新型Al-Zn-Mg-Sc-Er-Zr合金的热变形行为EI北大核心CSCD

采用Gleeble-3800热模拟机研究Al-8.9Zn-1.3Mg-0.1Sc-0.1Er-0.1Zr铝合金的热变形行为,构建温度380~440℃、应变速率0.01~10 s^(-1)区间内合金的热加工图,使用X射线衍射(XRD)、选区电子衍射(SAED)与能谱(EDS)对合金中存在的物相进行分析,并使用金相显微镜(OM)和透射电子显微镜(TEM)观察合金热变形后的微观组织。结果表明:合金的最佳热加工工艺参数区间为:400℃相似文献   

具有层片状α相组织的TB8钛合金热变形行为及本构方程

主要研究具有层片状α相组织的TB8钛合金在α+β双相区的热变形行为。结果表明,在应变速率为1s-1时,变形温度为650℃的流变曲线展现出连续的流变软化,当温度高于650℃时,流变曲线呈现出不连续屈服现象。不连续屈服现象随变形温度的增加和应变速率的降低而消失。当应变速率为0.001s-1时,750℃和800℃的流变曲线呈现出典型的动态再结晶特征。峰值应力σp,温度T和应变速率ε·三者之间的关系已通过Arrhenius-type本构方程进行表征,建立了材料常数α,A,n和Q值与真应变之间的关系模型,并分析了应变对α,A,n和Q值的影响。α值随真应变的增加而增加,而A,n和Q的值随真应变的增加而逐渐降低。实验应力值和预测应力值之间的相关系数和平均相对误差参数分别为0.945和9.08%。这表明本工作建立的应变补偿的热变形本构方程能够很好地预测具有层片状α相组织的TB8钛合金在α+β双相区热变形过程中的流变应力。     

锻态TB6钛合金β相区压缩变形行为和动态再结晶

使用圆柱形试样在Thermecmaster-Z型热模拟试验机上进行锻态TB6钛合金β相区的热压缩实验(变形温度950~1100℃,应变速率0.001~1 s^-1),研究了合金的高温压缩变形和动态再结晶行为。结果表明,这种合金在β相区的变形激活能为246.7 kJ/mol,其热变形机制是动态再结晶,动态再结晶新晶粒的主要形核机制是弓弯形核。当应变速率为0.01~0.1 s^-1、变形温度为<1000℃时动态再结晶的发展比较充分,变形组织明显细化;当变形温度高于1000℃、应变速率低于0.001 s^-1时,动态再结晶的晶粒明显粗化。在动态再结晶的晶粒尺寸D与Z参数之间存在着相关性,其函数关系为D=6.44×10²·Z^-0.1628。     

Cu-2.32Ni-0.57Si-0.05P合金热压缩变形研究

在Gleeble-1500D热模拟试验机上,对Cu-2.32Ni-0.57Si-0.05P合金在应变速率为0.01～5s-1、变形温度为600～800℃、最大变形程度为60%条件下,进行恒温压缩模拟实验研究.分析了实验合金在高温变形时的流变应力、应变速率及变形温度之间的关系,研究了变形温度对合金显微组织的影响.计算了合金高温热压缩变形时的应力指数n、应力参数α、结构因子A以及平均热变形激活能Q.结果表明:合金的流变应力随变形温度升高而降低,随应变速率提高而增大.热变形过程的流变应力可用双曲正弦本构关系来描述.当变形温度高于750℃时,合金流变曲线呈现出明显的动态再结晶特征,合金显微组织为完全的动态再结晶组织.合金的热加工宜在应变速率为0.1～1s-1、温度为700～800℃范围内进行.     

Mg-9Al-3Si-0.375Sr-0.78Y合金的热变形行为及本构模型

利用Gleeble-3500热模拟试验机对Mg-9Al-3Si-0.375Sr-0.78Y合金试样进行等温恒应变速率压缩实验,研究其在温度250~400℃、应变速率0.001~10s~(-1)条件下的热变形行为。结果表明:在热变形过程中,峰值应力随着应变速率的降低和温度的升高而减小,且峰值应力对应变速率的敏感性随着变形温度的下降而增强。建立了考虑应变的热变形Arrhenius本构模型,模型精度良好,在300,350℃及0.001~10s~(-1)范围内,模型的平均绝对误差分别为1.57%和1.76%;合金的平均变形激活能为183.58k J/mol,平均应变速率敏感指数为0.1616。热变形过程中,α-Mg相呈现明显的动态再结晶特征,β-Mg₁₇Al₁₂相尺寸减小且分布均匀,初生Mg_2Si相较小。在低温(250~300℃)变形时,动态再结晶仅发生在晶界处。在高温(350~400℃)变形时,初生α-Mg晶粒发生了明显的动态再结晶。随着温度的增加和应变速率的降低,再结晶程度提高,再结晶晶粒逐渐长大。     

