2019
DOI: 10.1007/s12598-019-01307-1
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Recent progress in thermal/environmental barrier coatings and their corrosion resistance

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Cited by 70 publications
(31 citation statements)
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“…The current commercial TBC material is 7-8 wt% Y 2 O 3 partially stabilized ZrO 2 (YSZ), which has good compromise among the selection requirements [3,4]. However, YSZ is vulnerable to molten airborne dust (main components: calciummagnesium-alumino-silicate, CMAS) damage at high operating temperatures [1,[5][6][7][8][9]. This disadvantage decreases the service-life and limits the long-term application of YSZ at enhanced temperatures.…”
Section: Introduction mentioning
confidence: 99%
“…The current commercial TBC material is 7-8 wt% Y 2 O 3 partially stabilized ZrO 2 (YSZ), which has good compromise among the selection requirements [3,4]. However, YSZ is vulnerable to molten airborne dust (main components: calciummagnesium-alumino-silicate, CMAS) damage at high operating temperatures [1,[5][6][7][8][9]. This disadvantage decreases the service-life and limits the long-term application of YSZ at enhanced temperatures.…”
Section: Introduction mentioning
confidence: 99%
“…Considering these data, it is reasonable to foresee an increase in demand for TBC systems in the near future. A typical TBC system consists of four layers: (i) metallic substrate at the bottom (generally Ni-superalloy), (ii) an intermediate bond coat (BC), (iii) thermally grown (Al 2 O 3 ) oxide (TGO) formed during service, and (iv) a ceramic top coat [ 12 , 13 ]. A schematic TBC system model is represented in Figure 1 .…”
Section: Introductionmentioning
confidence: 99%
“…At present, the most common thermal barrier coatings are composed of bond coat and ceramic working layer. Among them, the bond coat material is usually MCrAlY (M = Ni and/or Co), and the working layer material is mainly ceramics based on 8 wt.% Y 2 O 3 stable ZrO 2 (8YSZ) [1][2][3][4]. However, 8YSZ coating cannot be applied for a long time under high temperature conditions above 1200 • C, the reason is that when the long-term service temperature is higher than 1200 • C, YSZ will undergo phase transition (t'-ZrO 2 → t-ZrO 2 + c-ZrO 2 ) and sintering, accompanied by thermal physical and mechanical property degradation, strain tolerance reduction, and crack generation, and eventually lead to coating failure [2,5].…”
Section: Introductionmentioning
confidence: 99%
“…In addition, there are a large number of literature reports on the corrosion performance of La 2 Zr 2 O 7 thermal barrier coatings under oxygen [9,16,20,21], molten salts or oxides (such as Na 2 SO 4 , V 2 O 5 , etc.) [4,[22][23][24], CaO-MgO-Al 2 O 3 -SiO 2 (CMAS) [4,[25][26][27], simulated rain water after CMAS corrosion [28], and high-temperature water vapor [4,29], etc., but there are few literature reports on the corrosion performance of La 2 Zr 2 O 7 thermal barrier coating in seawater corrosive medium [30]. Considering that aircraft engines, turbines and turbine blades may be stored in a marine environment [28], it is necessary to study the corrosion resistance of La 2 Zr 2 O 7 thermal barrier coating in this case.…”
Section: Introductionmentioning
confidence: 99%