• 沒有找到結果。

近年來有許多學者都不斷地鑽研奈米尺度下之材料性質,單一金 屬結構於奈米尺度下,是否會因為尺寸效應與表面效應而改變材料的 楊氏係數。本研究主要在探金奈米線受到單軸拉伸時,其應力應變關 係討論,以及其塑性變形的產生。

以分子動力學來模擬巨觀的拉伸試驗,在微觀世界中奈米線會存 在一壓縮預應力,與巨觀拉伸試驗一開始近乎為零有很大的不同。在 應力應變曲線中,分子動力學模擬出來的結果並沒有像巨觀應力曲線 那樣平滑,會有微小應力震盪的現象,是因為拉伸過程中原子各別在 相對位置作平衡所以造成了曲線的微小震盪。在彈性區間內,原子雖 然有小幅的移動,不過每顆原子與其相鄰原子的相對位置並不會改 變,在降伏點時,此時原子相對位置還未改變,原子間勢能達到極值,

下一時間點原子瞬間滑移成核產生差排,應力值達最高後開始下降,

而其滑移平面為{111}面心立方的最緊密堆積平面。及其滑移平面不 斷重覆差排、滑動、形成另一個穩定結構的過程,此為降伏後應力應 變關係成鋸齒狀的主要原因。進一步改變模擬的奈米線尺寸後,降伏 應力會隨尺寸變大而變小,而主要原因為尺寸變大時,奈米線的表面 積因此而變大,使得差排成核的機率大大增加,而楊氏係數在[100]

40

方向會隨尺寸變大而有增加的趨勢,原因為其表面積對總體積的比值 會隨尺寸變大而減少,當減至趨近於零時,此時材料的表面效應對結 構影響已經非常小,材料性質接近塊材。拉伸應變率的部份,分子模 擬的結果與巨觀實驗的結果有相同的趨勢,即楊氏係數不會隨應變率 變化而改變,它會在一定值上下跳動。應變率對降伏強度有較顯著的 影響,因為滑移面的生成需要一段時間,應變率太大時,滑移面無法 生成以致於降伏強度不斷增加。此外,奈米線的強度及塑性變形的模 式,會因原子的排列(方向性)而有很大的差異。

在討論能量損耗的部份,雖然尺寸越大的奈米線其降伏後能量損 耗會越大,但如果我們將能量去除上系統體積後,發現在不同尺寸下 單位體積的能量差別不大,說明奈米線單位體積的滑移程度是與尺寸 無關的。在方向[111]的奈米線能量損耗明顯會比[100]方向來得小,

因為在[111]方向幾乎沒有滑移面生成。

奈米線含缺陷的模型討論空孔率對其結構強度的影響,發現空孔 率越大的奈米線,其降伏強度也會明顯地下降,但對結構的楊氏係數 幾乎沒影響,在小缺陷率(約1%)以下的情況,材料在降伏前仍維持線 彈性。另一方面比較缺陷位置的影響性,發現相同缺陷率下含構槽的 奈米線強度比含空孔奈米線小很多,因含構槽奈米線有更強的應力集 中效應。此外可以觀察得到奈米線的差排成核位置與缺陷位置有很密

41

切的關係,幾乎都會從缺陷附近最先開始發生差排成核的現象。而能 量損耗則以缺陷率最大的模型最小,即空孔越大其滑移程度規模最 小。

42

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48

附 表

表 1 模擬材料基本設定

晶格常數(a) 4.08 Å

原子模型 FCC結構

系統溫度 1.0 K

變形條件 等位移拉伸變形

表 2 模擬材料參數表[34]

Z

0

n

s

11.0 1.4475 0.1269 2.0 1.0809

表 3 金塊材勁度矩陣參數

C11 C22 C33 C12 C13 C23

174.2 174.2 174.2 136.9 136.9 136.9

單位:GPa

49

表 4 不同尺寸之應力應變數據

Size 8a 12a 16a 20a

Yield stress(GPa) 4.46 4.28 4.19 4.16

Yield strain 0.093 0.085 0.080 0.079

Young’s modulus(GPa) 47.20 49.90 51.50 51.77 a:晶格常數

表 5 應變率計算

Strain Rate(s-1) 2x10-7 2x10-8 2x10-9

Strain/Step 0.1% 0.1% 0.1%

Equilibrium Time (ps) 50 5 0.5

表 6 三晶向楊氏係數

Orientation [100] [110] [111] Exp.[55]

