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Preparation,Properties,and CMAS Corrosion Behavior(NdGdYErYb)2Zr2O7 High-entropy Ceramics

Posted on:2024-08-11Degree:MasterType:Thesis
Country:ChinaCandidate:G Q LinFull Text:PDF
GTID:2531307145977019Subject:Materials and Chemical Engineering (Professional Degree)
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With the development of high-performance gas turbines,the high-pressure turbine inlet temperature is increasing,which brings more severe service environment to the combustion chamber and blades and other hot-end components,and it is already difficult to meet the requirements of using single-crystal nickel-based high-temperature alloy alone.The application of thermal barrier coating on the alloy surface can effectively solve the above problems.Compared with the most widely used yttrium oxide stabilized zirconia(YSZ)thermal barrier coated ceramic materials,high entropy rare earth zirconate ceramic(HE-RE2Zr2O7)materials are rapidly developing due to lower thermal conductivity,excellent high temperature stability and sintering resistance.Therefore,in this paper,sintered blocks of(Nd Gd YEr Yb)2Zr2O7 high-entropy ceramics were prepared by high-temperature solid-phase reaction method using Nd2O3,Gd2O3,Y2O3,Er2O3,Yb2O3,and Zr O2 as raw materials.The thermal conductivity,thermal expansion coefficient,thermal stability,hardness and corrosion behavior of HE-RE2Zr2O7 with CMAS(Ca O-Mg O-Al2O3-Si O2)were investigated around the performance of HE-RE2Zr2O7 and the actual service environment.The main studies and conclusions of the paper are as follows:(1)By calculating the difference value of cationic radii(δ),equimolar high-entropy rare earth zirconate ceramics(Nd0.2Gd0.2Y0.2Er0.2Yb0.2)2Zr2O7 and non-equimolarhigh-entropyrareearthzirconateceramics(Nd0.58Gd0.05Y0.05Er0.05Yb0.27)2Zr2O7 withδgreater than 5.2%were prepared,and single-component Rare Earth Zirconate ceramic Nd2Zr2O7was used as a control.The phase structures of the three ceramic materials were analyzed by XRD and Raman spectroscopy.It was found that Nd2Zr2O7had a pyrochlore structure,non-equimolar(Nd0.58Gd0.05Y0.05Er0.05Yb0.27)2Zr2O7 had a dual-phase structure of pyrochlore and defect-fluorite,and equimolar(Nd0.2Gd0.2Y0.2Er0.2Yb0.2)2Zr2O7had a defect-fluorite structure.This indicates that High-Entropy Rare Earth Zirconate materials with a difference value of cationic radii(δ)greater than 5.2%can form ceramics with dual-phase structure of pyrochlore and fluorite.(2)Within the temperature range of room temperature to 1200℃,the average thermal expansion coefficients of(Nd0.58Gd0.05Y0.05Er0.05Yb0.27)2Zr2O7and(Nd0.2Gd0.2Y0.2Er0.2Yb0.2)2Zr2O7 are measured to be 12.6×10-6 and 12.9×10-6 K-1,respectively.These values are slightly higher than the thermal expansion coefficient of the single-component Nd2Zr2O7 ceramic,which is 11.2×10-6 K-1.This suggests that high-entropy design can increase the thermal expansion coefficient of the material to some extent.This observation may be attributed to the relatively lower electronegativity and lattice energy among the constituent elements.Furthermore,the thermal conductivity of high-entropy ceramic materials is lower than that of Nd2Zr2O7,with the dual-phase structured high-entropy ceramics exhibiting the lowest thermal conductivity.The mechanical analysis results indicate that the Vickers hardness of(Nd0.58Gd0.05Y0.05Er0.05Yb0.27)2Zr2O7 and(Nd0.2Gd0.2Y0.2Er0.2Yb0.2)2Zr2O7was better than that of YSZ,however,due to the lack of low-temperature phase transformation toughening and high-temperature iron-ballistic toughening mechanisms,their fracture toughness is relatively lower.The study of the high-temperature phase stability of HE-RE2Zr2O7 materials showed that they exhibited good phase stability without phase transformation occurring after annealing at 1300℃for 100 h and rapid cooling at different temperatures,which is in line with the selection requirements for ceramics used as thermal barrier coatings.(3)The corrosion behavior of(Nd0.2Gd0.2Y0.2Er0.2Yb0.2)2Zr2O7 high-entropy ceramic was studied in a molten CMAS(calcium-magnesium-aluminum-silicate)environment at 1250 and 1300℃.The corrosion mechanism is described as follows:Firstly,Ca O and Si O2 infiltrate along the defects or grain boundaries within the high-entropy ceramic and react with rare earth oxides to form apatite.The formation rate of apatite increases with the increasing ionic radius of RE3+ions.Simultaneously,the high-entropy ceramic undergoes decomposition,resulting in the formation of calcium and rare earth-stabilized Zr O2.With prolonged corrosion time,Mg O and a portion of Al2O3 on the sample surface form spinel compounds,specifically Mg Al2O4.Under corrosion at 1250℃,a continuous and dense layer of apatite is formed,which may serve as a barrier to the continuous penetration of CMAS.However,under the same conditions,the high-entropy ceramic exhibits persistent corrosion at 1300℃.
Keywords/Search Tags:Thermal barrier coating, High-entropy ceramic, Rare earth zirconate, Thermal conductivity, CMAS corrosion
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