Fatigue Crack Growth Mechanisms in Titanium Single Crystals
Fatigue Crack Growth Mechanisms in Titanium Single Crystals
批准号:
09650767
负责人:
TAKASHIMA Kazuki
金额:
$2.18万
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
1997
资助国家:
日本
项目状态:
已结题
起止时间:
1997 至 1998
中文摘要
本文研究了α-钛单晶在室温空气中的疲劳裂纹扩展行为。制备了A、B、C、D、E和F六种不同切口方向的CT标本。A试样的缺口平面和方向分别为(1210)和[1010],B试样的缺口平面和方向分别为(0110)和[2110]。C试样的缺口平面为(0110),D试样的缺口平面为(1210),缺口方向均为[0001]; E试样的缺口平面为(0001),缺口方向分别为[1010]和[2110]。A和B样本中的裂纹平行于(0110)[2110]扩展。因此,裂纹扩展是由两个相交的棱柱滑移系在裂纹尖端的交替剪切。在C-和D-试样中的裂纹扩展接近基面垂直于缺口方向。这表明,与平行于基面相比,疲劳裂纹难以沿着[0001]扩展。在E-和F-试样中,裂纹大致平行于基面扩展,并在裂纹面附近发现对应于{1012}孪晶系统的痕迹。在<1010>疲劳表面上观察到平行于{1012}孪晶的脊、痕迹和条带。这些结果表明,裂纹扩展可能是由于微孪晶的激活而发生的。获得了α-钛疲劳裂纹扩展行为的晶体学依赖性。
英文摘要
The fatigue crack growth behavior of alpha-titanium single crystals has been investigated in laboratory air at room temperature. Six types of CT specimens A, B, C, D, E and F with different notch orientations were prepared. The notch plane and direction in the A-specimen were (1210) and [1010], and those in the B-specimen were (0110) and [2110], respectively. The notch plane of the C-specimen was (0110) and that of the D-specimen was (1210), and the notch direction of both the C- and the D-specimens was [0001], In the E- and the F-specimens, the notch plane was (0001), and the notch directions were [1010] and [2110], respectively. The crack in the A- and the B-specimens propagates parallel to (0110) [2110]. Therefore, the crack is deduced to extend by alternating shear on two intersecting prismatic slip systems at the crack tip. The crack in the C- and the D-specimens propagates close to the basal plane which is perpendicular to the notch directions. This indicates that the fatigue crack is difficult to grow along [0001] compared with parallel to the basal plane. In the E- and the F-specimens, the crack propagates roughly parallel to the basal plane and the traces which correspond to {1012} twin systems are found near the crack plane. Ridges parallel to <1010>, and traces and bands due to {1012} twinning are observed on the fatigue surfaces. These results suggest that the crack growth might occur plausibly by the activation of micro-twins. A definite crystallographic dependence of fatigue crack growth behavior in alpha-titanium is obtained.
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K.Takashima et al.: "Fatigue Crack Propagation in Titanium Single Crystals" Key Engineering Materials. 145-149. 721-726 (1998)
K.Takashima等:“钛单晶中的疲劳裂纹扩展”关键工程材料。
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作者:
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通讯作者:
Y.Mine, T.Yamada, S.Ando, K.Takashima, H.Tonda, Y.Higo and P.Bowen: "Fatigue Crack Growth in Titanium Single Crystals" Key Eng.Materials. 145-149. 721-726 (1998)
Y.Mine、T.Yamada、S.Ando、K.Takashima、H.Tonda、Y.Higo 和 P.Bowen:“钛单晶中的疲劳裂纹生长”关键工程材料。
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通讯作者:
K.Takashima et al.: "Molecular Dynamics Simulation of Crack Propagation in a-Titanium Single Crystals" Modeling and Simulation Based Engineering. 2. 1227-1231 (1998)
K.Takashima 等人:“a-钛单晶中裂纹扩展的分子动力学模拟”基于建模和仿真的工程。
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通讯作者:
K.Takashima, Y.Mine, S.Ando, H.Tonda, Y.Higo and P.Bowen: "Effects of Crystallographic Oriniation on Fatigue Crack Growth in alpha-Titanium Single Crystals" Advances in Fracture Research. 3. 1645-1652 (1997)
K.Takashima、Y.Mine、S.Ando、H.Tonda、Y.Higo 和 P.Bowen:“晶体取向对 α-钛单晶疲劳裂纹扩展的影响”断裂研究进展。
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通讯作者:
高島 和希 他: "チタン単結晶における疲労き裂伝播の結晶方位依存性" 日本金属学会誌. 62. 708-717 (1998)
Kazuki Takashima 等人:“钛单晶中疲劳裂纹扩展的晶体取向依赖性”日本金属学会杂志 62. 708-717 (1998)。
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