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引入TaSi_2对ZrB_2-20%SiC抗氧化性能的影响 被引量:2

Effects of Ta-Additions on the Oxidation of ZrB_2-20% SiC
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摘要 将TaSi_2引入到ZrB_2-20%SiC中得到ZrB_2-10%SiC-10%TaSi_2,并在1 000、1 200、1 500和1650℃有氧条件下分别氧化5、15和30 min。复合材料通过热压烧结法制备(1 950℃/30 MPa/30 min),并通过XRD及SEM等方法对氧化后的质量变化及微观结构进行了分析。结果表明,TaSi_2的引入提高了Zr B2-20%SiC的致密度和力学性能,但是在1 200℃以上温度氧化时,ZrB_2-10%SiC-10%TaSi_2的抗氧化性有所降低。 TaSi2 was added into ZrB2-20%SiC to get ZrB2-10%SiC-10%TaSi2. Then composites were oxidized in stagnant air at 1000℃, 1200℃, 1500℃ and 1650℃ for 5 min, 15 min,30 min.The composites were prepared by hot pressed sintering ( 1950℃/30 MPa/30 min) and analyzed by X-ray diffraction and SEM.The weight change due to oxi- dation and microstructure were recorded. The results show the density and mechanical properties are increased by adding TaSi2 into ZrB2-20%SiC,but the oxidation resistance of ZrB2-10%SiC-10%TaSi2 is decreased above 1200℃.
作者 吴坤 徐林 杨文彬 张寅 张大海 WU Kun XU Lin YANG Wenbin ZHANG Yin ZHANG Dahai(Aerospace Research Institute of Materials & Processing Technology, Beijing 100076)
出处 《宇航材料工艺》 CSCD 北大核心 2017年第3期37-41,共5页 Aerospace Materials & Technology
基金 国家重点基础研究发展计划(973计划) 2015CB655200
关键词 TaSi2 ZrB2-20%SiC 力学性能 抗氧化性能 TaSi2, ZrB2-20%SIC , Mechanical property, Oxidation resistance
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  • 1周长灵,程之强,王英姿,高冬云,孙成功,陈达谦.无压烧结硼化锆基ZrB_2-SiC复相陶瓷的结构与性能[J].硅酸盐通报,2006,25(2):16-18. 被引量:10
  • 2Upadhya K,Yang J M,Hoffman W P.Materials for Ultrahigh Temperature Structural Applications[J].American Cennic Bulle-tin,1997,72(12):51-56.
  • 3Fahrenholtz W G,Hihnas G E,Talmy I G,et al.Refractory Di-borides of Zirconium and Hafnium[J].Journal of the American Ceramic Society,2007,90(5):.347-1364.
  • 4Levine S R,Opila E J,Halbig M C,et al.Evaluation of Ultra-High Temperature Ceramics for Aeropropulsion Use[J].Journal of the European Ceramic Society,2002,22(14/15):2757-2767.
  • 5Zhang Xinghong(张幸红),Hu Ping(胡平),Han Jiecai(韩杰才),et al.Ablation Behavior of ZrB2-SiC Ultra High Temper-sture Ceramics under Simulated Atmospheric Re-Entry Conditions[J].Composites Science and Technology,2008,68(7/8):1718-1726.
  • 6Opeka M M,Talmy I G,Zaykoski J A.Ocidation-Based Materi-als Selection for 2 000℃+Hypersonic Aerosurfaces:Theoretical Considerations and Historical Experience[J].Journal of Materials Science,2004,39(19):5 887-5 904.
  • 7Talmy I,Zaykoski J A,Opeka M M.High-Temperature Chemis-try and Oxidation of ZrB2 Ceramics Containing SiC,Si3N4,Ta5Si3,and Tasi2[J].Journal of the American Ceramic Society,2008,91(7):2 250-2 257.
  • 8Sciti D,Brach M,Bellosi A.Oxidation Behavior of a Pressure-less Sintered ZrB2-MoSi2 Ceramic Composite[J].Journal of Ma-serials Research,2005,20(4):922-930.
  • 9Opila E,Levine S,Lorincz J.Oxidation of ZrB2-and HfB2-Based Ultra-High Temperature Ceramics:Effect of Ta Additions[J].Journal of the Material Science,2004,39(19):5 969-5977.
  • 10Zhang Xinghong(张幸红),Hu Ping(胡平),Han Jiecai(韩杰才),et al.Effect of Various Additives on the Oxidation Be-havior of ZrB2-Based Ultra-High Temperature Ceramics at 1800℃[J].Journal of the American Ceramic Society,2010,93(2):345-349.

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