研究生: |
許智為 Zhi-wei Hsu |
---|---|
論文名稱: |
等徑轉角擠製(ECAE)對AZ61添加不同強化相鎂基複合材料之機械性質研究 Effect of equal channel angular extrusion on the mechanical properties of AZ61 matrix composites with different reinforcement |
指導教授: |
黃崧任
Song-jeng Huang |
口試委員: |
向四海
Su-hai Hsiang 周振嘉 Chen-chia Chou 汪俊延 Jun-yen Uan |
學位類別: |
碩士 Master |
系所名稱: |
工程學院 - 機械工程系 Department of Mechanical Engineering |
論文出版年: | 2014 |
畢業學年度: | 102 |
語文別: | 中文 |
論文頁數: | 82 |
中文關鍵詞: | 等徑轉角擠製(ECAE) 、AZ61鎂基複合材料 、強化相顆粒(Al2O3p、SiCp) |
外文關鍵詞: | Equal Channel Angular Extrusion (ECAE), AZ61 magnesium matrix composites, reinforcement particles (Al2O3p、SiCp) |
相關次數: | 點閱:252 下載:8 |
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鎂合金在常溫之塑性變形能力較差,若要克服此缺點,我們可以使用大量塑性變形法來改善。等徑轉角擠製使用大量塑性變形法來進行鎂合金機械性質的改善。本研究選用微米級氧化鋁(1、2、5wt%)及碳化矽顆粒(1、2、5wt%)為強化相,平均粒徑大小為10μm,利用等徑轉角擠型(Equal Channel Angular Extrusion, ECAE)製程對添加不同氧化鋁及碳化矽顆粒含量的鎂基複合材料進行擠製,並且探討鎂基複合材料經ECAE後之機械性質與微觀組織之差異。
本研究結果顯示,隨著強化相含量增加時,平均晶粒尺寸有明顯下降,對AZ61/5wt% SiCp鎂基複合材料進行ECAE擠製,經由BC路徑擠壓四道次後,平均晶粒尺寸可降低至5.2μm。
AZ61鎂基複合材料的降伏強度(Yield Strength, YS)以及硬度(Hardness)皆會隨著強化相含量的增加而明顯提升,對AZ61/5wt% SiCp鎂基複合材料進行BC路徑擠製四道次,可獲得最佳降伏強度及硬度,對AZ61/5wt% Al2O3p鎂基複合材料進行BC路徑擠製四道次,可獲得最佳極限強度(Ultimate Tensile Strength, UTS)及延展率(Ductility)。ECAE擠製比較四種不同路徑,由結果顯示,其中以BC路徑細化效果及機械性質為最佳,C路徑次之,而路徑A、BA為最差的。
AZ61/SiCp鎂基複合材料在添加1wt% SiCp後,其極限強度及延展率隨著含量增加而下降。在AZ61/5 wt% SiCp鑄錠經固溶處理後,由金相圖中之晶粒與晶界處皆有發現Mg2Si化合物存在,由數據結果顯示,此化合物會降低鎂基複材之機械性質。
Magnesium alloy has poor plastic deformation ability under room temperature, in order to overcome its shortcoming, we can use “severe plastic deformation” (SPD) to improve this defect. Severe Plastic Deformation (SPD) is widely used to improve the mechanical properties of magnesium. In this study, the average particles size are 10μm with 1,2 and 5wt% of micron sized Al2O3 and SiC particles for reinforcement . By using Equal angular extrusion (Equal Channel Angular Extrusion, ECAE) process of adding Al2O3 and SiC particles of different levels of magnesium matrix composites were extruded.To investigate the difference of mechanical properties and microstructure after ECAE apply on magnesium matrix composites.
The results shows that the average grain size will decrease with increasing the volume fraction of reinforcement. The average grain size of magnesium matrix composites will reduce to 5.2μm by ECAE four passes at route BC.
The results shows that the yielding strength and hardness of magnesium matrix composites will increase with increasing the volume fraction of reinforcement. For AZ61 / 5wt% SiCp magnesium matrix composites will get the best yield strength and hardness by extruding four passes at route BC. AZ61 / 5wt% Al2O3p magnesium matrix composites will get the best ultimate tensile strength and ductility by extruding four passes at route BC. ECAE extruded compare four different routes, the results shows that the effect of which route BC refinement and mechanical properties is the best, route C followed ,route A and BA is the worst.
In this study, microstructure of AZ61/1wt% SiCp shows that the ultimate tensile strength and ductility will decrease with increasing the volume fraction of reinforcement. Microstructure of AZ61/5wt% SiCp ingot shows Mg2Si compound at the grain boundaries after solid solution treatment. This compound will reduce the mechanical properties of magnesium matrix composites.
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