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Ballistic performance of titanium-based layered composites made using blended elemental powder metallurgy and hot isostatic pressing
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作者 Pavlo Markovsky Jacek Janiszewski +5 位作者 Dmytro Savvakin Oleksandr Stasyuk Bartosz Fikus Victor Samarov Vianey Ellison Sergey V.Prikhodko 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2024年第9期1-14,共14页
Metal matrix composites tiles based on Ti-6Al-4V(Ti64)alloy,reinforced with 10,20,and 40(vol%)of either TiC or TiB particles were made using press-and-sinter blended elemental powder metallurgy(BEPM)and then bonded to... Metal matrix composites tiles based on Ti-6Al-4V(Ti64)alloy,reinforced with 10,20,and 40(vol%)of either TiC or TiB particles were made using press-and-sinter blended elemental powder metallurgy(BEPM)and then bonded together into 3-layer laminated plates using hot isostatic pressing(HIP).The laminates were ballistically tested and demonstrated superior performance.The microstructure and properties of the laminates were analyzed to determine the effect of the BEPM and HIP processing on the ballistic properties of the layered plates.The effect of porosity in sintered composites on further diffusion bonding of the plates during HIP is analyzed to understand the bonding features at the interfaces between different adjacent layers in the laminate.Exceptional ballistic performance of fabricated structures was explained by a significant reduction in the residual porosity of the BEPM products by their additional processing using HIP,which provides an unprecedented increase in the hardness of the layered composites.It is argued that the combination of the used two technologies,BEPM and HIP is principally complimentary for the materials in question with the abilities to solve the essential problems of each used individually. 展开更多
关键词 metal matrix composites Powder metallurgy Titanium hydride powder Master alloy Titanium carbide Titanium boride Hot isostatic pressing Ballistic tests
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Ballistic performance of tungsten particle/metallic glass matrix composite long rod 被引量:8
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作者 Ji-cheng Li Xiao-wei Chen Feng-lei Huang 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2019年第2期132-145,共14页
In the present manuscript numerical analysis on the ballistic performance of a tungsten particle/metallic glass matrix(WP/MG) composite rod is conducted by integrating with related experimental investigations. In the ... In the present manuscript numerical analysis on the ballistic performance of a tungsten particle/metallic glass matrix(WP/MG) composite rod is conducted by integrating with related experimental investigations. In the corresponding finite element method(FEM) simulations a modified coupled thermomechanical constitutive model is employed to describe the mechanical properties of metallic glass(MG)matrix, and geometrical models of the WP/MG composite