2016
DOI: 10.1016/j.surfcoat.2015.12.053
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Molten silicate reactions with plasma sprayed ytterbium silicate coatings

Abstract: The reactions between molten calcium aluminum magnesium silicates (CMAS) at 1300°C and atmospheric plasma spray (APS) deposited environmental barrier coatings on SiC substrates have been investigated. The tri-layer coatings comprised a silicon bond coat protected by a layer of mullite and either Yb 2 SiO 5 (ytterbium monosilicate, YbMS) or Yb 2 Si 2 O 7 (ytterbium disilicate, YbDS) as the topcoat. The APS deposition process resulted in two-phase top coats; the YbMS coating contained Yb 2 O 3 regions in a matri… Show more

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Cited by 131 publications
(79 citation statements)
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“…Reactions of molten silicate deposits with RE monosilicates and disilicates exhibit significant similarities and differences. Disilicates frequently react with the deposits to form apatite, nominally of composition Ca 2 RE 8 (SiO 4 ) 6 O 2 .…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…Reactions of molten silicate deposits with RE monosilicates and disilicates exhibit significant similarities and differences. Disilicates frequently react with the deposits to form apatite, nominally of composition Ca 2 RE 8 (SiO 4 ) 6 O 2 .…”
Section: Introductionmentioning
confidence: 99%
“…Previous investigations on RE monosilicates have been limited to deposits with high Ca:Si ratios (~0.73) . In these cases, monosilicates consume both CaO and SiO 2 from the melt to form apatite:Y2SiO5+0.5CaOmelt+0.5SiO2melt0.25Ca2Y8)(SiO46O2…”
Section: Introductionmentioning
confidence: 99%
“…Siliceous debris ingested into aero‐engines produces molten deposits of calcium‐magnesium‐aluminosilicate (CMAS) glass. CMAS reacts with candidate EBC materials to form non‐protective phases . Because of mismatch in the thermal expansion coefficients of these phases relative to the underlying composite, both the deposits and the reaction products may crack upon cooling.…”
Section: Introductionmentioning
confidence: 99%
“…All known turbine hot section materials, whether metallic or the recently introduced ceramic composites (CMCs), rely on ceramic coatings. However, both the thermal barrier coatings (TBCs) used to protect metallic components and the environmental barrier coatings (EBCs) used to protect CMCs are temperature limited when exposed to molten dusts, which comprise highly corrosive calcium‐magnesium aluminosilicates (CMAS) . A second major barrier is associated with coating toughness limitations, as the consequences of coating loss become more critical with increasing reliance on their continued protection.…”
Section: Ceramics For Extreme Environmentsmentioning
confidence: 99%