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Hot Corrosion Behavior of Lapo4-Ysz Thermal Barrier Coating Exposed to Molten Calcium-Magnesium-Alumino-Silicate (Cmas) at 1250°C-1350°C

28 Pages Posted: 27 Feb 2025 Publication Status: Under Review

See all articles by Panhao Deng

Panhao Deng

National University of Defense Technology

Wenzhi Huang

National University of Defense Technology

Ruiqi Zhong

National University of Defense Technology

Yiping Yu

National University of Defense Technology

Junhua Lou

National University of Defense Technology

Zixin Deng

National University of Defense Technology

Xin Zhou

Yantai University

Multiple version iconThere are 2 versions of this paper

Abstract

The calcium-magnesium-alumina-silicate (CMAS) corrosion behavior of LaPO4-YSZ thermal barrier coatings (TBCs) was investigated at 1250°C-1350°C for 4 hours. Corrosion was observed to occur primarily at the grain boundaries, and the corrosion depth increased with increasing temperature. The melt infiltration reaction layer formed after CMAS corrosion was primarily composed of ZrO2, residual CMAS, and La-apatite (Ca2+xLa8-x(SiO4)6-x(PO4)xO2), regardless of the temperature. It was worth noting that a continuous dense reaction layer was formed after the corrosion test at 1250 °C, which further delayed the infiltration of CMAS. However, the molten CMAS could infiltrate into the coating more easily when the temperature exceeds 1300 °C, leading to more severe corrosion. The results show that the CMAS corrosion behaviors of coating at different temperatures were primarily controlled by the infiltration and reaction processes; When temperatures exceed 1300°C, CMAS infiltration becomes the dominant process due to the reduced viscosity of the CMAS melt.

Keywords: Thermal barrier coatings, CMAS resistance, Infiltration, grain boundary, La-apatite

Suggested Citation

Deng, Panhao and Huang, Wenzhi and Zhong, Ruiqi and Yu, Yiping and Lou, Junhua and Deng, Zixin and Zhou, Xin, Hot Corrosion Behavior of Lapo4-Ysz Thermal Barrier Coating Exposed to Molten Calcium-Magnesium-Alumino-Silicate (Cmas) at 1250°C-1350°C. Available at SSRN: https://ssrn.com/abstract=5154248 or http://dx.doi.org/10.2139/ssrn.5154248

Panhao Deng

National University of Defense Technology ( email )

Changsha Hunan, 410073
China

Wenzhi Huang (Contact Author)

National University of Defense Technology ( email )

Changsha Hunan, 410073
China

Ruiqi Zhong

National University of Defense Technology ( email )

Changsha Hunan, 410073
China

Yiping Yu

National University of Defense Technology ( email )

Changsha Hunan, 410073
China

Junhua Lou

National University of Defense Technology ( email )

Changsha Hunan, 410073
China

Zixin Deng

National University of Defense Technology ( email )

Changsha Hunan, 410073
China

Xin Zhou

Yantai University ( email )

32, Qingquan RD
Laishan District
Yantai, 264005
China

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