rod are established based on its inner structure. The deformation and failure characteristics of the rod and target materials are analyzed in detail,and the influences of various factors on the ballistic performance of the WP/MG composite long rod are discussed. Related analysis demonstrates that the penetrating performance of the WP/MG rod is similar to that of the tungsten fiber/metallic glass matrix(WF/MG) composite long rod, i.e., a "self-sharpening" behavior also occurs during the penetration process, and correspondingly its penetrating capability is better than that of the tungsten heavy alloy(WHA) rod. However, the mass erosion manner of the WP/MG rod is different and the erosion is relatively severe, thus its penetrating capability is a little lower compared with that of the WF/MG one. Moreover, the impact velocity and the target strength have significant influences on the ballistic performance of the WP/MG composite rod, whereas the effect of initial nose shape is very little. 展开更多
关键词 TUNGSTEN particle/metallic glass matrix (WP/MG)composite BALLISTIC performance Shear band Self-sharpening Numerical analysis
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Heat treatment optimization for tensile properties of 8011 Al/15% SiCp metal matrix composite using response surface methodology 被引量:7
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作者 V.VEMBU G.GANESAN 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2015年第4期390-395,共6页
In this study,a mathematical model was developed to optimize the heat treatment process for maximum tensile strength and ductility of aluminum(8011) silicon carbide particulate composites.The process parameters are so... In this study,a mathematical model was developed to optimize the heat treatment process for maximum tensile strength and ductility of aluminum(8011) silicon carbide particulate composites.The process parameters are solutionizing time,aging temperature,and aging time.The experiments were performed on an universal testing machine according to centre rotatable design matrix.A mathematical model was developed with the main and interactive effects of the parameters considered.The analysis of variance technique was used to check the adequacy of the developed model.The optimum parameters were obtained for maximum tensile strength.Fractographic examination shows the cracks and dimples on the fractured surfaces of heat-treated specimen. 展开更多
关键词 热处理工艺优化 颗粒复合材料 响应曲面法 拉伸性能 金属基体 万能试验机 开发模型
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Ultrafine and fine particle emission in turning titanium metal matrix composite(Ti-MMC)
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作者 Seyed Ali NIKNAM Masoud SABERI +3 位作者 Jules KOUAM Ramin HASHEMI Victor SONGMENE Marek BALAZINSKI 《Journal of Central South University》 SCIE EI CAS CSCD 2019年第6期1563-1572,共10页
