Al9Fe0.7Ni1.3相对喷射沉积Al-Zn-Mg-Cu-Ni合金组织和性能的影响

本文利用喷射沉积技术合成含Ni的Al-Zn-Mg-Cu合金,合金中的Ni元素以亚微米球状Al₉Fe_0.7Ni_1.3化合物的形式存在。利用扫描电镜和电子背散射衍射、透射电镜以及拉伸测试研究了Al₉Fe_0.7Ni_1.3颗粒对合金固溶处理后组织和性能的影响。结果发现：Al₉Fe_0.7Ni_1.3颗粒主要在晶界附近分布,说明该颗粒在固溶过程中具有有力的抑制再结晶作用。固溶处理后,合金的拉伸强度为603 MPa,断裂延伸率为11.79%,主要断裂方式为穿晶延性断裂。实验结果表明亚微米球状Al₉Fe_0.7Ni_1.3化合物对合金性能有重要影响,可以产生细晶强化和Orowan强化,是合金发生穿晶延性断裂的主要原因。     

保温时间对瞬时液相扩散连接的Ti3Al /Ti2AlNb接头微观结构及力学性能的影响

采用Ni-Ti复合箔片作为中间层,在990 ℃、低连接压力（0.1 MPa）下,通过瞬时液相（TLP）扩散连接制备了Ti₃Al/Ti₂AlNb异种合金接头。分析了保温时间（10~90 min）对Ti₃Al/Ti₂AlNb接头微观结构及力学性能的影响,并研究了TLP扩散连接接头的界面演变和形成机制。结果表明,Ti₃Al/Ti₂AlNb接头具有典型的“Ti₃Al | Al_0.5Nb_0.5Ti₃ | 残余 Ni | NiTi | NiTi₂ | 残余 Ti | Al_0.5Nb_0.5Ti₃ | Ti₂AlNb”多层梯度结构。随着保温时间的延长,接头的抗剪切强度先增大后减小,当保温时间达到60 min时,Ti₃Al/Ti₂AlNb接头的抗剪切强度最大,达到167±12 MPa。另外,接头的断裂主要发生在Ti₂AlNb/Ti附近的NiTi₂层,并向Ti层延伸,呈现出脆性断裂的特征。     

具有高非晶形成能力的高熵合金Cu29Zr32Ti15Al5Ni19

用铜模吸铸法成功地合成了由两个固溶体相构成的高熵合金(HEA) Cu₂₉Zr₃₂Ti₁₅Al₅Ni₁₉和相同成分的非晶态合金(HE-BMG)。实验结果表明该成分的高熵合金具有高的非晶形成能力。铸态高熵合金Cu₂₉Zr₃₂Ti₁₅Al₅Ni₁₉的抗压强度为1127MPa。在750℃保温2小时后的Cu₂₉Zr₃₂Ti₁₅Al₅Ni₁₉高熵合金的硬度仍高达826HV。     

功率对激光熔覆(Fe0.25Co0.25Ni0.25Cr0.125Mo0.125)86B14涂层组织均质性及磨损性能的影响*

目前激光熔覆缺少对涂层组织、相结构纵向均质性与性能关联的研究。采用激光熔覆技术,选取不同的激光功率,制备(Fe_0.25Co_0.25Ni_0.25Cr_0.125Mo_0.125)₈₆B₁₄ 高熵合金涂层;借助电子探针(EPMA)、扫描电子显微镜(SEM)、能谱仪(EDS)和 X 射线衍射仪(XRD)等观察涂层微观组织与物相纵向分布,利用显微硬度计和摩擦磨损试验机测试涂层不同深度部位显微硬度及磨损性能,分析激光功率对熔覆(Fe_0.25Co_0.25Ni_0.25Cr_0.125Mo_0.125)₈₆B₁₄ 涂层纵向组织、物相分布影响规律及磨损性能。结果表明：三种功率下,涂层均由 BCC+FCC 相、硬质相 Mo₂B 组成,Mo₂B 在枝晶间富集。随着功率的增加,涂层中底部显微组织由细枝晶向粗大的柱状晶转变。三种涂层硬度均由表及里先增加后降低,摩擦因数先降低后增加;但是当激光功率为 1.6 kW 时,涂层呈现以 BCC 相为主的 FCC+BCC 双相结构,且由表及里 BCC 相含量不断增加、Mo₂B 含量逐渐减少,涂层组织均质化最高,摩擦因数变化梯度最小,耐磨损性能最佳。激光功率会影响熔覆高熵合金耐磨涂层均质性,进而影响摩擦性能的稳定性。     

