在一个全尺寸的机翼模型上对阶段式复合材料修复的计算分析
Alihan Cambaz1, Huseyin Enes Salman1
1Department of Mechanical Engineering, TOBB University of Economics and Technology, Ankara 06560, Türkiye.
Polymers
|March 14, 2026
概括
这项研究评估了全尺寸复合材料翼模型的阶段性维修,发现碳纤维增强塑料 (CFRP) 组件的最佳维修策略取决于层配置和几何,以提高结构性能.
科学领域:
- 材料科学 材料科学 材料科学
- 航空航天工程 航空航天工程
- 结构力学 结构力学
背景情况:
- 碳纤维增强塑料 (CFRP) 组件越来越多地用于民用航空.
- 有效的维护和维修对于CFRP的耐用性和性能至关重要.
- 以前的修复研究仅限于小规模标本,而不是全尺寸模型.
研究的目的:
- 在一个全尺寸的复合机翼模型上评估阶梯式翻转维修.
- 探索各种修复场景及其对结构性能的影响.
- 优化航空中CFRP组件的维修策略.
主要方法:
- 利用二维外元素进行高效的维修模拟.
- 经过验证的数值模型与实验拉伸试验数据.
- 开发了单一和双重维修区域的数值模型.
主要成果:
- 对于单次维修,1-2个额外层提高了强度;3+层降低了性能.
- 双重维修受益于额外的层,但不如单重维修.
- 圆形修复显示了比方形修复更均的应力/应变分布.
结论:
- 优化维修几何和层配置对于CFRP的结构完整性至关重要.
- 数字模拟是设计有效复合材料维修的重要工具.
- 调查结果为大型航空复合结构的维护策略提供了信息.
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