Effects of Cu and Mn on mechanical properties and damping capacity of Mg-Cu-Mn alloy

The effects of Cu and Mn additions on mechanical properties and damping capacity of Mg-Cu-Mn alloy were investigated. The tensile properties and damping capacity at room temperature of as-cast Mg-Cu-Mn alloy were tested.The microstructurc was studied using optical microscope,X-ray diffraction and scanning electron microscope.The Hall-Perch relation and Granato-Lücke model were used to explain the influences of Cu and Mn additions on the tensile properties and damping capacity of Mg-Cu-Mn alloy.The result...     

铸态和挤压变形态Mg-Zn-Al-Re镁合金的室温和高温力学性能

采用透射电子显微镜、扫描电子显微镜及能谱分析、拉伸力学性能测试等手段比较分析了铸态和挤压变形态Mg-7Zn-3Al-0～0.7Re(质量分数,%)镁合金的室温和高温力学性能,探讨了稀土和变形加工对合金强度和塑性的影响规律。结果表明,适量稀土Er可以显著提高铸态Mg-Zn-Al合金的高温塑性,而稀土含量对合金室温力学性能和高温屈服强度影响不明显;挤压变形过程中动态弥散析出纳米级的球形析出相,显著提高Mg-Zn-Al-Er合金的高温力学性能,其200℃下的屈服强度和延伸率分别较铸态提高了105%和120%,断口显示其断裂方式呈明显的韧性断裂特征。     

变形态Mg-Nd合金的组织转变和拉伸性能特征

研究不同变形条件对Mg-2.2Nd-0.5Zn-0.5Zr合金室温拉伸性能和组织的影响.经过不同条件的热挤压变形后,该合金的强度和延性都有不同程度的增加,屈强比从0.58提高到0.87左右.固定变形温度时,强度随变形速率增大而降低,延性反之.固定变形速率时,升高变形温度则强度降低,延性增加.弥散于晶界的Mg9Nd化合物细化了晶粒.变形态Mg-Nd合金的高温超塑拉伸研究发现,375℃是该合金的最佳超塑变形温度,应变速率在1×10-2s-1时,延伸率达到329%;当变形速率提高到2×10-2s-1时,该合金的延伸率仍可达到213%.分析不同真应变下的组织发现,在变形初期发生动态再结晶,晶粒得到破碎而变得细小,随着变形程度的增加,晶粒长大程度较小.在变形后的断口形貌中发现,Mg-Nd合金的超塑变形机制为晶界滑移控制下的孔洞连接协调机制.     

Mechanical properties at room temperature of an Al-Zn-Mg-Cu alloy processed by equal channel angular pressing

Tensile tests were conducted to evaluate the influence of equal-channel angular pressing (ECAP) on the mechanical properties at room temperature of overaged Al 7075-O alloy. ECAP processing was performed using route B_C at different temperatures and number of passes, i.e. different processing severity conditions. The maximum load (F_max) recorded during the last pass of each ECAP path considered in this study is a very good estimation of the processing severity. The mechanical properties were studied in terms of the balance between tensile strength and ductility. In the processed Al 7075-O alloy, the grain size was reduced down to ∼150 nm. Consequently, tensile testing at room temperature revealed a significant increase in the maximum tensile strength after ECAP with respect to the as start material. In the present study, as the processing severity increases with the number of ECAP passes or with the decrease in processing temperature, there is a consistent trend of increment in ultimate tensile strength with minor decrease in uniform plastic elongation respect to the first ECAP pass at room temperature. This is in contrast to the behaviour after more severe plastic deformation conditions, where an increase in strength together with a strong decrease in elongation would be expected.     

Influence of impurities on damping properties of ZK60 magnesium alloy

The influence of impurities on damping capacities of ZK60 magnesium alloys in the as-cast, as-extruded and T4-treated states was investigated by dynamically mechanical analyzer at room temperature. Granato and Lucke dislocation pinning model was employed to explain damping properties of the alloys. It is found that reducing impurity content can decrease the amount of second-phase particles, increase grain size and improve damping capacity of the as-cast alloy slightly. The as-extruded alloy with lower impurity content is found to possess obviously higher damping capacity in the relatively high strain region than that with higher impurity concentration, which appears to originate mainly from different dislocation characteristics. The variation tendency of damping property with change of impurity content after solution-treatment is also similar to that in the as-extruded and as-cast states. Meanwhile, the purification of the alloy results in an evident improvement in tensile yield strength in the as-extruded state.     

