Preparation of high-strength Al-Mg-Si-Cu-Fe alloy via heat treatment and rolling

An Al-Mg-Si-Cu-Fe alloy was solid-solution treated at 560°C for 3 h and then cooled by water quenching or furnace cooling. The alloy samples which underwent cooling by these two methods were rolled at different temperatures. The microstructure and mechanical properties of the rolled alloys were investigated by optical microscopy, scanning electron microscopy, transmission electron microscopy, X-ray diffraction analysis, and tensile testing. For the water-quenched alloys, the peak tensile strength and elongation occurred at a rolling temperature of 180°C. For the furnace-cooled alloys, the tensile strength decreased initially, until the rolling temperature of 420°C, and then increased; the elongation increased consistently with increasing rolling temperature. The effects of grain boundary hardening and dislocation hardening on the mechanical properties of these rolled alloys decreased with increases in rolling temperature. The mechanical properties of the 180°C rolling water-quenched alloy were also improved by the presence of β″ phase. Above 420°C, the effect of solid-solution hardening on the mechanical properties of the rolled alloys increased with increases in rolling temperature.     

挤压铸造对ZL201性能组织的影响

以铸造铝合金ZL201为研究对象,系统研究了挤压铸造成形工艺条件下,挤压压力、浇注温度、模具温度等工艺参数对合金显微组织和力学性能的影响。实验结果表明,ZL201的挤压铸造组织细密均匀,且随着挤压压力的增大,铸件的组织越加细密;结合实验结果,确定了ZL201合适的挤压工艺参数：浇注温度750℃、挤压压力60MPa、模具温度保持在250℃左右。在合适的工艺条件下,铸件的组织和性能良好,经过T4热处理后,铸件本体试样的抗拉强度和延伸率可以达到310MPa和9.27%。     

Effect of heat treatment on microstructures and properties of a novel Al-Zn-Mg-Cu alloy for oil drilling

In view of the special requirements for strength, heat resistance and corrosion resistance of Al-Zn-Mg-Cu alloy for oil drilling, the Al-6.2 Zn-2.5 Mg-1.6 Cu alloy was prepared by increasing Cu content on basis of Russian Series 1953 alloy. The effect of heat treatment on the microstructures and properties of the alloy was characterized by optical microscope(OM), scanning electron microscope(SEM) and transmission electron microscope(TEM), and investigated by tensile test at room temperature, thermal exposure test and corrosion test. The results show that the strength after T6 aging treatment exhibit a decrease trend as an increase of the solution temperature from465 °C to 480 °C. After the solution treated by the rate of 470 °C/1 h, second phases dissolve into the matrix very well and the strength property reaches optimum. The alloy has better comprehensive properties treated by a solution treatment of 470 °C/1 h and then followed by an aging treatment of 120 °C/24 h + 170 °C/1 h + 120 °C/24 h. Under the aging state, the precipitated phases inside the grains are suitable in size, while on the grain boundary distribute discontinuously and the precipitate-free zone is obvious. Besides, the alloy still maintain high tensile properties. The yield strength, tensile strength and elongation are 650 MPa, 686 MPa,12.0%, respectively. The yield strength retention after heat exposure is 92%. The alloy has good corrosion resistance and the exfoliation corrosion degree. The average corrosion rate in the H_2S and CO_2 environment is 0.0024 mm/a, which is far less than the required 0.12 mm/a. It is insensitive to H_2S and CO_2 environments.     

High temperature tensile properties,fracture behaviors and nanoscale precipitate variation of an Al-Zn-Mg-Cu alloy

In order to assess Al-Zn-Mg-Cu alloys as potential high temperature structural materials,the hardness,tensile properties and fracture behaviors of 7085 Al alloy were investigated at various temperatures from room temperature to 175℃.High-resolution transmission electron microscopy was used to investigate the evolutions of precipitates at different temperatures,particularly on the relationship between microstructural evolution and tensile strength.The results reveal that both the microstructure and mechanical properties of the alloy are quite sensitive to the environmental temperature.As the temperature increases,the hardness and strength decrease while the elongation and reduction of area increase.As tensile testing temperature rises,the strain hardening exponent(n) decreases due to the thermal softening effect.The fracture mode of the alloy transforms from mixture of intergranular and transgranular fracture to completely transgranular dimples when tensile testing temperature reaches 150℃.The precipitate sequence during high temperature tests is coincident with that of aging.With the increase of tensile testing temperature,the mean precipitate radius grows larger,and the distribution of grain boundary precipitates transforms from continuous to discontinuous.     