Dynamic recrystallization behavior of GH4169G alloy during hot compressive deformation

The microstructure evolutions and nucleation mechanisms of GH4169 G alloy were studied by optical microscope, electron backscatter diffraction (EBSD) and transmission electron microscope (TEM). The hot compression tests were performed different imposed reductions in the range of true strain from 0.12 to 1.2 at the temperatures of 930 ℃-1050 ℃ with strain rates of 0.01 s⁻¹-1 s⁻¹. It is found that cumulative and local misorientation increase firstly and then decrease when the strain is increased due to the progress of dynamic recrystallization (DRX). The low angle boundaries (LAGBs) rapidly develop to high angle boundaries (HAGBs) at relatively high deformation temperature or the low strain rate. There are three DRX mechanisms observed for GH4169 G alloy during hot deformation. Discontinuous dynamic recrystallization (DDRX) as the dominant mechanism for GH4169 G alloy is characterized by typical necklace structures and bulged-original boundaries. Besides, different deformation bands with dislocation cells formed in deformed matrix at low temperature and large strain, which indicates that continuous dynamic recrystallization (CDRX) contributed to the DRX process. The twin boundaries lost their coherent characteristics and provide sites for nucleation, which also accelerates the nucleation of DRX.     

基于动态再结晶37CrS4特种钢的流变应力预测模型

使用Gleeble-1500D热模拟实验机对37CrS4特种钢进行单道次热压缩实验,研究了37CrS4钢在950～1100℃和0.01 s-1～10 s-1条件下的热压缩流变应力行为.结果 表明:这种钢的真应力应变曲线出现了明显的高温塑性变形动态再结晶行为;热变形后的微观组织为典型的板条状马氏体,发生动态再结晶行为的临...     

HMn62-3-3合金的热变形行为及热加工图

通过Gleeble-1500热模拟机在500~600℃、应变速率0.01~10s~(-1)条件下的近等温热模拟压缩试验,建立合金本构方程和热加工图。结果表明:HMn62-3-3合金在热变形过程中发生动态再结晶行为,其峰值应力随变形温度的升高或应变速率的降低而降低;采用Arrhenius方程能够较好地拟合HMn62-3-3合金的流变行为,其热变形激活能为201.525kJ·mol~(-1);根据DMM模型,计算并建立了HMn62-3-3材料的热加工图,由此确定热变形过程中的最佳工艺参数为变形温度610~640℃,应变速率为2~10s~(-1)。     

TB6钛合金β区变形的动态再结晶动力学

使用圆柱形TB6钛合金试样在Thermecmaster-Z型热模拟试验机上进行热模拟压缩实验(变形温度为825~1100℃,应变速率为0.001~1 s^-1)。对采集的流变数据进行加工硬化率处理,确定动态再结晶体积分数,研究了TB6钛合金β区变形的动态再结晶动力学。结果表明,流变应力随着变形温度的降低或应变速率的提高而增大,流变曲线呈现出动态再结晶类型的特征。随着应变速率的降低和变形温度的提高,动态再结晶的体积分数和晶粒尺寸增大。在变形温度高于950℃、应变速率低于0.001 s^-1条件下,动态再结晶的晶粒严重粗化。动态再结晶动力学曲线经历缓慢增加—快速增加—缓慢增加三个阶段,呈现出典型的“S”型特征。确定了动态再结晶的体积分数达到50%时的应变,建立了TB6钛合金的动态再结晶动力学模型。     

9Mn27Al10Ni3Si低密度钢的高温压缩变形行为及其机制

使用Gleeble热模拟试验机、XRD、OM、SEM和TEM等手段研究了9Mn27Al10Ni3Si低密度钢在850~1050℃和0.01~5 s^-1条件下的热压缩变形特征及其机制。结果表明,对这种钢在850~950℃进行低应变速率(0.01~1 s^-1)热压缩时,κ-碳化物的析出和粗化以及在热压缩过程中摩擦系数的增大使其应变达到临界值后流变应力明显增大;随着应变速率的提高,实验钢的孪生显著增强,显著加快了奥氏体的动态再结晶过程,使其在高应变速率热压缩时动态再结晶的程度比低应变速率压缩时更为显著。再结晶的软化作用,使上述流变应力异常增大的现象逐渐减弱甚至消失。     

