7075铝合金热压缩过程变形行为和载荷研究

采用MMS-300多功能材料试验机对7075铝合金在变形温度300-450℃、应变速率0．01～40s^-1下单道次压缩过程进行了实验研究,并根据其流变曲线对热压缩过程进行了数值模拟,分析了变形速度、温度和摩擦对变形栽荷的影响规律。结果表明：7075铝合金变形过程发生了动态再结晶,应力-应变曲线表现出波浪形,波动周期大致相同,振幅随着应变增加逐渐减小;变形速度较小时,变形速度增加,临界应变增加,变形速度增加到一定程度时临界应变反而降低。随着变形速率增加和变形温度降低,载荷增加,而摩擦对7075铝合金热压缩过程的栽荷影响不大;当变形速率增加到一定值时,载荷值对速度敏感度降低。     

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...     

6013铝合金热变形行为研究

以6013铝合金为试验材料,采用热压缩镦粗法,在Gleeble-1500热模拟试验机上进行等温热压缩试验.结果表明:随变形速率增加和变形温度降低,合金的流变应力增加.随变形程度增加,流变应力先迅速增加到一峰值,然后缓慢下降到渐趋平稳,呈现明显动态再结晶特征.该合金的流变应力行为可用包含Arrhenius项的Zener-Hollomon参数来描述,其变形激活能Q为145.75kJ/mol.     

6061铝合金板材锯齿形屈服行为的研究

对6061铝合金板材锯齿形屈服行为中应力跌幅、跌落时间等多个特征物理量随应变率的变化规律进行了系统的研究,探讨了锯齿形行为对材料力学性能的影响。结果表明,应力跌幅个数,跌落时间及其个数,再加载时间及其个数均随着应变率的增大而逐渐减少;当应变率为1.4×10-3s-1时,6061铝合金板材的锯齿形屈服行为最弱,板材的力学性能最好。     

Al-35Si高硅铝合金热变形行为的研究

采用Gleeble-1500热模拟机对电子封装用Al-35Si高硅铝合金进行了恒温和恒应变速率下的热压缩变形实验,温度范围为370～550℃,应变速率为0.05～0.45s-1,得到了其真应力-真应变曲线.结果表明:在实验范围内,此合金的流变应力随变形温度的升高、应变速率的降低而降低,在不同变形条件下真应力软化机制分别受动态回复和动态再结晶控制,并且应变速率敏感性指数m随温度的升高呈上升趋势.     

铝合金盒形件充液成形法兰变形特性及其失稳影响分析

通过有限元模拟和实验对铝合金盒形件充液成形过程进行研究,分析了铝合金盒形件充液成形法兰直边区和圆角区的变形特性,以及法兰变形对起皱和破裂等失稳形式的影响.结果表明:法兰圆角区变形复杂,存在径向压应力,根据变形特征可分为五个变形区;长直边法兰抗皱能力比短直边法兰小,容易起皱;短直边侧壁变薄量大,在与凸模圆角相切处的板料容易破裂;合理的压边间隙可以有效控制长直边法兰起皱和短直边侧壁破裂,实验结果证明了数值模拟结果的准确性.     

铝合金板材热成形-淬火一体化工艺研究进展

为解决铝合金室温塑性差和成形后热处理变形的问题,发展起来了一种铝合金板材热成形-淬火一体化新工艺。该工艺是将热处理和热成形在同一工步完成,即固溶后板材快速转移到模具中成形,然后完成模内淬火,最后通过时效来提高其强度。高温成形可提高板材成形性能,模内淬火能够保证其强度和尺寸精度。重点介绍了铝合金板材热成形-淬火一体化工艺关键技术及最新研究进展,总结了铝合金板材热成形-淬火一体化工艺实验研究和数值模拟的研究现状。     

热变形中的动态回复过程

本文提出了动态回复型金属在热变形过程中应力—应变曲线的数学模型,并与实验数据进行了详细比较,结果证明理论曲线与实验曲线符合甚好。     

铝合金汽车顶盖充液成形的数值模拟

目的研究铝合金汽车顶盖拉延工序的充液成形工艺。方法基于有限元分析软件Dynaform,利用带局部刚性凹模整形的被动式充液成形工艺,通过建立有限元分析模型,优化成形过程中的关键工艺参数,分析变形规律并进行质量控制。结果成形过程中的液室压力加载路径、压边力、拉延筋,以及坯料形状等工艺参数对成形影响较大。液室压力不宜过早加载。液室压力过大或压边力过小不利于顶部产生充分塑性变形。压边力过大极易造成顶盖圆角处的破裂。结论该成形工艺可行,且数值模拟的准确性及适用性较高,采用该成形工艺可得到表面质量良好,未出现起皱、破裂缺陷的合格零件。     

LD7铝合金热变形研究

在Gleeble-1500热模拟机上对LD7铝合金进行等温热变形实验,变形温度为300～500℃,应变速率为0.01～10s-1,研究其热变形的流变应力行为、显微组织及软化机制.结果表明LD7铝合金真应力-真应变曲线表现出动态回复特征,在应变速率ε=1.0s-1,变形温度高于420℃时,应力出现锯齿波动,表现出不连续动态再结晶特征.合金在压缩过程中主要软化机制为动态回复,同时也存在动态再结晶.变形后晶粒尺寸随变形温度升高而增大,随变形速率增加而减小.     