Improving the tensile properties of extruded Mg–Ga alloy by ageing treatment

A hot-extruded Mg-5Ga alloy was subjected to ageing treatment at 150 ?°C, 190 ?°C and 230 ?°C. The microstructures and mechanical properties of the extruded and aged alloy were examined in this study. Microstructure examinations suggested that particle-shaped and rod-shaped Mg₅Ga₂ were precipitated in the alloy after peak ageing treatment. The extruded alloy showed the yield strength, ultimate tensile strength and elongation to fracture of 157.6 ?MPa, 248.6 ?MPa and 17.5%, respectively. After peak ageing, the yield strength and ultimate tensile strength can be enhanced by as much as 15.7% and 8.6% reaching 182.3 ?MPa and 270 ?MPa, respectively. The improvement of the tensile strengths is mainly attributed to the enhanced precipitation strengthening by newly formed fine Mg₅Ga₂ precipitates. The ductility of the alloy was slightly increased by peak ageing at low temperatures (150 ?°C and 190 ?°C), but remarkably decreased by peak ageing at high temperature (230 ?°C) due to the formation of coarsened Mg₅Ga₂ particles which easily initiated the cracks during tensile deformation.     

Effects of heat treatment on microstructure and mechanical properties of SLMed Sc-modified AlSi10Mg alloy

The influence of heat treatments on the microstructures and mechanical properties of the selective laser melting manufactured AlSi10Mg alloy modified with Sc was systematically investigated. The results showed that the addition of Sc element introduced primary Al₃Sc, which increased the heterogeneous nucleation during the solidification of AlSi10Mg alloy, and then the ultrafine network eutectic structure was obtained, and hence the tensile strength was improved significantly (nearly 23 ​%). During the heat treatment process, the network eutectic structure transformed from continuous to discontinuous, and the grain refinement was weakened with an increasing heating temperature, both of which affected the mechanical properties of the Sc modified AlSi10Mg alloy. The tensile strength decreased from 438 ​± ​10 ​MPa for the Sc-modified alloy to 208 ​± ​6 ​MPa, while the fracture strain significantly increased from 6 ​± ​0.2 ​% to 30.2 ​± ​1.2 ​% when the Sc-modified alloy was heat-treated at 325 ​°C for 12 ​h. It has been found that the desirable microstructure and mechanical properties of SLM Sc-modified AlSi10Mg alloy can be realized by controlling the heat treatment process parameters.     

静态再结晶处理对Co36Fe36Cr18Ni8Ti2合金力学性能与耐腐蚀性的影响

对冷变形后的Co₃₆Fe₃₆Cr₁₈Ni₈Ti₂合金在700 ℃和800 ℃下再结晶退火，制备成具有高强度及良好耐蚀性的多主元合金。采用电子背散射衍射（electron back-scattered diffraction, EBSD）表征了合金的相分布、再结晶组织以及晶界分布等微观结构特征，采用静态拉伸试验测试了合金的力学性能。结果表明，700 ℃退火的合金断后伸长率较低，但其抗拉强度与屈服强度分别达到了1 038和956 MPa。采用电化学工作站与扫描电子显微镜（scanning electron microscope, SEM）表征了合金在模拟体液中的耐蚀性。结果表明，700 ℃退火的样品具有较好的耐蚀性，腐蚀后的样品表面较为均匀。结合力学性能可知，700 ℃退火的样品具有作为新型医用金属材料的潜力。     

6201铝合金管材半固态连续扩展成形实验研究

采用半固态连续扩展成形技术,成功地试制了扩展比为3 52的6201铝合金管材·对其微观组织和力学性能的变化及机理进行了研究·实验表明:出模温度超过510℃时,其组织发生完全再结晶;T6,TA状态半固态连续扩展成形管材的强度随着时效时间的增加呈明显的上升趋势,而延伸率则呈明显的下降趋势·扩展成形工艺的关键在于确保成形终了温度高于520℃,T6状态的管材抗拉强度为299MPa,延伸率为9 4%;TA状态的管材抗拉强度为258MPa,延伸率为12 4%;力学性能演化机理分析表明,采用合适的连续扩展成形工艺与时效处理工艺能保证获得拉伸强度和延伸率匹配最佳的6201母线管材·     

热处理工艺对Mg-RE-Zn-Zr系合金显微组织及力学性能的影响

通过气体保护制备了Mg-RE-Zn-Zr[RE-Ce-40La（wt％）的富铈稀土]合金,并对合金进行了热处理,测试了不同状态下合金的硬度、抗拉强度及伸长率等力学性能,采用光学显微镜、X射线衍射仪及扫描电镜对合金显微组织、拉伸断口进行了分析。结果发现,采用T6热处理工艺后,合金的晶粒尺寸明显细化,硬度、抗拉强度、屈服强度和伸长率显著提高,分别提高了11％,24％,7．3％和102％。     

