降级(电信)
热障涂层
熔盐
渗透(HVAC)
腐蚀
稳定器(航空)
材料科学
热的
盐(化学)
压力(语言学)
化学工程
化学
复合材料
冶金
涂层
有机化学
工程类
热力学
机械工程
电气工程
哲学
物理
语言学
作者
Chongwei Li,Zening Wang,Chengcai Li,Xiaosong Zhou,Shifeng Wen,Zhifeng Xie
标识
DOI:10.1108/acmm-03-2025-3206
摘要
Purpose This study aims to systematically investigate the synergistic effects of molten salt corrosion (75 Wt.% Na2SO4–25 Wt.% NaCl), external stress and high temperatures (1,220/1,260°C) on the degradation mechanisms of 7 Wt.% yttria-stabilized zirconia thermal barrier coatings (TBCs), with the aim of guiding the design of corrosion-resistant coatings for next-generation turbine engines. Design/methodology/approach High-temperature exposure tests under controlled molten salt corrosion and external compressive stress were conducted. Coating damage behavior at 1,220°C and 1,260°C were comparatively analyzed, including stabilizer depletion kinetics, ceramic layer thinning and interfacial damage progression. Findings Through coupled experimental characterization, two distinct degradation pathways are identified: At 1,220°C, molten salt infiltration through vertical cracks drives progressive Y2O3 stabilizer depletion, resulting in 17% ceramic layer thinning over 10 h, whereas continuous Al2O3-rich thermally grown oxide (TGO) temporarily impedes interfacial damage. In contrast, 1,260°C exposure accelerates stabilizer consumption, enabling rapid salt penetration to the TC/BC interface within 10 h, causing > 40% spallation and substrate delamination via CrCl3 vapor-induced stress concentrations. External compressive stress reduces premature ceramic densification, reducing porosity by 66% and restricting salt penetration depth. Mechanochemical coupling alters failure mode dominance – suppressing interfacial cracks through TGO growth retardation while promoting stabilizer depletion-driven thinning. Originality/value These findings reveal critical stress-temperature-corrosion synergies governing TBC degradation, the competition between molten salt diffusion kinetics and TGO reformation capability emerges as the governing factor in lifetime prediction, providing fundamental insights for designing corrosion-resistant coatings under high temperature in next-generation turbine engines.
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