5083铝合金表面钛铝基耐蚀涂层与TA2钛合金接触腐蚀

针对5083铝合金与TA2钛合金接触腐蚀问题,采用超音速微粒沉积技术在5083铝合金表面制备Ti-45Al-7Nb-4Cr耐蚀涂层,采用扫描电子显微镜(SEM)和能谱仪(EDS)对涂层截面和与基体界面进行测试,分析涂层孔隙率和与5083铝合金基体的结合机制;采用电化学工作站测试5083铝合金、TA2钛合金、TiAl合金铸锭和涂层的极化曲线,并对比研究5083铝合金、TiAl合金铸锭和涂层与TA2钛合金接触腐蚀敏感性。结果表明:涂层孔隙率为1.4%,涂层与基体结合机制为机械结合,通过在5083铝合金表面制备Ti-45Al-7Nb-4Cr合金防护涂层后,可使材料电极电位由-913.90mV升高到-572.47mV,与TA2钛合金的接触腐蚀电流密度由16.2μA/cm2降为0.21μA/cm2,接触腐蚀敏感性由E级降到A级,解决了铝合金与钛合金的接触腐蚀防护问题。     

搅拌摩擦焊焊接5083铝合金板材焊核区的晶体取向

采用搅拌摩擦焊焊接了5083铝合金板材,借助电子背散射衍射技术和取向成像分析软件,对比性地分析了母材和焊核区的晶粒形貌、取向差分布、织构组分及取向分布函数,分析了焊核区晶体取向的变化.结果表明,在热-力作用下,焊核区发生动态再结晶,显示等轴晶粒形貌,平均晶粒尺寸约为15.8μm,同时大角度晶界比例明显增加.母材的黄铜织构B{011} <211> 和S织构{123} <634> 的比例分别达到30.6%和13.6%以上;搅拌摩擦焊后,焊核区的B织构和S织构的比例分别降至4%和1.8%,原位再结晶形成的R{124} <211> 织构组分约为7.7%,焊核区其它常见面心立方金属织构组分的比例均低于8%,意味着焊核区由强取向组织转变为弱取向组织.     

脉冲激光再制造船用5083铝合金防护板试验研究

针对远洋舰船铝合金防护板受风浪、潮汐以及随机性爆炸冲击波影响,易萌生裂纹或产生断裂的工程实际,通过控制有限单元"生死"状态,动态模拟了防护板脉冲激光再制造温度场变化历程,获取了再制造过程温度变化规律,并对脉冲激光再制造工艺进行了优化。分析和试验结果表明:脉冲模式优化工艺参数为激光功率3 kW,光斑直径3 mm,扫描速度6mm/s,脉冲激光脉宽10 ms,占空比1:1。成形后防护板热影响区变形量控制在0.02 mm以内,硬度(HV0.1)最大值出现在热影响区,约为950 MPa。焊缝区与母材呈致密的冶金结合,主要为致密的细晶组织,抗拉强度达到222 MPa。     

Influence of electric current on superplastic deformation mechanism of 5083 aluminium alloy

5083 aluminium alloy superplastic forming adopted resistance heating can not only improve efficiency and cut energy but also generate electroplastic/electrosuperplastic effect to make the material deformation possess lower flow stress and higher plasticity. By analysing the influence of current on dislocation slipping, grain boundary migration and dynamic recrystallisation, it is found that the electron wind force can enhance the mobility of dislocations; meanwhile, the current also can reduce the activation heat of dislocation motion by joule heating effect. What is more, the grain size of resistance heating forming sample is significantly smaller than furnace heating, and the cavities in the sample become small and dispersive, so the resistance heating forming specimen possesses better performance.     