High temperature tensile properties and fracture behavior of cast nickel-base K445 superalloy

The tensile properties and fracture behavior of a cast nickel-base superalloy K445 in the temperature range of 25-1 000℃were investigated.The microstructure and fracture surfaces of the alloy were investigated by OM,SEM and TEM.The results revealed that an anomalous yield strength phenomenon exists in the alloy at medium high temperature.The yield strength decreases gradually with the increase of temperature,reaches the minimum value at 650℃,and then increases again to obtain 940 MPa,which is almost the ...     

电池包用6061铝合金型材成分与挤压成型性关系

由于现有6061铝合金挤压成型性及力学性能较差，在实际生产中应用范围受限，通过改变合金成分开发新型6061铝合金，将Si的质量分数调整至国标上限0.73%～0.80%，Mg的质量分数调整至国标下限0.82%～0.90%，同时分别设计了多细晶元素（Mn+Cr的质量分数为0.40%）与少细晶元素（Mn+Cr的质量分数为0.14%）两种配比方式，分别命名为6061-A铝合金和6061-B铝合金。通过观察微观组织、测试力学性能、调整挤压速度，研究6061-A铝合金和6061-B铝合金的力学性能、挤压成型性。结果表明，6061-A铝合金挤压成型性更好，同时经（175±5）℃×8 h热处理后，型材屈服强度达到312 MPa，抗拉强度达到325 MPa，伸长率为9%，均高于标准要求。     

Effects of solidification parameters on microstructure and mechanical properties of continuous columnar-grained Cu–Al–Ni alloy

Effects of melt temperature and casting speed on microstructure and mechanical properties of Cu-14%Al-3.8%Ni(mass fraction) alloy wires fabricated by continuous unidirectional solidification technology were investigated.It was found that the average size of columnar grain in the alloy decreased and grain boundary turned clear and straight with increasing the casting speed at a given melt temperature.When the melt temperature was up to 1 280℃,theβ_1 phase gradually transformed into lozenged and lanciformγ...     

钨合金力学行为的计算机数值模拟─—宏观力学性能

在微观力学行为分析的基础上，对90W合金宏观力学性能及其与微观结构因素（粘结相力学参数）之间的关系进行了计算机数值模拟研究．结果表明：钨合金性能与粘结相力学参数密切相关．随着粘结相弹性模量增加，合金的抗拉强度增加，但延伸率降低．当粘结相屈服强度800MPa时，合金抗拉强度随粘结相屈服强度增加而增大，在粘结相屈服度为800MPa时达到最大值．随粘结相抗拉强度增加，合金抗拉强度和延伸率均呈近似线性规律增加．合金延伸率对粘结相应变硬化模量极为敏感．     

微滴喷射法制备植物乳杆菌微胶囊的试验研究

通过对6005A合金铸锭均匀化制度和挤压工模具结构进行调整,来改善挤压制品的晶粒组织结构,进而达到提高6005A铝合金汽车梁挤压制品的力学性能及稳定性的目的。试验结果表明,适当调整铸锭均匀化制度以及减少模具工作带长度,对减轻挤压制品再结晶层厚度有明显作用,即当铸锭均匀化制度调整到510 ℃、保温6 h,降低模具工作带长度至3 mm时,可明显降低挤压型材制品再结晶层厚度,使型材组织更加均匀细小。型材T6状态下屈服强度由274 MPa提升到298 MPa,抗拉强度由291 MPa提升到313 MPa,断后伸长率则由9%提升到15%,达到稳定辊弯加工成形性的目的。     

固溶制度对Al-5.6Cu-1.7Mg-0.2Zr-0.1Sr-0.6Ti合金挤压材组织性能的影响

通过金相组织分析、扫描电子显微镜分析、X射线衍射、硬度、电导率、室温拉伸性能、断后伸长率和抗晶间腐蚀等微观组织观察及性能表征,研究了四种不同固溶制度对Al-5.6Cu-1.7Mg-0.2Zr-0.1Sr-0.6Ti合金微观组织和性能的影响。结果表明：随着固溶温度的升高,合金中的晶粒逐渐变大;当固溶温度低于520℃时,合金中的未溶相的数量和尺寸随着固溶温度的升高而减小;当固溶制度为510℃×2 h+520℃×2 h时,合金中的未溶相开始增多,合金出现轻微过烧,断后伸长率及抗晶间腐蚀性能变差,但抗拉强度最高,达到了490.14 MPa。合金的位错强度和位错贡献值随着固溶温度的升高而减小,合金中的强化效果主要来源于固溶强化和时效析出强化。合金在T6状态下,(490℃×2 h+500℃×2 h)和(500℃×2 h+510℃×2 h)两种不同固溶制度下的抗拉强度和断后伸长率等力学性能和抗晶间腐蚀性能都较优,这两种固溶制度均是适合Al-5.6Cu-1.7Mg-0.2Zr-0.1Sr-0.6Ti合金的固溶制度。     