Yield stress(GPa) 4.46 3.67 3.18 3.5-5.6

Young’s modulus(GPa) 47.20 89.18 106.81 7011

50

表 7 不同尺寸臨界應變平衡前後能量差異

Size 8a 12a 16a 20a

Energy loss(eV) 118.6 260.6 453.5 732.1

Energy loss/vol 6.82E-4 6.66E-4 6.52E-4 6.73E-4

表 8 不同晶向臨界應變平衡前後能量差異

Orientation [100] [110] [111]

Energy loss(eV) 118.6 61.9 20.1

Energy loss/vol 6.82E-4 3.56E-4 1.12E-4

表 9 缺陷率計算

State Vacancies Disorder %

perfect 0 0.0

2x3 51 0.44

2x5 85 0.73

2x7 119 1.02

51

表 10 不同缺陷率臨界應變平衡前後能量差異

Energy perfect 2x3 2x5 2x7

Energy loss(eV) 118.6 108.3 89.5 68.4

Energy loss/vol 6.82E-4 6.27E-4 5.22E-4 4.01E-4

表 11 不同缺陷位置臨界應變平衡前後能量差異

Energy perfect 2x3 vacancy 2x3 notch

Energy loss(eV) 118.6 108.3 52.89

Energy loss/vol 6.82x10-4 6.27x10-4 3.06x10-4

表 12 FCC 滑移系統

Plane (111) (-1 -1 1)

Direction [0 -1 1] [1 0 -1] [-1 1 0] [0 1 1] [-1 0 1] [1 -1 0]

System a1 a2 a3 b1 b2 b3

Plane (-111) (1 -1 1)

Direction [0 -1 1] [-1 0 -1] [1 1 0] [0 1 1] [1 0 -1] [-1 -1 0]

System c1 c2 c3 d1 d2 d3

52

表 13 [100]晶向拉伸之 schmid’s factor

System a1 a2 a3 b1 b2 b3

m 0 0.408 0.408 0 0.408 0.408

System c1 c2 c3 d1 d2 d3

m 0.408 0.408 0.408 0 0.408 0.408

表 14 [110]晶向拉伸之 schmid’s factor

System a1 a2 a3 b1 b2 b3

m 0.408 0.408 0 0.408 0.408 0

System c1 c2 c3 d1 d2 d3

m 0 0 0 0 0 0

表 15 [111]晶向拉伸之 schmid’s factor

System a1 a2 a3 b1 b2 b3

m 0 0 0 0.272 0 0

System c1 c2 c3 d1 d2 d3

m 0 0 0.272 0.272 0 0

53

附 圖

圖 2.1 截斷半徑 rc示意圖

圖 2.2 Centro-Symmetry Parameter 計算之原子示意圖

54

圖 2.3 Schmid’s Law 示意圖

X

Y Z

圖 3.1 金奈米線結構

55

圖 3.2 拉伸示意圖

X Y

Z

圖 3.3 金塊材示意圖

56

57 Time (ps)

Stress(GPa)

0 25 50 75 100

-2 -1 0 1 2 3 4

XX

YY

ZZ

圖 3.6 8a x 8a 結構應力對時間變化

Time (ps)

Energy(eV)

0 25 50 75 100

-44600 -44550 -44500

圖 3.7 8a x 8a 結構能量對時間變化

58

圖 3.8 6a x 6a 平衡後結構圖

圖 3.9 8a x 8a 平衡後結構圖

圖 3.10 12a x 12a 平衡後結構圖

圖 3.11 16a x 16a 平衡後結構圖

59

Time (ps)

Equilibriumstrain%

0 25 50 75 100

-20 -15 -10 -5 0 5 10 15

6a x 6a 8a x 8a 12a x 12a 16a x 16a 20a x 20a

圖 3.12 平衡應變量對時間關係

圖 3.13 不同截面下應力應變關係圖(strain rate=2x107s-1)

60

Cubic lattice unit (a)

Young'sModulus(GPa)

8 10 12 14 16 18 20

35 40 45 50 55 60 65

bulk

圖 3.14 不同截面與楊氏係數關係(strain rate=2x107s-1)

Cubic lattice unit (a)

Yieldstress(GPa)

8 10 12 14 16 18 20

4 5

圖 3.15 不同截面與降伏應力關係(strain rate=2x107s-1)

61

圖 3.16 金奈米線結構在應變率為 2x10-7s-1下變形圖 ([100]晶 向)