Cu-Fe64Ni32Co4合金显微组织及热物理性能研究

本研究利用相图计算的CALPHAD方法和真空电弧熔炼技术,设计并制备了Cu_x(Fe_0.64Ni_0.32Co_0.04)_100-x(x=30, 45, 60, wt. %)系列合金。实验研究了该系列合金在不同热处理工艺时的显微组织,热导率以及热膨胀系数。研究结果表明：Cu-Fe₆₄Ni₃₂Co₄系列合金在600 °C和800 °C时效处理后均为fcc富铜相和fcc富因瓦(铁镍钴)相组成的各向同性的多晶合金。该系列合金在1000 °C淬火并在600 °C时效处理50 h后,其热膨胀系数变化范围为6.88~12.36×10_-6 K_-1;热导率变化范围为22.91~56.13 W.m_-1.K_-1;其热导率明显高于因瓦合金,其中Cu₃₀(Fe_0.64Ni_0.32Co_0.04)₇₀与 Cu₄₅(Fe_0.64Ni_0.32Co_0.04)₅₅合金的热膨胀系数可以与电子封装中半导体材料的热膨胀系数相匹配。     

激光热喷涂Co30Cr8W1.6C3Ni1.4Si涂层在PAO+2.5%MoDTC油中摩擦学特性

为了提高TC4合金的耐磨性能,采用激光热喷涂技术在其表面制备了Co₃₀Cr₈W_1.6C₃Ni_1.4Si涂层。通过扫描电子显微镜（SEM）和X射线衍射（XRD）分析了涂层的形貌和物相,并通过摩擦磨损实验研究了涂层在PAO+2.5% MoDTC（质量分数）油中的磨损行为。结果表明,激光热喷涂的Co₃₀Cr₈W_1.6C₃Ni_1.4Si涂层主要由Ti、WC_1-x、CoO、Co₂Ti₄O和CoAl相组成,在涂层界面形成冶金结合。在激光功率为1000、1200和1400 W时所制备的涂层平均摩擦因数分别为0.151、0.120和0.171,其对应的磨损率分别为1.17×10^-6、1.33×10^-6和2.80×10^-6 mm³?N^-1?m^-1,磨损机理为磨粒磨损,其枝晶尺寸对降磨起主要作用。     

Ti3AlC2掺杂SPS法制备Ti2AlC/TiAl复合材料的研究

通过2TiC-Ti-1.2Al体系的原位热压反应制备了Ti₃AlC₂陶瓷,然后以59.2Ti-30.8Al-10Ti₃AlC₂(wt%)为反应体系,采用放电等离子烧结技术制备出Ti₂AlC/TiAl基复合材料。借助XRD、SEM分析了产物的相组成和微观结构,并测量了其室温力学性能。结果表明：原位热压烧结产物由Ti₃AlC₂和TiC相组成,Ti₃AlC₂呈典型的层状结构,TiC颗粒分布在其间。SPS法制备的Ti₂AlC/TiAl基复合材料主要由TiAl、Ti₃Al和Ti₂AlC相组成,Ti₂AlC增强相主要分布于基体晶界处,表现为晶界/晶内强化作用。力学性能测试表明：Ti₂AlC/TiAl基复合材料的密度、维氏硬度、断裂韧性和抗弯强度分别为3.85 g/cm₃、5.37 GPa、7.17 MPa?m_1/2和494.85 MPa。     

