热压缩铝合金LY12流变应力的影响因素分析

采用Ｇｌｅｅｂｌｅ－１５００热力模拟机高温等温压缩实验,研究了铝合金ＬＹ１２高温塑性变形时的流变应力行为,研究结果表明,应变速率和变形温度的变化明显影响合金稳态流变应力的大小,且变形温度、应变速率、变形程序对流变应力也有一定的影响。     

铝合金7050高温流变应力特征及本构方程

在高温分离式Hopkinson压杆装置进行高温冲击压缩试验，研究航空铝合金7050—77451在温度范围200—550℃及应变率范围1400—2800s’内压缩变形时的流变应力变化和特征。结果表明，流变应力随着温度的升高而降低，随应变率的升高而增大。温度对流动应力的影响较应变率对流动应力的影响更为显著。用修正的Johnson—Cook模型建立7050-T7451铝合金的本构方程，描述了该合金材料高温下流变应力、应变与应变率之间的关系。     

Al-10Sn-4Si合金高温塑性变形的流变应力特征

采用高温压缩试验法,测定了新型Ａｌ－１０Ｓｎ－４Ｓｉ合金高温变形过程的真应力一直应变曲线;在温度为１００－４００℃范围和应变速率为０．０１－１．０ｓ＾－１范围的变形条件下,研究了该合金的流变应力变化规律。结果表明,Ａｌ－１０Ｓｎ－４Ｓｉ合金为正应变速率敏感材料,表现出稳态流变特征：稳态流变阶段,流变应力基本保持不变;稳态流变应力随变速率的增加而增大,随变形温度的升高而降低,进一步分析表明,这种稳态     

石墨烯增强铝基复合材料的热变形本构方程研究

采用热模拟实验机对石墨烯增强7075铝合金复合材料进行高温热压缩实验,变形温度为300～450℃、应变速率为0.001～1 s^-1,分析其在不同应变速率及温度条件下的高温流变应力特征,并以实验数据为基础,通过函数拟合确定包含应变、应变速率和温度等变形参数的双曲正弦本构方程。研究结果表明：铝基复合材料热压缩变形时流变应力随应变增加迅速增大,达到峰值应力后略有下降且出现锯齿状波动;给出的双曲正弦本构方程可以较好地描述流变应力与应变、应变速率及温度之间的关系,计算值与实验值吻合良好。     

Al-Si-Cu-Mg-Ni活塞合金热压缩变形行为研究

针对高功率柴油发动机活塞在高温下变形和烧蚀严重,导致活塞早期失效,使用寿命不能满足设计要求的问题,文中采用光学显微镜(OM)、透射电子显微镜(TEM)和热模拟实验机等实验仪器,研究了在不同热压缩变形参数下,Al-Si-Cu-Mg-Ni活塞合金显微组织以及流变应力的变化规律,利用Zener-Hollomon参数的双曲正弦函数来描述Al-Si-Cu-Mg-Ni活塞合金热压缩变形流变应力行为。研究结果表明:该合金在高温压缩变形过程中存在动态回复和动态再结晶现象,流变应力值随应变速率的增大而增大,随温度的升高而减少;在高温低应变速率下,组织形貌由于动态再结晶而形成完整的亚晶结构;该合金的热变形激活能Q=294.08 kJ·mol~(-1),建立了Al-Si-Cu-Mg-Ni活塞合金热压缩变形条件下的流变应力本构方程。     

原位颗粒增强钛基复合材料高温流变行为

通过等温热压缩实验,研究了原位合成TiB和TiC增强Ti基复合材料在550°C~750°C、0.0001s~(-1)~0.0004s~(-1)应变速率条件下的高温流变行为。结果表明:该复合材料在高温塑性变形时,压缩流变应力随变形温度的提高而降低,随应变速率的提高而提高;材料的软化机制以动态回复为主,动态再结晶为辅;利用Arrhenius方程模型结合Zener-Hollomon修正参数计算出材料的热变形参数,建立了双曲正弦形式的本构方程。     

AZ81E镁合金的高温流变应力模型及热加工图研究

在应变速率为0．003—3．0s^-1、温度为340～430℃的变形条件下,采用Gleeble-1500热模拟机对AZ81E镁合金进行高温热压缩变形特性研究。结果表明：流变应力随变形温度的升高和应变速率的降低而减小,峰值应力随温度的降低和应变速率的升高向应变较大处转移,进入稳态阶段的临界应变明显增大。结合Arrhenius方程并引入Zener-Hollomon参数,构建AZ81E镁合金的高温流变应力模型,其平均变形激活能为166．15kJ／mol。根据材料动态模型,计算并分析AZ81E镁合金的热加工图。利用热加工图确定热变形的流变失稳区,获得试验参数范围内的热变形过程最佳工艺参数：热加工温度范围为380～420℃,应变速率范围为0．01～0．03S^-1.     

