01094-5.pdf
Reference118 articles.
1. Ni, M., Zhu, H. Y., Qiu, Y., Xu, D. C., & Liu, S. L. (2005). Review of aero-engine turbine blade cooling technology. Gas Turbine Technology, 4, 25–33+38. https://doi.org/10.16120/j.cnki.issn1009-2889.2005.04.006
2. Guo, W., & Wang, P. F. (2020). Analysis of turbine blade cooling technology. Aviation Power, 17(6), 55–58.
3. Lai, J. H. (2021). A review of aero-engine turbine blade cooling technology. New Industrialization, 11(8), 39–40. https://doi.org/10.19335/j.cnki.2095-6649.2021.8.019
4. Li, S. F., Huang, K., Ma, Y. S., & Chen, D. Y. (2022). Progress in the design and preparation of film cooling holes for aero-engine turbine blades. Thermal Power Engineering, 37(9), 1–11. https://doi.org/10.16146/j.cnki.rndlgc.2022.09.001
5. BUNKER, R.S. (2002). Film cooling effectiveness due to discrete holes within a transverse surface slot. In ASME Turbo Expo 2002: Power for Land, Sea, and Air: GT2002–30178. https://doi.org/10.1115/GT2002-30178.
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