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Ballistic behavior of boron carbide reinforced AA7075 aluminium alloy using friction stir processing-An experimental study and analytical approach 被引量:1
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作者 I.SUDHAKAR G.MADHUSUDHAN REDDY K.SRINIVASA RAO 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2016年第1期25-31,共7页
High strength-to-weight ratio of non-ferrous alloys, such as aluminium, magnesium and titanium alloys, are considered to be possible replacement of widely accepted steels in transportation and automobile sectors. Amon... High strength-to-weight ratio of non-ferrous alloys, such as aluminium, magnesium and titanium alloys, are considered to be possible replacement of widely accepted steels in transportation and automobile sectors. Among these alloys, magnesium is self explosive and titanium is costlier, and aluminium is most likely to replace steels. Application of aluminium or its alloys is also thought of as an appropriate replacement in defence field, especially to enhance the easiness in mobility of combat vehicles while maintaining the same standard as that of conventional armour grade steels. Hence most of the investigations have been confined to aluminium or its alloys as base material and open an era of developing the newer composite materials to address the major limitation, i.e. tribological properties. The surface composites can be fabricated by incorporating the ceramic carbides like silicon carbide, carbides of transition metals and oxides of aluminium using surface modification techniques, such as high energy laser melt treatment, high energy electron beam irradiation and thermal spray process which are based on fusion route. These techniques yield the fusion related problems, such as interfacial reaction, pin holes, shrinkage cavities or voids and other casting related defects, and pave the way to need of an efficient technique which must be based on solid state. Recently developed friction stir processing technique was used in the present investigation for surface modification of AA7075 aluminum alloy, which is an alternative to steels. In the present investigation, 160 μm sized boron carbide powder was procured and was reduced to 60 μm and 30 μm using high energy ball mill. Subsequently these powders were used to fabricate the surface composites using friction stir processing.Ballistic performance testing as per the military standard(JIS.0108.01) was carried out. In the present work, an analytical method of predicting the ballistic behavior of surface composites was developed. This method was based on energy balance, i.e., the initial energy of impact is same as that of energy absorbed by multi layers. An attempt also has been made to validate the analytical results with the experimental findings. Variation between the analytical and experimental results may be accounted due to the assumptions considering such as isotropic behavior of target and shearing area of contact as cylindrical instead of conical interface As the analytical model yields the ballistic performance in the closer proximity of experimentally obtained, it can be considered to be an approximation to evaluate the ballistic performance of targets. 展开更多
关键词 AA7075 aluminium alloy Friction stir processing(FSP) Surface metal matrix composite(SMMC) boron carbide(B4C) Ballistic performance TARGET
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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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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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基于硼二十面体的高硬度B_(4)C材料结构设计及基本物性研究
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作者 张新欣 师文建 +6 位作者 赵宇 薛慧春 禹国梁 李美霖 陈辉 张嘉 成泰民 《沈阳化工大学学报》 CAS 2021年第1期90-96,共7页
富硼材料常由难以压缩的硼二十面体结构单元构成,因此硬度较高,是研发新型硬质或超硬材料的重要候选体系.利用原子替换方法,从理论上设计一种基于硼二十面体结构单元的新型立方B_(4)C结构,这一新B_(4)C结构由B_(12)二十面体通过C原子相... 富硼材料常由难以压缩的硼二十面体结构单元构成,因此硬度较高,是研发新型硬质或超硬材料的重要候选体系.利用原子替换方法,从理论上设计一种基于硼二十面体结构单元的新型立方B_(4)C结构,这一新B_(4)C结构由B_(12)二十面体通过C原子相连.利用基于密度泛函理论的第一性原理方法系统研究这一结构的原子成键、热学及动力学稳定性、电子性质、弹性性质及理论硬度等.研究结果表明:在立方B_(4)C结构中B-B之间多以三中心多电子共价键结合,并形成难以压缩的B_(12)二十面体构型,二十面体之间通过C-B双中心共价键结合;该结构在50 GPa压强下,能量低于实验提出的菱方相B_(4)C,且动力学声子谱稳定,因此有望从实验获得;该结构理论计算维氏硬度高于20 GPa,且同时兼具金属性,是潜在的导电硬质材料.该研究将为后期实验工作提供理论依据. 展开更多
关键词 硬质材料 第一性原理方法 B_(4)C 硼二十面体结构
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硼铝复合材料硼含量置信度临界安全分析研究 被引量:1
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作者 邵增 易璇 +2 位作者 李云龙 杨海峰 于淼 《核科学与工程》 CAS CSCD 北大核心 2021年第4期862-868,共7页
为评价临界安全设计中硼铝复合材料所需的硼含量置信度,本文以某核电厂乏燃料贮存格架为例,通过详细模拟硼铝复合材料中B_(4)C颗粒的弥散分布,分别分析其所采用的2.7 mm厚硼铝板和4.0 mm厚硼铝板在不同的硼含量下,不同粒径的B_(4)C颗粒... 为评价临界安全设计中硼铝复合材料所需的硼含量置信度,本文以某核电厂乏燃料贮存格架为例,通过详细模拟硼铝复合材料中B_(4)C颗粒的弥散分布,分别分析其所采用的2.7 mm厚硼铝板和4.0 mm厚硼铝板在不同的硼含量下,不同粒径的B_(4)C颗粒弥散分布对格架整体反应性的影响,并对比分析了湿法贮存与干法贮存的情形。分析结果表明,在使用20%以上B_(4)C含量、B_(4)C粒径100μm以下的硼铝复合材料进行临界安全控制时,临界安全分析中可以根据对B_(4)C含量采用高达95%的置信度;如若B_(4)C粒径达到150μm,则临界安全分析中宜采用90%的置信度;对相同的硼铝复合材料,干法贮存条件下可以对B_(4)C含量采用更高的置信度。此外,还对不同贮存条件下中子隧道效应的不同规律进行了分析探讨。 展开更多
关键词 硼铝复合材料 硼含量 置信度 B_(4)C颗粒 弥散分布 临界安全
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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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