HAL62—3—3—0.7合金的高温本构方程

采用压缩试验法研究了HAL62-3-3-0.7合金的热变形规律，在不同的变形参数条件下，根据其真实σ-ε曲线拟合了可以反映HAL62-3-3-0.7合金流变应力与各变形参数之间关系的高温本构方程，研究结果表明：HAL62-3-3-0.7合金热变形的流变应力随温度的升高和应变速率的降低而减小，在变形过程中，应力很快达到高峰，而后出现软化过程，其真实σ-ε曲线趋于平缓，证明该合金在高变形速率的条件下动态再结晶过程十分明显。     

挤压态ZK60镁合金的高温力学性能及其超塑性

针对挤压态ZK60镁合金的高温力学性能及其超塑性行为进行了研究.结果表明,挤压态ZK60镁合金的高温力学性能与试验温度、应变速率密切相关.通常,屈服强度和抗拉强度随试验温度的降低和应变速率的增加而提高,而延伸率则随试验温度的升高和应变速率的降低而增大.塑性变形流变应力与温度的倒数之间呈线性关系,而且在应变速率为5×10-4/s下的激活能为93 4kJ/mol.     

1050铝合金热压缩变形道次间软化规律

在Gleeble—1500热模拟试验机上，采用高温等温压缩试验，对1050铝合金两道次间的软化规律进行了研究。结果表明，在热压缩变形两道次间保温停歇之后，流变应力出现了明显的软化现象，保温时间越长，合金软化率越高；变形及停歇保温温度越高，合金软化越严重。     

Deformation behavior and microstructure of an Al-Zn-Mg-Cu-Zr alloy during hot deformation

The hot deformation behavior and microstructures of Al-7055 commercial alloy were investigated by axisymmetric hot compression at temperatures ranging from 300°C to 450°C and strain rates from 10-2 to 10 s-1,respectively.Microstructures of deformed 7055 alloy were investigated by transmission electron microscopy (TEM).The dependence of peak stress on deformation temperature and strain rate can be expressed by the hyperbolic-sine type equation.The hot deformation activation energy of the alloy is 146 kJ/mol....     

Deformation Behavior of 6063 Aluminum Alloy During High-Speed Compression

The deformation behavior characteristics of 6063 aluminum alloy were studied experimentally by isothermal compression tests on a Gleeble- 1500 thermal-mechanical simulator. Cylindrical specimens of 14mm in height and 10mm in diameter were compressed dynamically at temperatures ranging from 473 to 723K and at higher strain rntes from 5 to 30s^-1. It is fouud that the flow curves not only depend on the strain rate and temperature but nlso on the dynamic recovery aud recrystallization behavior. The results show that the flow stress decreased with the increase of temperature, while increased with the increase of strain rate. The discontinuous dynamic recrystallization （DDRX） may take place at a high strain rate of 20s^-1 under the tested conditions. At 30s^-1 , the flow curve can exhibit,flow softening due to the effect of temperature rise that raised the temperature by aboat 32K in less than 0.05s.     

AZ31B镁合金和6065铝合金动态压缩行为数值模拟

为了研究帽状试样AZ31B镁合金和6065铝合金在动态压缩变形过程中的温度、应力与应变演变规律,采用Johnson-Cook本构方程和累积塑性损伤方程进行了数值模拟,运用有限元软件ANSYS/LS-DYNA模拟了AZ31B镁合金和6065铝合金帽状试样的动态变形过程.结果表明,两种合金的裂纹萌生和扩展过程相似,局域化变形带内塑性应变由内向外对称分布.相比于AZ31B镁合金,6065铝合金的塑性应变影响区域更为狭小,其应变和应变率硬化效果更强.6065铝合金的变形温度能够达到其动态再结晶临界点,因而易于绝热剪切带的形成.     

Flow stress behavior of Al-Cu-Li-Zr alloy containing Sc during hot compression deformation

The flow stress behavior of Al-3.5Cu-1.5Li-0.25（Sc＋Zr） alloy during hot compression deformation was studied by isothermal compression test using Gleeble-1500 thermal-mechanical simulator. Compression tests were preformed in the temperature range of 653-773 K and in the strain rate range of 0.001-10 s^-1 up to a true plastic strain of 0.7. The results indicate that the flow stress of the alloy increases with increasing strain rate at a given temperature,and decreases with increasing temperature at a given imposed strain rate. The relationship between the flow stress and the strain rate and the temperature was derived by analyzing the experimental data. The flow stress is in a hyperbolic sine relationship with the strain rate,and in an Arrhenius relationship with the temperature,which imply that the process of plastic deformation at an elevated temperature for this material is thermally activated. The flow stress of the alloy during the elevated temperature deformation can be represented by a Zener-Hollomon parameter with the inclusion of the Arrhenius term. The values of n,α and A in the analytical expressions of flow stress σ are fitted to be 5.62,0.019 MPa^-1 and 1.51×10^16 s^-1,respectively. The hot deformation activation energy is 240.85 kJ/mol.     

