玻璃包覆Fe79-xCox Si8 B13非晶合金微丝的磁性能

实验以熔融纺丝法制备的玻璃包覆Fe79-xCoxSi8B13非晶合金微丝为对象,分析了微丝成分、尺寸以及玻璃包覆层去除对微丝静磁性能的影响。研究结果表明,玻璃包覆Fe79-xCoxSi8B13非晶合金微丝存在明显的磁各向异性,微丝轴向为易磁化方向;随着Co含量的增加,微丝的饱和磁化强度先增大后减小,Co含量为10%的Fe69Co10Si8B13非晶合金微丝饱和磁化强度最高,为1323emu·cm-3;对于玻璃包覆Fe69Co10Si8B13非晶合金微丝,当芯丝半径与玻璃包覆层厚度比值k约小于0.5时,其轴向磁滞回线为近矩形,表现出大巴克豪森效应;微丝的轴向剩磁比随k值的增大而减小,而微丝径向剩磁比保持很小,仅0.03左右;微丝的轴向和径向矫顽力均随比值k的增大而减小;当芯丝半径为10.9μm、玻璃包覆层厚度为9.7μm(k为1.12)时,去除包覆层后微丝的轴向矫顽力降低30%、径向矫顽力降低11%;而轴向剩磁比降低33%、径向剩磁比降低67%。     

不同直径玻璃包覆非晶微丝的制备及其磁性能

采用熔融拉丝法制备了直径范围分别在6.1～28.0μm和14.0～35.2μm之间的玻璃包覆非晶Fe基和Co基合金微丝, 测试了不同合金直径和不同玻璃包覆层厚度的玻璃包覆合金微丝样品的静磁性能. 结果表明: 轴向矫顽力和轴向剩磁比随着微丝直径的增大而降低, 随着玻璃包覆层的增大而升高; 径向剩磁比的变化趋势则相反. 微丝合金直径和玻璃包覆层厚度改变, 静磁性能变化的主要原因是作用在合金芯上的内应力的变化, 导致了具有不同磁畴结构的合金内芯区和合金外壳区体积比的改变.     

共沉淀法制备的锶铁氧体磁粉的结构、形貌及磁性能(英文)

采用共沉淀法按照n(Fe)∶n(Sr)=10∶1合成M型锶铁氧体.通过把样品在不同的温度下退火,研究了退火温度对晶体结构、形貌和磁性能的影响.所制备的样品用FTIR、XRD、SEM和VSM进行表征.结果表明,当退火温度为1000℃时样品颗粒分布规则且比饱和磁化强度达最大值,为77.87emu/g.当退火温度为1100℃时样品颗粒变成球形且矫顽力最小,为1601Oe.此外,通过控制退火温度可使矫顽力在1601～4591Oe范围内变化.     

直径对玻璃包覆非晶合金微丝磁性的影响

采用Taylor-Ulitovsky方法制备了直径分别在6.3～28.0μm、20.2～28.0μm和14.0～35.2μm之间的玻璃包覆非晶态FeCuNbVSiB、FeBSiCMn和CoNiFeSiB微丝。通过X射线衍射、扫描电镜、振动样品磁强计分别测试了玻璃包覆微丝的组织结构、微观形貌和磁性,研究了不同成分玻璃包覆磁性合金微丝的玻璃包覆层厚度、合金芯直径对微丝磁性能的影响。结果表明了,玻璃包覆磁性合金微丝的磁性能的影响因素由大到小依次为：饱和磁致伸缩系数、微丝成分和微丝尺寸。轴向磁化时随着微丝直径及玻璃包覆层厚度的增大,3 种微丝的径向饱和场强度降低,FeCuNbVSiB和FeBSiCMn微丝的轴向矫顽力先分别由508 A/m和390 A/m降低到486 A/m和278 A/m后再升高到2570 A/m和342 A/m,CoNiFeSiB微丝的轴向矫顽力由171 A/m降低到63 A/m。     

