退火工艺对搅拌摩擦加工镁合金微观组织和显微硬度的影响

采用搅拌摩擦加工(Friction stir processing,FSP)技术对AZ31镁合金进行加工,通过采取不同温度及保温时间的退火工艺,研究了FSP镁合金在退火过程中的微观组织演变过程及硬度变化规律。结果表明,FSP成功制备了细晶AZ31镁合金,其平均晶粒尺寸细化程度达54.9%。当退火温度在200～300 ℃时,加工区(SZ)晶粒尺寸较为稳定,且组织发生不同程度的均匀化和细化;当温度超过300 ℃时,加工区晶粒互相吞噬而快速长大。在退火温度较低、短时间保温时热影响区(HAZ)组织变化不明显,而延长保温时间或者升高温度,HAZ区组织会迅速细化、均匀化;当退火温度超过300 ℃时,再结晶会在短时间内完成,随后晶粒继续长大。在300 ℃下保温60 min为最优退火工艺,可使SZ、HAZ组织分别细化10.9%、35.6%。     

7055铝合金挤压材黑线缺陷分析

利用高倍组织观察,结合能谱分析,对7055铝合金挤压材阳极氧化后的“黑线”缺陷进行了分析。结果表明:“黑线”区域为AlZr聚集导致。通过严格控制原料质量,改善AlZr中间合金组织;在合金成分范围内,适当降低Zr元素的含量;熔炼过程中适当提高加热温度及时间,使Al₃Zr粒子熔解等手段,可消除“黑线”缺陷。     

Effect of Mo on corrosion behavior of Ni20Cr–xMo alloys in air with NaCl–KCl–CaCl2 vapor at 570°C

The effect of Mo on the corrosion behavior of Ni20Cr–xMo alloys in an oxidizing chlorine-containing atmosphere using air mixed with the salt-vapor mixture of NaCl–KCl–CaCl₂ at 570°C was investigated. The results revealed that the corrosion performance of the Ni20Cr alloys in the oxidizing chlorine atmosphere was improved by Mo addition of up to 3 wt%. The Mo-free alloy formed a potassium chromate during corrosion as a result of the reaction between the Cr₂O₃ scale and KCl vapor. The chromate formation increased the chlorine potential at the scale surface and induced the breakdown of the protective Cr₂O₃ scale, resulting in internal chromium chloride precipitates and a Cr-depleted zone. In contrast, the presence of Mo resulted in the formation of a NiO scale, which did not react with the salt vapors and, therefore, prevented the formation of chromates. The beneficial effect of Mo on the high-temperature chlorination of Ni–Cr alloys in salt-vapor-containing atmospheres was ascribed to the suppression of chlorine generation due to NiO scale formation.     

HF刻蚀工艺对AZ91D镁合金疏水膜性能的影响

为了改善AZ91D镁合金表面疏水膜的疏水性,对以HF和N^MoOq为主要成分的刻蚀液进行了研究。通过改变刻蚀温度、刻蚀时间、HF的浓度及Na2MoO4的质量浓度,确定了最佳的刻蚀工艺条件为:HF 0.10 mol/L,Na2MoO41.00 g/L,1525°C,90 so实验结果表明:使用HF刻蚀液可以在镁合金表面形成理想的微纳结构。通过刻蚀构建的微纳结构可以明显提高疏水膜的疏水性。     

Microstructure and hydrogen absorption/desorption properties of Mg24Y3M (M = Ni,Co, Cu,Al) alloys

Ternary alloys with the nominal composition of Mg₂₄Y₃M (M = Ni, Co, Cu, Al) have been fabricated by using vacuum induction melting method. Their microstructure and phase composition are characterized by using X-ray diffraction (XRD) and scanning electron microscopy (SEM). The isothermal hydrogen absorption and desorption kinetics are measured by a Sievert's-type apparatus. The dehydrogenation behaviors of the full hydrogenated alloys are also analyzed by differential scanning calorimetry (DSC) method. Results show that each and every alloy has a distinct multiphase structure containing the main phase Mg₂₄Y₅ and some amount of Mg. Intermetallic compounds of YCo₂ and Al₂Y are detected in the M = Co and M = Al alloy, while long-period stacking ordered (LPSO) phase can be also observed in M = Ni and M = Cu alloy. The hydrogen absorption and desorption kinetics shows a decreased trend in the following order: (M = Ni) > (M = Al) > (M = Co) > (M = Cu). The M = Ni alloy has the best hydrogen storage performance among the investigated alloys. The dehydrogenation activation energy (E_a) of the M = Ni alloy decreases to 66 kJ/mol, and its decomposition peak temperature is also reduced to 313 °C. Moreover, the p–c–T (pressure-composition isotherms) curves of the studied alloys are also discussed.     

