熱處理對ZK60鎂合金顯微組織及疲勞斷裂行為的影響
[Abstract]:Magnesium alloys have the advantages of low density, high strength, good damping and damping properties, low heat capacity, fast solidification speed and good casting formability. ZK60 magnesium alloy is regarded as the most developed green engineering material in the 21st century. As the highest strength of commercial wrought magnesium alloy, improving the plasticity of components is very important for expanding the application of magnesium alloy. Therefore, this paper studies the microstructure changes of ZK60 magnesium alloy under heat treatment, and discusses its influence on fatigue fracture behavior, which has certain significance for further promoting the application of ZK60 magnesium alloy in practical production and life. The tensile properties of ZK60 magnesium alloy were analyzed by fatigue testing machine and the fatigue crack propagation characteristics were analyzed by SEM and XRD. The grain size of ZK60 magnesium alloy sheet was 26 micron. The average grain size of ZK60 magnesium alloy after solution treatment was about 31 micron. The tensile strength of ZK60 magnesium alloy sheet is 294 MPa and 301 MPa respectively after solution treatment. The strength of the sample after aging treatment is 325 MPa, which is higher than that of ZK60 magnesium alloy sheet. The elongation and yield strength are both improved by XRD analysis. It is known that ZK60 magnesium alloy sheet is mainly composed of a-Mg, MgZn and MgZn2 phases. After solution treatment, all MgZn phases in the sample are incorporated into the matrix, while Mg-Zn2 is dissolved into the matrix with a small amount of residual, but MgZn and MgZn2 are re-precipitated after aging treatment. The fatigue strength of ZK60 magnesium alloy sheet is 9 when the number of cyclic loading is 107. The fatigue strength of the specimens after solution treatment (T4) and solution aging treatment (T6) were 102.46 MPa and 117.76 MPa, respectively. The fatigue strength of the specimens after aging treatment was 28.31% higher than that of ZK60 magnesium alloy sheet. The fatigue fracture of ZK60 magnesium alloy sheet was brittle fracture, and the crack initiation zone was found after heat treatment. The crack growth rate test showed that the crack growth rate of the specimens aged for 5 h was slightly slower than that of the specimens treated by solid solution. The crack growth rate of ZK60 magnesium alloy increases at h, so the crack growth resistance of ZK60 magnesium alloy is the best after solution treatment and aging for 10 h. By analyzing the fracture surface of crack growth rate, at the beginning of crack growth stage, the fracture surface of the sample treated by solution treatment contains pits, which belongs to brittle fracture surface, and the fracture surface of aging treatment is relatively smooth. Secondary cracks can be found in the stable propagation zone of the specimens.There are many dimples in the transient fracture zone after aging treatment,which can improve the resistance to crack propagation.The plastic radius of ZK60 magnesium alloy sheet is calculated by the plastic radius formula.The plastic radius of the crack tip of the solution treated specimens and the aging treated specimens are 10.5 and 10.1 microns,respectively. The grain size is larger than the plastic radius. It is found that the aging treatment ZK60 magnesium alloy has a smaller plastic radius than the solution treatment ZK60 magnesium alloy, that is, there is a smaller plastic zone, which makes the specimen more resistant to crack propagation.
【學(xué)位授予單位】:太原理工大學(xué)
【學(xué)位級別】:碩士
【學(xué)位授予年份】:2017
【分類號】:TG146.22;TG166.4
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