熔体快淬速度对Nd_8 Fe_(73) Ti_2 Zr_2 B_(13.6) C_(1.4)双相纳米晶永磁合金磁性能的影响

对名义成分为Nd_8Fe_(73)Ti_2Zr_2B_(13.6)C_(1.4)的合金,采用不同的甩带速度(6,8,10,12,15,18,20,30 m/s)及后续的热处理工艺制备出Nd_2Fe_(14)B/α-Fe纳米晶复合永磁带。结果表明:当冷却铜辊表面线速度V_s12 m/s时,淬态带由非晶相组成。随V_s的减小,淬态样品的析晶峰之间的温度差距增大。退火态薄带的矫顽力随甩带速度降低而提高,6 m/s淬态样品经680℃真空热处理10min后得到最大矫顽力H_(ci)=1114 kA/m。随着甩带速度的提高,退火态带的剩磁比(J_r/J_s)和磁能积(BH)_m皆表现为先增加后降低。最大剩磁比和最佳磁能积都出现在12 m/s淬态样品经780℃退火10 min状态下:J_r/J_s=0.749;(BH)_m=84.6 kJ/m~3;H_(ci)=732 kA/m,此样品淬态时为部分非晶。     

磁场退火对纳米晶Fe_(74.5)Cu_1Nb_2Si_(17.5)B_5合金饱和磁致伸缩系数和μi-T曲线的影响研究

研究了不同退火温度下形成的纳米晶Fe_(74.5)Cu_1Nb_2Si_(17.5)B_5合金经过磁场退火后,其饱和磁致伸缩系数λ_S、矫顽力H_C和μi-T曲线的变化。研究表明,经过磁场退火后,纳米晶合金的矫顽力出现不同程度的降低,温度在350℃以下时,初始磁导率表现出明显的提高,这些性能的改善归因于合金饱和磁致伸缩的减小。     

退火温度对Ti-50.8Ni-0.1Zr形状记忆合金丝记忆行为和力学性能的影响

用拉伸试验、差示扫描量热仪、光学显微镜和扫描电子显微镜研究了退火温度对Ti-50.8Ni-0.1Zr合金丝形状记忆效应、超弹性、力学性能和断口形貌的影响.结果表明:350～400℃和600～700℃退火态Ti-50.8Ni-0.1Zr合金丝呈超弹性(SE),600℃退火态合金丝的平台应力最大(483 MPa)、残余应变最小(0.1％),350～400℃退火态合金丝SE稳定性最好;450～550℃退火态合金丝呈现形状记忆效应(SME),500℃退火态合金丝的平台应力最小(190 MPa),450℃退火态合金丝的残余应变最大(4.9％)、SME稳定性最好.600～700℃退火态合金丝的塑性高于350～550℃退火态,但强度低于后者;400℃退火态合金丝的抗拉强度最大(1489 MPa),650℃退火态合金丝的伸长率最大(35.1％).退火态Ti-50.8Ni-0.1Zr合金丝的断口形貌呈韧窝状,属微孔聚集型韧性断裂,韧窝处存在第二相颗粒和孔洞,退火温度对断口形貌的影响不大.     

纳米晶MnFe2O4的水热法合成及其磁性能

采用水热法制备了软磁材料MnFezO4纳米晶,借助XRD、IR、SEM和VSM对产物进行了表征,着重研究了水热条件如温度和时间等对MnFe2O4纳米晶的形成及其结构和磁性能的影响。结果表明水热温度较低时的产物晶化度和纯度低,表现出较差的磁性能,温度为120℃的产物其饱和磁化强度为15．34emu／g,剩磁比为0．08,矫顽力为8lOe,而在200℃下水热产物饱和磁化强度为51．49emu／g,剩磁比达到0．14,矫顽力为121Oe。     

机械零部件用高强镁合金加工工艺与组织性能研究

针对Mg-Gd-Y合金塑性较差的问题,研究了固溶态和不同温度锻造加工态高强Mg-Gd-Y合金的组织与性能。结果表明,固溶态Mg-Gd合金的晶粒尺寸不均匀,平均尺寸约225μm;当锻造加工温度为440℃和410℃时,合金中第二相的数量较多,大量弥散分布的第二相的存在可以抑制动态再结晶的形成;随着锻造加工温度的降低,Mg-Gd合金的抗拉强度和屈服强度呈现逐渐升高的趋势,在锻造加工温度为470℃时,Mg-Gd合金的断后伸长率达到最大值19.2%,降低锻造加工温度至440℃和410℃时,断后伸长率反而有所降低;固溶态Mg-Gd合金的拉伸断口呈现脆性断裂的特征;锻造加工温度为500℃的拉伸断口呈现混合断裂特征,而锻造加工温度为410℃、440℃和470℃时Mg-Gd合金的断口都呈现为韧性断裂特征。     