空气气氛下碳热还原筛分法制备Magnéli相Ti n O2 n -1

介绍了一种在空气气氛中通过碳热还原筛分法制备Magnéli相（Ti_nO_2n-1，4＜n＜10）低价钛氧化物的方法，研究了还原温度和还原时间对还原产物的物相、电阻率的影响。结果表明，提高还原温度和延长还原时间有利于将TiO₂还原为Magnéli相Ti_nO_2n-1。将Magnéli相Ti_nO_2n-1 (n=4，5) 粉末在1350 ℃下干燥20 min，通过扫描电子显微镜观察，其粒径为0.5~8 μm。在还原温度为1350 ℃时，还原产物的电阻率随还原时间的延长而显著降低。在1350 ℃下还原50 min的产物的电阻率最小，为79.3 Ω?cm，其物相组成几乎全部为Ti₃O₅。     

Ti-Cu-Ni-Nb-Al-Zr-Hf非晶钎料合金真空钎焊Ti50Al50 接头的界面组织与剪切强度

在钎焊温度1140~1220 ℃、钎焊时间30 min的工艺参数下,采用Ti-9.5Cu-8Ni-8Nb-7Al-2.5Zr-1.8Hf（质量分数,%）非晶钎料成功实现了Ti₅₀Al₅₀ (at%)合金的真空钎焊连接,并研究了钎焊温度对钎焊接头的显微组织、剪切强度的影响规律。结果表明,在任何钎焊温度下获得的Ti₅₀Al₅₀钎焊接头均有3个界面反应层且每个反应层都含有α₂-Ti₃Al和Ti₂Cu(Ni) 2个物相。随着钎焊温度的增加,α₂-Ti₃Al和Ti₂Cu(Ni)在钎焊接头中的尺寸与分布发生了明显的变化,尤其是等温凝固层Ⅱ中的Ti₂Cu(Ni)相。1200 ℃下稳定存在的连续α₂-Ti₃Al层Ⅰ对母材和钎料原子的相互扩散具有阻隔壁垒作用,温度一旦超过1200 ℃,α₂-Ti₃Al相变得不稳定使得连续α₂-Ti₃Al层被打破从而失去阻隔壁垒效应。在钎缝中析出且弥散分布的α₂-Ti₃Al对焊缝中物相的形成可以起到抑制形核和细化晶粒的作用。随着钎焊温度升高,Ti₅₀Al₅₀钎焊接头平均抗剪切强度先增加后减小,在钎焊温度1180 ℃、钎焊时间30 min时钎焊接头的抗剪切强度最大,达184 MPa。剪切断口表面呈典型解理断裂特征且α₂-Ti₃Al占绝大多数。     

Al2O3/Ti2AlN复合材料在900℃,1000℃和1100℃空气中的氧化行为

利用综合热分析仪、背散射扫描电镜(BSE)和能谱分析(EDS)对Al₂O₃/Ti₂AlN复合材料在900 ℃,1 000 ℃和1 100 ℃/20 h空气中连续氧化20h后的氧化增重及氧化层截面进行了研究。结果表明：Al₂O₃/Ti₂AlN复合材料在空气中的氧化行为符合抛物线规律,在900 ℃,1 000 ℃和1 100 ℃/20 h氧化增重分别为2.78×10_-2 kg/m₂、10.4 ×10_-2 kg/m₂、21.9 ×10_-2 kg/m₂,抛物线速率常数相应为1.08×10_-8 kg₂/m₄s、1.44×10_-7 kg₂/m₄s、6.56×10_-7 kg₂/m₄s,氧化激活能为274 kJ/mol。氧化层主要由TiO₂和Al₂O₃组成的,连续的Al₂O₃次外层可以提高其抗氧化性能。氧化层结构的改变是由于氧化温度对Ti₄₊、Al₃₊由基体表面向外扩散和O_2-向内扩散的影响,以及TiO₂和Al₂O₃在不同温度下的形核生长速率导致的。对Al₂O₃/Ti₂AlN而言,控制材料与氧化气氛的界面是提高该材料抗氧化性能的关键。     

