2020
DOI: 10.1016/j.ceramint.2019.09.037
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Effect of TGO evolution and element diffusion on the life span of YSZ/Pt–Al and YSZ/NiCrAlY coatings at high temperature

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Cited by 27 publications
(6 citation statements)
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“…However, the above research mainly considers the growth of α-Al2O3, which serves as the resistance to oxidation. Moreover, the induced stress can be almost released by creep Nowadays, many researchers focus on continuous TGO growth and the induced stress evolution in TBCs [54][55][56][57][58][59][60]. Evans et al [61] utilized Eshelby's elastic inclusion method to make TGO growth equivalent to the self-assembly process of the free expansive TGO shell, and then established a sphere model of TGO growth.…”
Section: Research Advance On Tgo Growthmentioning
confidence: 99%
“…However, the above research mainly considers the growth of α-Al2O3, which serves as the resistance to oxidation. Moreover, the induced stress can be almost released by creep Nowadays, many researchers focus on continuous TGO growth and the induced stress evolution in TBCs [54][55][56][57][58][59][60]. Evans et al [61] utilized Eshelby's elastic inclusion method to make TGO growth equivalent to the self-assembly process of the free expansive TGO shell, and then established a sphere model of TGO growth.…”
Section: Research Advance On Tgo Growthmentioning
confidence: 99%
“…Therefore, the use of plasma torches, plasma spray, and jets demands an indispensable consideration to generate highly efficient materials and overwhelming technology for developing nations. The plasma jet plants can implement a circular economy framework for the rising needs [68][69][70][71][72][73].…”
Section: Plasma Technologymentioning
confidence: 99%
“…8,9 During hightemperature service, there will be a thermally grown oxide (TGO) layer formed between the TC layer and the BC layer, which consists of mixed oxide clusters of chromium (Cr, Al) 2 O 3 , spinel Ni(Cr, Al) 2 O 4 , and nickel oxide NiO (CSN). [10][11][12] However, the hot components covered with TBCs serve in the harsh environment of high temperature, high pressure, and high thermal stress during the takeoff, cruise, and landing of the aircraft, which will accelerate the premature spallation failure of TBCs. Therefore, it is important to prolong the thermal cycling lifetimes and improve the thermal shock resistance of TBCs.…”
Section: Introductionmentioning
confidence: 99%
“…The common BC material is MCrAlY (M: Ni, Co, and Ni + Co), which is necessary to accommodate the thermal expansion misfit between the ceramic coating and the substrate 8,9 . During high‐temperature service, there will be a thermally grown oxide (TGO) layer formed between the TC layer and the BC layer, which consists of mixed oxide clusters of chromium (Cr, Al) 2 O 3 , spinel Ni(Cr, Al) 2 O 4 , and nickel oxide NiO (CSN) 10–12 . However, the hot components covered with TBCs serve in the harsh environment of high temperature, high pressure, and high thermal stress during the takeoff, cruise, and landing of the aircraft, which will accelerate the premature spallation failure of TBCs.…”
Section: Introductionmentioning
confidence: 99%