淬火转移时间对A357 铝合金力学性能与微观组织的影响

 采用OM、DSC、SEM 与TEM,结合力学性能测试研究淬火转移时间对A357 铝合金力学性能与微观组织的影响。结果表明:随着淬火转移时间由3 s 延长至49 s,A357 铝合金经T6 热处理后的抗拉强度、屈服强度与延伸率分别由351 MPa、275MPa 与12.4%降低至320 MPa、254 MPa 与6.5%,合金材料的抗拉强度连续下降,屈服强度变化较小,延伸率呈现出先上升后下降的变化趋势。初生与共晶Si 相逐渐由细长的针状或片层状转变为椭圆球状或棒状,平均长度为10~25 μm,平均宽度为5~10 μm,当淬火转移时间超过35 s 后,初生与共晶Si 相则仍以细长的针状或片层状形貌为主。拉伸断口形貌以韧窝断裂为主,附带部分沿晶断裂,随着淬火转移时间的增加,断口表面韧窝数量随之减少,沿晶断裂裂纹数量不断增加;Mg 与Si 元素集中分布于晶粒边界处的二元与三元共晶组织中,Al 元素广泛分布于晶粒内部及晶粒边界处;人工时效过程析出的Mg₂Si 强化相长度约为0.2~1 μm,宽度为0.02~0.08 μm,且随着淬火转移时间的延长,Mg₂Si 强化相的析出数大量减少,长径比不断下降,合金材料的强度与塑性随之降低。     

Effect of Al on microstructure and mechanical properties of as-extruded Mg–1Mn alloy sheet

The effect of Al addition on microstructure and mechanical properties of hot extruded Mg–1 Mn alloy sheet was investigated. The results revealed that the dynamic recrystallization was promoted by increasing Al content. The ultimate tensile strength and yield strength of the alloy increased with the increase of Al content. The Mg–9 Al–1 Mn alloy exhibited the highest strength, with tensile strength of 308 MPa, 307 MPa, 319 MPa, yield strength of 199 MPa, 207 MPa, 220 MPa and the elongation of 20.9%, 20.1%, 19.2% in 0°, 45°, 90°, respectively.The high strength was mainly attributed to the formation of fine dynamically recrystallized grains and large amounts of the second phase. The strengthening mechanism of the alloys was explained.     

热处理对含Y元素AZ31镁合金板材组织和性能的影响

对含Y元素AZ31镁合金板材进行退火处理后的组织和性能进行了研究.结果表明:随着退火温度的升高,镁合金晶粒尺寸逐渐增大,力学性能略有提高然后降低;退火时间对镁合金晶粒尺寸影响不大;在300℃下退火1 h后板材性能达到最佳,抗拉强度为255 MPa,屈服强度为170 MPa,延伸率为24%;经过热处理后镁合金断裂方式为准解理断裂和韧性断裂的复合形式.     

氩气保护条件下碳对AM60镁合金组织性能的影响

在氩气保护精炼条件下研究了煤粉、石墨粉、碳纤维等形态的碳元素对AM60镁合金组织与性能的影响,探讨了C元素对其合金组织的细化机理。研究结果表明,在AM60镁合金中加入少量不同形态的碳元素能有效地改善其显微组织,使AM60镁合金的铸态室温力学性能有了不同程度的提高;当碳以纤维状态加入时,合金室温铸态力学性能的提高幅度最大,其抗拉强度和延伸率分别达到了242.4 MPa和13.2%,分别在原合金的基础上提高了23%和2.5倍。     

涂层烧结及热处理工艺对GH2O2合金组织性能的影响

研究了涂层烧结及热处理工艺对GH202合金基材组织性能的影响．运用电子拉伸机、扫描电镜及光学显微镜,测定了拉伸试样的力学性能,并分析了试样的显微组织和拉伸断口．试验结果表明,GH202合金在1150℃固溶处理5h后,合金表面进行高温涂层与烧结,在850℃时效6h出炉空冷,合金基体晶粒细小,均匀;强化相γ弥散分布;合金强度提高,塑性改善,拉伸断口为韧性断裂．