时效制度对6013铝合金挤压型材屈强比的影响  

Effect of the aging process on the yield ratio of 6013 aluminum alloy extruded profile

作　　者：张瑞芳 许吉 冯鑫明 赵帆 张志豪 ZHANG Rui-fang;XU Ji;FENG Xin-ming;ZHAO Fan;ZHANG Zhi-hao(Institute for Advanced Materials and Technology,University of Science and Technology Beijing,Beijing 100083,China;Key Laboratory for Advanced Materials Processing(MOE),Institute for Advanced Materials and Technology,Beijing 100083,China)

机构地区：[1]北京科技大学新材料技术研究院,北京100083 [2]材料先进制备技术教育部重点实验室,北京100083

出　　处：《工程科学学报》2023年第4期569-576,共8页Chinese Journal of Engineering

基　　金：佛山市核心技术攻关资助项目(1920001000409);国家自然科学基金–辽宁联合基金资助项目(U1708251)。

摘　　要：以挤压态的6013铝合金为研究对象,通过显微硬度测试、单向拉伸实验和组织分析,研究了自然时效、人工时效和回归再时效处理时合金的力学性能变化规律.结果表明:自然时效峰值状态(16 d)的抗拉强度为286 MPa,屈服强度为158 MPa,屈强比为0.54,适合塑性成形;将自然时效峰值状态下的试样进行回归再时效处理(210℃回归0.5 h+170℃峰值时效2 h),抗拉强度为362 MPa,屈服强度为336 MPa,屈强比达到0.92,抗塑性变形能力显著增强.这是因为回归再时效后析出相的尺寸减小,数密度显著增大,析出强化效果显著增强.而析出强化对屈服强度和抗拉强度的影响程度不同,因此可通过时效热处理来调控屈强比,即通过自然峰值时效提高合金的塑性变形性能以成形零件,而在零件成形后采用回归再时效提高其抗变形能力.Because of its high strength and good fracture toughness,6013 aluminum alloy is widely used in auto and aircraft parts,such as the outer hood,outer decklid,and outer fuselage skin.An aluminum alloy must have good plastic forming ability in forming auto and aircraft parts and must have high deformation resistance in service.These performance requirements mainly depend on the yield ratio,that is,the ratio of yield strength to tensile strength.A lower yield ratio means larger deformation from the start of plastic deformation to the final fracture,which benefits formability.A higher yield ratio means higher plastic deformation resistance,which benefits service safety.In this paper,the mechanical properties and microstructure of the extruded 6013 aluminum alloy after natural aging,artificial aging,and retrogression re-aging are studied using microhardness tests,tensile tests,scanning electron microscopy,and transmission electron microscopy.The samples after the solid solution were naturally aged at room temperature and artificially aged at 170,180,and 190℃to determine the peak aging time.Then,after natural peak aging,the samples were heat-treated using the retrogression and re-aging process(retrogression at 200/210℃for 0.5 h and re-aging at 170℃).The results show that the tensile strength was 286 MPa,the yield strength was 158 MPa,and the yield ratio was 0.54 after natural peak aging for 16 d,which is suitable for plastic forming.The tensile strength was 362 MPa,the yield strength was 336 MPa,and the yield ratio reached 0.92 after the retrogression and re-aging process(retrogression at 210℃for 0.5 h and peak re-aging at 170℃for 2 h);the plastic deformation resistance was considerably enhanced.Compared with single-stage artificial aging,retrogression and re-aging can enhance the yield strength of 6013 aluminum alloy more substantially to break through the yield ratio limit in single-stage aging.Because the size of the precipitated phase decreases and the number density increases considerably after retrogressi

关 键 词：6013铝合金 屈强比 自然时效 人工时效 回归再时效 

分 类 号：TG166.3[金属学及工艺—热处理]