Nb添加对Zr_(50.5-x)Al_9Ni_(4.05)Cu_(36.45)Nb_x非晶合金热稳定性及力学性能的影响

采用铜模铸造法,制备了直径为2 mm的Zr50.5-xAl9Ni4.05Cu36.45Nbx(x=0,1,2,4,摩尔分数,%)完全非晶棒材。分别采用X射线衍射仪(XRD)、扫描电镜(SEM)、透射电镜(TEM)、差示扫描量热计(DSC)和力学性能试验机对合金的相组成、结构、热物性参数和力学性能进行研究。结果表明:添加Nb对所研究合金的玻璃转变温度Tg影响不大,但提高了晶化温度Tx和过冷液相区ΔTx;当x=4时,合金具有最高的玻璃转变温度Tx=773.4 K和最大过冷液相区ΔTx=68.1 K。依据耐温和热塑性成形要求,非晶合金的热稳定性可用玻璃转变温度Tx和过冷液相区ΔTx来分别表示。随着合金中Nb添加量的增加,非晶合金的双重热稳定性提高。非晶合金的断裂强度随着Nb添加量的增加先减小后增加,当x=4时,合金的最高断裂强度为2032 MPa。     

Fe61Co10Zr5W4B20块体非晶合金的晶化行为与力学性能研究

采用铜模吸铸法制备Ф2mm的Fe61Co10Zr5W4B20块体非晶台金．采用XRD、SEM、DSC、硬度和压缩实验研究了非晶合金的结构组织、热稳定性、晶化特征、硬度和压缩性能。设块体非晶合金表现出二级晶化,其玻璃转变温度为561.1℃．晶化温度为619．0℃．第一晶化峰温度为632.6℃．第二晶化峰比之高约117℃;用Kissinger和Ozawa方法获得的玻璃转变激活能特别为595.1KJ/mol．578.7kJ/mol．晶化激活能分别为413.9kJ／mol,407.4kJ／mol;非晶合金的晶化行为比其玻璃转变表现出更为明显的动力学效应;非晶合金的显做硬度为1207HV．压缩强度为1707．6MPa．呈典型的脆性断裂．断口中光滑区与脉状花纹区并存。     

95W-5(Ni/Fe/Co)合金的低温显微组织和力学性能

分析了95W-5(Ni/Fe/Co)合金的粉末冶金工艺特点及低温显微组织与力学性能,给出了力学性能与温度的关系曲线.通过对合金拉伸试样断口的扫描电镜分析,揭示了该合金低温力学性能与组织变化的微观本质.结果表明:95W-5(Ni/Fe/Co)合金室温下具有较高的强度及一定的塑性;该合金低温脆化的主要原因是由于屈服强度随温度的降低而增加,钨颗粒过早解理及粘结相变形极小引起的;95W-5(Ni/Fe/Co)合金的冷脆性转变温度在-50℃左右,此时脆性断裂以钨颗粒的自身解理为主.     

快速凝固Cu-5Ag-0.5Zr-0.4Cr-0.35Nb合金的组织与力学性能

采用快速凝固方法制备了Cu-5Ag-0.5Zr及Cu-5Ag-0.5Zr-0.4Cr-0.35Nb(wt%)合金粉末,采用热等静压将粉末压制成坯料,随后进行热锻、冷轧处理。测试了合金在室温及高温(500 ℃)下的力学性能,并分析了合金的显微组织及断口形貌。结果表明,冷轧态合金具有更优异的室温拉伸性能,冷轧态Cu-Ag-Zr合金抗拉强度为739.3 MPa,伸长率7.1%,这与铜基体中密集的Cu₄AgZr颗粒及纳米级Ag颗粒有关。除Cu₄AgZr颗粒及Ag颗粒外,Cr、Nb元素的添加还生成高温稳定的Cr₂Nb颗粒,同时提高了合金的室温和500 ℃拉伸强度。冷轧态Cu-Ag-Zr-Cr-Nb合金的室温极限抗拉强度和伸长率分别为799.1 MPa与5.3%。因为热锻态合金晶粒尺寸粗大,Ag颗粒尺寸细小,相比冷轧态合金拥有更好的抗高温弱化性能。热锻态Cu-Ag-Zr-Cr-Nb和Cu-Ag-Zr合金的500 ℃抗拉强度分别为186.8和129.2 MPa,而冷轧态Cu-Ag-Zr-Cr-Nb和Cu-Ag-Zr合金在500 ℃抗拉强度分别仅为113.1和95.4 MPa。     

Phase transformations and mechanical properties of a Ti36Nb5Zr alloy subjected to thermomechanical treatments

Various solid state phase transformations exist in metastable β-type Ti alloys,which can be employed to optimize the mechanical properties.In this paper,synchrotron X-ray diffraction(SXRD)experiments were carried out to study the phase transformations of a Ti36Nb5Zr alloy subjected to different thermomechanical treatments.Furthermore,the correlation between the phase constitutions and the mechanical properties was discussed.The a" texture formed,and high-density defects were introduced after cold rolling of the solution treated specimen,leading to the decrease in Young’s modulus and the increase in strength.The cold-rolled specimens were then annealed at temperatures from 423 to 773 K for 30 min.Both the Young’s modulus and strength increased with annealing temperatures increasing up to 673 K,which resulted from the precipitation of the ω and/or α phases.With further increase in annealing temperatures to 773 K,the β→α precipitation replaced the β→ω_iso phase transformation,and the density of defects decreased,leading to the decrease in both the Young’s modulus and strength.These results provide theoretical basis for the design biomedical Ti alloys with both low Young’s modulus and high strength.     

