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研究生:林漢輝
研究生(外文):Hon-Fai Lam
論文名稱:35NCD16鋼材在靜態及動態壓縮荷載下之機械行為及顯微結構特性分析
論文名稱(外文):The analysis of microstructure characteristics and mechanical properties of 35NCD16 alloy steel under quasi-static and dynamic compression loading conditions
指導教授:李偉賢李偉賢引用關係
指導教授(外文):Woei-Shyan Lee
學位類別:碩士
校院名稱:國立成功大學
系所名稱:機械工程研究所
學門:工程學門
學類:電資工程學類
論文種類:學術論文
論文出版年:1993
畢業學年度:81
語文別:中文
論文頁數:183
中文關鍵詞:統制方程式差排環熱活化体積
外文關鍵詞:Constitutive EquationDislocation CellThermally Activities Volume
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本研究之主要目的是在探討高強度35NCD16鋼材在靜態及動態壓縮荷載下
之機械行為及顯微結構變化的特性,並分析兩者之間的相關性,同時藉助
變形統制方程式來描述材料之塑變行為。靜態機械測試是採用
SAGINOMIYA 100 噸金屬成形試驗機,針對材料作低應變速率(10^-2 至1
S^-1)及較大變形量(10%-80%)的測試。動態則採用一維彈性波理論為分析
之基礎和霍普金森桿測試裝置,來探討材料在較高應變速率(10^2 至5*10
^3 S^-1)及低變形量(5%-25 %)下之衝擊變形的特性。由機械測試分析之
結果可得知流變應力會隨應變速率之增加而增加,其應變速率之敏感性與
熱活化体積皆會隨應變速率及變形量的增加而改變,由此可判別不同應變
速率區間變形機構。當應變速率小於10^3S^-1時,材料變形主要受熱活化
機構所控制,若超過此值則轉由差排黏滯機構所主宰。有關材料顯微結構
分析則分別利用光學顯微鏡 (OM)與掃描式電子顯微鏡(SEM)觀測金相及
破壞行為,材料靜態區間破壞行為分別以拉張與滑移二種模式之構成,其
破斷面出現穿晶式及晶粒間之韌窩結構,是屬延性破壞機構。並且利用掃
描穿透式電子顯微鏡(STEM)分析及觀測材料的顯微組織,如差排密度和差
排環之形成等。最後,分別在靜態及動態區間引介變形統制方程式來描
述35NCD1 6鋼材之塑變行為,其數值模擬與實驗結果非常吻合;在靜態時
其塑流應力之誤差在2%之內,而動態時則在5%之內。此統制方程式之建立
可提供工程及軍事應用時之設計依據與參考。

The purpose of this thesis is to investigate the misro-
structure characteristics and mechanical properties of (NF)
35NCD16 high strength alloy steel under quasi-static and
dynamic compression loading conditions. At the same time,
deformation constitutive equation is used to descibe the
plastic deformation behaviour of material properties. Quasi-
static mechanical tests adopt the SAGINOMIYA 100 tons forging
machine for testing material at low strain rate from 10^-2 to 1
s^-1, and the strainrange from 10% to 80%. Fro dymanic tests,
one dimensional elastic wave theory as analysis a basis and
the Hopkinson bar tester device are used to invesgate the
impact properties of present material at high strain rate from
10^2 to 5*10^3 s^-1 and a low defor- mation from 5% to 25%.Form
the result of mechanical tests analysis, it is found that the
flow stress increases with the rise of strain rate. The strain
rate sensitivity and the activation volume are changed with the
incresing of strain rate and strain. Therefore, the different
strain rate regions for deformation mechanism can be
distinguished. The material deformation is maniniy controlled
by thermally activated mech- anism as the strain rate regions
for deformation is mainly controlled by thermally activated
mechanism as the strain rate less than 10^3 s^-1. If the strain
rate is larger than 10^3 s^ -1, the thermally activated
meshanism will transform to a dis- location drag mechanism.
Microstructural evaluation are made by (OM) AND (SEM) for
observing the metallographic structer and the fracture
behaviour.Furthermore, with (STEM), microstructure of this
material, such as dislocation desity and dislocation cells is
analysed and observed.

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