Effect of temperature on deformation behavior and microstructures of TC11 titanium alloy

The isothermal compression deformation behavior of TC11 titanium alloy with beta microstructure was studied between 750 °C and 1100 °C under the strain rate ranging from 0.001 s⁻¹ to 10 s⁻¹ by THERMECMASTOR-Z simulator. In addition, the effect of temperature on microstructure was observed using optical microscope. The results showed that the temperature greatly affected the flow stress and microstructure of TC11 titanium alloy cooled from beta phase region in air. During hot deformation of TC11 titanium alloy, the steady state flow characteristic was observed at higher temperature or lower strain rate. In the α + β phase region, spheroidization fraction of α lamellar decreased with increasing temperature, while in near-β and β phase regions, dynamic recrystallization fraction increased with increasing temperature in all strain rates except at the strain rate of 0.001 s⁻¹.     

基于修正的Arrhennius方程钛合金高温本构方程研究

为了更准确地描述钛合金的高温变形行为,对Arrhennius方程进行修正得到钛合金高温本构方程.通过对一种新型钛合金在热模拟试验机上进行恒应变速率等温压缩实验,研究其在700~1 000℃、应变速率0.01~10 s-1条件下的热变形行为,分析了材料的真实应力-真实应变曲线.采用最小二乘拟合的数据回归处理,得到该钛合金在α+β双相区和β单相区的热变形激活能,并通过引入温度变量,获得了Arrhennius方程参数A随温度变化的函数关系,建立了该材料的高温流变应力本构方程.实验结果表明,随着变形增加,流变应力开始急剧增加,随后出现软化并趋于稳态,同时峰值应力对于温度和应变速率具有很强的敏感性.通过在Arrhenius方程中引入温度变量,有利于提高本构方程的准确性.     

轧制态7A60铝合金的热压缩显微组织及流变行为

对轧制态7A60铝合金在应变速率为0.1~0.01s-1、变形温度为250~350℃条件下热压缩的显微组织特征和流变应力进行实验研究。结果表明:随着应变速率的降低和温度的升高,材料的各向异性减弱,均匀性增强,晶粒发生明显粗化;在热变形的过程中该合金的主要软化机制为动态回复和动态再结晶,峰值应力随应变速率的增加而增大,随温度的升高而降低,在应变速率为0.01s-1时发生了明显的非连续动态再结晶行为。合金热变形的流变应力行为可用双曲正弦函数来表示,其热激活能为438.981kJ/mol。     

新型Al-Zn-Mg-Cu合金热变形组织演化

采用Gleeble-1500D热力模拟试验机研究新型Al-Zn-Mg-Cu高强铝合金在变形温度为300~450℃,应变速率为0.001~10s~(-1)条件下的热变形组织演化。利用光学显微镜(OM)和透射电子显微镜(TEM)观察合金不同热变形条件下的组织形貌特征。结果表明:随着变形温度的升高和应变速率的减小,位错密度减小,亚晶粒尺寸增大;合金热压缩变形过程中主要的软化机制为动态回复和动态再结晶。变形温度为300~400℃时,主要发生动态回复;变形温度为450℃,应变速率为0.001~10s~(-1)时,软化机制以动态再结晶为主,存在晶界弓出、亚晶长大、亚晶合并3种再结晶形核机制。     

Dynamic recrystallization behavior of Ti–5Al–5Mo–5V–1Cr–1Fe alloy

Dynamic recrystallization process was considered as an important method to fabricate titanium workpieces with desired properties. The objective of this study was to investigate dynamic recrystallization behavior of Ti–5Al–5Mo–5V–1Cr–1Fe alloy through isothermal compression experiments. The volume fraction of dynamic recrystallization was quantified with the net softening effect by dynamic recrystallization (DRX). The saturated stress during hot deformation process was analyzed based on dislocation evolution influenced by working-hardening and dynamic recovery. The linear relationship between the saturated stress and peak stress has been obtained. The dependence of DRX process on deformation parameters has been discussed in detail and a model based on Avrami kinetics has been proposed to track DRX process with strain. A constitutive model incorporating DRX process has been proposed to describe the flow curves at large strains.     

