2017
DOI: 10.1016/j.jallcom.2017.04.022
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Hot corrosion studies on plasma sprayed bi-layered YSZ/La 2 Ce 2 O 7 thermal barrier coating fabricated from synthesized powders

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Cited by 30 publications
(8 citation statements)
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“…Unlike the SPS GZO/YSZ TBCs [12], the present study illustrates that the plasma sprayed bilayer coating without columnar microstructure is a better option to design a TBC with improved hot corrosion resistance. Furthermore, the hot corrosion properties of YSZ/La 2 Ce 2 O 7 (LCO) bilayer TBCs have been studied in our previous work [26].In comparison to YSZ/LCO bilayer TBCs, the YSZ/GZO coatings exhibited better corrosion resistance properties. The weight gain results of YSZ and bilayer YSZ/GDZ coatings exposed to 1100 °C thermal cycling revealed higher weight gain for YSZ single layer TBCs.…”
Section: Discussionmentioning
confidence: 99%
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“…Unlike the SPS GZO/YSZ TBCs [12], the present study illustrates that the plasma sprayed bilayer coating without columnar microstructure is a better option to design a TBC with improved hot corrosion resistance. Furthermore, the hot corrosion properties of YSZ/La 2 Ce 2 O 7 (LCO) bilayer TBCs have been studied in our previous work [26].In comparison to YSZ/LCO bilayer TBCs, the YSZ/GZO coatings exhibited better corrosion resistance properties. The weight gain results of YSZ and bilayer YSZ/GDZ coatings exposed to 1100 °C thermal cycling revealed higher weight gain for YSZ single layer TBCs.…”
Section: Discussionmentioning
confidence: 99%
“…Plasma grade flowable 8 wt% YSZ and GZO powders were prepared by a single step co-precipitation technique. The detailed experimental procedure for the synthesis of flowable 8 wt% YSZ powders has already been described in our previous work [26]. The steps involved in the preparation of GZO powders are as follows: gadolinium nitrate solution was prepared by adding dilute nitric acid to 50 g of Gd 2 O 3 powder (99.9% purity, Mincometsal).…”
Section: Synthesis Of Plasma Grade Powdersmentioning
confidence: 99%
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“…However, there are disadvantages such as excoriation, hot corrosion, and phase transition, which reduce the service life of the coating . Hot corrosion is one of the main damage factors in thermal barrier coatings due to the effect of molten salts on the coating‐gas interface . Transport fuels usually contain sundries such as Na and V, leading to the formation of Na 2 SO 4 and V 2 O 5 salts on the surface of turbine blades .…”
Section: Introductionmentioning
confidence: 99%