Titanium metal matrix composite(Ti-MMC)has excellent features and capabilities which can be considered a potential candidate to replace commercial titanium and superalloys within an extensive range of products and ind... Titanium metal matrix composite(Ti-MMC)has excellent features and capabilities which can be considered a potential candidate to replace commercial titanium and superalloys within an extensive range of products and industrial sectors.Regardless of the superior features in Ti-MMC,however,referring to several factors including high unit cost and existence of rigid and abrasive ceramic particles in the generated matrices of the work part,the Ti-MMC is grouped as extremely difficult to cut with a poor level of machinability.Furthermore,adequate process parameters for machining Ti-MMCs under several lubrication methods are rarely studied.Therefore,adequate knowledge of this regard is strongly demanded.Among machinability attributes,ultrafine particles(UFPs)and fine particles(FPs)have been selected as the main machinability attributes and the factors leading to minimized emission have been studied.According to experimental observations,despite the type of coating used,the use of higher levels of flow rate led to less UFPs,while no significant effects were observed on UFPs.Under similar cutting conditions,higher levels of FPs were recorded under the use of uncoated inserts.Moreover,cutting speed had no significant influence on UFPs;nevertheless,it significantly affects the FPs despite the type of insert used. 展开更多
关键词 metal matrix composites(MMCs) particle emission dust emission TURNING lubrication mode
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基于纳米压痕的B_(4)C/7075Al复合材料界面本构方程反演分析
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作者 薛克敏 王可成 +3 位作者 代良伟 田辙环 石文超 李萍 《塑性工程学报》 北大核心 2025年第4期131-140,共10页
为研究热处理后高压扭转B_(4)C/7075Al复合材料界面的介观尺度力学性能,利用纳米压痕实验获取复合材料界面的载荷-位移曲线,提出了一种结合量纲法和有限元反演分析法来确定复合材料界面弹塑性本构关系的逆向分析方法。并基于获得的弹塑... 为研究热处理后高压扭转B_(4)C/7075Al复合材料界面的介观尺度力学性能,利用纳米压痕实验获取复合材料界面的载荷-位移曲线,提出了一种结合量纲法和有限元反演分析法来确定复合材料界面弹塑性本构关系的逆向分析方法。并基于获得的弹塑性本构关系开展有限元模拟,将模拟结果与实验结果进行对比。结果表明:热处理后高压扭转B_(4)C/7075Al复合材料界面的弹性模量、应变硬化指数和屈服强度分别为117.44 GPa、0.296和978 MPa。模拟得到的弹性模量和纳米硬度与实验值的相对误差分别为5.8%和2.9%,证实了基于纳米压痕反演分析B_(4)C/7075Al复合材料界面本构方程的可行性。 展开更多
关键词 金属基复合材料 高压扭转 纳米压痕 反演分析
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冷喷涂固态增材制造技术:演变、现状与机遇挑战
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作者 李文亚 黄春杰 徐雅欣 《航空制造技术》 北大核心 2025年第15期22-34,共13页
增材制造技术是一种典型的颠覆性制造技术,通过“自下而上”的材料累加成形方式,可实现传统制造方法难以完成的复杂结构。冷喷涂固态增材制造技术,因其独特的固态金属粉末高速碰撞沉积特性,展现出显著的技术优势和应用潜力。本文系统阐... 增材制造技术是一种典型的颠覆性制造技术,通过“自下而上”的材料累加成形方式,可实现传统制造方法难以完成的复杂结构。冷喷涂固态增材制造技术,因其独特的固态金属粉末高速碰撞沉积特性,展现出显著的技术优势和应用潜力。本文系统阐述了冷喷涂固态增材制造技术的概念、发展历史、技术优势及挑战,并重点分析了此技术在受损零部件修复与再制造等领域的典型应用。研究表明,冷喷涂固态增材制造技术具备沉积效率高、结合强度高、涂层致密性好等优点,尤其在高强高塑性沉积体制备和复杂构件修复方面展现出独特优势。然而,该技术也面临沉积体塑韧性不足、薄壁构件易变形开裂及喷嘴寿命短等挑战。本文总结了冷喷涂固态增材制造技术的研究进展,指出了未来发展方向,为推动该技术在航空航天、汽车制造等领域的广泛应用提供了理论参考和实践指导。 展开更多
关键词 冷喷涂 冷喷涂固态增材制造 金属 金属基复合材料 修复
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原位自生TiB_(2)陶瓷颗粒增强铝基复合材料及其在航天领域的应用
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作者 刘钧 陈哲 +4 位作者 陈东 李险峰 吴一 夏存娟 王浩伟 《载人航天》 北大核心 2025年第2期241-247,共7页
