Reduction of TBC delamination through a two-step strategy in nanosecond laser drilling of inclined film cooling holes
The pursuit of extreme thrust and efficiency in aero engines demands unprecedentedly high working temperatures in combustion chamber liners and turbine blades. Thermal barrier coatings (TBC) and film cooling holes (FCH) are two indispensable components which work together to protect the high-tempera...
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2025-05-01
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| Series: | Journal of Materials Research and Technology |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2238785425011561 |
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