钛合金激光清洗及其对激光焊接气孔的影响

采用砂纸打磨、酸洗、激光清洗等方式对Ti6Al4V钛合金进行焊前清洗。通过扫描电镜、白光干涉仪、能谱仪分析了各种清洗方式下的表面形貌、粗糙度和化学成分，研究了不同清洗方式及参数对清洗效果的影响。在均匀熔透和表面质量良好的同一激光焊接条件下，比较了不同清洗条件对气孔率的影响。合适的激光清洗可有效清除焊接试件表面氧化层，并改善表面粗糙度，得到较低的气孔率，其焊缝可达到中国航天工业行业标准I级焊缝要求。     

热处理工艺对TC4钛合金冲击磨损性能的影响

研究了退火和固溶时效处理对热轧态TC4钛合金的力学性能和组织的影响,并考察了其冲击磨损性能。结果表明:退火处理后试样组织中转变β相增加,强度、塑性和韧性均较热轧态有所提升;而固溶时效处理后试样组织的晶粒细化且尺寸更为均匀,同时具有最高的强度,而塑性和韧性则较热轧态有所降低。经过10 h的冲击磨损试验后,退火态试样的磨损率最低,而固溶时效态试样的磨损率最高。通过磨损断口观察发现退火态试样表面冲刷犁沟较短,且终点处存在合金的塑性堆积,同时磨损面组织发生塑性变形,晶粒延展拉长。退火态试样较高的塑性和韧性有助于吸收冲击能量,因此表现出较好的耐冲击磨损性能。     

Corrosion behaviour of AA2024 aluminium alloy in different tempers in NaCl solution and with the CeCl3 corrosion inhibitor

The paper analyses the corrosion behaviour of naturally and artificially aged AA2024 alloy in NaCl solution and in the presence of an environment-friendly corrosion inhibitor, CeCl₃. On the basis of the values of polarisation resistance and corrosion current density, the corrosion resistance of the protective inhibitor film is established as well as the general corrosion resistance of this aluminium alloy. Resistance to pit formation is determined based on the difference in pitting and corrosion potentials while resistance to pit growth is determined based on the amount of charge consumed during pit growth. A scanning electron microscope is used to examine the morphology of the pits formed during the pitting corrosion testing, as well as to determine the cerium content on intermetallic particles and the matrix AA2024 alloy. The corrosion behaviour of AA2024 alloy is investigated after different test periods in NaCl solution and in the same solution with the CeCl₃ inhibitor. The corrosion resistance of both tempers of AA2024 alloy is more than one order of magnitude higher in the presence of CeCl₃. An explanation of the observed differences in the corrosion behaviour of the naturally and artificially aged AA2024 alloy is proposed. Different corrosion behaviour of the alloy after different test periods is also explained.     

薄壁弱刚性钛合金结构件制造工艺

随着新型材料冶金技术的发展与进步,钛合金作为“崛起的第三代金属”已完全替代了铝镁合金和钢构件,成为航天飞行器上应用范围最广的材料之一。从某新研制航天飞行器外部结构件用钛合金材料的特性及切削特点入手,针对薄壁弱刚性钛合金结构件在实际加工过程中遇到的诸多难点,提出了相应的解决办法,并重新设计了零件工装。结果表明,改进措施不仅保证了零件质量,而且提高了零件加工效率,使单件零件的生产周期缩短了近10h。     

微观组织对2A14铝合金轮毂力学性能和腐蚀性能的影响

通过电子背散射衍射(EBSD)、场发射扫描电子显微镜(SEM)、透射电子显微镜(TEM)、室温拉伸、浸泡腐蚀、电化学极化等测试分析方法，研究了2A14铝合金轮毂内部不同区域上微观组织的差异及其对力学性能和腐蚀性能的影响。结果表明，2A14铝合金轮毂的芯部和1/4层的晶粒尺寸分别是113和54 μm，再结晶分数分别是16%和36%。1/4层的合金相和时效析出相的含量都大于芯部，其中两种时效析出相(θ’和Q相)的数量密度均为芯部的2倍左右。芯部具有较大的晶粒尺寸和较少的时效析出相，因此具有较低的力学性能。同时，芯部相对于1/4层具有较少的合金相和较大的晶界相间距，因而芯部的电化学腐蚀和晶间腐蚀倾向均低于1/4层。