| 研究生: |
楊茜文 Yang, Chein-Wen |
|---|---|
| 論文名稱: |
鋁合金(6061-T6)之高溫高速撞擊與微觀特徵分析 High temperature impact deformation and microstructure evolution of 6061-T6 aluminum alloy |
| 指導教授: |
李偉賢
Lee, Woei-Shyan |
| 學位類別: |
碩士 Master |
| 系所名稱: |
工學院 - 機械工程學系 Department of Mechanical Engineering |
| 論文出版年: | 2013 |
| 畢業學年度: | 101 |
| 語文別: | 中文 |
| 論文頁數: | 115 |
| 中文關鍵詞: | 霍普金森桿 、6061-T6鋁合金 、核反應器內結構材料 、高溫 、高應變速率 、差排密度 、疊差缺陷 |
| 外文關鍵詞: | split Hopkinson bar, 6061-T6 aluminum alloy, structural materials of nuclear reactors, high temperature, high strain rate, dislocation density, stacking fault |
| 相關次數: | 點閱:167 下載:1 |
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6061-T6鋁合金具有相當優異的機械性能,如良好的成形性、耐腐蝕性、高強度比,因此大量應用於結構元件、飛機零組件、裝甲系統和高速機械等,甚至可以做為核反應器內部的結構材料。因此本實驗利用霍普金森高速撞擊試驗機及高溫加熱裝置,針對材料從100℃到350℃,應變速率分別為由1000s-1至5000 s-1下進行高速撞擊,以探討溫度及應變速率相對於材料之塑變行為及微觀結構之影響。
實驗結果,溫度與應變速率對6061-T6鋁合金的影響很大,相同溫度條件之下,其塑流應力值、加工硬化率及應變速率敏感性係數均隨應變速率增加而增加,而熱活化體積則會下降。反之,相同應變速率條件下,其塑流應力值、加工硬化率及應變速率敏感性係數均隨溫度增加而下降,而熱活化體積則會上升。此外,藉由Zerilli-Armstrong構成方程式,可精準預測此合金在不同溫度及應變速率下的塑變行為。
微觀結果方面,於穿透式電子顯微鏡下則可觀察到差排密度隨著應變速率上升而增加,隨溫度上升而減少,且可於高溫高應變速率時發現疊差缺陷的產生。最後結合巨觀與微觀之結果證明塑流應力與差排密度符合Bailey-Hirsch type關係式之線性關係。
6061-T6 aluminum alloy has been used extensively as structural materials for internals of experimental nuclear reactors, aircraft fittings, amour systems and high-speed machinery for years due to its superior mechanical properties. In this study, the high temperature deformation and micro-structural evolution of 6061-T6 aluminum alloy under high strain rate loading condition are investigated by means of a split-Hopkinson bar. The specimens with longitudinal direction are heated using a clam-shell radiant-heating furnace. Impact tests are performed at strain rate ranging from 1×103 to 5×103 s-1 and temperatures between 100℃ and 350℃. The experimental results indicate that the flow response of 6061-T6 aluminum alloy is related to temperature and strain rate. At a constant temperature, plastic stress, work hardening rate and strain rate sensitivity all increase with the increasing strain rate, while the thermal activation volume decreases.
However, at a constant strain rate, plastic stress, work hardening rate and strain rate sensitivity decrease with increasing temperature, while the thermal activation volume increases. The observed that high temperature and high strain rate deformation behavior of 6061-T6 aluminum alloy can be adequately described using the Zerilli-Armstrong constitutive equation. Transmission electron microscopy observations reveal that the dislocation density increases with an increasing strain rate, but decreases with an increasing temperature. The strengthening effect observed at higher strain rates and lower temperatures is attributed to a greater dislocation density. The stacking fault is also found in high temperature and high strain rate. A linear relationship between the square root of the dislocation density and the true stress is also found.
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