Thermal property and failure behavior of LaSmZrO thermal barrier coatings by EB-PVD

La(2)Zr(2)O(7) coatings are promising candidates to substitute YSZ coatings in advanced gas turbine engines. In this work, Sm-doped La(2)Zr(2)O(7) coatings were deposited by physical vapor deposition. This work focuses on the crystal structure, thermal conductivity, thermal expansion coefficient, mo...

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Detalles Bibliográficos
Autores principales: Shen, Zaoyu, Liu, Guanxi, Zhang, Rujing, Dai, Jianwei, He, Limin, Mu, Rende
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Elsevier 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8983386/
https://www.ncbi.nlm.nih.gov/pubmed/35402886
http://dx.doi.org/10.1016/j.isci.2022.104106
Descripción
Sumario:La(2)Zr(2)O(7) coatings are promising candidates to substitute YSZ coatings in advanced gas turbine engines. In this work, Sm-doped La(2)Zr(2)O(7) coatings were deposited by physical vapor deposition. This work focuses on the crystal structure, thermal conductivity, thermal expansion coefficient, morphology, composition, and thermal durability of LaSmZrO coatings. The LaSmZrO ceramics exhibit low thermal conductivity (1.69 W/mK at 800°C) and high thermal expansion coefficient (9.72∗10(−6) K(−1) at 1500°C) compared with La(2)Zr(2)O(7). The LaSmZrO/YSZ coatings with feathery microstructure show relatively good thermal durability (8183 cycles or 856 h) under high temperature. The broken regions are observed at the ceramic coating/bond coating interface. The failure behaviors are relevant with crack evolution and thermally grown oxide growth. This work might guide the investigation of advanced coatings under high temperature.

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