内压对镁合金差温内压成形起皱行为的影响

针对镁合金管材热态内压成形存在的壁厚不均、膨胀率小等问题,本文提出利用温度差控制变形的差温内压成形新方法,沿管材轴向建立了具有不同温度梯度的温度场,开展非均匀温度场作用下的镁合金管材塑性失稳起皱行为研究,研究了内压对镁合金差温内压成形起皱参数的影响规律。当恒定内压8MPa时,成形后形成均匀的三个皱纹;采用线性增加的内压补料,成形后仅形成均匀的两个皱纹。恒定内压下轴向补料有助于形成更均匀的多点起皱,变内压轴向补料会改变起皱临界条件,提高了成形区材料的稳定性,抑制后续皱纹的形成。     

Investigation of the corrosion behavior of aluminum bronze alloy in alkaline environment

In this study, the effect of amino-based additives including ammonia, ethanolamine and a mixture of two additives on the pH change of condenser water and corrosion behavior of aluminum bronze alloy as a structural material of condenser were investigated. The results of polarization curves, wheel tests and inductively coupled plasma showed that by increasing the pH from 8.5 to 10.5, the corrosion rate of aluminum bronze alloy and the dissolution rate of alloying elements are increased. The effect of amino-based additives at the same pH is similar to each other. A comparison of corrosion rates determined by polarization curves. The corrosion rates for solutions contained ammonia and ethanolamine additives at pH = 10.5, were 2.92 ⋅ 10⁻² and 4.55 ⋅ 10⁻² mm/y respectively. The wheel test results indicated that the corrosion rates of solutions containing different additives increased to 1.1028 mm/y and 0.4504 mm/y for solutions containing ammonia and ethanolamine, respectively. Therefore, due to similar environmental conditions in the condenser and the wheel test because of the presence perturbation and biphasic fluid, it can be concluded that at pH above 10, aluminum bronze alloy has lower corrosion rate in the cooling water containing ethanolamine than ammonia additives.     

激光冲击2024 铝合金诱导动态应力应变实验研究

为了研究激光冲击波动态加载过程中金属材料的动态应力应变特性,采用高功率激光器单次冲击2024 铝合金薄板,利     

Hot deformation behavior of an extruded Mg-Li-Zn-RE alloy

A new Mg-7.8%Li-4.6%Zn-0.96%Ce-0.85%Y-0.30%Zr alloy has been developed. α phase, β phase and RE-containing intermetallics formed in the alloy. It is found that the alloy can easily be extruded at 260 °C with σ_0.2 = 256 MPa, σ_b = 260 MPa and δ = 14%. Hot deformation behavior of the extruded alloy was studied using the processing map technique. Compression tests were conducted in the temperature range of 250-450 °C and strain rate range of 0.001-10 s⁻¹ and the flow stress data obtained from the tests were used to develop the processing map. The different efficiency domains and flow instability region corresponding to various microstructural characteristics have been identified as follows: (1) Domain I occurs in the temperature range of 250-275 °C and strain rate range of 1-10 s⁻¹, with a peak efficiency of about 50% at 250 °C/10 s⁻¹. Incomplete DRX process has occurred in β phase and DRX process hardly occurs in α phase; (2) Domain II occurs in the temperature range of 250-275 ?C and strain rate range of 0.001-0.003 s⁻¹, with a peak efficiency of about 42% at 250 °C/0.001 s ⁻¹. Incomplete DRX process has occurred in β phase and α phase; (3) Domain III occurs in the temperature range of 400-450 °C and strain rate range of 1-10 s⁻¹, with a peak efficiency of about 42% at 450 °C/10 s⁻¹. Complete DRX process has occurred in β phase and α phase. No cracking, cavity and band of flow localization are observed in flow instability region. The optimum parameters for hot working of the alloy are 250 °C/10 s⁻¹ and 250 °C/0.001 s⁻¹, at which fine dynamic recrystallization microstructure will be achieved. RE-containing intermetallics and α phase accelerate the DRX process in β phase. The softer β phase reduces the driving force for DRX process in α phase, so DRX process in α phase is retarded.     