固态回收法制备Mg-Zn-Y-Zr合金的微观组织和力学性能

采用冷压法压实Mg-Zn-Y-Zr合金碎屑,在不同温度和不同挤压比下进行热挤压。结果表明：在低于320℃时挤压,微观组织由大量再结晶晶粒和少量未再结晶晶粒组成,合金具有较高的强度和较低的韧性;当挤压温度升高到360℃时,发生完全再结晶,微观组织由等轴晶组成,合金具有较低的强度和较高的韧性;当挤压温度升高到420℃时,微观组织由粗大的等轴晶组成,导致了合金的力学性能下降;当挤压比从8增加到16时,晶粒明显细化,力学性能显著提高,然而,随着挤压比的进一步增加,屈服强度和极限抗拉强度升高幅度不大。     

Effect of microstructure on tensile properties and fracture behavior of intermetallic Ti2AlNb alloys

The tensile properties and fracture behaviors of Ti-22Al-27Nb and Ti-22Al-20Nb-7Ta alloys were investigated in the temperature range of 25-800℃ Three typical microstructures were obtained by ifferent thermomechanical processing techniques.The results indicate that the duplex microstructure has an optimum combination of tensile yield strength and ductility both at room and elevated temperatures.Adding Ta to Ti2AlNb alloy can improve the yield strength,especially at high temperature while retain a good ductility.The study on crack initiation and propagation in dedformed microstructure of Ti2AlNb alloys indicates that microstructure has ikmportant effect on the tensile fracture mechanism of the alloys.The cracks initiate within primary O/α2 grains along O/B2 boundaries or O phase laths in B2 matrix,and propagate along primary B2 grain boundaries for the duplex microstructure.The fracture mode is transgranular with ductile dimples for the duplex and the equiaxed microstructures,but intergranular for the lath microstructure.     

挤压态Mg-10Gd-3Y-0.5Zr镁合金的低温力学性能(英文)

研究多循环低温交变(液氮浸泡处理)和拉伸温度对挤压态Mg10Gd3Y0.5Zr镁合金的微观组织、力学性能以及断裂机制的影响。结果表明,Mg10Gd3Y0.5Zr合金经10d液氮浸泡或10个周期高低温交变循环后,合金室温力学性能基本不变;而经过20个周期高低温循环后,合金的室温抗拉强度由398MPa升高到417MPa。在196°C下拉伸时,挤压态Mg10Gd3Y0.5Zr镁合金的屈服强度和抗拉强度均大幅度提高,分别为349MPa和506MPa,分别增长了18%和27%。合金室温断裂机制为穿晶解理断裂,而低温条件下为韧性断裂和解理断裂并存的混合断裂机制。     

退火温度对ECAP变形高氮奥氏体不锈钢力学性能的影响

为研究等通道转角挤压(ECAP)+退火对高氮钢力学行为的影响,室温条件下对高氮钢进行1道次ECAP变形,之后分别在700、800、850、900 ℃下对不同N含量的试验钢进行退火处理,分析其力学性能变化规律。结果表明:高氮钢随着退火温度的升高,屈服强度和抗拉强度整体上呈下降的趋势,塑性随退火温度的升高而上升;不同状态高氮钢的抗拉强度与均匀延伸率之间都呈现了传统的强塑性之间的矛盾关系,随N含量的增加,呈现强度和均匀延伸率同步提高的趋势;高氮钢ECAP+低温退火后的拉伸断口呈现沿晶断裂形貌,随N含量的升高,沿晶断裂倾向更加明显。     

Tensile properties and fracture characteristics of spray cast alloy IC6 （Ni-7.8Al-14Mo-0.05B）

Tensile testing results of spray cast Ni3Al-based superalloy indicated that the yield strength and tensile strength increase with the increasing of temperature and reached maximum at around 760℃, then decrease with the increasing of temperature. After high temperature isostatic pressing (HIP), yield strength decreased and ductility and tensile strength increased. Stereographic projection showed that no matter at room temperature, medium temperature or high temperature, cracks extend along (111).     

