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Microstructure And CMAS Corrosion Behaviour Of Rare-earth Zirconate Thermal Barrier Coatings

Posted on:2013-10-31Degree:MasterType:Thesis
Country:ChinaCandidate:W H ZhangFull Text:PDF
GTID:2251330392468363Subject:Materials science
Abstract/Summary:PDF Full Text Request
Rare–earth zirconates have generated substantial interest as the next generationof TBC (Thermal barrier coatings) based primarily on their intrinsically lowerthermal conductivity, higher phase stability and resistance to sintering than thestate–of–the–art TBC materials YSZ. Sm2Zr2O7, Sm4/3Yb2/3Zr2O7and La1.6Eu0.4–Zr2O7powders were synthesized by solid reaction. Free–stand coatings of YSZ,Sm2Zr2O7,Sm4/3Yb2/3Zr2O7and La1.6Eu0.4Zr2O7were prepared by atmosphereplasma spray. YSZ and double ceramic layered Sm2Zr2O7/YSZ,(Sm2/3Yb1/3)2–Zr2O7/YSZ and La1.6Eu0.4Zr2O7/YSZ were sprayed on GH99super–alloy substratewith NiCoCrAlY as bond–coat.Sm2Zr2O7and La1.6Eu0.4Zr2O7exhibit pyrochlore–type structure while Sm4/3–Yb2/3Zr2O7consists of most defect fluorite–type phase and a little of pyrochlore–type phase.Energy Diffraction Spectrum imply that a part of rare–earth oxide in rare–earthzirconates was lost during plasma spray where the most loss happened in Sm2Zr2O7and the least in Sm4/3Yb2/3Zr2O7. The content of loss increased in step with spraypower. XRD results show that spray power have a significant impact on phasecompositions of rare–earth zirconate coatings. Sm4/3Yb2/3Zr2O7coatings sprayed onGH99super–alloy substrate at40kW exhibit defect fluorite–type structure whileSm2Zr2O7and La1.6Eu0.4Zr2O7coatings present a mixture of defect fluorite–typephase and a small amount of tetragonal ZrO2.CMAS (Calcium–Magnesium Alumino Silicate) attacks on TBC wereinvestigated with free–standing coatings. Results show that a dense sealing layerbetween rare–earth zirconate coatings and molten CMAS is quickly produced assoon as they contact each other. The sealing layer comprised of grains of the apatitetype phase and fluorite type phase can arrest molten CMAS. The smaller ionicradius of rare–earth apply, the more quickly reaction become between correspondingrare–earth zirconate and molten CMAS, consequently the higher resistance coatingspossess to the penetration of molten CMAS.The thermal shock resistance performances of the four as–sprayed coatingswith matrix at1250oC were tested by heating–water method. The results indicatethat the thermal shock resistance ability of Sm4/3Yb2/3Zr2O7/YSZ andLa1.6Eu0.4Zr2O7/YSZ coatings are equal to YSZ coatings while Sm2Zr2O7/YSZcoatings is much higher than YSZ coatings. The existences of tetragonal ZrO2which can toughen Sm2Zr2O7coatings facilitate the higher thermal shock resistance abilityof Sm2Zr2O7/YSZ coatings.
Keywords/Search Tags:rare–earth zirconate, thermal barrier coatings, CMAS, atmosphereplasma spray, microstructure
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