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温度对B_(4)C涂层氧化防护性能和防护机制的影响
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作者 胡凯飞 王佩佩 +4 位作者 孙万昌 侯兆琪 易大伟 罗欢 任宣儒 《表面技术》 EI CAS CSCD 北大核心 2024年第4期89-97,共9页
目的研究温度对B_(4)C涂层氧化防护性能和防护机制的影响,得出B_(4)C涂层最佳氧化防护温度范围,以及B_(4)C涂层在不同温度的氧化防护机制演变。方法以石墨为基体,采用放电等离子烧结法在石墨表面制备B_(4)C涂层,通过不同恒温氧化试验(80... 目的研究温度对B_(4)C涂层氧化防护性能和防护机制的影响,得出B_(4)C涂层最佳氧化防护温度范围,以及B_(4)C涂层在不同温度的氧化防护机制演变。方法以石墨为基体,采用放电等离子烧结法在石墨表面制备B_(4)C涂层,通过不同恒温氧化试验(800、1000、1200、1400℃)和室温至1400℃宽温域动态氧化试验来测试其氧化防护性能,并通过X射线衍射(XRD)、扫描电子显微镜(SEM)和能谱仪(EDS)对B_(4)C涂层石墨试样氧化前后的物相组成、微观形貌、氧扩散等进行分析。结果B_(4)C涂层氧化后可生成B2O3玻璃膜,在800、1000、1200、1400℃恒温氧化的防护效率分别为98.43%、98.61%、94.4%和92.8%,在室温至1400℃宽温域动态氧化的防护效率为93.1%。B_(4)C涂层在800℃以下主要依赖结构阻氧,800至900℃由结构阻氧向惰化阻氧转变,900℃以上主要依赖惰化阻氧。1100℃以上,随温度升高B2O3玻璃膜的挥发加剧,B_(4)C涂层惰化阻氧能力减弱。结论B_(4)C涂层的氧化防护效率随温度上升先增大后减小,结构阻氧机制逐渐降低,惰化阻氧机制先升高后降低。B_(4)C涂层在800至1100℃具有良好的氧化防护性能。 展开更多
关键词 涂层 石墨 碳化硼(b_(4)c) 玻璃膜 氧化防护 阻氧机制
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B_(4)C(0001)及Al-B_(4)C(0001)表面的结构和电子性质
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作者 赵玉文 张航舶 朱岩 《河北科技师范学院学报》 CAS 2021年第3期36-41,共6页
为了从微观的角度揭示Al与B_(4)C(0001)面的相互作用情况,确定Al原子在B_(4)C(0001)表面吸附这一过程的反应机理和Al原子在B_(4)C表面的结构信息,采用密度泛函理论,通过计算表面自由能、吸附能和电子结构性能,推导出在不同的化学势下C... 为了从微观的角度揭示Al与B_(4)C(0001)面的相互作用情况,确定Al原子在B_(4)C(0001)表面吸附这一过程的反应机理和Al原子在B_(4)C表面的结构信息,采用密度泛函理论,通过计算表面自由能、吸附能和电子结构性能,推导出在不同的化学势下C原子暴露的B_(4)C(0001)表面均为最稳定的表面结构;给出了Al原子在C-B_(4)C(0001)表面的最佳吸附位置。 展开更多
关键词 碳化硼 b_(4)c(0001)表面 表面结构 电子性质 第一性原理
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Advanced research on the preparation and application of carbide ceramic fibers
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作者 Zhongqian Zhao Wei Liao +3 位作者 Jing Chen Jian Jiao Cuilan Wu Yanzi Gou 《Journal of Advanced Ceramics》 SCIE EI CAS CSCD 2024年第9期1291-1336,共46页
Carbide ceramic fibers are of significant importance for application in the high-tech areas of advanced aircraft engines,aerospace vehicles,and the nuclear industry due to their excellent properties,such as high tensi... Carbide ceramic fibers are of significant importance for application in the high-tech areas of advanced aircraft engines,aerospace vehicles,and the nuclear industry due to their excellent properties,such as high tensile strength and elastic modulus,excellent high-temperature resistance,and oxidation resistance.This paper reviews the preparation and application of different carbide ceramic fibers,including SiC fibers and transition metal carbide(e.g.,ZrC,HfC,and TaC)ceramic fibers.The preparation methods of carbide ceramic fibers are discussed in terms of different fiber diameters,represented by SiC fibers with variable weaving properties and functions due to their differences in diameter.Subsequently,the application of carbide ceramic fibers as high-temperature-resistant structural materials,catalyst carriers,sensors,and supercapacitors are summarized,and strategies for the future development of carbide ceramic fibers are proposed.This review aims to help researchers enhance their understanding of the preparation and utilization of carbide ceramic micro/nanofibers,advancing the development of high-performance carbide ceramic fibers. 展开更多
