Mechanical Properties and Thermal Shock Resistance of SrAl_(2)Si_(2)O_(8) Reinforced BN Ceramic CompositesOA北大核心CSTPCD
Hexagonal boron nitride(h-BN)ceramics have become exceptional materials for heat-resistant components in hypersonic vehicles,owing to their superior thermal stability and excellent dielectric properties.However,their densification during sintering still poses challenges for researchers,and their mechanical properties are rather unsatisfactory.In this study,SrAl_(2)Si_(2)O_(8)(SAS),with low melting point and high strength,was introduced into the h-BN ceramics to facilitate the sintering and reinforce the strength and toughness.Then,BN-SAS ceramic composites were fabricated via hot press sintering using h-BN,SrCO_(3),Al_(2)O_(3),and SiO_(2) as raw materials,and effects of sintering pressure on their microstructure,mechanical property,and thermal property were investigated.The thermal shock resistance of BN-SAS ceramic composites was evaluated.Results show that phases of as-preparedBN-SAS ceramic composites are h-BN and h-SrAl_(2)Si_(2)O_(8).With the increase of sintering pressure,the composites’densities increase,and the mechanical properties shew a rising trend followed by a slight decline.At a sintering pressure of 20 MPa,their bending strength and fracture toughness are(138±4)MPa and(1.84±0.05)MPa·m^(1/2),respectively.Composites sintered at 10 MPa exhibit a low coefficient of thermal expansion,with an average of 2.96×10^(-6) K^(-1) in the temperature range from 200 to 1200℃.The BN-SAS ceramic composites prepared at 20 MPa display higher thermal conductivity from 12.42 to 28.42 W·m^(-1)·K^(-1) within the temperature range from room temperature to 1000℃.Notably,BN-SAS composites exhibit remarkable thermal shock resistance,with residual bending strength peaking and subsequently declining sharply under a thermal shock temperature difference ranging from 600 to 1400℃.The maximum residual bending strength is recorded at a temperature difference of 800℃,with a residual strength retention rate of 101%.As the thermal shock temperature difference increase,the degree of oxidation on the ceramic surface and cracks due to thermal stress are also increased gradually.
WANG Bo;CAI Delong;ZHU Qishuai;LI Daxin;YANG Zhihua;DUAN Xiaoming;LI Yanan;WANG Xuan;JIA Dechang;ZHOU Yu;
International Joint Laboratory of Advanced Nanomaterials of Heilongjiang Province,College of Materials Science and Chemical Engineering,Harbin Engineering University,Harbin 150001,China Key Laboratory of Advanced Structural-Functional Integration Materials,School of Materials Science and Engineering,Harbin Institute of Technology,Harbin 150001,ChinaInternational Joint Laboratory of Advanced Nanomaterials of Heilongjiang Province,College of Materials Science and Chemical Engineering,Harbin Engineering University,Harbin 150001,ChinaKey Laboratory of Advanced Structural-Functional Integration Materials,School of Materials Science and Engineering,Harbin Institute of Technology,Harbin 150001,China China Resources Cement Technology R&D Co.,Ltd,Guangzhou 510000,ChinaKey Laboratory of Advanced Structural-Functional Integration Materials,School of Materials Science and Engineering,Harbin Institute of Technology,Harbin 150001,ChinaThe First Military Representative Office of the Army Equipment Department in Beijing,Beijing 100072,ChinaThe Fourth System Design Department,Fourth Academy,China Aerospace Science and Industry Corporation Limited,Beijing 100048,ChinaKey Laboratory of Advanced Structural-Functional Integration Materials,School of Materials Science and Engineering,Harbin Institute of Technology,Harbin 150001,China School of Materials Science and Engineering,Harbin Institute of Technology(Shenzhen),Shenzhen 518055,China
化学工程
BNmatrixcompositehot-presssinteringmechanicalpropertythermalshockresistanceservicereliability
《无机材料学报》 2024 (010)
P.1182-1188 / 7
National Natural Science Foundation of China (52072088, 52072089);Natural Science Foundation of Heilongjiang Province (LH2023E061);Scientific and Technological Innovation Leading Talent of Harbin Manufacturing (2022CXRCCG001);Fundamental Research Funds for the Central Universities (3072023CFJ1003)。
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