Powder metallurgical production of TiNiNb and TiNiCu shape memory alloys by combination of pre-alloyed and elemental powders

The common Ti₄₄Ni₄₇Nb₉ and Ti₅₀Ni₄₀Cu₁₀ ternary shape memory alloys were produced by sintering techniques and the microstructure, phase structure and phase transformation behaviour were investigated. A combination of pre-alloyed binary TiNi powder and elemental Nb, Ni and Cu, Ti powders, respectively, were used. In contrast to the use of pre-alloyed ternary powders, which have to be produced in each new composition, a higher flexibility in the alloy composition becomes possible. In case of the Ti₄₄Ni₄₇Nb₉ alloy, liquid phase sintering was done to obtain the eutectic phase structure known from cast material. In case of the Ti₅₀Ni₄₀Cu₁₀ alloy, the pore size and porosity can be improved by choosing a two-step sintering process, as a eutectic melt between Ti and Cu is formed at low temperatures which influences the sintering behaviour. Controlling the impurity contents and the resulting secondary phases is necessary for both alloys in the same way as for binary TiNi alloys.     

Effect of electroplastic rolling on deformability and oxidation of NiTiNb shape memory alloy

Ni₄₇Ti₄₄Nb₉ strips were successfully processed by electroplastic rolling at relatively low temperature compared to the traditional hot rolling. The result shows the deformability of Ni₄₇Ti₄₄Nb₉ is improved by electropulse, with the maximum thickness reduction of 24% in a single pass. X-ray spectrum and TEM analysis indicates the main structure of Ni₄₇Ti₄₄Nb₉ after electroplastic rolling is polycrystalline and Vickers hardness test shows electropulse can reduce the work hardening. In addition, electroplastic rolling can improve the surface quality of Ni₄₇Ti₄₄Nb₉ owing to the short heat treatment time and low heat treatment temperature.     

Temperature memory effect of Ni47Ti44Nb9 wide hysteresis shape memory alloy

The temperature memory effect (TME) phenomenon of Ni₄₇Ti₄₄Nb₉ wide hysteresis shape memory alloy was studied. It was found that TME occurred during the reverse transformation for the thermally-induced martensite (TIM) but not for the stress-induced martensite after incomplete transformation cycling. The reverse transformation temperature interval of TIM can be doubly broadened after 10 incomplete transformation cycles.     

Microstructure and martensitic transformation of TiNiNbB shape memory alloys

In present work, microstructure, martensitic transformation and mechanical properties of Ti₄₄Ni_47−xNb₉B_x (x = 0, 0.5, 1, 5 at.%) alloys were investigated as a function of B content. The results show that the addition of B significantly influences the microstructure of the alloys. The microstructure of Ti₄₄Ni₄₇Nb₉ alloy consists of B2 parent phase matrix and β-Nb phase. When the B content is 0.5 at.%, Nb₃B₂ phase presents. With further increasing B content to above 1 at.%, TiB and NbB phases present instead of Nb₃B₂ phase. With increasing B content, the transformation temperatures increase due to the reduced Ni/Ti ratio and Nb content in the matrix. The mechanical properties can be optimized by the addition of 1 at.% B.     

