在典型的过载下研究纤维/Al-Li层的疲劳裂纹传播行为
Weiying Meng1,2, Jiayi Tan1, Sihui Li3
1School of Mechanical Engineering, Shenyang Jianzhu University, No. 25 Hunnan Middle Road, Hunnan District, Shenyang 110168, China.
Materials (Basel, Switzerland)
|August 28, 2025
概括
这项研究分析了过载条件下的纤维/合金层材的疲劳裂纹传播. 新的模型准确地预测了拉伸和压力过载下的裂增长,提高了航空航天安全.
科学领域:
- 材料科学
- 航空航天工程
- 机械工程
背景情况:
- 金属纤维层材在航空航天应用中具有出色的裂传播性能.
- 预测这些层状材料的裂纹行为是很有挑战性的,因为它们的合过载和纤维桥接效应.
研究的目的:
- 在典型的过载条件下分析和预测纤维/Al-Li层材的疲劳裂纹传播行为.
- 在拉力和压力过载下开发精确的裂增长模型.
主要方法:
- 在恒定振幅和单峰拉力/压力过载下进行疲劳裂纹传播试验.
- 改进了包含厚度效应的等效裂纹长度模型的开发.
- 应用改进的惠勒理论和增量可塑性理论,用于超载效应.
主要成果:
- 在过载条件下分析了裂传播特性.
- 为了改善裂长度建模,引入了厚度大小效应因子.
- 拉力和压力过载的预测模型显示出较低的错误率 (分别为9.7%和8.1%).
结论:
- 开发的模型有效地预测过载下的纤维/合金层材的疲劳裂传播.
- 这些模型与现有的较厚层材的方法相比,显示出了进步和有效性.
- 这项研究提高了由金属纤维层制成的航空器械部件的结构完整性评估.
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