Ti3Al基合金的拉伸形变和断裂

测试了三种显微组织Ｔｉ３Ａｌ基合金的室、高温拉伸性能；并用ＳＥＭ和ＴＥＭ详细观察样品的形变和断裂特征，结果发现，材料的力学性能与断口和位错组态的变化密切相关，随实验温度升高，强度降低，延性增加；随固溶温度提高，强度增加，延性降低，三种组织室温拉伸均为解理断裂，温度呈现解理与沿晶混合断裂。     

电子束快速成形TC18钛合金柱状晶组织的拉伸性能

采用电子束快速成形方法,获得了一种TC18钛合金的柱状晶组织,研究了热处理工艺对该类组织析出相和拉伸性能的影响。结果表明,在740～830℃温度范围内固溶、在550℃时效处理,随着固溶温度的升高,快速成形样品沿柱状晶方向的强度呈上升趋势,塑性呈下降趋势;在830℃固溶处理后,在550～650℃时效温度范围内,随着时效温度的升高,沿柱状晶方向的强度呈下降趋势,而塑性呈上升趋势;拉伸性能随热处理工艺的变化主要取决于热处理过程中产生的二次α相;发现了延性韧窝和沿晶+准解理两种不同类型的断口形貌,并对其形成原因进行了分析。     

铝合金板材温热成形性能

在20℃～300℃的温度范围内,分别对7B04-T6和6061-T6铝合金薄板进行了单拉试验,结果表明,7B04-T6高强度铝合金的断后延伸率和拉伸极限应变在温热状态下都有显著的提高,比较适合于温热成形,而6061-T6则不太适合。另外,基于Fields&Backofen本构方程,对7B04-T6在不同温度状态下的强化规律进行了分析和探讨,结果表明,随着温度的逐渐升高,应变强化指数n值不断减小,应变率敏感系数m值则显著增大,应变率强化明显增强,这也是在温热状态下其成形性能提高的主要原因。     

大塑性变形6013铝合金的时效特性与力学性能

利用X射线衍射分析（XRD）、差示扫描量热法（DSC）和拉伸试验,研究不同温度等通道转角挤压（ECAP）和常规静态时效处理后6013 Al-Mg-Si铝合金的微观结构、时效行为、析出动力学以及力学性能。XRD测得的ECAP变形后合金的平均晶粒尺寸在66-112 nm范围内,平均位错密度在1.20×10^14-1.70×10^14 m^-2范围内。DSC分析表明,由于ECAP后试样比常规时效处理试样拥有更细小的晶粒和更高的位错密度,因此,ECAP变形后合金的析出动力学更快。与未变形合金相比,ECAP后试样的屈服强度和抗拉强度都得到了显著提高。室温ECAP后试样的强度达到最大,其屈服强度是静态峰时效屈服强度的1.6倍。细晶强化、位错强化以及由于ECAP过程中的动态析出而产生的析出相强化,是ECAP合金获得高强度的几种主要强化机制。     

固溶时效处理对挤压态6082铝合金力学性能和组织的影响

采用拉伸试验机、光学显微镜和透射电镜等方法研究了固溶和时效处理工艺对挤压态6082铝合金力学性能和组织的影响。结果表明,经530 ℃固溶处理的试样强度高于550 ℃固溶处理的试样,经不同固溶温度处理后合金表现出不同的力学性能各向异性行为,而经时效处理后合金的屈服强度显著提升。550 ℃固溶处理的合金,晶粒明显长大。经时效处理后的试验合金中分布着大量的针状析出相,能有效阻碍位错的运动,提升材料的强度。经不同固溶+时效处理后的挤压态试验合金拉伸断口处均发现大量的韧窝,表现出韧性断裂的特征。     

Effects of deviations from stoichiometry on the strength anomaly and fracture behavior of B-doped FeAl

