应变速率对GH4169合金焊接接头拉伸变形行为的影响

研究了应变速率对GH4169合金激光焊接接头变形行为的影响,探讨了接头拉伸变形对应变速率敏感性的机理。结果表明,与母材相比,GH4169合金激光焊接接头的拉伸变形对应变速率敏感性的影响更显著。应变速率低于10-1s-1时,接头强度受应变速率的影响不大;当应变速率高于100s-1时,随着应变速率增加接头屈服强度、抗拉强度均呈增加趋势,屈服强度增加的幅度更为显著。随着应变速率增加接头塑性总体呈下降的趋势,但是在101~102s-1范围内有所回升,并出现峰值。随着应变速率的增加,合金接头断裂的位置由母材经过热影响区向熔合区靠近。高应变速率的接头不同位置变形行为对应变速率敏感性的差异,是接头变形和断裂行为产生应变速率敏感性的主要原因。     

不同温度环境下Al–7Zn–2.5Mg–2.0Cu–0.1Zr–0.2Sc合金的力学行为研究

目的 研究不同时效时间对Al–7Zn–2.5Mg–2.0Cu–0.1Zr–0.2Sc合金强度的影响,以及室温和-40℃这2种温度环境对该合金疲劳行为的影响。方法 在不同时效时间下对Al–7Zn–2.5Mg–2.0Cu–0.1Zr–0.2Sc合金进行热处理,并采用透射电镜观察其显微结构以解释不同时效时间下强度变化的原因。在不同外加总应变幅的条件下,对T6态该合金进行低周疲劳实验,对比研究Al–7Zn–2.5Mg–2.0Cu–0.1Zr–0.2Sc合金在不同温度环境下的低周疲劳行为。结果 随着时效时间的延长,不同温度环境下Al–7Zn–2.5Mg–2.0Cu–0.1Zr–0.2Sc合金的屈服强度和抗拉强度都先升高后降低,-40℃环境下的屈服强度和抗拉强度均高于室温环境下的。在低应变幅时,合金的循环应力响应行为特征总体呈稳定趋势,在高应变幅时,合金的循环应力响应行为先表现为循环稳定特征,后表现为循环硬化特征。同一应变幅下,-40℃环境下合金的循环应力幅值高于室温环境下的,而合金的低周疲劳寿命则随着温度的降低而下降。此外,在室温和-40℃低周疲劳加载条件下,疲劳变形机制为平面滑移机制。当应变幅...     

Mg-3Al-2Zn-2Y合金的动态力学性能研究

在不同应变率压缩与拉伸下,研究了Mg-3Al-2Zn-2Y合金的力学性能,发现2种条件下合金力学性能变化规律不同。压缩情况下,随应变率增大,极限强度与屈服强度先增大后减小,高应变率下(1300～4800s-1)的流变应力大于中低应变率(0.001～1s-1);在0.001～1450s-1拉伸下,随应变率增大,合金的流变应力呈增大趋势,极限强度、屈服强度增大,破坏应变先减小后增大。压缩情况下合金流变应力的应变率敏感性高于拉伸情况。     

变形温度与应变速率耦合作用对TWIP效应Ti-15Mo合金力学性能的影响EI北大核心CSCD

变形温度和应变速率均影响β型钛合金的力学性能,且其影响均关联塑性变形过程中变形方式的变化。利用TEM,EBSD,SEM,XRD,OM和拉伸试验机研究变形温度和应变速率耦合作用对{332}〈113〉孪生诱发塑性效应Ti-15Mo合金力学性能的影响。结果表明:在298 K和573 K下,屈服强度均随应变速率的增加逐渐升高,即依赖于位错热激活过程,且573 K下显著的位错热激活作用使得屈服强度表现出更大的应变速率依赖性。不同于298 K下,Ti-15Mo合金在573 K下通过{332}〈113〉孪生和位错滑移耦合变形;构建的流变应力模型表明位错强化成为其主要强化方式。高应变速率下,塑性变形早期形成的更多孪晶虽然会抑制孪生的进一步产生降低加工硬化率,但同时有效降低位错不均匀分布引起的局部应力集中延缓颈缩的发生;两个方面的共同作用使得Ti-15Mo合金在变形温度和应变速率耦合作用下呈现出更小的应变速率依赖性。     