(Nd1-xPrx)10.5(FeCoZr)83.5B6合金显微结构和磁性能研究

采用部分过快淬加后续晶化退火工艺,制备出了最佳磁性能的(Nd1-xPrx)10.5(FeCoZr)83.5 B6(x=O、0.2、0.4、0.6、0.8、1.0)系列粘结磁体,研究了稀土Pr元素对快淬合金DTA曲线转折温度点、合金显微组织结构和粘结磁体磁性能的影响.Pr元素使合金非晶态的晶化转变温度和转化能降低,合金的显微组织结构变得较粗大和较不均匀,从而使快淬粘结磁体剩磁降低.随Pr含量的增加,磁体的内禀矫顽力Hci单调上升,剩磁Br单调下降,在x=0.6～0.8处(BH)m达到最大值70.6kJ·m3.     

添加Sc、Zr和退火对Al-Si合金铸态力学性能的影响

使用OM、TEM、SEM、显微硬度和室温拉伸等手段研究了Sc和Zr的复合添加对Al-5.5Si合金铸态的组织和性能的影响,以及在不同温度退火后其性能的变化规律。结果表明,Sc、Zr的添加使Al-5.5Si合金的硬度提高了33%、抗拉强度提高了38%、屈服强度提高了52%、延伸率基本上不变。在Al-5.5Si合金中复合添加Sc、Zr使α-Al的平均晶粒尺寸从203 μm减小到130 μm,在α-Al基体中析出大量的Al₃(Sc_1-xZr_x)纳米粒子(10~15 nm),并使共晶Si内的层错或微孪晶的密度显著提高。退火温度对铸态合金的性能有较大的影响：在较低温度(低于160℃)退火时合金的硬度呈上升趋势,而在较高温度(高于280℃)退火时合金的硬度呈显著下降趋势。这些结果与二次析出的纳米Si相密切相关。     

135°ECAP+旋锻变形工业纯钛的热稳定性研究

对经过135°ECAP+旋锻变形后的工业纯钛100,150,200,250,300,350,400,450℃和500℃下保温1h退火。采用透射电子显微镜(TEM)、扫描电子显微镜(SEM)、拉伸试验机及显微硬度仪等技术研究ECAP+旋锻变形工业纯钛退火后的组织与性能变化。结果表明:在400℃以下退火时,显微组织中位错密度降低,晶界逐渐清晰,变形组织未发生明显变化,材料的抗拉强度和显微硬度略有降低,伸长率增加不明显;在400℃以上退火时,随着退火温度的升高,发生再结晶,晶粒尺寸明显增大,平均晶粒尺寸约为5μm,材料的抗拉强度和显微硬度均出现明显降低,伸长率增加。拉伸断口表明,ECAP+旋锻变形退火后工业纯钛的拉伸断裂均为韧性断裂。随着退火温度的升高,韧窝尺寸变大,韧窝深度变深。     

Microstructure and mechanical properties of novel Al-Y-Sc alloys with high thermal stability and electrical conductivity