原位自生TiB_(2)陶瓷颗粒增强铝基复合材料兼具高模量、高强塑性、高抗疲劳与良好的加工成形性能,作为结构材料应用于航天飞行器,有助于实现相关构件的轻量化设计,且仅通过常规铝合金加工方法与设备,即可实现铝基复合材料构件的规模化... 原位自生TiB_(2)陶瓷颗粒增强铝基复合材料兼具高模量、高强塑性、高抗疲劳与良好的加工成形性能,作为结构材料应用于航天飞行器,有助于实现相关构件的轻量化设计,且仅通过常规铝合金加工方法与设备,即可实现铝基复合材料构件的规模化制造。对比分析了原位自生TiB_(2)陶瓷颗粒增强铝基复合材料与铝合金、传统铝基复合材料的优缺点,介绍了铸造、变形和增材制造三大系列原位自生铝基复合材料的组织性能与研究现状,以及相关系列铝基复合材料在航天领域的典型应用情况,并展望了原位自生TiB_(2)陶瓷颗粒增强铝基复合材料的发展方向。 展开更多
关键词 金属基复合材料 陶瓷颗粒 原位自生 铸造成形 塑性加工 增材制造
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电子封装用功能梯度铝基复合材料研究应用进展
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作者 方杰 刘彦强 +8 位作者 杨志宇 樊建中 刁恩泽 崔西会 黎康杰 彭颐豫 张坤 孔欣 杨博 《有色金属(中英文)》 北大核心 2025年第8期1295-1305,共11页
电子信息系统小型化、轻量化、无人化、一体化的发展趋势要求电子封装持续减小尺寸、降低重量和减少功耗(SWaP,即Size,Weight and Power)。传统的基于可伐合金、铝合金和高硅铝的微电子封装材料难以同时满足大跨度热匹配、良好的钎焊与... 电子信息系统小型化、轻量化、无人化、一体化的发展趋势要求电子封装持续减小尺寸、降低重量和减少功耗(SWaP,即Size,Weight and Power)。传统的基于可伐合金、铝合金和高硅铝的微电子封装材料难以同时满足大跨度热匹配、良好的钎焊与激光熔焊性能、高导热、高比刚度、高比强度和良好的可制造性,无法适应SWaP要求。功能梯度铝基复合材料综合了铝合金与铝硅、碳化硅铝等先进复合材料的优点,既具备大跨度热匹配、高导热率的特点,又具备精细加工和良好的激光熔焊等工艺性能,是新一代微电子封装材料的研究热点。本文综述了功能梯度铝基复合材料的优势、制备方法和封装应用情况,并对该材料制备与应用中存在的问题进行了总结,最后对其未来研究方向进行了展望。 展开更多
关键词 先进金属基复合材料 功能梯度材料 铝基复合材料 电子封装 研究应用进展
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金属/陶瓷互穿网络结构复合材料:制备方法、结构特征与性能特点
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作者 刘子瑞 肖和 +2 位作者 彭超群 王日初 王小锋 《中国有色金属学报》 北大核心 2025年第6期1895-1916,共22页
金属/陶瓷互穿网络结构复合材料是一种具有特殊增强相结构的金属基复合材料,其增强相与基体相均呈现连续网络状三维结构。凭借其优异性能,金属/陶瓷互穿网络结构复合材料在电子封装、交通工具及武器装甲等领域展现出巨大应用潜力。本文... 金属/陶瓷互穿网络结构复合材料是一种具有特殊增强相结构的金属基复合材料,其增强相与基体相均呈现连续网络状三维结构。凭借其优异性能,金属/陶瓷互穿网络结构复合材料在电子封装、交通工具及武器装甲等领域展现出巨大应用潜力。本文梳理了金属/陶瓷互穿网络结构复合材料的制备方法,包括增强相多孔预制体制备方法如固相烧结法、有机泡沫浸渍法、生物模板法、添加剂法、溶胶-凝胶法、冷冻干燥法及3D打印法等,以及复合方法如无压浸渗法、挤压铸造法及真空压力浸渗法等。分析了金属/陶瓷互穿网络结构复合材料的力学性能、耐磨性能、热学性能特点以及相关机理。最后展望了金属/陶瓷互穿网络结构复合材料的发展前景及未来研究方向。 展开更多
关键词 金属基复合材料 互穿网络结构复合材料 多孔预制体 浸渗 力学性能 热学性能 耐磨性能
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激光熔覆石墨烯增强金属基复合涂层摩擦学性能研究进展
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作者 张楚怡 刘秀波 +4 位作者 张飞志 孟元 解芳 赵红亮 朱锦鹏 《材料工程》 北大核心 2025年第8期58-71,共14页
金属基复合材料(metal matrix composites,MMC)因综合了金属相的延展性和增强相的高强度、高硬度等特性,在耐磨减摩领域具有较大应用潜力。传统的MMC硬质涂层主要通过提高增强相的含量来提高涂层的硬度和耐磨性,然而由于两相间理化性质... 金属基复合材料(metal matrix composites,MMC)因综合了金属相的延展性和增强相的高强度、高硬度等特性,在耐磨减摩领域具有较大应用潜力。传统的MMC硬质涂层主要通过提高增强相的含量来提高涂层的硬度和耐磨性,然而由于两相间理化性质差异较大,涂层内易产生较大的热应力或相变应力,导致涂层韧性下降,裂纹敏感性升高。与传统表面改性技术相比,激光熔覆(laser cladding,LC)使用高能激光束作为热源,涂层形成过程迅速,有利于获得细晶组织,降低涂层开裂敏感性。此外,石墨烯(graphane,Gr)因具有特殊的二维结构与优异的热学性能、力学性能以及自润滑性能,将其作为增强相加入金属基体中,可以形成多尺度结构涂层,在提升涂层硬度、改善减摩耐磨性能的同时,提高涂层的断裂韧性。因此本文以采用激光熔覆法制备石墨烯增强钛基、镍基、钴基复合涂层为主线,系统综述了石墨烯对金属基复合涂层微观组织演变和摩擦学性能的影响。本文首先概述了石墨烯的结构与性质,并针对石墨烯在基体中的分散难题,归纳了常用的制备激光熔覆用石墨烯材料的表面改性方法;介绍了目前采用激光熔覆法制备MMC耐磨涂层的研究现状,并归纳总结了石墨烯的减摩耐磨机理。最后提出LC加工制备Gr/MMC涂层过程中存在的若干难点,并对涂层制备工艺的进一步优化和石墨烯增强机理模型的构建进行了展望,以期为后续相关研究和实际应用提供参考。 展开更多
关键词 激光熔覆 石墨烯 金属基复合材料 摩擦学性能
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Al_(2)O_(3)颗粒增强灰铸铁基复合材料的制备与组织研究
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作者 孙佳琪 郑顺奇 王瑈 《兵器材料科学与工程》 北大核心 2025年第1期81-86,共6页