AZ31镁合金温变形对其性能影响的研究

为了研究温变形对铸态AZ31镁合金力学性能的影响,在210～300℃温度范围内对均匀化后的合金进行了不同程度的平面应变压缩,并根据微观组织的演变对其进行了分析.结果表明:随变形温度的升高,在相同的变形程度下晶粒有长大的趋势,其抗拉强度增量下降;在同一温度下变形,强度增量随着变形程度的增加而增大,变形到一定程度时,呈现减小的趋势.在210℃下变形,当ε达到2.07时,其抗拉强度最大可达305MPa,较铸态提高近50%.表明AZ31合金温变形时,通过形变强化与细晶强化的合理组合,可获得细小均匀的等轴组织,大幅度提高镁合金的强度.     

再结晶Mi_3Al基合金中弥散无序γ相的强化作用EI

通过控制化学成分和处理工艺，得到一种弥散无序γ相强化的Ｎｉ_３Ａｌ基合金。ＴＥＭ分析发现：弥散无序的γ相是在有序γ＇基体｛００１｝面上析出的，且与基体保持共格关系。在不同温度下对该合金进行拉伸试验发现：弥散γ相的强化作用，使Ｍ_３Ａｌ基合金拉伸屈服强度的峰值温度升高到８５０℃左右；与相同处理条件下成分相近的ＩＣ２１８合金相比较，该合金的高温屈服强度和拉伸强度以及峰值温度以下的形变硬化率都发生显著的提高。文中在ＳＥＭ下对拉伸试样的断口特征进行了分析，并对无序γ相的弥散强化机理进行了探讨。     

再结晶Mi_3Al基合金中弥散无序γ相的强化作用

通过控制化学成分和处理工艺，得到一种弥散无序γ相强化的Ｎｉ_３Ａｌ基合金。ＴＥＭ分析发现：弥散无序的γ相是在有序γ＇基体｛００１｝面上析出的，且与基体保持共格关系。在不同温度下对该合金进行拉伸试验发现：弥散γ相的强化作用，使Ｍ_３Ａｌ基合金拉伸屈服强度的峰值温度升高到８５０℃左右；与相同处理条件下成分相近的ＩＣ２１８合金相比较，该合金的高温屈服强度和拉伸强度以及峰值温度以下的形变硬化率都发生显著的提高。文中在ＳＥＭ下对拉伸试样的断口特征进行了分析，并对无序γ相的弥散强化机理进行了探讨。     

5050铝合金板材高温流变行为研究

在303～673K的温度范围内和应变速率为0.001～0.1s-1下对5050铝合金薄板进行高温拉伸试验,研究了5050铝合金高温拉伸性能,以及该合金在升温条件下流变应力与变形温度、应变速率之间的关系.结果表明:5050铝合金的流变应力随温度的升高而降低,随应变速率的升高而升高;高温拉伸试样的伸长率随变形温度的升高而升...     

一种第二相粒子强化的再结晶Ni3Al基合金的拉伸性能

在不同温度下对一种ＴｉＣ和Ｃｒ２３Ｃ６第二相粒子沉淀强化的变形再结晶Ｎｉ３Ａｌ基合金进行了拉伸试验。结果发现，该合金的拉伸屈服强度的峰伍温度升高到８５０℃左右。与相同处理条件下的Ｎｉ３Ａｌ基合金ＩＣ２１８相比较，该合金的高温屈服强度和拉伸强度都有显著的提高，而高温韧性损失不大。在７５０℃左右该合金的动态脆化程度最大，在该温度下的延伸率大于１０．０％。     

形变温度对Fe-20Mn-3Cu-1.3C TWIP钢拉伸变形行为的影响EI北大核心CSCD

运用温控拉伸实验,分析了在-100~200℃范围内变形时形变温度对Fe-20Mn-3Cu-1.3C钢力学性能和形变机理的影响。观察分析了拉伸试样的显微组织,并利用热力学经典模型,估算了温度对孪晶诱发塑性(TWIP)钢层错能的影响。结果表明:随着形变温度的升高,TWIP钢的层错能显著增加,基体中形变孪晶的体积分数逐渐减少,抗拉强度和屈服强度呈下降趋势,而伸长率先升高后降低,塑性变形机制也由孪生为主逐渐转变为以滑移为主。层错能的拟合公式为γSFE=26.73+9.38×10^(-2) T+4.22×10^(-4 )T2-4.47×10^(-7) T^3,与滑移相比,孪生可获得更高的应变硬化率,从而使TWIP钢获得高强度和高塑性。     

