2016
DOI: 10.1179/1878641315y.0000000017
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The degradation of thermal barrier coatings by molten deposits: introducing the concept of basicity

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Cited by 13 publications
(7 citation statements)
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“…Air pressures up to approximately 30 bar are possible [2]. Gas turbines operate globally and as such experience a wide range of contaminants including salt, calcium magnesium alumina silicate (CMAS) and all atmospheric pollutants [3]. Operating stresses are such that the cyclic yield strength of the material is commonly exceeded in stress concentration features (particularly for discs), and for aerofoils high cycle fatigue (HCF) loading may dictate component design.…”
Section: Industrial Application (A) Applications Load Regimes and Opmentioning
confidence: 99%
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“…Air pressures up to approximately 30 bar are possible [2]. Gas turbines operate globally and as such experience a wide range of contaminants including salt, calcium magnesium alumina silicate (CMAS) and all atmospheric pollutants [3]. Operating stresses are such that the cyclic yield strength of the material is commonly exceeded in stress concentration features (particularly for discs), and for aerofoils high cycle fatigue (HCF) loading may dictate component design.…”
Section: Industrial Application (A) Applications Load Regimes and Opmentioning
confidence: 99%
“…Hydrides form in a δ-ZrH(111) || α-Zr(0002), [1][2][3][4][5][6][7][8][9][10] || [11][12][13][14][15][16][17][18][19][20] orientation relationship, where the habit plane is the basal (0002) plane; hydrides in Ti have the same behaviour. In zirconium, Carpenter rationalized the appearance of the macro-hydride packets at 14-17°from the (0002) plane as being a consequence of the arrangement of nano-hydride platelets in such as manner as to autocatalytically accommodate each other's strain fields [77].…”
Section: (F) Hydrogen Effects On Deformation Behaviourmentioning
confidence: 99%
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“…It has a high melting point, typically around 1240 • C (Poerschke & Levi 2015) (although it can be significantly higher; see e.g. Wiesner, Vempati & Bansal (2016) and references therein), which allows it to exist in the molten state even at high temperatures encountered in modern aviation gas turbine engines (Clarke, Oechsner & Padture 2012;Ndamka, Wellman & Nicholls 2016). With high viscosity, high density and high surface tension, CMAS tends to form non-volatile droplets with θ eq / = 0 rather than completely wetting the surfaces (Grant et al 2007;Vidal-Setif et al 2012;Nieto et al 2021).…”
Section: Introductionmentioning
confidence: 99%
“…When it solidifies, it forms a glass-like material that can adhere to surfaces and resist erosion. The buildup of CMAS on turbine engine components can lead to clogging of the cooling passages and degradation of the protective coatings, resulting in engine performance issues and even damage or failure (Clarke et al 2012;Ndamka et al 2016;Song et al 2016;Wiesner et al 2016).…”
Section: Introductionmentioning
confidence: 99%