摘要
To solve the optimization problem of edge distance in titanium alloy sheet during a new aircraft development stage, a three dimensional FE model was built on ABAQUS platfom. The effect of edge distance on residual stress distribution was analysised with TC4 titanium alloy by interference-fit strengthening technique under cylic loading. The study indicates that a considerble reduction of fatigue life is found with a lower egde distance ratio(L/D), also, the location of fatigue damage is moving against the hole. Fatigue damage happens in the margin part with edge distance ratio(L/D) less than 2.
| 投稿的翻译标题 | Process research of edge distance on an interference-fit strengthening technique of titanium alloy sheet |
|---|---|
| 源语言 | 繁体中文 |
| 页(从-至) | 1432-1437 |
| 页数 | 6 |
| 期刊 | Jixie Qiangdu/Journal of Mechanical Strength |
| 卷 | 39 |
| 期 | 6 |
| DOI | |
| 出版状态 | 已出版 - 15 12月 2017 |
关键词
- Edge distance
- Fatigue life
- Finite element method
- Interference-fit strengthening
- Titanium
指纹
探究 '钛合金薄壁板干涉强化孔边距工艺研究' 的科研主题。它们共同构成独一无二的指纹。引用此
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