Al_2O_3弥散强化铜棒材高温力学性能与软化行为研究

研究了ODS15、ODS20和ODS60三种Al_2O_3弥散强化铜棒材在650℃下保温1 min和15 min的高温力学性能,并依据ISO5182对ODS60弥散强化铜棒材的硬度、抗拉强度、屈服强度、软化行为进行研究。结果表明,铝含量不同的三种弥散强化铜棒材在650℃保温1 min与保温15 min的高温强度基本一致;随着铝含量的增加,高温强度随之升高;ODS60弥散强化铜硬度、屈服强度、抗拉强度的软化温度分别为970℃、950~960℃、960~970℃。     

Effect of Deformation Temperature on Microstructure and Mechanical Properties of AZ31 Mg Alloy Processed by Differential-Speed Rolling

A differential-speed rolling(DSR) was applied to AZ31 magnesium alloy sample at different rolling temperatures of 473,523,573,and 623 K with 1-pass and 2-pass operations.The microstructural evolution and mechanical properties of the deformed samples were investigated.The rolling temperature was found to be an important parameter affecting the microstructural development.After DSR at 473 K,the microstructure was more homogeneous than that obtained after deformation by equal-speed rolling(ESR).The fully recrystallized microstructures were generated after DSR at 573 and 623 K.As to mechanical properties,the yield strength(YS) and ultimate tensile strength(UTS) decreased monotonously with increasing rolling temperature.In contrast,the elongation of the DSR-deformed samples was improved as the rolling temperature increased.The strain hardening exponent(n) calculated by Hollomon equation increased with increasing the rolling temperature,which would explain an increase in the uniform elongation.     

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。     

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.     

温度对V-5Cr-5Ti合金拉伸性能及组织结构的影响

对真空自耗重熔制备的V-5Cr-5Ti合金进行了室温到1150℃温度范围的拉伸性能测试,获得了不同温度下的拉伸应力应变曲线,用SEM和光学显微镜对断口形貌和金相组织进行了观察,分析了温度对断口形貌和组织的影响。结果表明:V-5Cr-5Ti合金的屈服强度和极限强度总体上随温度升高而降低,但在300℃到700℃之间出现应变失效效应,断裂伸长率随温度升高而降低,断面收缩率随温度升高先增大再而降低,在400℃时断面收缩率最大;温度较低时塑性变形以滑移为主,温度较高时以晶界开裂为主,并伴随有晶界熔化的现象,高温断口表现为韧性断裂为主,具有韧性与脆性共存的现象。     

Parametric Analysis of Tensile Properties of Bimodal Al Alloys by Finite Element Method

An axisymmetrical unit cell model was used to represent a bimodal Al alloy that was composed of both nano-grained (NG) and coarse-grained (CG) aluminum. Effects of microstructural and materials parameters on tensile properties of bimodal Al alloy were investigated by finite element method (FEM). The parameters analyzed included aspect ratios of CG Al and the unit cell, volume fraction of CG Al (VFCG), and yield strength and strain hardening exponent of CG Al. Aspect ratios of CG Al and the unit cell have no significant influence on tensile stress-strain response of the bimodal Al alloy. This phenomenon derives from the similarity in elastic modulus and coefficient of thermal expansion between CG Al and NG Al. Conversely, tensile properties of bimodal Al alloy are extremely sensitive to VFCG, yield strength and strain hardening exponent of CG Al.Specifically, as VFCG increases, both yield strength and ultimate tensile strength (UTS) of the bimodal Al alloy decreases, while uniform strain of bimodal Al alloy increases. In addition, an increase in yield strength of CG Al results in an increase in both yield stress and UTS of bimodal Al alloy and a decrease in uniform strain of bimodal Al alloy. The lower capability in lowering the increase of stress concentration in NG Al due to a higher yield strength of CG Al causes the lower uniform strain of the bimodal Al alloy. When strain hardening exponent of CG Al increases, 0.2% yield stress, UT5, and uniform strain of the bimodal Al alloy increases. This can be attributed to the increased work-hardening ability of CG Al with a higher strain hardening exponent.     

