2021
DOI: 10.1016/j.surfcoat.2021.127071
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Effect of cooling rate on phase transformation in 6–8 wt% YSZ APS TBCs

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Cited by 29 publications
(5 citation statements)
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“…As shown from the XRD results of different life stages in Figure 8, the phase structure of the two coatings in each life stage is consistent, and they are all single tetra phase. Previous studies have shown that the phase transition from t-ZrO 2 to c-ZrO 2 and m-ZrO 2 exists only when the temperature is 1300 • C and the sintering time is more significant than 150 h, especially the transition from t-ZrO 2 to m-ZrO 2 [24]. In addition, it has been proved that the high-speed cooling rate can inhibit the phase transition of zirconia coatings [25].…”
Section: Lifementioning
confidence: 99%
“…As shown from the XRD results of different life stages in Figure 8, the phase structure of the two coatings in each life stage is consistent, and they are all single tetra phase. Previous studies have shown that the phase transition from t-ZrO 2 to c-ZrO 2 and m-ZrO 2 exists only when the temperature is 1300 • C and the sintering time is more significant than 150 h, especially the transition from t-ZrO 2 to m-ZrO 2 [24]. In addition, it has been proved that the high-speed cooling rate can inhibit the phase transition of zirconia coatings [25].…”
Section: Lifementioning
confidence: 99%
“…Among the spraying processes, the study of improving the microstructure of thermal barrier coatings has been widely concerned. It is expected that by optimizing the spraying process, the thermal barrier coatings with excellent performance can be prepared, so as to extend the service life of thermal barrier coatings [10][11][12][13][14][15].…”
Section: Introductionmentioning
confidence: 99%
“…This has motivated the search for materials capable of satisfying the requirements of advanced TBCs. 36,[43][44][45] RE 2 SiO 5 and RE 2 Si 2 O 7 have been widely studied as EBCs 2 ; however their phase transition and poor CaO-MgO-AlO 1.5 -SiO 2 (CMAS) corrosion resistance limit their further applications. 40,41,[46][47][48] CMAS particles in the atmosphere originating mainly from volcanoes eruptions and sandstorms, can melt and corrode TBCs and EBCs at high temperatures (≧1200 • C).…”
Section: Introductionmentioning
confidence: 99%
“…Yttria‐stabilized zirconia (6∼8 wt% YSZ) ceramics, currently used as TBCs, suffer from two prominent shortcomings: low working temperatures (≦1200°C) and high thermal conductivities (2.5–3.6 W·m −1 ·K −1 at 25–1000°C). This has motivated the search for materials capable of satisfying the requirements of advanced TBCs 36,43–45 . RE 2 SiO 5 and RE 2 Si 2 O 7 have been widely studied as EBCs 2 ; however their phase transition and poor CaO‐MgO‐AlO 1.5 ‐SiO 2 (CMAS) corrosion resistance limit their further applications 40,41,46–48 .…”
Section: Introductionmentioning
confidence: 99%