在拉力负载下对CFRP混合粘接螺栓干扰连接结构的故障的机械研究
Bin Luo1, Liyang Xue1, Qingsong Wang2
1School of Mechanical Engineering, Northwestern Polytechnical University, Xi'an 710072, China.
Materials (Basel, Switzerland)
|May 11, 2024
概括
混合粘合螺栓复合材料连接增强了飞机结构. 通过管理粘合剂和复合材料的故障,最佳干扰适合尺寸 (1.1%) 减少损坏,提高强度和疲劳寿命.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 航空航天工程 航空航天工程
背景情况:
- 混合粘合螺栓复合材料连接为飞机结构提供了优越的承载能力和疲劳寿命.
- 干扰适合螺栓的安装可能会导致粘合层和周围复合板层的损坏,损害关节的完整性.
研究的目的:
- 在干扰适应条件下调查复合粘接螺栓混合接头的损伤机制.
- 分析不同干扰适应尺寸对关节损伤,承载行为和故障模式的影响.
- 开发和验证一个有限元模型,准确预测损坏和性能.
主要方法:
- 在插入螺栓时,对不同干扰尺寸的损伤演变进行实验分析.
- 开发一种有限元拉伸模型,其中包括安装后对粘合剂和复合材料的损坏.
- 对实验和模拟结果进行比较分析,以验证预测模型.
主要成果:
- 结合初始损伤的有限元模型提供了有效的预测.
- 干扰适合尺寸的增加会导致粘合剂损坏,从表面脱到裂.
- 复合矩阵损伤从轻微的压缩失败演变为严重的分层和纤维断裂.
结论:
- 最佳干扰适应尺寸为1.1%,通过平衡有益的前应力和有害损伤来最大限度地提高结构强度.
- 了解和建模干扰引起的损伤对于设计可靠的混合复合材料接头至关重要.
- 这项研究为航空航天结构中干扰适合技术的应用和优化提供了关键的见解.
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