温态超声冲击强化对AA6061-T6空蚀行为的影响

目的 进一步提高超声冲击处理对AA6061-T6抗空蚀性能的强化效果。方法 通过不同温度（RT、50、100和150℃）温态超声冲击强化处理,结合冲击强化与动态应变时效（DSA）的优点,获得应变速率更高、密度位错更高的塑性变形强化层,以提高其抗空蚀性能。利用X射线衍射技术（XRD）、金相显微镜研究了强化层的微观组织。利用显微硬度仪研究了强化层深度方向的硬度分布。利用超声振动空蚀平台、扫描电子显微镜（SEM）和激光共聚焦显微镜,研究了强化试样的空蚀性能及空蚀机理。结果 随温度的升高,强化后的铝合金近表层分别形成30、50、70、90μm的晶粒细化层,表面择优取向由（200）转变为（111）;强化温度为50℃时的表面显微硬度最高,较原始试样提高了108.2%;经300 min空化腐蚀后,常温、50、100、150℃条件下处理的超声冲击试样的抗空蚀性能分别是未处理试样的1.77、2.03、1.49和1.38倍;温态冲击强化后,试样的空化腐蚀损伤机制不仅包括初始的韧性断裂破坏,还增加了脆性及疲劳损伤形式。结论 经过温态超声冲击强化处理后,AA6061-T6的抗空蚀性能随温度的升高呈先增后减的趋...     

AA6061-T6与AZ31合金异种搅拌摩擦焊接头的微观组织

研究了AA6061-T6和AZ31合金异种搅拌摩擦焊接头的微观组织。在异种搅拌摩擦焊接AA6061-T6与AZ31合金时,采用偏置条件,即将搅拌针插入时偏向AZ31合金,从而得到异种对接接头。通过预备实验来优化搅拌针的前进速度、旋转速度。运用电子背散射衍射技术观察搅拌区的纹理,并得到粒径分布和错位角分布,在搅拌区存在相对精细的晶粒结构。在AA6061-T6搅拌区出现随机或弱面取向,而在AZ31搅拌区出现旋转底面取向。再结晶颗粒的平均尺寸只有2．5～4．5μm。与基础合金相比,在AA6061-T6搅拌区的大角度晶界的分数增大,而在AZ31搅拌区的小角度晶界的分数降低。     

Static shear strength and fatigue life of refill friction stir spot welded AA 6061-T6 sheets

This study was aimed at evaluating the static shear strength and fatigue properties of the newly developed refilled friction stir spot welded AA 6061-T6 joints. The keyhole, the process disadvantage of conventional friction stir spot welding, was refilled successfully, using an additional filler plate, with specially designed tools. Two different tool profiles, namely, convex and concave, were used for the refilling process. Sound and defect free joints were obtained by the refilling process. Joints refilled with convex tools showed better static shear strength than those with the concave ones. The variation of microhardness in different regions of the weld was analysed. Fatigue tests were conducted on the lap shear specimens at a stress ratio of R?=?0·1. The optical micrographs of the welds after fatigue failure in both the conventional and refilled processes were examined to study the fatigue crack propagation and failure modes.     

6061-T6铝合金单轴时间相关循环变形行为

对6061-T6铝合金进行系统的单轴应变循环和应力循环实验，揭示该材料在室温和高温下的循环变形行为，讨论环境温度、加载速率、峰，谷值保持对其应变循环特性及棘轮行为的影响。结果表明，6061-T6铝合金表现出弱的循环软化特性，其棘轮行为不仅依赖于平均应力和应力幅值的大小，还依赖于加载历史。尽管该合金的单拉行为对应变率的变化不敏感，但其循环变形行为却体现出明显的时间相关特性，即；应变循环下，在峰／谷值有保持时的响应应力幅值明显小于没有保持时的值，且随着保持时间的增加，响应应力幅值将进一步减小；应力循环下，在峰值有保持时产生的棘轮应变比没有保持时的值大，且随着峰值保持时间的增加及应力率的降低，棘轮应变明显增大。     

回填搅拌摩擦点焊和传统搅拌摩擦点焊AA6061-T6接头的微观结构和力学性能的比较

在搅拌摩擦点焊过程中,通过添加填充板来改善摩擦成形过程,这种新工艺被称为回填搅拌摩擦点焊。分别采用回填搅拌摩擦点焊和传统的搅拌摩擦点焊工艺焊接AA6061-T6搭接焊样品,研究搅拌头的旋转速度对接头的力学性能和金相组织的影响。在不同的旋转速度下,回填搅拌摩擦点焊接头的静态剪切强度都比传统搅拌摩擦点焊接头的好。这归因于在回填搅拌摩擦点焊时,添加了填充板从而有更多的材料来填充孔洞,消除了形成的孔洞缺陷,从而使点焊焊核区的有效截面积增加。借助扫描电镜观察讨论了材料的失效机制,分析了断裂表面形貌。2种焊接接头的硬度曲线都呈W形,最小的硬度出现在热影响区。     