在通过数值模拟优选液体铸浸浇注系统的基础上,采用横截面积较大的直浇道和高度较低的横浇道制备Al_(2)O_(3)颗粒增强灰铸铁基复合材料,进行了组织结构分析和力学性能测试。结果表明:采用横截面积较大的直浇道和高度较低的横浇道,充型... 在通过数值模拟优选液体铸浸浇注系统的基础上,采用横截面积较大的直浇道和高度较低的横浇道制备Al_(2)O_(3)颗粒增强灰铸铁基复合材料,进行了组织结构分析和力学性能测试。结果表明:采用横截面积较大的直浇道和高度较低的横浇道,充型过程中紊流较少;Al_(2)O_(3)颗粒增强灰铸铁基复合材料存在以Si、Na为主要成分的过渡区;Al、O、Si扩散形成的Na_(2)SiO_(3)等化合物和Fe扩散进入Al_(2)O_(3)颗粒,都可改善Al_(2)O_(3)颗粒润湿性,优化铸渗效果,促进Al_(2)O_(3)颗粒与灰铸铁基体的结合;过渡层的显微硬度最低为165HV~235HV,Al_(2)O_(3)颗粒的显微硬度随着与界面距离的增加而逐渐增至2005HV~2230HV,铁基体的显微硬度随着与界面距离的增加而增大最终稳定在230HV~294HV;Al_(2)O_(3)颗粒增强灰铸铁基复合材料的屈服强度为319.1 MPa,抗压强度为519.5 MPa。 展开更多
关键词 金属基复合材料 陶瓷颗粒增强 液态铸渗 界面结合
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激光粉末床熔融对NiTi/Zr复合材料显微组织及性能的调控机制
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作者 李晟 唐柳琳 +4 位作者 闫星辰 邓朝阳 褚清坤 黄正华 郑李娟 《机床与液压》 北大核心 2025年第4期191-198,共8页
采用激光粉末床熔融增材制造的NiTi形状记忆合金普遍存在延展性低、缺陷多、形状记忆性能调控困难等问题。针对此,通过在近等原子比NiTi合金粉末中加入质量分数为1%的ZrH_(2)粉末,形成NiTi/Zr金属基复合材料,以改善NiTi合金的成形性和... 采用激光粉末床熔融增材制造的NiTi形状记忆合金普遍存在延展性低、缺陷多、形状记忆性能调控困难等问题。针对此,通过在近等原子比NiTi合金粉末中加入质量分数为1%的ZrH_(2)粉末,形成NiTi/Zr金属基复合材料,以改善NiTi合金的成形性和力学性能,并通过工艺参数有效调控NiTi合金的相变性能。结果表明:Zr掺杂在合适的成形参数条件下有效抑制了球化现象,从而减少了未熔合缺陷。同时分析了Zr掺杂NiTi形状记忆复合材料的显微组织。结果表明:激光工艺参数能够改变Zr在NiTi基体中的状态,形成Zr单质、固溶体、析出相等不同显微组织。示差扫描量热仪和拉伸实验表明:Zr掺杂结合不同的工艺参数能够实现形状记忆性能调控,并在不显著改变弹性模量的前提下同时提高材料的抗拉强度和断裂韧性。 展开更多
关键词 激光粉末床熔融 NiTi/Zr金属基复合材料 力学性能 显微组织
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三维网络结构陶瓷增强金属基复合材料的制备原理与现状
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作者 刘俊伟 方杰 +1 位作者 范才河 欧玲 《中国有色金属学报》 北大核心 2025年第6期1917-1941,共25页
本文综述了三维网络结构陶瓷增强金属基复合材料(Three-dimensional network structure ceramic reinforced metal matrix composite,3DNSCMMCs)的制备方法、机理及研究现状。重点对陶瓷预制体的孔隙调控机理、金属熔体浸渗原理及金属-... 本文综述了三维网络结构陶瓷增强金属基复合材料(Three-dimensional network structure ceramic reinforced metal matrix composite,3DNSCMMCs)的制备方法、机理及研究现状。重点对陶瓷预制体的孔隙调控机理、金属熔体浸渗原理及金属-陶瓷界面润湿和界面结合理论予以详细的介绍,并对多孔陶瓷预制体的主要制备方法及其熔体浸渗方法进行探讨,概述了3DNSCMMCs当前的研究现状,认为“增材制造(3D打印)陶瓷预制体+金属熔体真空压力浸渗”技术制备金属基复合材料将取得快速发展,获得低热膨胀、复杂结构、高体积分数增强体、高强度陶瓷增强金属基复合材料是目前研究的热点,实现其低成本、短周期、高性能及大批量化是未来发展趋势。 展开更多
关键词 金属基复合材料 多孔陶瓷 液相浸渗 3D打印
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金属基复合泡沫材料基体及力学性能研究进展
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作者 许磊 孙少祥 +2 位作者 历长云 唐玲 高琦 《粉末冶金技术》 北大核心 2025年第3期377-390,共14页
金属基复合泡沫(metal matrix syntactic foam,MMSF)是由空心微球和金属基体复合而成的一种新型多孔复合材料。本文总结了近些年有关铝基、镁基和钢基等复合泡沫研究的进展情况,并分类概述了不同基体材料的选择和制备工艺对金属基复合... 金属基复合泡沫(metal matrix syntactic foam,MMSF)是由空心微球和金属基体复合而成的一种新型多孔复合材料。本文总结了近些年有关铝基、镁基和钢基等复合泡沫研究的进展情况,并分类概述了不同基体材料的选择和制备工艺对金属基复合泡沫组织结构和力学性能的影响。结果表明,基体材料是金属基复合泡沫的重要组成部分,并直接影响其结构和性能。铝及其合金具有密度小、强度高、可塑性好等特点,是金属基复合泡沫中应用最广泛的基体材料之一。镁及其合金也有低密度、高强度、延展性好等特点,也是一种重要的金属基体材料。钢基复合泡沫的抗压强度和吸能能力优于大多数铝、镁基复合泡沫,并且在受力过程中表现出较好的变形状态,但是其密度普遍高于铝、镁基复合泡沫材料。以高熵合金作为复合泡沫材料基体是一个新的研究方向,该种材料表现出优异的性能。由于高熵合金内部结构复杂,需对制备出的复合泡沫微观结构及力学性能做进一步研究。除了金属基体材料,填充材料、制备工艺、孔隙率、界面反应、后处理技术等都对金属基复合泡沫的结构和性能有着很大的影响。 展开更多
关键词 金属基复合泡沫 金属基体 制备工艺 力学性能 吸能能力
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颗粒增强铝基复合材料电弧增材技术研究
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作者 匡锐 薛帅 +6 位作者 闫亮亮 范玉虎 张伟强 夏岽尊 来钰人 赵拴勃 张春耕 《热加工工艺》 北大核心 2025年第12期161-166,共6页
