Mg-11.21Gd-2.26Y-0.44Zr稀土镁合金热变形行为

采用差热分析、金相显微镜等手段,分析了Mg-11.21Gd-2.26Y-0.44Zr稀土镁合金的微观组织,结果发现,在温度530℃均匀化热处理4h,可使大部分合金元素固溶。采用Gleeble3800热模拟实验机,在温度为320℃～480℃、应变速率为0.001s-1～0.1s-1、最大变形程度为60%的条件下,对该镁合金进行热压缩实验,结果表现,材料流变应力行为和显微组织受到变形温度和变形速率的严重影响;合金的流动应力可以采用Sellars方程形式描述;计算出的变形激活能为225.67kJ.mol-1。     

Mg-Gd-Y-Zr耐热镁合金的压缩变形行为

采用GLEEBLE-1500热模拟机对Mg-Gd-Y-Zr稀土镁合金在温度为300～500℃、应变速率为0.000 1～1.0 s-1、最大变形程度为50%的条件下,进行了恒应变速率高温压缩模拟实验研究,分析了实验合金高温变形时流变应力与应变速率及变形温度之间的关系以及组织变化,计算了塑性变形表观激活能及相应的应力指数,为选择这种合金的热变形加工条件提供实验依据.结果表明:合金的稳态流变应力随应变速率的增大而增大,在恒应变速率条件下,合金的真应力水平随温度的升高而降低;在给定的变形条件下,计算得出的塑性变形表观激活能和应力指数分别为260 kJ/mol和5.6.根据实验分析,合金的热加工宜在400～500℃温度范围内进行.     

Mg-Gd-Y-Mn耐热镁合金的压缩变形行为研究

采用Gleeble-1500热模拟机对Mg-Gd-Y-Mn稀土镁合金在温度为300～500℃、应变速率为0.001～1.0s-1、最大变形程度为60%的条件下,进行恒应变速率高温压缩模拟实验研究.分析了实验合金高温变形时流变应力与应变速率及变形温度之间的关系以及组织变化,计算了表观激活能及相应的应力指数,为选择这种合金的热变形加工条件提供了实验依据.结果表明:合金的稳态流变应力随应变速率的增大而增大,在恒应变速率条件下,合金的真应力水平随温度的升高而降低;在给定的变形条件下,计算得出的表观激活能和应力指数分别为200kJ·mol-1和5.1.根据实验分析,合金的热加工宜在400～500℃温度范围内进行.     

铸态Mg-7Gd-5Y-1.2Nd-Zr镁合金热变形行为研究

针对Mg-7Gd-5Y-1.2Nd-Zr镁合金,研究了其铸态显微组织以及在Gleeble-1500D热模拟机上单向压缩的力学行为。变形速率为0.002~1s-1,变形温度为573~723K,下压量为60%。铸态Mg-7Gd-5Y-1.2Nd-Zr合金组织由α-Mg基体和网状的共晶构成;变形温度和变形速率对合金的峰值应力有明显的影响,在相同温度条件下,峰值应力随变形速率的增加而升高,在相同的应变速率条件下,峰值应力随变温度的升高而降低;高温条件下的共晶组织的软化也是合金变形抗力下降的重要原因;应变速率为0.1s-1时,合金不连续动态再结晶最为明显,合金易于失效;同时计算出了平均热变形激活能Q为243.5kJ/mol和应力指数n为4.1972,分析得出变形激活能直接受到温度的影响,间接受到应变速率的影响。     

Mg-Gd-Y-Zr镁合金热压缩流变应力的研究

采用恒应变速率高温压缩模拟实验，对Mg-Gd-Y-Zr镁合金在应变速率为0．001～1．0s^-1、变形温度为150～500℃条件下的流变应力行为进行了研究，计算了变形激活能及相应的应力指数，建立了峰值流变应力方程。结果表明：在恒温条件下，合金的流变应力随应变速率的增大而增大；在恒应变速率条件下，合金的流变应力随温度的升高而降低；在350-500℃，0．001～1．s^-1的变形条件下，变形激活能和应力指数分别为2215kJ／mol和368；流变应力方程计算出的峰值应力与真实值基本吻合。     

铸态Mg-7Gd-5Y-1．2Nd—Zr镁合金热变形行为研究

针对Mg-7Gd-5Y-1.2Nd-Zr镁合金,研究了其铸态显微组织以及在Gleeble-1500D热模拟机上单向压缩的力学行为,其应变速率为2×10-3～1 s-1,变形温度为573～723 K,压下量为60%.铸态Mg-7Gd-5Y-1.2Nd-Zr合金组织由α-Mg基体和网状的共晶构成;变形温度和应变速率对合金的峰值应力有明显的影响,在相同变形温度条件下,峰值应力随应变速率的增加而升高;在相同的应变速率条件下,峰值应力随变形温度的升高而降低;高温条件下的共晶组织的软化也是合金变形抗力下降的重要原因;应变速率为10-1 s-1 时,合金不连续动态再结晶最为明显,合金易于失效;同时计算出了平均热变形激活能Q为243.5 kJ/mol和应力指数n为4.197 2,分析得出变形激活能直接受到变形温度的影响,间接受到应变速率的影响.     

