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ECAP变形及二次挤压对Mg-Zn-Ca-Mn合金组织与性能的影响
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摘要
本文采用等通道角变形( ECAP)对挤压态Mg-5.25%Zn-0.6%Ca-0.3%Mn合金在250℃和300℃进行不同道次的塑性变形,并对ECAP变形后的合金在100℃和150℃进行二次挤压变形。采用光学显微镜、扫描电子显微镜和透射电子显微镜研究挤压态、ECAP变形及二次挤压镁合金显微组织变化。采用中子衍射和背散射电子衍射(EBSD)对ECAP变形及二次挤压前后镁合金的织构演变进行了分析,并对挤压态镁合金、ECAP变形及二次挤压变形镁合金室温拉伸性能进行了测试,对其变形机理进行了分析。挤压态镁合金的初始晶粒尺寸约为4μm左右,第二相Ca2Mg6Zn3沿挤压方向呈带状分布。在ECAP变形过程中,第二相破碎弥散分布在基体合金中,同时有一些纳米尺寸的第二相析出。ECAP变形可以显著细化合金晶粒,在250℃经4道次ECAP变形后,平均晶粒尺寸细化至1.0μm,达到亚微米超细晶水平。随着ECAP变形道次的增加,合金的强度升高,室温延伸率得到了显著的提高。在300℃经4道次ECAP变形以后,合金的延伸率达到了22.7%,是原始挤压态的2倍,同时强度达到了323.2MPa,这主要是晶粒细化和ECAP变形过程中织构的变化所致。
     ECAP变形之后再对合金在100℃和150℃进行二次挤压。二次挤压之后,合金晶粒进一步细化,组织更加均匀。低温下进行二次挤压可以提高合金的强度和硬度,较高温度二次挤压可以提高合金的强度和延伸率。250℃4道次ECAP变形试样进行100℃二次挤压后,合金晶粒尺寸达到0.96μm,抗拉强度达到356MPa。300℃4道次ECAP变形试样进行150℃二次挤压后,合金晶粒尺寸达到1.1μm,抗拉强度达到334.62MPa,延伸率达到了15.2%。这主要是晶粒细化、组织均匀化及二次挤压过程中织构的演变所致。
Equal channel angular pressing (ECAP) was performed on the as-extruded Mg-5.25wt%Zn-0.6wt%Ca-0.3wt%Mn magnesium alloy at 250℃and 300℃for different passes, with subsequent extrusion at 100℃and 150℃on the ECAPed magnesium alloy. The microstructure of the as-extruded magnesium, ECAPed ultrafine grained magnesium alloy and subsequent extruded alloy were examined by means of optical microscopy (OM), scanning electronic microscopy (SEM) and transmission electron microscopy (TEM). Texture development of as-extruded magnesium alloy, ECAPed magnesium alloy and subsequent extruded alloy were investigated by neutron diffractometer and EBSD. Tensile properties at room temperature and damping behavior of magnesium alloy, ECAPed magnesium alloy and subsequent extruded alloy were investigated and mechanism was discussed.
     The as-extruded magnesium alloy had an initial grain size of about 4μm, with bands of second phrase parallel to the extrusion direction. During ECAP, the second phrase were broken and dispersed in the matrix and some nano-phrase precipitated from the matrix. After the as-extruded magnesium alloy was subjected to 4-pass ECAP at 250℃, the grain size was refined to about 1.0μm. With repeating passes, the yield stress and the elongation to failure of the alloy increased. After 4-pass ECAP at 300℃, the elongation to failure reached 22.7%, which was two times of that of the as-extruded alloy, with ultimate tensile strength reaching 323.2MPa, which resulted from the grain refinement and texture modification during ECAP.
     Perform subsequent extrusion at 100℃and 150℃on the ECAPed magnesium alloy. The subsequent extrusion lead to further grain refinement and more homogeneous microstructure. Subsequent extrusion at lower temperature can improve yield stress and hardness of magnesium alloy, while subsequent extrusion at higher temperature can cause a rise to the yield stress and elongation to failure. After 250℃4-pass ECAPed magnesium alloy were extruded at 100℃, grain size was refined to 0.96μm with ultimate tensile strength reaching 356MPa. After 300℃4-pass ECAPed magnesium alloy were extruded at 100℃, its grain was refined to 1.1μm with ultimate tensile strength reaching 334.62MPa, obtaining the elongation to failure of 15.2%. Grain refinement, homogeneous microstructure and texture development during subsequent extrusion gave sire to the result above.
引文
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