Influence of annealing temperature on electrochemical properties of rapidly quenched LPC （NiAlMn） 4.25 Co0. 75 hydrogen storage alloy electrodes

The influence of annealing temperature on the electrochemical properties and structure of the rapidly quenched LPC(NiAIMn)4.25 Co0.75 hydrogen storage alloys was investigated, in which LPC represents the abbreviation of Nd-free La-Ce-Pr mischmetal after the extraction of most of Ce and Nd. After the annealing treatment between 700-900℃ for rapidly quenched alloys, their discharge capacity becomes larger and the P-C-T plateau tends to be flatter and lower. The alloy annealed at 700 *C has the highest discharge capacity and flattest plateau. The analyses by X-ray diffraction (XRD), different thermal analysis(DTA), scanning electron microscopy (SEM) and transmission electron microscopy (TEM) indicate that the microstructure reversion and recrystallization occur during the heating, and their feature temperatures are 477℃ and 696℃ respectively. The annealing treatments make cell volume increase, dislocations and strain decrease, and the distribution of alloy composition become homogeneous.     

Al-Cu-Mg-Ag合金的高温力学性能

利用高温短时拉伸试验、扫描电镜和透射电镜等分析手段,研究了经165℃×2 h时效处理的Al-Cu-Mg-Ag合金在不同温度下的显微组织和力学性能.结果表明:随着温度的升高,强度逐渐下降,而伸长率先降后升.在200℃时合金具有最低的伸长率(12%),在温度高于200℃时,合金强度下降较快.当温度升至350℃时,抗拉强度、屈服强度分别降至105 MPa、98 MPa,伸长率增至23%.在高温条件下,该合金力学性能的下降主要是由于析出相的粗化与转变引起的.     

Crystallization of amorphous Zr60Al15Ni25 alloy

The phase formation and crystallization kinetics during the thermal treatment of amorphous Zr₆₀Al₁₅Ni₂₅ alloy were investigated by differential scanning calorimetry (DSC) and X-ray diffraction (XRD). By lowering the isothermal annealing temperatures, it is revealed that the crystallization of the amorphous Zr₆₀Al₁₅Ni₂₅ alloy consists of a primary transformation followed by a polymorphic transformation, corresponding to the precipitations of hexagonal Zr₆Al₂Ni and the Zr₅AlNi₄ with a U₃Si₂-typed superstructure. The primary phase being Zr₆Al₂Ni rather than Zr₅AlNi₄ in the crystallization is because the latter has a complex structure and its formation requires the diffusion of Al and Zr atoms on a large scale.     

固溶处理对奥氏体不锈钢07Cr18Ni11Nb高温力学性能的影响

研究了固溶处理对奥氏体不锈钢07Cr18Ni11Nb高温力学性能的影响。结果发现,500、600 ℃高温屈服强度随固溶处理温度的升高逐渐降低,500、600 ℃高温抗拉强度无明显变化。当固溶处理温度≤1100 ℃时,奥氏体晶粒尺寸基本保持不变;当固溶处理温度＞1100 ℃后,奥氏体晶粒逐渐长大,固溶处理温度达到1200 ℃时,奥氏体晶粒尺寸可增大至100 μm以上。在600 ℃以下进行高温拉伸试验时,奥氏体晶界仍然是决定强化效果的重要因素,晶粒尺寸越小,高温屈服强度越高。     

NbCr2/ Nb合金高温力学行为

在800～1200℃的变形温度,0.001～0.1 s~(-1)的应变速率条件下对通过机械合金化+热压工艺制备的成分为Nb-22.5Cr的NbCr_2/Nb合金进行了高温压缩试验,研究了合金的高温力学行为,并通过透射电子显微镜观察分析了合金的变形机制。结果表明:NbCr_2/Nb合金的峰值强度随着变形温度的升高,应变速率的降低而下降。基体Nb的变形机制主要为位错的滑移;而NbCr_2的变形机制是通过层错、孪晶、不全位错等方式进行。     

非晶55Mg35Ni10Si块体的制备及力学性能

利用机械合金化方法制备55Mg35Ni10Si三元非晶合金粉末,以该非晶粉末为基础材料,采用真空热压法制备55Mg35Ni10Si非晶块体,利用显微硬度测试等手段考察其力学性能。DSC和XRD分析表明,粉体和块体材料中均出现一个明显的放热峰,结合高分辨电子显微镜观察证明,真空热压后块体材料总体上仍以非晶相为主并含少量纳米晶,而块体材料的晶化峰温度要略低于非晶粉末。力学性能测试表明,块体材料的显微硬度为7 834-8 048 MPa,且随载荷的增加而下降,与传统晶态材料的硬度-载荷依赖关系相似。块体材料的断口呈山峦状,没有明显塑性形变的特征,断裂裂纹扩展沿压痕对角线呈放射状。     

Zr55Al10Ni5Cu30 amorphous alloy film prepared by magnetron sputtering method

In this work,amorphous Zr55Al10Ni5Cu30 alloy thin film was prepared on D36 steel substrate by magnetron sputtering method.The film was characterized by scanning...     