2519铝合金热压缩变形流变应力行为

在 Gleeble- 15 0 0热模拟机上对 2 5 19铝合金进行等温热压缩实验 ,变形温度为 30 0～ 5 0 0℃ ,应变速率为0 .0 5～ 2 5 s- 1 ,研究其热压缩变形的流变应力行为。结果表明 :2 5 19铝合金真应力 -应变曲线在低应变速率 (ε<2 5 s- 1 )条件下 ,流变应力开始随应变增加而增大 ,达到峰值后趋于平稳 ,表现出动态回复特征 ;而在高应变速率 (ε≥ 2 5 s- 1 )条件下 ,应力出现锯齿波动达到峰值后逐渐下降 ,表现出不连续再结晶特征。在用 Arrhenius方程描述 2 5 19铝合金热变形行为时 ,其变形激活能 Q为 16 7.81k J/ mol     

AZ80镁合金高温热变形流变应力研究

在Gleeble2000热模拟机上对铸态AZ80镁合金在应变速率为0.001～1s-1、变形温度为240～440℃条件下的热压缩变形行为进行了研究.结果表明:AZ80镁合金热压缩变形的流变应力受到变形温度和应变速率的显著影响,可以用Zener-Hollomon参数的双曲正弦函数形式进行描述.本实验条件下,AZ80镁合金热压缩变形时的应力指数n为5,其热变形激活能Q为183 kJ·mol-1,建立了流变应力的数学模型,其结果可为变形镁合金的塑性成形工艺的制订提供更为科学的依据.     

Mg-AI-Zn-Nd稀土镁合金成形性能研究

采用Gleeble-1500D热模拟机对AZ31B-0．8Nd稀土镁合金在应变速率为0．01～1s^-1，温度为300～450℃，最大变形量约为70％的条件下，进行了恒应变速率高温压缩模拟实验，研究了实验合金在高温变形时的流变应力与应变速率及变形温度之间的关系和组织变化。结果表明：合金的流变应力随应变速率的增大而增加．随应变温度的升高而减小；在应变速率和变形温度相同时，挤压态试样的流变应力明显低于铸态试样的流变应力。压缩变形量对应力应变关系的影响很小。探明了镁合金变形软化的主要机制是动态再结晶。根据实验分析，合金的热加工宜在400～450℃温度范围内进行，并且挤压态较铸态更易热挤压成型，更有助于晶粒细化。     

AZ80镁合金热变形流变应力研究

在应变速率为0.001s-1～10s-1,变形温度为200℃～400℃条件下,在Gleeble-3800热模拟机上对AZ80合金的流变应力进行了研究。结果表明,AZ80合金的流变应力强烈地受变形温度的影响,当变形温度低于300℃时,其峰值流变应力呈现幂指数关系;当变形温度高于300℃时,其峰值流变应力呈现指数关系。在该文实验条件下,AZ80合金热变形应力指数n=8.43,热变形激活能Q=165.83kJ/mol。     

Hot-compression constitutive relation of as-cast AZ31 magnesium alloy

In hot-compression process, the various factors have obvious effects on the deformation behavior of AZ31 magnesium alloy deformation behavior. To understand the hot-compression constitutive relation thoroughly, the stress-strain behavior of AZ31 magnesium alloy at various strain rates and different deformation temperatures were investigated under maximum strain of 60%. The microstructure of the experimental alloy was studied in the hot-compression procedure. The experimental results show that the relation of peak flow stress, strain rate and temperature can be described by Z parameter which contains Arrheniues item. The strain rate and the deformation temperature are the key parameters affecting deformation activation energy.     

Hot compression deformation behavior of the Mg-Al-Y-Zn magnesium alloy

The hot deformation behavior of a Mg-Al-Y-Zn magnesium alloy was investigated by hot compressive testing on a Gleeble-1500 thermal simulator at the temperanging from 523 to 673 K with the swain rate varying from 0.001 to 1s-1.The relationships among flow stress,swain rate,and deformation temperature were analyzed,and the deformation activation energy and stress exponent were calculated.Microstructure evolution of the alloy under different conditions was examined.The results indicated that the maximum value of the flow stress increased with the decrease of deformation temperature or the increase of swain rate.Under the present deformation conditions,dynamic recrystallization (DRX) oeettrred in the alloy,which was the main softening mechanism during deformation at elevated temperature.The deformation temperature and strain had significant effects on the microstructure of the alloy.     