Al2O3弥散强化铜合金轧制性能试验研究

通过热模拟试验机对Al2O3弥散强化铜合金在不同温度、不同应变速率、相同变形量条件下进行热压缩试验,分析了Al2O3弥散强化铜合金应力-应变关系,依据动态材料理论和试验数据绘制弥散铜热加工图,并选取了3组试验温度进行热轧试验验证.结果表明,不同的应变速率变形机制不一致,分别通过不连续屈服和动态再结晶实现塑性变形;轧制试验验证了该合金最佳变形区温度为750~850℃、应变速率为1~10s-1.     

Research on the hot deformation behavior of Ti40 alloy using processing map

The deformation behavior of a Ti40 titanium alloy was investigated with compression tests at different temperatures and strain rates to evaluate the activation energy and to establish the constitutive equation, which reveals the dependence of the flow stress on strain, strain rate and deformation temperature. The tests were carried out in the temperature range between 900 and 1100 °C and at strain rates between 0.01 and 10 s⁻¹. Hot deformation activation energy of the Ti40 alloy was calculated to be about 372.96 kJ/mol. In order to demonstrate the workability of Ti40 alloy further, the processing maps at strain of 0.5 and 0.6 were generated respectively based on the dynamic materials model. It is found that the dynamic recrystallization of Ti40 alloy occurs at the temperatures of 1050-1100 °C and strain rates of 0.01-0.1 s⁻¹, with peak efficiency of power dissipation of 64% occurring at about 1050 °C and 0.01 s⁻¹, indicating that this domain is optimum processing window for hot working. Flow instability domains were noticed at higher stain rate (≥1 s⁻¹) and stain (≥0.6), which located at the upper part of the processing maps. The evidence of deformation in these domains has been identified by the microstructure observations of Ti40 titanium alloy.     

一种新型近β型Ti-5.5Mo-6V-7Cr-4Al-2Sn-1Fe合金热变形行为

采用Gleeble-3800型热模拟试验机对一种新型近β型Ti-5.5Mo-6V-7Cr-4Al-2Sn-1Fe(质量分数/%)钛合金进行等温恒应变速率压缩实验。变形温度范围为:655~855℃,应变速率范围为:0.001~10s^-1 ,最大真应变为0.8。根据实验数据,建立了该合金的高温流变应力模型,计算出热变形激活能约为255kJ/mol,并绘制出热加工图。结合热加工图与材料的显微组织分析可知,在高应变速率(1~10s^-1 )条件下变形时,在热加工图上表现为材料的功率耗散值(η)低,为失稳区域,易产生绝热剪切带与局部塑性流动、开裂等现象。在应变速率小于0.01s^-1 和相变点( T β)温度以下(655~755℃)进行热变形时,组织变化主要以动态回复为主;在应变速率小于0.01s^-1 和 T β以上(755~855℃)进行热变形时,组织发生动态再结晶,且随着温度的升高,新产生的再结晶晶粒逐渐长大。在相变点附近(755~770℃),变形速率为0.001~0.003s^-1 区域内变形时,功率耗散值达到最大值,组织发生动态再结晶,该区域为合金热变形的“安全区”。     

Hot Deformation Behavior of an As—cast Duplex Stainless Steel

The hot deformation behavior of an as-cast 0Crl7Mnl4Mo2N duplex stainless steel has been studied by hot com-pression test at the temperature range from 1000℃ to 1200℃, and the strain rates are 0.1 s^-1, 1 s^-1 and 5 s^-1,respectively. It was found that during hot deformation there is only dynamic recovery taking place within the δ-ferrite phase, but the γ-austenite phase undergoes dynamic recrystallization. The activation energy of the steel for hot compression is estimated to be 480 kJ/mol.     

热压缩过程中2205双相不锈钢的组织演变和软化机制

在不同变形温度和应变速率条件下对2205双相不锈钢进行高温压缩实验,研究了变形温度、应变速率和变形量对其显微组织中铁素体和奥氏体两相的影响,分析了高温变形软化机制。结果表明：随着变形温度的提高这种钢的峰值应力及其对应的应变逐渐减小。随着变形温度从850℃提高到950℃,2205双相不锈钢显微组织中的铁素体向奥氏体的转变占主导地位;变形温度高于950℃时,随着变形温度的提高铁素体与奥氏体之间的强度水平之差逐渐减小,显微组织中的奥氏体向铁素体的转变占主导地位。在本文的热变形条件下2205双相不锈钢的显微组织中铁素体呈现出与奥氏体不同的软化机制,铁素体的软化机制为动态回复和动态再结晶,而奥氏体因层错能较低其软化只能通过有限程度的动态回复进行。