Enhanced mechanical properties in an Al-Cu-Mg-Ag alloy by duplex aging

A type of duplex aging heat treatment was developed to improve the mechanical properties at room temperature and elevated temperatures in a pre-strained Al-Cu-Mg-Ag alloy. In contrast to the conventional T8 temper at 165 °C and 200 °C, the hardening response of the alloy to aging was increased by duplex aging treatment, the ultimate tensile strength and yield strength of duplex aging temper were improved by approximately 3-7%, which was attributed to the fact that the recovery of dislocations occurred and the precipitation of θ′ phase was restrained effectively at high aging temperature, and more Ω precipitates were formed during secondary aging.     

AZ31B镁合金管材热态内压成形性能的研究

为了研究变形镁合金AZ31B管材的热态内压成形性能,通过单向拉伸测试了不同温度和应变速率下其力学性能的变化,通过胀形实验研究了温度对内高压成形性能的影响,以及相应变形条件下微观组织的变化.实验结果表明:在20～300℃时,AZ31B的屈服强度和抗拉强度随着温度的升高而降低,总伸长率随着温度的升高而提高,均匀伸长率随着温度的升高先增大后减小;当应变速率在0.001～0.1s-1时,屈服强度和抗拉强度随应变速率的增大而升高,总伸长率随着应变速率的增大而减小,均匀伸长率随着应变速率的增大先增加后减小;当温度在20～250℃时,镁合金管材的极限胀形率随温度的升高先增大后减小,在175℃时达到最大值.微观组织观察表明,175℃下不完全动态再结晶和孪晶两种微观组织的出现是使镁合金管材极限胀形率提高的主要原因.     

Influences of Ag and Au Additions on Structure and Tensile Strength of Sn-5Sb Lead Free Solder Alloy

It is important, for electronic application, to decrease the melting point of Sn-5Sb solder alloy because it is relatively high as compared with the most popular eutectic Pb-Sn solder alloy. Adding Au or Ag can decrease the onset melting temperature （233℃） of this alloy to 203,5℃ and 216℃, respectively. The results indicate that the Sn-5Sb-i.5Au alloy has very good ultimate tensile strength （UTS）, ductility, and fusion heat, which are better than both those of the Sn-5Sb-3.SAg and Sn-5Sb alloys. The formation of intermetallic compounds （IMCs） AuSn4 and Ag3Sn enhanced the SbSn precipitates in the solidification microstructure microstructure stability, while retained the formation of thus significantly improved the strength and ductility For all alloys, both UTS and yield stress （σy） increase with increasing strain rate and decrease with increasing temperature in tensile tests, but changes of ductility are generally small with inconsistent trends.     

Effect of strain rate and temperature on strain hardening behavior of a dissimilar joint between Ti–6Al–4V and Ti17 alloys

The aim of this study was to evaluate the influence of strain rate and temperature on the tensile properties, strain hardening behavior, strain rate sensitivity, and fracture characteristics of electron beam welded (EBWed) dissimilar joints between Ti–6Al–4V and Ti17 (Ti–5Al–4Mo–4Cr–2Sn–2Zr) titanium alloys. The welding led to significant microstructural changes across the joint, with hexagonal close-packed martensite (α′) and orthorhombic martensite (α″) in the fusion zone (FZ), α′ in the heat-affected zone (HAZ) on the Ti–6Al–4V side, and coarse β in the HAZ on the Ti17 side. A distinctive asymmetrical hardness profile across the dissimilar joint was observed with the highest hardness in the FZ and a lower hardness on the Ti–6Al–4V side than on the Ti17 side, where a soft zone was present. Despite a slight reduction in ductility, the yield strength (YS) and ultimate tensile strength (UTS) of the joints lay in-between the two base metals (BMs) of Ti–6Al–4V and Ti17, with the Ti17 alloy having a higher strength. While the YS, UTS, and Voce stress of the joints increased, both hardening capacity and strain hardening exponent decreased with increasing strain rate or decreasing temperature. Stage III hardening occurred in the joints after yielding. The hardening rate was strongly dependent on the strain rate and temperature. As the strain rate increased or temperature decreased, the strain hardening rate increased at a given true stress. The strain rate sensitivity evaluated via both common approach and Lindholm approach was observed to decrease with increasing true strain. The welded joints basically failed in the Ti–6Al–4V BM near the HAZ, and the fracture surfaces exhibited dimple fracture characteristics at different temperatures.