62

圖 3.17 降伏點(strain=0.093) 時其應力變化(a)t=10ps(b)t=20ps (c)t=30ps (d)t=40ps (e)t=50ps

63

圖 3.18 CSP 分佈圖(a)ε=0.092 (b)ε=0.093 t=10ps (c)ε=0.093

t=20ps (d)ε=0.093 t=30ps (e) ε=0.093 t=40ps (f)ε=0.093 t=50ps

64

圖 3.19 csp 分佈圖 ε=0.093 (a)~(e)分別代 t=18~t=22ps (f) t=35ps (g) t=40ps (h) t=45ps (i) t=50ps (j) t=80ps

圖 3.20 鋸齒狀應力示意圖

65

圖 3.21 應變率分別為 2 x107 S-1、2 x108 S-1、2 x109 S-1應力應 變關係圖

Strain rate (s-1)

Yieldstress(GPa)

107 108 109

4 4.4 4.8 5.2

log

圖 3.22 應變率對降伏應力關係

66 Strain rate (s-1)

Yieldstrain

107 108 109

0.08 0.09 0.1 0.11 0.12

log

圖 3.23 應變率對降伏應變關係

67

圖 3.24 [100]、[110]及[111]晶向

68

圖 3.25 8 倍晶格邊長在應變率 2 x107s-1下應力應變圖( [110]

晶向)

69

(a)

strain=0.025

(b)

strain=0.030 t=10ps

(c)

strain=0.030 t=20ps

(d)

strain=0.030 t=30ps

圖 3.26 金奈米線結構變形圖( [110]晶向)

70 (b)strain=0.03,t=10ps (c) strain=0.03,t=20ps (d) strain=0.03,t=30ps

71

圖 3.28 8 倍晶格邊長在應變率 2 x107s-1下應力應變圖([111]晶 向)

72

圖 3.29 金奈米線結構變形圖([111]晶向)

73

圖 3.30 [111] 晶向拉伸變形 CSP 圖 (a)strain=0.027 (b)strain=0.031 (c) strain=0.032 (d) strain=0.033

74

圖 3.31 [100]、[110] 、[111]晶向拉伸應力應變圖

圖 3.32 坐標軸轉換

75

圖 3.33 奈米線差排成核點 (a) [100] (b) [110]

Time (ps)

Energy(eV)

0 25 50 75 100

-44540 -44520 -44500 -44480 -44460 -44440 -44420

圖 3.34 8 倍晶格常數線寛在臨界應變下勢能變化圖

76

[100] [110] [111]

圖 3.36 降伏應力及能量損耗對方向性關係

77

78

圖 4.2 2x3、2x5 及 2x7 三種空孔率示意圖

圖 4.3 穩定前後含空孔結構(a) 2x3 (b) 2x5 (c) 2x7

79

圖 4.4 含空孔奈米線應力應變圖

Disorder %

Yieldstress(GPa)

0 0.25 0.5 0.75 1

0 1 2 3 4 5 6 7

圖 4.5 奈米線缺陷率對降伏應力關係圖

80

圖 4.6 2x3 空孔奈米線在不同應變下結構圖

81

圖 4.7 含 2X3 空孔結構臨界應變 ε=0.087 下 CSP 分佈圖(a)t=10 (b)t=14 (c)t=15 (d)t=16 (e)t=17 (f)t=18 (g)t=20 (h)t=30 (i)t=40

(j)t=50

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perfect 2x3 2x5 2x7

圖 4.8 降伏應力及能量損耗對缺陷率的關係

圖 4.9 含溝槽奈米線示意

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圖 4.10 含溝槽奈米線結構穩定

圖 4.11 含構槽奈米線拉伸變形圖

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圖 4.12 含溝槽 CSP 分佈圖 ε=0.068 (a)t=10ps(b)t=20 ps (c) t=30ps (d) t=40ps (e) t=50ps

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perfect 2x3 vacancy 2x3 notch

圖 4.14 降伏應力及能量損耗對缺陷型式的關係

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圖 4.15 含 2x3 空孔及溝槽應力應變圖

圖 4.16 缺陷位置應力集中程度比較 (a)含溝構缺陷 (b)含空孔 缺陷

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圖 4.17 奈米線差排成核點 (a) 2x3 notch (b) 2x3 vacancy (c) 2x5 vacancy (d) 2x7 vacancy

在文檔中 金奈米線的機械性質模擬 (頁 55-103)

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