颗粒增强铝基复合材料因其优异的高比强度和高比刚度,被广泛应用于交通、航空航天、船舶等领域。对于结构复杂的筒体、箱体等薄壁结构件,其成型难度大,机械加工余量大,生产周期长。而采用WAAM技术可以快速打印成形此类结构件。开展颗粒... 颗粒增强铝基复合材料因其优异的高比强度和高比刚度,被广泛应用于交通、航空航天、船舶等领域。对于结构复杂的筒体、箱体等薄壁结构件,其成型难度大,机械加工余量大,生产周期长。而采用WAAM技术可以快速打印成形此类结构件。开展颗粒增强铝基复合材料制备、焊丝制备、电弧增材制造(WAAM)试验等,分析了T6热处理后颗粒增强铝基复合材料WAAM试样的力学性能。结果表明:采用金属型模具浇注颗粒增强铝基复合材料,提高了冷却速率,从而细化晶粒,使成分偏析程度减小,保证了组织的均匀性。通过控制单道次粗拉伸和精拉伸的变形比,辅以中间退火处理(410℃±10℃,保温1.5 h),可制备出满足WAAM要求的焊丝。采用制备的焊丝在合适的工艺参数下获得了成形良好、无孔隙的墙体增材制造样品。WAAM样品经T6热处理后,抗拉强度为370~390 MPa、屈服强度为320~335MPa、伸长率为2.5%~4.5%,满足使用要求。 展开更多
关键词 颗粒增强铝基复合材料 电弧增材制造 金属型模具 拉拔
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颗粒/短纤维增强铝镁合金金属基复合材料温度相关性屈服强度理论预测模型
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作者 贺屹 董攀 《有色金属(中英文)》 北大核心 2025年第5期756-761,共6页
颗粒/短纤维增强金属基复合材料在航空航天等领域应用时常遭受不同的温度环境,鉴于其屈服强度直接关系到部件的安全性,合理表征和预测其温度相关性屈服强度成为研究的重点。针对颗粒/短纤维增强铝镁合金金属基复合材料,结合修正的剪切... 颗粒/短纤维增强金属基复合材料在航空航天等领域应用时常遭受不同的温度环境,鉴于其屈服强度直接关系到部件的安全性,合理表征和预测其温度相关性屈服强度成为研究的重点。针对颗粒/短纤维增强铝镁合金金属基复合材料,结合修正的剪切滞后模型并考虑了纤维、基体材料的杨氏模量及其随温度的演化,建立了一个温度相关性屈服强度理论预测模型σ_(cy)(T)={A[1+8V_(f)^(2)s^(2)(E_(f)(T)-E_(m)(T)/3(E_(f)(T)+4V_(f)s^(2)E_(m)(T)]·(E_(m)(T)+v_(m)(T_(0))T_(m)-T/E_(m)(T_(0))1+v_(m)(T)T_(m)-T_(0))^(0.5)·σ_(my)(T_(0))for RT≤T≤473K A[1+8V_(f)^(2)s^(2)(E_(f)(T)-E_(m)(T)/3(E_(f)(T)+4V_(f)s^(2)E_(m)(T)]·(E_(m)(T)+v_(m)(T_(0))T_(m)-T/E_(m)(T_(0))1+v_(m)(T)T_(m)-T_(0))^(1)·σ_(my)(T_(0))for 473K<T。模型的预测结果与所有可获取的不同温度下的实验数据均取得了很好的一致性,为方便地预测颗粒/短纤维增强铝镁合金金属基复合材料温度相关性屈服强度提供了一种新方法。 展开更多
关键词 金属基复合材料 温度相关性屈服强度 理论预测模型 颗粒增强 短纤维增强
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Fabrication of AA7005/TiB2-B4C surface composite by friction stir processing: Evaluation of ballistic behaviour 被引量:3
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作者 Nitinkumar Pol Gaurav Verma +1 位作者 R.P.Pandey T.Shanmugasundaram 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2019年第3期363-368,共6页
The present work aims to enhance the ballistic resistance of AA7005 alloy by incorporating the TiB2 and B4C ceramic reinforcement particles. Surface composites with different weight fractions of TiB2 and B4C particles... The present work aims to enhance the ballistic resistance of AA7005 alloy by incorporating the TiB2 and B4C ceramic reinforcement particles. Surface composites with different weight fractions of TiB2 and B4C particles were processed by friction stir processing. Micro-hardness and depth of penetration tests were carried out to evaluate the ballistic properties of the surface composites. The surface hardness of the composite was found to be nearly 70 HV higher than base alloy. The depth of penetration of the steel projectile was 20e26mm in the composites as compared to 37mm in the base alloy. Ballistic mass efficiency factor of the surface composite was found to be 1.6 times higher than base alloy. This is mainly attributed to the dispersion strengthening from the reinforcement particles. 展开更多
关键词 Aluminum ALLOYS metal matrix composite BALLISTIC testing FRICTION STIR processing
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Effect of tool plunge depth on reinforcement particles distribution in surface composite fabrication via friction stir processing 被引量:1