Unified Principal S-N Equation for Friction Stir Welding of 5083 and 6061 Aluminum Alloys

With the popularization of friction stir welding(FSW),5083-H321 and 6061-T6 aluminum alloy materials are widely used during the FSW process.In this study,the fatigue life of friction stir welding with two materials,i.e.,5083-H321 and 6061-T6 aluminum alloy,are studied.Fatigue tests were carried out on the base metal of these two materials as well as on the butt joints and overlapping FSW samples.The principle of the equivalent structural stress method is used to analyze the FSW test data of these two materials.The fatigue resistances of these two materials were com-pared and a unified principal S-N curve equation was fitted.Two key parameters of the unified principal S-N curve obtained by fitting,Cd is 4222.5,and h is 0.2693.A new method for an FSW fatigue life assessment was developed in this study and can be used to calculate the fatigue life of different welding forms with a single S-N curve.Two main fatigue tests of bending and tension were used to verify the unified principal S-N curve equation.The results show that the fatigue life calculated by the unified mean 50％master S-N curve parameters are the closest to the fatigue test results.The reliability,practicability,and generality of the master S-N curve fitting parameters were verified using the test data.The unified principal S-N curve acquired in this study can not only be used in aluminum alloy materials but can also be applied to other materials.     

5083铝合金的类超塑性行为

研究了冷轧退火状态下Al Mg系5083合金的高温形变行为。结果表明,合金在较宽的温度区间及应变速率范围内显示出高的伸长率。合金在形变过程中,晶粒发生细化。机理研究表明,高伸长率并不是超塑性变形的结果,而是溶质原子拖拽或粘性流动控制蠕变的结果。     

基于最大m值法的商用5083铝合金材料性能测试

采用最大m值法在450、475、500℃下测试商用AA5083合金材料性能,并与恒速度、恒应变速率法拉伸试验结果进行了对比分析.结果表明:该商用AA5083铝合金塑性较差,在450、475、500℃下恒应变速率、恒速度拉伸,伸长率普遍小于100％,超塑性不明显.采用最大m值法测试材料性能,其在450、475、500℃下伸长率分别为105％、107％、154％,但超塑性依然不明显.随着变形程度增大与温度的升高,该商用铝合金原始的长条状组织不断开始断裂并趋于变短,最后变成等轴组织.     

Influence of Zn Content on Microstructures,Mechanical Properties and Stress Corrosion Behavior of AA5083 Aluminum Alloy

To enhance the stress corrosion cracking (SCC) resistance, Zn was utilized as an alloy element to add in the AA5083 aluminum alloys. The effects of Zn content on the microstructures, mechanical properties and SCC resistance were systematically evaluated. The results demonstrate that in the studied range adding Zn can significantly improve the SCC resistance of the AA5083 alloys. This is related to the relatively low amount of continuous β (Al₃Mg₂) phase along grain boundary and the formation of Zn-containing phase such as Al₅Mg₁₁Zn₄ phase. Based on the results, the optimal Zn content with respect to SCC resistance is approximately 0.50 wt.%. Further increasing Zn content results in coarse precipitates discontinuously distributed along grain boundaries.     

Processing,characterization, room temperature mechanical properties and fracture behavior of hot extruded multi-scale B4C reinforced 5083 aluminum alloy based composites

Microstructural characteristics and mechanical behavior of hot extruded Al5083/B₄C nanocomposites were studied. Al5083 and Al5083/B₄C powders were milled for 50 h under argon atmosphere in attrition mill with rotational speed of 400 r/min. For increasing the elongation, milled powders were mixed with 30% and 50% unmilled aluminum powder (mass fraction) with mean particle size of >100 μm and <100 μm and then consolidated by hot pressing and hot extrusion with 9:1 extrusion ratio. Hot extruded samples were studied by optical microscopy, scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS), transmission electron microscopy (TEM), tensile and hardness tests. The results showed that mechanical milling process and presence of B₄C particles increase the yield strength of Al5083 alloy from 130 to 566 MPa but strongly decrease elongation (from 11.3% to 0.49%). Adding <100 μm unmilled particles enhanced the ductility and reduced tensile strength and hardness, but using the >100 μm unmilled particles reduced the tensile strength and ductility at the same time. By increasing the content of unmilled particles failure mechanism changed from brittle to ductile.     

冷轧变形量和退火制度对超快速加热下5083铝合金晶粒尺寸的影响

利用Gleeble-3500 热模拟系统和电子背散射衍射(EBSD)技术对5083 铝合金的超快速退火组织演变规律进行研究,探讨了快速加热速度、退火温度及冷轧变形量对5083 铝合金晶粒尺寸的影响.结果表明,5083 铝合金经80％的冷轧变形后分别以25、250、500℃/s 的加热速度升温至450℃保温3s 后以40...