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熱處理對ZK60鎂合金顯微組織及疲勞斷裂行為的影響

發(fā)布時(shí)間:2018-09-12 15:05
【摘要】:鎂合金具有密度低、強(qiáng)度高、良好的阻尼性和減震性能,而且它的熱容量低、凝固速度快、鑄造成型性能好。鎂合金的循環(huán)利用性好,回收再利用率高,回收熔化時(shí)所消耗的能量較少,并且使用回收的鎂合金制作構(gòu)件時(shí)不會降低其力學(xué)性能。被譽(yù)為“21世紀(jì)最具發(fā)展的綠色工程材料”。ZK60鎂合金作為目前商用變形鎂合金中強(qiáng)度最高者,提高構(gòu)件的塑性,對擴(kuò)大鎂合金的應(yīng)用至關(guān)重要。但是商業(yè)鎂合金板材總會存在一定的缺陷,進(jìn)而影響性能,使用熱處理的方法可以有效地減少缺陷。因此,論文通過研究熱處理?xiàng)l件下ZK60鎂合金微觀組織的變化,探討其對疲勞斷裂行為的影響,這對進(jìn)一步推動ZK60鎂合金在實(shí)際生產(chǎn)生活中的應(yīng)用具有一定的意義。論文采用萬能試驗(yàn)機(jī)對ZK60鎂合金板材以及熱處理后試樣的拉伸性能進(jìn)行分析,利用疲勞試驗(yàn)機(jī)分析鎂合金的疲勞裂紋擴(kuò)展特征。利用SEM、XRD等測試手段對熱處理后鎂合金進(jìn)行物相分析。ZK60鎂合金板材晶粒尺寸26μm,固溶處理以后的試件晶粒平均尺寸大約是31μm。之后進(jìn)行時(shí)效熱處理從5h~20h時(shí),晶粒尺寸先減少后變得粗大。時(shí)效10h時(shí),晶粒的尺寸最小。ZK60鎂合金板材和固溶處理以后的拉伸強(qiáng)度分別是294MPa和301MPa。時(shí)效處理后試樣的強(qiáng)度為325MPa,相對ZK60鎂合金板材來說有較大的提高,延伸率以及屈服強(qiáng)度都有所提高,通過XRD分析可知,ZK60鎂合金板材主要有由α-Mg,MgZn,MgZn2相組成,固溶處理之后試樣中的MgZn相全部融入基體中,Mg Zn2大量溶入到基體中只有少量殘余,但是時(shí)效處理后有MgZn和MgZn2重新析出。試樣受到循環(huán)載荷次數(shù)為107時(shí),ZK60鎂合金板材的疲勞強(qiáng)度為91.62MPa,試件在經(jīng)過固溶處理(T4)及固溶時(shí)效處理(T6)之后疲勞強(qiáng)度分別為102.46MPa和117.76MPa,經(jīng)過時(shí)效處理之后試件的疲勞強(qiáng)度相對于ZK60鎂合金板材提高28.31%。ZK60鎂合金板材的疲勞斷口為脆性斷裂斷口,而熱處理之后在裂紋萌生區(qū)發(fā)現(xiàn)許多凹坑,裂紋擴(kuò)展區(qū)域存在準(zhǔn)解理斷裂特征。裂紋擴(kuò)展速率試驗(yàn)表明,時(shí)效5h的試件裂紋的擴(kuò)展速率稍慢于固溶處理的試件。ZK60鎂合金時(shí)效10h,抵御裂紋擴(kuò)展能力得到提高。時(shí)效15h時(shí),裂紋擴(kuò)展速率沒有繼續(xù)下降,反而有所提高。當(dāng)時(shí)效20h時(shí)裂紋擴(kuò)展速率加快。所以固溶處理之后,時(shí)效10h時(shí),ZK60鎂合金的抵抗裂紋擴(kuò)展的性能最優(yōu)。通過分析裂紋擴(kuò)展速率的斷口,在裂紋開始擴(kuò)展階段,固溶處理的試樣斷口含有小坑,屬于脆性斷裂斷口,時(shí)效處理的斷口相對平滑。在時(shí)效處理試件的穩(wěn)定擴(kuò)展區(qū)可以發(fā)現(xiàn)二次裂紋。在時(shí)效處理的瞬斷區(qū)內(nèi)有許多韌窩,它可以提高抵御裂紋擴(kuò)展的能力。通過塑性半徑公式計(jì)算出ZK60鎂合金板材,固溶處理的試樣和時(shí)效處理后的試樣裂紋尖端的塑性半徑分別為10.5μm和10.1μm,平均晶粒尺寸大于塑性半徑,發(fā)現(xiàn)時(shí)效處理的ZK60鎂合金相對于固溶處理的ZK60鎂合金具有更小的塑性半徑,即有更小的塑性區(qū),所以使得試件抵御裂紋擴(kuò)展能力加強(qiáng)。
[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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