The microstructure and mechanical properties of novel Al-Y-Sc alloys with high thermal stability and electrical conductivity were investigated.Eutectic Al3 Y-phase particles of size 100-200 nm were detected in the as-cast microstructure of the alloys.Al3 Y-phase particles provided a higher hardness to as cast alloys than homogenized alloys in the temperature range of 370-440℃.L12 precipitates of the Al3(ScxYy) phase were nucleated homogenously within the aluminium matrix and heterogeneously on the dislocations during annealing at 400℃.The average size of the L12 precipitates was 11±2 nm after annealing for 1 h,and 25-30 nm after annealing for 5 h,which led to a decrease in the hardness of the Al-0.2 Y-0.2 Sc alloy to15 HV.The recrystallization temperature exceeded 350℃and 450℃for the Al-0.2 Y-0.05 Sc and Al-0.2 Y-0.2 Sc alloys,respectively.The investigated alloys demonstrated good thermal stability of the hardness and tensile properties after annealing the rolled alloys at 200 and 300℃,due to fixing of the dislocations and grain boundaries by L12 precipitates and eutectic Al3 Y-phase particles.The good combination of strength,plasticity,and electrical conductivity of the investigated Al-0.2 Y-0.2 Sc alloys make it a promising candidate for electrical conductors.The alloys exhibited a yield stress of 177-183 MPa,ultimate tensile stress of 199-202 MPa,elongation of 15.2-15.8%,and electrical conductivity of 60.8%-61.5% IACS.     

Al-7Sn-1.1Ni-Cu-0.2Ti轴承合金微观组织与力学性能

采用扫描电镜、能谱分析、金相显微镜与WDW-100KN万能拉伸试验机研究Al-7Sn-1.1Ni-Cu-0.2Ti轴承合金的微观组织与力学性能,结合盘-销式摩擦磨损试验机考察合金不同组织状态的润滑性能。结果表明:Al-7Sn-1.1Ni-Cu-0.2Ti合金凝固收缩率为1.13%,铸态抗拉强度、屈服强度、伸长率与布氏硬度分别为191,147MPa,15.6%与34.6HBS,随着低温时效与退火热处理过程的进行,抗拉强度略有上升,屈服强度保持不变,伸长率与布氏硬度均呈现出先上升后下降的变化趋势;沿晶界分布的共晶Sn相形貌受界面张力作用逐步由板片状与骨骼状转变为层片状与短棒状,部分吸热脱溶析出在晶界处形成空腔结构,初生α-Al基体平均晶粒尺寸为182μm。与铸态和340℃退火6h相比,经175℃时效10h后,摩擦因数降低了28.6%与78.6%,体积磨损量减少了157.1%与471.4%,断口形貌以沿晶断裂与韧窝断裂为主。     

超支化聚酯基二茂铁/环氧树脂复合材料的制备及性能

以第3代环氧端基脂肪族超支化聚酯（EHBP）增韧的环氧树脂（E-51）为基体材料,超支化聚酯基二茂铁（HBPE-Fc）为吸波剂,制备具有一定力学承载及电磁性能的超支化聚酯基二茂铁/环氧树脂（HBPE-Fc/E-51）复合材料,并通过力学性能测试及扫描电镜、矢量网络分析仪等研究了该复合材料的力学及电磁性能。结果表明,添加较低含量的HBPE-Fc能较好地改善环氧树脂体系的拉伸及冲击性能,第4代HBPE-Fc质量分数为2%时,与纯环氧树脂体系相比,HBPE-Fc/E-51复合材料的拉伸强度、断裂伸长率和冲击强度分别提高了21.81%、34.32%和15.41%,对固化体系的拉伸断面分析发现引入HBPE-Fc后材料表现出韧性断裂。HBPE-Fc/E-51复合材料的玻璃化转变温度在105.29~130.27 ℃之间,具有良好的热稳定性,同时该复合材料具有一定的电磁特性。     

微量Cu和形变热处理对Al-Fe合金性能的影响

观察Al-Fe合金的显微组织并测量其力学性能和导电性能,研究了Cu元素和形变热处理对其性能的影响。结果表明：在铸态Al-Fe-Cu合金组织中,Cu元素在基体内均匀分布,而Fe元素在晶界处偏析;挤压态的Al-0.7Fe-0.2Cu合金其性能最优：导电率为59.90%IACS,抗拉强度为108 MPa,硬度为31.2HV;随着退火温度的提高Al-0.7Fe-0.2Cu合金的抗拉强度急剧降低,在400℃退火时其抗拉强度最低(100 MPa),伸长率最高(31.3%);在250℃退火时导电率出现峰值(62.61%IACS)。在退火Al-0.7Cu-0.2Cu合金中有许多细小针状的θ(Al₂Cu)相析出,并与位错交互缠结。随着退火温度的提高合金中的位错密度降低,晶粒细化。     

