| SiCf/SiC matrix composites are regarded as one of the promising candidates in aero engine hot-section parts owing to their excellent high-temperature mechanical properties and low density.However,the service life of SiC parts is limited by the poor water vapor corrosion resistance in the combustion chamber.Fortunately,environmental barrier coatings(EBCs)prepared on the surface of SiC matrix can effectively improve the high temperature water vapor corrosion resistance.Among all the EBCs materials,ytterbium silicates(Yb2SiO5and Yb2Si2O7)are one of the research hotspots of EBCs owing to their low coefficient of thermal expansion,excellent corrosion resistance,good phase stability and chemical compatibility.In this thesis,the effects of Yb2Si2O7doping on the microstructure,mechanical properties,thermal conductivity and high temperature sintering behavior of Yb2SiO5-Yb2Si2O7composite ceramics were studied.The stoichiometric Yb2Si2O7middle layer and Yb2SiO5-Yb2Si2O7working layer were prepared by plasma spraying technology.The deposition mechanism,thermal cycling performance and high temperature water vapor corrosion behavior of the coatings were studied.The research results lay a theoretical foundation for promoting the application of SiCf/SiC matrix composites in aero engine hot section components.The main results are as follows:(1)The effects of Yb2Si2O7doping on the thermal conductivity,mechanical properties and high-temperature sintering resistance of Yb2SiO5-Yb2Si2O7 composite ceramics were studied.The 0.5Yb2SiO5-0.5Yb2Si2O7composite ceramics were only composed of monoclinic X2-Yb2SiO5andβ-Yb2Si2O7phases. Compared with pure Yb2SiO5ceramics,the fracture toughness of 0.5Yb2SiO5-0.5Yb2Si2O7composite ceramic was increased by 60%,and high-temperature sintering performance was greatly improved.The thermal conductivity remained at a low level.The grain size and density remained unchanged after sintering at 1400℃ for 100 h.(2)The preparation and phase structure control technology of plasma-sprayed Yb2Si2O7coating were mastered.The plasma-sprayed Yb2Si2O7coating has a typical layered structure composed of dark gray structure(Yb2Si2O7),light gray structure(Yb2Si2O7+Yb2SiO5)and light strip structure(Yb2SiO5).It was mainly due to the volatilization of SiO2with the different degrees in the sprayed powder during the spraying process.The plasma-sprayed Yb2Si2O7coating after heat-treatment was composed of 90.68 mol.%Yb2Si2O7and 9.32 mol.% Yb2SiO5two phases.The content of Yb2Si2O7phase after heat-treatment reached 99.41 mol.%when added 10 mol.%SiO2to the Yb2Si2O7sprayed powder.It was proved that adding excessive SiO2to Yb2Si2O7can effectively offset the problem of SiO2volatilization in the process of coating preparation,so as to prepare Yb2Si2O7coating with high purity.(3)Thermal cycling failure performance and high-temperature water-oxygen corrosion resistance of the plasma-sprayed Si/Yb2Si2O7/0.5Yb2SiO5-0.5Yb2Si2O7 coatings at 1350℃ were clarified.The microstructure of the plasma-sprayed 0.5Yb2SiO5-0.5Yb2Si2O7coating was relatively dense.The relative content of Yb2SiO5in the coating was 52.96 mol.%,and the relative content of Yb2Si2O7 was 47.04 mol.%due to a small amount of volatilization of SiO2.It still maintained good high-temperature phase stability after sintered at 1350℃ for 100 h.The Si/Yb2Si2O7/0.5Yb2SiO5-0.5Yb2Si2O7coating peeled off due to the thickening and cracking of the SiO2TGO layer after 672 thermal cycles at 1350℃.Compared with the traditional Si/Mullite/Yb2SiO5coating(257 cycles), its thermal cycling performance was improved by 160%.The water vapor corrosion resistance of Si/Yb2Si2O7/0.5Yb2SiO5-0.5Yb2Si2O7coating was comparable to that of traditional Si/Mullite/Yb2SiO5coating at 1350℃.Although the Yb2Si2O7phase in the working coat decreased due to the reaction with high-temperature water vapor,the structure of the coating still remained stable, compact,and no spalling occurred after the water-oxygen corrosion for 200 h. |