Corrosion behaviors of Al-Si-Cu-based filler metals and 6061-T6 brazements

The corrosion behaviors of a series of Al-Si-Cu-based filler metals and the 6061-T6 butt joints brazed with these filler metals are evaluated by polarization tests and immersion tests in a 3.5% NaCl aqueous solution. For comparison, a traditional Al-12Si filler metal is also employed. The results indicate that the Al-Si-Cu-based filler metals before brazing possess much higher corrosion current densities and pitting tendencies than the Al-12Si filler metal. However, brazing of the 6061-T6 alloy with an Al-12Si filler metal produces a wider butt joint, which, in this case, creates a more extensive corrosion region. Severe galvanic corrosion occurs at the 6061-T6 joints when brazed with Al-Si-Cu-based filler metals. However, in the case of the 6061-T6/Al-12Si brazements, selective corrosion of the Al-12Si eutectic phase can be observed. The bonding strengths of the 6061-T6 butt joints brazed with various filler metals are also measured before and after the immersion tests.     

Brazeability of the 6061-T6 aluminum alloy with Al-Si-20Cu-based filler metals

The bond strength of the 6061-T6 aluminum alloy brazed with Al-12Si, Al-9.6Si-20Cu, and Al-7Si-20Cu-2Sn filer metals at a low temperature of 550°C is evaluated. The fractography of these brazements after tensile tests was observed using scanning electron microscopy (SEM). It was found that joints with good integrity can be produced with Al-7Si-20Cu-2Sn filler metal because it can be used in a temperature range of 504 to 526 °C, about 70 °C lower than the traditional Al-12Si filler metal. It was shown that joints of 6061-T6 aluminum alloy as the base metal, when brazed at 550 °C for 60 min using this new filler metal and ward, and after being subjected to a T6 treatment, possessed a high bonding strength of about 121 Mpa.     

Cold hole expansion effect on the fatigue crack growth in welds of a 6061-T6 aluminum alloy

Compact test specimens were extracted from a 6061-T6 aluminum alloy welded plate with a thickness of 9 mm to analyze the cold hole expansion effect on fatigue crack growth tests conducted in mode I cyclic loading. At R = 0.1, a sharp crack in base metal, weld metal and heat affected zone was propagated from 17 to 24 mm. The fatigue crack growth at 24 mm (α = a/W = 0.3) was delayed by drilling a hole at the crack tip and applying a cold hole expansion of 4.1%. The residual stress fields due to cold hole expansion were determined with the finite element method. The fatigue crack growth testing was continued up to a crack length of 35 mm (α ∼ 0.43) at the same R, and crack opening displacements of the post-expansion crack were also determined with the finite element method. The results were expressed in terms of crack length versus number of cycles, as well as, fatigue crack growth rate as a function of applied and effective stress intensity factor range. The cold hole expansion contributed to delay the fatigue crack growth in base metal, and to a lesser extent in the weld metal and heat affected zone. A crack closure effect was determined by means of load versus crack opening displacement curves of the post-expansion crack, which was, completely or partially closed, in welded zones with compressive residual stress fields. The fracture surfaces of each welded zone were analyzed to elucidate the crack nucleation zone and its relation with the residual stress field. In all cases the crack was initiated at the surface of the specimen where the residual stresses were positive.     

6061-T6铝合金高温本构模型及温成形数值模拟

基于6061-T6铝合金在高温变形过程中的动态回复、动态再结晶及变形硬化特性,分析其在不同温度阶段的黏塑性特征,在高温阶段进一步引入软化因子修正传统Field-Backofen模型,使之适用于铝合金温成形的热力本构描述。通过NAKAJIMA凸模胀形数值仿真及试验对比发现:高低温(25~400℃)相结合的软化型热拉伸本构方程可以准确地描述板料破裂前的集中软化特征,且可以有效满足6061铝合金高温成形性能的仿真需求。     

析出硬化AA7022-T6铝合金高温流变行为的本构模型（英文）

在温度623～773 K和应变速率0.01～1 s^-1条件下,采用等温压缩试验研究析出硬化AA7022-T6铝合金的热力学行为。结果表明,动态再结晶是主要的热变形机制,特别是在高温和低应变速率下。采用改进的JohnsonCook (J-C)模型和应变补偿Arrhenius模型预测不同变形条件下的热流变行为。这两种模型的线性相关系数分别为0.9914和0.9972,平均相对误差(ARE)分别为6.074%和4.465%,均方根误差(RMSE)分别为10.611和1.665 MPa。结果表明,应变补偿Arrhenius模型能准确预测AA7022-T6铝合金的热流变应力。