关键词 carbide ceramic fibers Sic fibers boron carbide(b_(4)c)fibers ultra-high temperature ceramics Sic ceramic fiber-reinforced Sic(Sicf/Sic)composites
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钨球对碳纤维增强复合材料包覆碳化硼陶瓷侵彻效应
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作者 王逸凡 李永鹏 +3 位作者 徐豫新 刘铁磊 焦晓龙 王若素 《兵工学报》 EI CAS CSCD 北大核心 2024年第8期2487-2496,共10页
为研究碳纤维增强复合材料(Carbon Fiber Reinforced Composite,CFRP)包覆碳化硼(B_(4)C)陶瓷在钨球侵彻下的破坏机制与防护性能,开展不同弹靶径厚比D/T(D为钨球直径,T为陶瓷厚度)下钨球对CFRP包覆B_(4)C陶瓷板(下文简称靶板)的侵彻试... 为研究碳纤维增强复合材料(Carbon Fiber Reinforced Composite,CFRP)包覆碳化硼(B_(4)C)陶瓷在钨球侵彻下的破坏机制与防护性能,开展不同弹靶径厚比D/T(D为钨球直径,T为陶瓷厚度)下钨球对CFRP包覆B_(4)C陶瓷板(下文简称靶板)的侵彻试验和数值仿真研究。通过弹道冲击试验,掌握钨球穿靶后的剩余速度以及靶板破坏形貌,分析钨球以不同速度侵彻靶板后B_(4)C陶瓷和CFRP的破坏特征;构建钨球侵彻靶板的数值仿真模型,通过再现试验结果验证模型准确性,对比分析CFRP对钨球侵彻效果的影响;基于仿真模型计算得到的数值仿真数据建立钨球垂直侵彻靶板的剩余速度计算模型,并通过试验数据验证计算模型的精度。研究结果表明:钨球垂直侵彻下,CFRP迎弹面呈圆形破口,背弹面呈十字形破口,背弹面破坏面积大于迎弹面,且随撞击速度和靶板厚度的增加,背弹面破坏面积的变化幅度大于迎弹面;与单一B_(4)C陶瓷板相比,CFRP包覆B_(4)C陶瓷板的抗侵彻性能提高4.8%;所建立的钨球垂直侵彻靶板的剩余速度计算模型计算结果的相对误差绝对值不大于15%。 展开更多
关键词 钨球 b_(4)c陶瓷 碳纤维增强复合材料 侵彻
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Thermal conductivity of boron carbide under fast neutron irradiation 被引量:1
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作者 Zhixue QU Chuanjin YU +2 位作者 Yitong WE Xiping SU Aibing DU 《Journal of Advanced Ceramics》 SCIE EI CAS CSCD 2022年第3期482-494,共13页
Due to the complex products and irradiation-induced defects, it is hard to understand and even predict the thermal conductivity variation of materials under fast neutron irradiation, such as the abrupt degradation of ... Due to the complex products and irradiation-induced defects, it is hard to understand and even predict the thermal conductivity variation of materials under fast neutron irradiation, such as the abrupt degradation of thermal conductivity of boron carbide (B_(4)C) at the very beginning of the irradiation process. In this work, the contributions of various irradiation-induced defects in B_(4)C primarily consisting of the substitutional defects, Frenkel defect pairs, and helium bubbles were re-evaluated separately and quantitatively in terms of the phonon scattering theory. A theoretical model with an overall consideration of the contributions of all these irradiation-induced defects was proposed without any adjustable parameters, and validated to predict the thermal conductivity variation under irradiation based on the experimental data of the unirradiated, irradiated, and annealed B_(4)C samples. The predicted thermal conductivities by this model show a good agreement with the experimental data after irradiation. The calculation results and theoretical analysis in light of the experimental data demonstrate that the substitutional defects of boron atoms by lithium atoms, and the Frenkel defect pairs due to the collisions with the fast neutrons, rather than the helium bubbles with strain fields surrounding them, play determining roles in the abrupt degradation of thermal conductivity with burnup. 展开更多
关键词 boron carbide(b_(4)c) thermal conductivity fast neutron irradiation
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