Prediction of 2A70 aluminum alloy flow stress based on BP artificial neural network

Recently ,withtherapiddevelopmentofthecompu tationtechnique ,thefiniteelementmethodisappliedmoreandmoretothenumericalsimulationofthemetalformingprocess .Therelationshipbetweenflowstressanddeformationconditionssuchasstrain ,strainratesandtemperatures,whichembodiestheresponseofamaterialtothedeformationparameters ,isveryimportantforthenumericalsimulationbyfiniteelementmethod .Butduringthehotdeformationprocess ,therearemanyfactorsthatinfluencetheflowstressofthemetal .Theeffectsofthesefactorsonthef…     

TC4钛合金在不同温度下的剪压缩失效

利用Fallwerk试验装置,在高应变率(102s-1)下,采用动态剪压缩试验研究TC4钛合金不同温度下的剪压缩失效现象。通过试验发现:相同温度下,流变应力随应变的增大不断增加,到达峰值后发生应力塌陷,即剪切失效;相同应变下,温度越高,材料的屈服强度和流变应力均明显下降,且峰值应力向应变增大的方向移动,即塑性变形能力逐渐加强;温度升高,材料的剪切失效能力减弱,在673 K至873 K温度区间内存在一个温度极限值。在该极限值以下,材料易发生剪切失效。同时,根据试验数据拟合了峰值应力和最大塑性应变与温度的曲线方程,为钛合金的研究提供了理论依据。     

Flow stress behavior and processing map of Al-Cu-Mg-Ag alloy during hot compression

The hot deformation behavior of Al-Cu-Mg-Ag was studied by isothermal hot compression tests in the temperature range of 573-773 K and strain rate range of 0.001-1 s^-1 on a Gleeble 1500 D thermal mechanical simulator. The results show the flow stress of Al-Cu-Mg-Ag alloy increases with strain rate and decreases after a peak value, indicating dynamic recovery and recrystallization. A hyperbolic sine relationship is found to correlate well the flow stress with the strain rate and temperature, the flow stress equation is estimated to illustrate the relation of strain rate and stress and temperature during high temperature deformation process. The processing maps exhibit two domains as optimum fields for hot deformation at different strains, including the high strain rate domain in 623-773 K and the low strain rate domain in 573-673 K.     

Flow stress equation for multipass hot-rolling of aluminum alloys

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Microstructure and flow stress of Mg-12Gd-3Y-0.5Zr magnesium alloy

The microstructure and flow stress of the Mg-12Gd-3Y-0.5Zr magnesium alloy was investigated by compression test at temperatures ranging from 350 to 500 ℃ and the strain rates ranging from 0.01 to 20 s-1. The flow stress of the magnesium alloy increased with strain rate and decreased with deformation temperature. Flow stress can be expressed in terms of the Zener-Hollomon parameter Z, which describes the combined influence of the strain rate and temperature using an Arrhenius function.The values of the deformation activation energy were estimated to be 245.9 and 171.5 kJ/mol at deformation temperatures below 400 ℃ and above 400 ℃, respectively. Two constitutive equations were developed to quantify the effect of the deformation conditions on the flow stress of the magnesium alloy. The effects of deformation temperature and strain rate on the microstructure of the magnesium alloy were also examined and quantified by measuring the volume fraction of dynamically recrystallized grain Xd. Xd increased with increasing of deformation temperature. When the deformation temperature was below 475 ℃, Xd decreased with strain rate until it reached 0.15 s-1, then it increased again. When the deformation temperature was above 475 ℃, Xd increased with strain rate.     

碳化硅颗粒增强6168铝基复合材料热变形本构关系

利用Gleeble-3500热模拟试验机研究碳化硅颗粒增强6168铝基复合材料(SiCp/6168Al)在变形温度为340~540 ℃、应变速率为0.001~10 s-1、真应变为0.7的条件下的热变形行为。结果表明:应变速率和变形温度对流变应力有明显的影响,在应变速率相同的条件下,流变应力随变形温度的升高而降低,相同的变形温度下,随应变速率的增加,流变应力也随之升高。采用双曲正弦模型求解SiCp/6168Al复合材料在不同真应变ε下的材料常数,并使用5次指数函数拟合出n、lnA、α和Q与真应变ε的关系式,建立流变应力σ与真应变ε的本构方程。利用该方程可以计算任意变形条件下的流变应力,该模型能较好地反映该复合材料的实际热变形行为。