石墨烯增强铝基复合材料的制备及热变形研究

为了探究石墨烯增强铝基复合材料的制备工艺及其热变形行为,本文采用湿混球磨结合真空热压烧结法制备了0.5wt.％石墨烯增强铝基复合材料,并利用场发射扫描电子显微镜、能谱仪和X射线衍射仪对其进行微观组织观察、成分和物相分析,用Gleeble 3800热模拟机对复合材料进行等温压缩试验,建立了材料的本构方程并分析其热变形机理...     

2A16 铝合金锥形件多级充液热成形仿真及优化分析

目的解决2A16铝合金锥形件常温充液成形困难、表面质量差的问题。方法介绍了充液热成形工艺,并提出了3种锥形件成形方案,通过专用有限元软件Dynaform对所有方案进行了数值仿真;同时,对一步成形方案进行了试验。结果通过试验验证了有限元模型的正确性。由仿真分析可知,成形缺陷包括悬空区起皱和凹模圆角及底部破裂,一步成形方案不可取,两步成形方案均可以将减薄率控制在13%以下。起皱危险主要发生在零件法兰以下30~55 mm处。结论充液热成形与常温充液成形相比,可以显著提高材料的成形性;两步充液热成形方案可以获得2A16铝合金锥形件;预成形凸模的形状设计对零件的表面质量影响明显;最终确定用先热冲压筒形件,后充液热成形的工艺方案,来成形2A16铝合金锥形件。     

7075-H18铝合金板材的淬火敏感性与等温转变行为EI北大核心CSCD

以2 mm厚的7075-H18高强度铝合金板材为研究对象,采用微观组织分析、显微硬度测试、动力学建模与计算相结合的方法,对板材的淬火敏感性、等温相变行为及转变动力学进行系统研究,构建"时间-温度-性能"关系图。结果表明:7075-H18板材具有较高的淬火敏感性。"时间-温度-性能"关系图的鼻尖温度约为350℃,孕育期仅为0.23 s,淬火敏感温度区间为271~404℃,转变量为0.5%的曲线对应的临界线性冷却速率为969.7℃/s,超过了冷模淬火所能达到的冷却速率。板材在等温淬火过程中主要形成粗大的η平衡相,等温时间越长,晶内与晶界的η相尺寸越大,晶界η相越趋于连续分布,且无沉淀析出带变宽。基于实验数据构建的等温转变动力学模型,对7075-H18板材的等温相变过程进行准确预测,板材在350℃等温过程中沉淀相的析出速率最大,等温相变类型为"形核-长大"型相变,相变过程为层片状沉淀相的长大、增厚及互相吞并。理论计算结果与透射电子显微镜下观测到的η相特征以及"时间-温度-性能"关系图相一致。     

Study on plastic deformation behavior of hot splitting spinning of TA15 titanium alloy

The plastic deformation behavior of hot splitting spinning of TA15 titanium alloy is a complex metal forming problem with multi-factor coupling interactive effects. In this paper, on condition of considering various thermal effects, a three-dimensional (3D) elastic–plastic coupled thermo-mechanical finite element (FE) model of hot splitting spinning of TA15 titanium alloy is established using the dynamic, temp-disp, explicit module of FE software ABAQUS. Based on the analysis of flow behaviors of TA15 titanium alloy, the mechanism and influence of materials plastic deformation behavior during the forming process are studied. The results show that, the flow stress of TA15 titanium alloy generally decreases with the increase of deformation temperature; at the same strain rate, the higher temperature is, the lower flow stress is. The temperature distributions along the circumferential direction of disk blank are even and the temperature of plastic deformation area is about 984 °C. The heat from plastic deformation and friction at local plastic deformation area is less than the dissipated heat, so the temperature just falls into approximately 945 °C. Radial spinning force as the driving force of plastic deformation increases gradually and reaches about 35 kN at the end. The maximum value of equivalent stress is presented in fillet part between disk blank and two mandrels. The distributions of equivalent plastic strain appear the large strain gradients and the obvious characteristics of inhomogeneous deformation. When friction factor on interfaces between disk blank and dies ranges from 0.4 to 0.6, the forming quality and precision are highest.     

应变速率对(Zr72Cu16.5Ni11.5)90Al10大块非晶合金超塑性变形行为的影响

通过合理配置成分及优化工艺参数,用铜模吸铸法成功制备出具有室温超塑性变形能力的(Zr72Cu16.5Ni11.5)(90)Al(10)大块非晶合金,并对其塑变效应进行研究,结果表明,在4.2×10-4-6.0×10-5s(-1)应变速率范围内合金试样均呈现出室温超塑性,即经历85.5%工程应变或193.1%真应变仍无脆...