High-temperature brazing of molybdenum to 12Cr18Ni10Ti steel with the CTEMET 1301 rapidly quenched nickel brazing alloy

Extensive studies are being carried out to develop a divertor (Divertor: a device in a thermonuclear reactor, intended for receiving of particle flows and radiation from the periphery of the plasma column. It is the most heavily loaded part of the reactor chamber surfaces with energy fluxes.) for tokamaks with a container for supplying liquid metal to the reception surface, with the construction of actual structures with high reliability and long service life. In this case, it is necessary to develop methods for joining dissimilar materials. In the transition section, molybdenum and steel (12Cr18Ni10Ti) pipes are joined by brazing. In this work, the method of producing a strong, heat resisting and hermetic joint between molybdenum and 12Cr18Ni10Ti corrosion-resisting steel is developed. Brazing is carried out using a paste based on CTEMET-1301 brazing alloy. The method of assembling the components in order to produce optimum gaps in brazing resulting in the homogeneous brazed joint without the formation of a brittle eutectic interlayer is developed. The brazed specimens were tested for heat resistance, leak tightness and service life at the given load. All the specimens withstood the tests. The mechanical properties of the brazed joints were determined by measuring the microhardness of the region of the welded joint and by shear tests. The results show that the strength characteristics depend strongly on the size of the gap between the brazed components. For the specimens assembled with the optimum gap the ultimatum shear strength was 500 ± 50 MPa.     

Formation and properties of Zr48Nb8Cu14Ni12Be18 bulk metallic glass

Zr₄₈Nb₈Cu₁₄Ni₁₂Be₁₈ bulk metallic glass (BMG) with excellent glass-forming ability was prepared by water quenching method. The BMG exhibits high glass transition temperature T_g and onset crystallization temperature T_x, compared with Zr₄₁Ti₁₄Cu_12.5Ni₁₀Be_22.5 BMG. The crystallization processes, change of elastic constants, and density and hardness in the crystallization process were studied by using X-ray diffraction, differential scanning calorimetry and acoustic method. The shear modulus, Poisson ratio, density and hardness are found to be sensitive to the crystallization process. A striking softening of long-wavelength transverse acoustic phonons in the BMG relative to its crystallized state is observed. The linear expansion coefficient, determined by a dilatometer method, is α_TG=1.04×10⁻⁵ K⁻¹ (300–656 K) for the BMG and α_TC=1.11×10⁻⁵ K⁻¹ (356–890 K) for the crystalline alloy. The Mie potential function and the equation of state of the BMG are determined from the expansion coefficient and acoustic experiments.     

An in situ bulk Zr58Al9Ni9Cu14Nb10 quasicrystal-glass composite with superior room temperature mechanical properties

An in situ bulk Zr₅₈Al₉Ni₉Cu₁₄Nb₁₀ quasicrystal-glass composite has been fabricated by means of copper mould casting. The microstructure and constituent phases of the alloy composite have been analyzed by using X-ray diffraction, transmission electron microscopy and high-resolution transmission electron microscopy. Icosahedral quasicrystals were found to be the majority phase and the grain size is in half-μm scale. In between the I-phase grains is a glassy phase. Optical microscopy and scanning electron microscopy revealed that the as-cast alloys were pore-free. The microhardness of the composite is about 5.90 ± 0.30 GPa. The room temperature compression stress–true strain curve exhibits a 2% elastic deformation up to failure, and a maximum fracture stress of 1850 MPa at a quasi-static loading rate of 4.4 × 10⁻⁴ s⁻¹. The mechanical property is superior to the early developed quasicrystal alloys, and is comparable to Zr-based bulk metallic glasses and their nanocomposites. The quasicrystal-glass composite exhibits basically a brittle fracture mode at room temperature.     

新型Cr18Ni31Al合金的高温抗氧化性

利用氧化增量法测得新型Cr18Ni31Al合金的不同温度下的高温氧化动力学曲线,使用X射线衍射仪(XRD)、扫描电镜(SEM)和能谱仪(EDS)对合金表面高温氧化膜的形貌及组成进行了分析和检测。结果表明,新型Cr18Ni31Al合金的高温氧化动力学曲线为Δm。700 ℃和800 ℃氧化后,氧化膜均由Fe₂O₃和NiCr₂O₄组成;900 ℃氧化后,氧化膜表面有尖晶石结构的Fe(Cr, Al)₂O₄氧化物生成。＝atⁿ