研究T6处理、深冷处理和T6+深冷处理对ZCuAl 10 Fe 3Mn 2合金微观组织、力学性能以及在室温至450℃下的热疲劳行为。通过XRD,OM,SEM,EDS对合金组织和裂纹形貌进行观察分析。结果表明:T6+深冷复合处理工艺能够显著改善ZCuAl 10 Fe 3Mn 2...研究T6处理、深冷处理和T6+深冷处理对ZCuAl 10 Fe 3Mn 2合金微观组织、力学性能以及在室温至450℃下的热疲劳行为。通过XRD,OM,SEM,EDS对合金组织和裂纹形貌进行观察分析。结果表明:T6+深冷复合处理工艺能够显著改善ZCuAl 10 Fe 3Mn 2合金的力学性能和微观组织。与T6处理相比,其抗拉强度、硬度以及伸长率分别提高了7.28%,16.96%和23.53%;其α相进一步细化且分布更加均匀,位错密度增加,使得合金整体的组织均匀性、致密性更好。综合性能的提高也有效地提高了合金的热疲劳性能,其抗热应力和氧化腐蚀的能力增强。在相同冷热循环次数下,疲劳裂纹长度最短,裂纹生长速率最慢。展开更多
The materials used in variable temperature conditions are required to have excellent thermal fatigue performance.The effects of laser shock processing(LSP),solid solution and aging treatment(T6),and cryogenic treatmen...The materials used in variable temperature conditions are required to have excellent thermal fatigue performance.The effects of laser shock processing(LSP),solid solution and aging treatment(T6),and cryogenic treatment(CT)on both microstructure and thermal fatigue performance of ZCuAl_(10)Fe_(3)Mn_(2) alloys were studied.Microstructure and crack morphology were then examined by scanning electron microscopy(SEM)and energy-dispersive X-ray spectroscopy(EDS).The result showed that,after being subjected to the combination treatment of T6+CT+LSP,the optimal mechanical properties and thermal fatigue performance were obtained for the ZCuAl_(10)Fe_(3)Mn_(2) alloy with the tensile strength,hardness,and elongation of 720 MPa,300.16 HB,and 16%,respectively,and the thermal fatigue life could reach 7,100 cycles when the crack length was 0.1 mm.Moreover,the ZCuAl_(10)Fe_(3)Mn_(2) after combination treatment shows high resistance to oxidation,good adhesion between the matrix and grain boundaries,and dramatically reduced growth rate of crack.During thermal fatigue testing,under the combined action of thermal and alternating stresses,the microstructure around the sample notch oxidized and became loose and porous,which then converted to micro-cracks.Fatigue crack expanded along the grain boundary in the early stage.In the later stage,under the cyclic stress accumulation,the oxidized microstructure separated from the matrix,and the fatigue crack expanded in both intergranular and transgranular ways.The main crack was thick,and the path was meandering.展开更多
文摘研究T6处理、深冷处理和T6+深冷处理对ZCuAl 10 Fe 3Mn 2合金微观组织、力学性能以及在室温至450℃下的热疲劳行为。通过XRD,OM,SEM,EDS对合金组织和裂纹形貌进行观察分析。结果表明:T6+深冷复合处理工艺能够显著改善ZCuAl 10 Fe 3Mn 2合金的力学性能和微观组织。与T6处理相比,其抗拉强度、硬度以及伸长率分别提高了7.28%,16.96%和23.53%;其α相进一步细化且分布更加均匀,位错密度增加,使得合金整体的组织均匀性、致密性更好。综合性能的提高也有效地提高了合金的热疲劳性能,其抗热应力和氧化腐蚀的能力增强。在相同冷热循环次数下,疲劳裂纹长度最短,裂纹生长速率最慢。
基金National Natural Science Foundation of China(51801076)Natural Science Research of Jiangsu Higher Education Institutions of China(18KJB430009)+1 种基金Jiangsu Province Postdoctoral Science Foundation(1601055C)Senior Talents Research Startup of Jiangsu University(14JDG126)。
文摘The materials used in variable temperature conditions are required to have excellent thermal fatigue performance.The effects of laser shock processing(LSP),solid solution and aging treatment(T6),and cryogenic treatment(CT)on both microstructure and thermal fatigue performance of ZCuAl_(10)Fe_(3)Mn_(2) alloys were studied.Microstructure and crack morphology were then examined by scanning electron microscopy(SEM)and energy-dispersive X-ray spectroscopy(EDS).The result showed that,after being subjected to the combination treatment of T6+CT+LSP,the optimal mechanical properties and thermal fatigue performance were obtained for the ZCuAl_(10)Fe_(3)Mn_(2) alloy with the tensile strength,hardness,and elongation of 720 MPa,300.16 HB,and 16%,respectively,and the thermal fatigue life could reach 7,100 cycles when the crack length was 0.1 mm.Moreover,the ZCuAl_(10)Fe_(3)Mn_(2) after combination treatment shows high resistance to oxidation,good adhesion between the matrix and grain boundaries,and dramatically reduced growth rate of crack.During thermal fatigue testing,under the combined action of thermal and alternating stresses,the microstructure around the sample notch oxidized and became loose and porous,which then converted to micro-cracks.Fatigue crack expanded along the grain boundary in the early stage.In the later stage,under the cyclic stress accumulation,the oxidized microstructure separated from the matrix,and the fatigue crack expanded in both intergranular and transgranular ways.The main crack was thick,and the path was meandering.