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作者 Sandeep Rathee Sachin Maheshwari +1 位作者 Arshad Noor Siddiquee Manu Srivastava 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2017年第2期86-91,共6页
Aluminium matrix surface composites are gaining alluring role especially in aerospace, defence, and marine industries. Friction stir processing(FSP) is a promising novel solid state technique for surface composites fa... Aluminium matrix surface composites are gaining alluring role especially in aerospace, defence, and marine industries. Friction stir processing(FSP) is a promising novel solid state technique for surface composites fabrication. In this study, AA6061/SiC surface composites were fabricated and the effect of tool plunge depth on pattern of reinforcement particles dispersion in metal matrix was investigated. Six varying tool plunge depths were chosen at constant levels of shoulder diameter and tool tilt angle to observe the exclusive effect of plunge variation. Process parameters chosen for the experimentation are speed of rotation, travel speed and tool tilt angle which were taken as 1400 rpm, 40 mm/min, and 2.5 °respectively. Macro and the microstructural study were performed using stereo zoom and optical microscope respectively. Results reflected that lower plunge depth levels lead to insufficient heat generation and cavity formation towards the stir zone center. On the other hand, higher levels of plunge depth result in ejection of reinforcement particles and even sticking of material to tool shoulder. Thus, an optimal plunge depth is needed in developing defect free surface composites. 展开更多
关键词 metal matrix composites FRICTION STIR processing TOOL plunge DEPTH MICROSTRUCTURAL characterization
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Joining of hybrid AA6063-6SiCp-3Grp composite and AISI1030 steel by friction welding
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作者 N.Rajesh Jesudoss Hynes M.Vivek Prabhu P.Nagaraj Senior 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2017年第5期338-345,共8页
Joining of metals and aluminium hybrid metal matrix composites has significant applications in aviation,ship building and automotive industries. In the present work, investigation is carried out on Friction Welding of... Joining of metals and aluminium hybrid metal matrix composites has significant applications in aviation,ship building and automotive industries. In the present work, investigation is carried out on Friction Welding of AISI 1030 steel and hybrid AA6063-6 SiC_p-3 Gr_pcomposite, that are difficult to weld by fusion welding technique. Silicon carbide and graphite particle reinforced AA6063 matrix hybrid composite was developed successfully using stir casting method and the joining feasibility of AISI1030 steel with AA6063-6 SiC_p-3 Gr_p hybrid composite was tried out by friction stud welding technique. During friction stage of welding process, the particulates(SiC & Graphite) used for reinforcement, tend to increase the viscosity and lead to improper mixing of matrix and reinforcement. This eventually results in lower strength in dissimilar