2022
DOI: 10.1016/j.surfcoat.2022.128645
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Investigation of vermiculite infiltration effect on microstructural properties of thermal barrier coatings (TBCs) produced by electron beam physical vapor deposition method (EB-PVD)

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Cited by 42 publications
(7 citation statements)
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“…For example, in terms of materials, thermal barrier coatings (TBC) are widely used to extend the lifespan of components. Experts [ 21 , 22 ] have found that in high temperature environments of 718 °C, high temperatures lead to an increase in the oxidation cycle of this material layer, affecting the components’ lifespan. However, considering that it is difficult to control the temperature in the experiment, and according to the literature [ 18 ], it can also be concluded that temperature has less influence on the erosion and wear of the servo valve compared with other factors, in this study, temperature was not taken into account as one of the experimental working conditions.…”
Section: Experimental Design and Data Analysis Of Performance Degrada...mentioning
confidence: 99%
“…For example, in terms of materials, thermal barrier coatings (TBC) are widely used to extend the lifespan of components. Experts [ 21 , 22 ] have found that in high temperature environments of 718 °C, high temperatures lead to an increase in the oxidation cycle of this material layer, affecting the components’ lifespan. However, considering that it is difficult to control the temperature in the experiment, and according to the literature [ 18 ], it can also be concluded that temperature has less influence on the erosion and wear of the servo valve compared with other factors, in this study, temperature was not taken into account as one of the experimental working conditions.…”
Section: Experimental Design and Data Analysis Of Performance Degrada...mentioning
confidence: 99%
“…Thermal barrier coatings (TBCs) are functional coatings used to protect high-temperature components and extend their service life, which have been used for many years on the surfaces of advanced gas turbines, aero-engine blades and other related components 1 , 2 . TBCs layers generally consist of a ceramic top coat (TC) and metal bond coat (BC).…”
Section: Introductionmentioning
confidence: 99%
“…Thermal corrosion under high‐temperature environment and molten salt corrosion such as CaO–MgO–Al 2 O 3 –SiO 2 (CMAS) are the external factors for the failure of TBCs systems. Ozgurluk 30–40 et al. studied the influence of thermal corrosion effect and CMAS effect at high temperature (1000°C) and analyzed the failure mechanism of TBCs system.…”
Section: Introductionmentioning
confidence: 99%
“…Thermal corrosion under high-temperature environment and molten salt corrosion such as CaO-MgO-Al 2 O 3 -SiO 2 (CMAS) are the external factors for the failure of TBCs systems. Ozgurluk [30][31][32][33][34][35][36][37][38][39][40] et al studied the influence of thermal corrosion effect and CMAS effect at high temperature (1000 • C) and analyzed the failure mechanism of TBCs system. The results show that the molten salt in the air (such as molten vermiculite) interacts with YSZ to generate thermomechanical CMAS damage on the coating surface, the molten salt causes the phase transition of ZrO 2 in the coating, and the volume of ZrO 2 changes during the cooling process, all these lead to the failure of the TBCs system.…”
Section: Introductionmentioning
confidence: 99%