Hot compression deformation behavior of the Mg-AI-Y-Zn magnesium alloy

The hot deformation behavior of a Mg-Al-Y-Zn magnesium alloy was investigated by hot compressive testing on a Gleeble-1500 thermal simulator at the temperanging from 523 to 673 K with the swain rate varying from 0.001 to 1s-1.The relationships among flow stress,swain rate,and deformation temperature were analyzed,and the deformation activation energy and stress exponent were calculated.Microstructure evolution of the alloy under different conditions was examined.The results indicated that the maximum value of the flow stress increased with the decrease of deformation temperature or the increase of swain rate.Under the present deformation conditions,dynamic recrystallization (DRX) oeettrred in the alloy,which was the main softening mechanism during deformation at elevated temperature.The deformation temperature and strain had significant effects on the microstructure of the alloy.     

铸态Mg-Nd-Zn-Zr镁合金用腐蚀剂比较

采用光学显微镜和扫描电子显微镜对不同腐蚀剂腐蚀后的Mg-Nd-Zn-Zr镁合金铸态显微组织进行观察。结果表明,Mg-Nd-Zn-Zr合金的铸态组织主要由α-Mg和晶界处的Mg12(Nd, Zn)两相组成,另外还有小块状Mg12(Nd, Zn)相及近圆形的富Zr相区域。1号传统腐蚀剂（4 mL硝酸+96 mL乙醇）可较好显示组织;经2号腐蚀剂（12 g苦味酸+80 mL乙酸+80 mL蒸馏水+350 mL乙醇）腐蚀5 s和10 s后,组织发黑,晶界不明显,但可部分显示出富Zr相区,延长腐蚀时间到20 s,晶粒显现出来,发黑现象得到缓解,富Zr区域明显,但晶界附近出现大量气泡;3号腐蚀剂（60 mL乙二醇+20 mL乙酸+19 mL蒸馏水+ 1 mL硝酸）腐蚀组织表明,其对晶粒的显示效果明显好于2号,然而很难观察到富Zr区域。     

Hot compression deformation behavior of MB26 magnesium alloy

The flow stress features of MB26 magnesium alloy were studied by isothermal compression at 300-450 ℃ and strain rate of 0.001^-1 s J with Gleeble 1500 thermal simulator. In addition, the deformation activation energy Q was calculated. The results show that the strain rate and deformation temperature have obvious effect on the true stress. The peak value of flow stress becomes larger with increasing strain rate at the same temperature, and gets smaller with the increasing deformation temperature at the same strain rate. The alloy shows partial dynamic recrystallization. The flow stress of MB26 magnesium alloy during high temperature deformation can be represented by Zener-Hollomon parameter including the Arrhemius term. The temperatt, re range of 350-400℃ is suggested for hot-forming of this alloy.     

AZ70镁合金热压缩变形特性

在温度为300℃～420℃、应变速率为0.001s-1～1s-1的变形条件下,采用Gleeble-1500热模拟机对AZ70镁合金热压缩变形特性进行了研究。结果表明,合金的流变应力随应变速率的增大而增大,随温度的升高而降低;在给定的变形条件下,计算出合金的变形激活能为132kJ/mol,应力指数为6.2;建立了合金高温变形的本构方程;降低变形温度和提高应变速率可使再结晶晶粒平均尺寸减小。根据实验分析得出,材料的最佳热加工工艺条件为变形温度340℃～400℃,应变速率0.001s-1～0.1s-1,并提出以低速为宜。     

Effect of gadolinium on aged hardening behavior,microstructure and mechanical properties of Mg-Nd-Zn-Zr alloy

Mg-3.4Nd-0.1 Zn-0.40Zr alloy samples with and without containing gadolinium(0.6%,mass fraction)were prepared by sand casting.The aged hardening behavior,solidification microstructures and mechanical properties of the alloys were investigated by using the analysis methods of OM,XRD,TEM,hardness tests and mechanical property tests.The main research results are as follows.1)Compared with the alloy without the addition of gadolinium.the alloys with the addition of gadolinium shows the more remarkable age-hardening response.2) The as-cast microstructure of the alloy with and without containing gadolinium consists of α-Mg grains with Mg12Nd phase on the grain boundary.After solution heat-treatment,Mg12Nd phase of the alloy without containing gadolinium is dissolved in the matrix,however,there iS still discontinued Mg12Nd phase at grain boundary of the alloy with containing gadolinium.The more finely dispersed precipitates in Mg matrix are formed in the alloy with containing gadolinium during age-treatment.3)The room temperature and high temperature mechanical properties ofthe alloy are satisfactory.with σb=280 MPa,σ0.2=165 MPa at RT and aσb=215 MPa,σ0.2=155 MPa at 250℃.The high temperature mechanical properties decrease slightly with the increase of temperature.