均匀化处理对Mg-13Gd-3.5Y-2Zn-0.5Zr镁合金组织和力学性能的影响

对Mg-13Gd-3.5Y-2Zn-0.5Zr镁合金铸锭进行均匀化处理,温度为505～525℃,时间为4～24h,并采用光学显微镜(OM)、扫描电子显微镜(SEM)、X射线衍射仪(XRD)和万能材料试验机等检测手段分析均匀化处理前后合金微观组织和力学性能的变化。结果表明:均匀化处理后,原始组织中网状分布共晶化合物转化成晶界处不连续分布的块状LPSO相,离散分布的方块状富稀土相溶解。力学性能测试显示,铸态镁合金的抗拉强度为172.9MPa,伸长率为1.8%,经过均匀化处理后合金的力学性能得到提高,在515℃/16h均匀化制度下,合金室温抗拉强度为212.3MPa,伸长率为3.1%;在200℃下抗拉强度为237.2MPa,伸长率为9.7%,性能达到最佳。断口扫描显示,铸态合金是以撕裂棱与解理台阶为主的解理脆性断裂,均匀化处理后的合金中出现小而浅的韧窝,但仍然是以解理台阶为主的准解理断裂,塑性提高有限,长程有序相可成为裂纹的萌生源。     

Microstructure and compressive/tensile characteristic of large size Zr-based bulk metallic glass prepared by laser solid forming

The large size, crack-free Zr_(55)Cu_(30)Al_(10)Ni_(5) bulk metallic glass(BMGs) with the diameter of 54 mm and the height of 15 mm was built by laser solid forming additive manufacturing technology, whose size is larger than the critical diameter by casting. The microstructure, tensile and compressive deformation behaviors and fracture morphology of laser solid formed Zr_(55)Cu_(30)Al_(10)Ni_5 BMGs were investigated. It is found that the crystallization mainly occurs in the heat-affected zones of deposition layers, which consist of Al_5Ni_3Zr_2, NiZr_2, ZrCu, CuZr_2 phases. The content of amorphous phase in the deposit is about 63%.Under the compressive loading, the deposit presents no plasticity before fracture occurs. The fracture process is mainly controlled by the shear stress and the compressive shear fracture angles of about39?. The compressive strength reaches 1452 MPa, which is equivalent to that of as-Cast Zr_(55)Cu_(30)Al_(10)Ni_5 BMGs, and there exist vein-like patterns, river-like patterns and smooth regions at the compressive fractography. Under the tensile loading, the deposit presents the brittle fracture pattern without plastic deformation. The fracture process exhibits normal fracture model, and the tensile shear fracture angle of about 90?. The tensile strength is only about 609 MPa, and the tensile fractography mainly consists of micro-scaled cores and vein-like patterns, dimple-like patterns, chocolate-like patterns and smooth regions. The results further verified the feasibility and large potential of laser additive manufacturing on fabrication and industrial application of large-scale BMGs parts.     

Microstructure evolution and mechanical properties at high temperature of selective laser melted AlSi10Mg

In this study,the microstructure and tensile properties of selective laser melted AlSilOMg at elevated temperature were investigated with focus on the interfacial region.In-situ SEM and in-situ EBSD analysis were proposed to characterize the microstructural evolution with temperature.The as-fabricated AlSilOMg sample presents high tensile strength with the ultimate tensile strength(UTS)of~450 MPa and yield strength(YS)of~300 MPa,which results from the mixed strengthening mechanism among grain boundary,solid solution,dislocation and Orowan looping mechanism.When holding at the temperature below 200℃for 30 min,the micro structure presents little change,and only a slight decrement of yield strength appears due to the relief of the residual stress.However,when the holding temperature further increases to 300℃and 400℃,the coarsening and precipitation of Si particles inα-Al matrix occur obviously,which leads to an obvious decrease of solid solution strength.At the same time,matrix softening and the weakness of dislocation strengthening also play important roles.When the holding temperature reaches to 400℃,the yield strength decreases significantly to about 25 MPa which is very similar to the as-cast Al alloy.This might be concluded that the YS is dominated by the matrix materials.Because the softening mechanism counteracts work hardening,the extremely high elongation occurs.