Microstructure and Properties of Deformation Processed Polycrystalline Ni47Ti44Nb9 Shape Memory Alloy

The objective of this work was to investigate the relationships between process and microstructure and property in polycrystalline Ni₄₇Ti₄₄Nb₉ alloy. Three processes: (1) hot-forged, (2) cold-drawn, and (3) cold-rolled were investigated. The microstructure was tested by means of optical microscope, x-ray diffraction, and electron backscatter diffraction, and then crystalline orientation distribution functions and inverse pole figures were measured. The results indicated that hot-forging eliminated dendritic microstructure and fined the eutectic structure. It also induced a 〈113〉 fiber texture, which paralleled to the axial direction. The cold drawing and cold-rolling had a further effect in grain refinement. And the cold-drawn specimens contained a strong 〈111〉 fiber texture paralleling to the deformation direction, while the cold-rolled tubes formed 〈111〉 crystalline directions paralleling the axial direction and 〈110〉 crystalline directions of crystalline arranged along the circumferential direction. The notably distinctive recoverability of different processed materials was observed and discussed.     

自生TiCp/Ti复合材料中TiC的生长习性

利用配位多面体生长基元理论研究了自生TiCp/Ti复合材料中TiC的生长习性。TiC晶体的配位多面体生长基元为TiC6。生长基元进入{100}面时为4个棱边同时联结，生长速率最快，不易显露；进入{111}面时为共面联结，生长速率最慢，容易显露。因此，TiC晶体的理想形态为{111} 面为显露面的八面体。TiC晶胚在熔体中生长时，受传热传质过程的影响，6个顶角所处的{100}方向生长速率加快，形态失稳，从{100}方向顶角部位生长出二次枝晶臂，最终形成棱面枝晶状TiC。如枝晶形成时低生长速度的晶面上形成大量的晶体缺陷，则它们的生长速度加快，棱面消失，成为光滑枝晶。     

不同冷却条件下Cu60Co30Cr10合金的快速凝固（英文）

利用电磁悬浮和快淬实验研究Cu60Co30Cr10合金在亚稳不混溶区的液相分离和快速凝固特征。结果表明,合金的显微组织为富(Co,Cr)相分布在富Cu相基体中,且富(Co,Cr)相颗粒的形状和大小随着冷却速率的变化而有明显的区别。在悬浮凝固条件下冷却速率较低,富(Co,Cr)相较粗大,有明显的聚集粗化趋势,富(Cu)相中有大量富(Co,Cr)相枝晶。而在快淬凝固条件下富(Co,Cr)相明显细化,富(Cu)相中未发现富(Co,Cr)相枝晶形成,这可能与较高的冷却速率、较大的过冷度和较高的界面张力有关。     

Stress-induced martensitic transformation in （Ni47Ti44）100-xNbx shape memory alloys with wide hysteresis

The effect of deformation via stress-induced martensitic transformation on the reverse transformation behavior of the （Ni47Ti44）100-xNbx （x=3, 9, 15, 20, 30, mole fraction, %） shape memory alloys was investigated in detail by differential scanning calorimetry （DSC） after performing cryogenic tensile tests at a temperature of Ms＋30 ℃. The results show that Nb-content has obvious effect on the process of stress-induced martensitic transformation. It is also observed that the stress-induced martensite is stabilized relative to the thermally-induced martensite （TIM） formed on cooling, and Nb-content in Ni-Ti-Nb alloy has great influence on the reverse transformation start temperature and transformation temperature hysteresis of stress-induced martensite（SIM）. The mechanism of wide transformation temperature hysteresis was fully explained based on the microscopic structure and the distribution of the elastic strain energy of （Ni47Ti44）100-xNbx alloys.     

Effects of Hydrogen on Ni47Ti44Nb9 Shape Memory Alloy

The effects of hydrogen on the transformation characteristics of Ni₄₇Ti₄₄Nb₉ shape memory alloy were investigated. Cathodic hydrogen charging was performed at a current density of 20 mA/cm² in 0.5 mol/L H₂SO₄ solution at room temperature. The transformations of the hydrogenated specimens were characterized by differential scanning calorimetry, x-ray diffraction, and electrical resistivity measurement in details. For the hydrogen-charged NiTiNb alloy, the original reversible transformation between B2 and B19′ phase disappeared. Meanwhile, new transformation around 120 °C was present. This high temperature reversible transformation was confirmed to be the transformation between β-NbH phase and α-Nb(H) solid solution phase.