joints. To overcome this difficulty AA1100 interlayer is used while joining hybrid composite to AISI 1030 steel. Experimentation was carried out using Taguchi based design of experiments(DOE) technique. Multiple regression methods were applied to understand the relationship between process parameters of the friction stud welding process. Micro structural examination reveals three separate zones namely fully plasticized zone, partially deformed zone and unaffected base material zone. Ultra fine dynamically recrystallized grains of about 341 nm were observed at the fully plasticized zone. EDX analysis confirms the presence of intermetallic compound Fe_2 Al_5 at the joint interface. According to the experimental analysis using DOE, rotational speed and interlayer sheet thickness contribute about 39% and 36% respectively in determining the impact strength of the welded joints. It is found that joining with 0.5 mm interlayer sheet provides efficient joints. Developed regression model could be used to predict the axial shortening distance and impact strength of the welded joint with reasonable accuracy. 展开更多
关键词 metal matrix compositE WELDING Mechanical properties SCANNING ELECTRON MICROSCOPY
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Age hardening process modeling and optimization of aluminum alloy A356/Cow horn particulate composite for brake drum application using RSM,ANN and simulated annealing
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作者 Chidozie Chukwuemeka Nwobi-Okoye Basil Quent Ochieze 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2018年第4期336-345,共10页
Most conventional ceramic based aluminum metal matrix composites(MMCs) are either heavy,costly or combination of both. In order to reduce cost and weight,while at the same time maintaining quality,cow horn particles(C... Most conventional ceramic based aluminum metal matrix composites(MMCs) are either heavy,costly or combination of both. In order to reduce cost and weight,while at the same time maintaining quality,cow horn particles(CHp) was used with aluminum alloy A356 to produce MMC for brake drum application and other engineering uses. The aim of this research is to model the age hardening process of the produced composite using response surface methodology(RSM) and artificial neural network(ANN),and to use the developed ANN as fitness function for a simulated annealing optimization algorithm(SA-NN system) for optimization of age hardening process parameters. The results show that ANN modeled the age hardening data excellently and better than RSM with a correlation coefficient of experimental response with ANN predictions being 0.9921 as against 0.9583 for the RSM. The SA-NN system optimized process parameters were in very close agreement with the experimental values with the maximum relative error of 1.2%,minimum of 0.35% and average of 0.71%. 展开更多
关键词 Artificial neural network Response surface methodology Simulated ANNEALING Age HARDENING metal matrix composite
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