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Structural evolution and failure mechanisms of APS tantalate high-entropy ceramic coatings in response to thermal cycle up to 1500 °C

Thermal barrier coatings (TBCs) with high working temperatures and long service life are indispensable for the hot-end components of gas turbines and aircraft engines. This work designs and verifies that tantalate high-entropy ceramic (HEC) coatings are excellent TBCs with working temperatures reach...

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Principais autores: Jiankun Wang, Lin Chen, Luyang Zhang, Hao Xu, Qinglin Zhou, Jing Feng
Formato: Artigo
Idioma:Inglês
Publicado em: Tsinghua University Press 2026-04-01
coleção:Journal of Advanced Ceramics
Assuntos:
thermal barrier coatings (tbcs)
high-entropy ceramic coatings
failure mechanisms
thermal cycle
thermal stress
Acesso em linha:https://www.sciopen.com/article/10.26599/JAC.2026.9221261
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