Tensile tests were conducted at temperatures ranging from 145–1123 K on four different FeAl alloys, containing 40, 43, 45, and 48 at.% Al, each doped with 0.12 at.% B. The alloys were initially heat treated to obtain a relatively large grain size (˜200 μm), after which they were given a long, low-temperature anneal (673 K for 5 d), to minimize, respectively, the effects of grain boundary strengthening and thermal vacancies on the measured yield strengths. Each alloy displayed bcc-type behavior at low temperatures (yield strength decreasing with increasing temperature), followed by a strength anomaly at intermediate temperatures (yield strength increasing with increasing temperature), and a sharp drop in yield strength at elevated temperatures (beyond the anomalous strength peak). Thermal vacancies that are generated during the hold time at the test temperature may contribute to the production of the strength anomaly. In specimens not given the vacancy-minimizing anneal, quenched-in vacancies were found to substantially increase low-temperature strength, thereby masking the yield strength anomaly. As the Al concentration of FeAl increased, the prominence of the yield strength anomaly decreased. Ductility also exhibited a peak at elevated temperatures, first increasing with temperature until it reached a maximum value and then decreasing with further increases in temperature. The peak in ductility occured at lower temperatures as the Al content increased. The fracture mode in all four alloys was mixed (intergranular + transgranular) at cryogenic temperatures, predominantly intergranular at around room temperature, dimpled rupture at peak ductility, and intergranular cavitation at elevated temperatures where the ductility dropped.     

温度和氧含量对Ti-2Al合金拉伸力学行为和断裂方式的耦合影响

研究高氧含量(0.30%,质量分数,下同)、工业水平氧含量(0.16%)和极低氧含量(0.06%) 3种Ti-2Al合金在低温(77 K)、室温和高温(673 K)下的拉伸力学行为。结果表明：低温和室温下,随着氧含量的升高,材料强度提高,塑性降低。然而,高温673 K下,不同氧含量Ti-2Al合金强度和塑性基本相同,材料强度和塑性对氧含量的依赖性显著降低。氧含量较低时,温度对Ti-2Al合金塑性影响很小。微观组织观察表明,随着温度的升高,工业水平及高氧含量Ti-2Al合金拉伸断口由脆性解理转变为延性韧窝。高温环境下,固溶氧原子扩散速率提高使Cottrel气团对位错滑移的阻碍减弱,均匀变形的结果导致高氧含量Ti-2Al合金延性改善。     

Mg-Bi合金的显微组织和力学性能

采用挤压铸造和挤压变形工艺制备了Mg-Bi二元合金,通过金相显微镜分析,室温拉伸性能测试,X射线衍射分析,SEM和EDS等手段,研究了Mg-Bi合金在铸态和热挤压态的显微组织和力学性能.结果表明:铸态Mg-Bi合金随着Bi含量的增加,伸长率逐渐降低,抗拉强度逐渐增加,当Bi含量达10wt.％以上,抗拉强度降低;Mg-Bi合金铸锭经450℃、3h保温,挤压比为12.76热挤压后,随Bi含量的增加,抗拉强度与伸长率均逐渐增加,当Bi含量达12wt.％时,抗拉强度为219.68 MPa,伸长率为13.43％,Bi含量继续增加,合金抗拉强度及伸长率呈下降趋势;挤压态Mg-Bi合金的力学性能是晶粒细化与Mg3Bi2综合作用的结果,当Bi含量大于12wt.％后,形成较多粗大的Mg3Bi2相是导致合金力学性能下降的主要原因.     

Improving mechanical properties of Mg-Al-Zn alloy sheets through accumulative roll-bonding

Experiments were conducted to evaluate the potential for improving the mechanical properties of Mg-Al-Zn alloy at room temperature by subjecting to accumulative roll-bonding（ARB）. It is shown that ARB may be applied successfully to Mg-Al-Zn alloy at elevated temperatures and it leads to grain refinement and significant improvements in the ductility. The strength of the as-rolled Mg-Al-Zn alloy sheet after ARB processing is slightly decreased and basal texture is weakened by ARB processing.     

Mo-Si合金室温及高温拉伸力学性能研究

采用粉末冶金技术制备了不同Si含量(0,0.1,0.3wt%Si)的Mo-Si合金板材,并在25,300,800和1200℃下进行了静拉伸试验,研究了试验温度对Mo-Si合金板材力学性能、断裂方式及微观组织的影响。结果表明:随试验温度升高,纯钼及Mo-Si合金板材强度明显下降,但延伸率以300℃为分界点呈现出先升后降的趋势。室温下Mo-Si合金的断裂方式为穿晶解理断裂,在300及800℃时主要为韧窝延性断裂,而1200℃时为沿晶断裂。对Mo-Si合金强化机制的分析表明,室温下的强化主要来源于弥散强化和固溶强化,而在高温时,固溶作用明显减弱,颗粒弥散和粗化晶粒为主要的强化手段。