对破裂的合金飞机结构与单面粘合粘合复合贴片的修复方法的比较
Junshan Hu1,2, Chengyu Li1, Jinrong Fang1
1College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
Materials (Basel, Switzerland)
|October 14, 2023
概括
对于破裂的飞机部件,单向预合金复合贴片提供了最佳的维修效率和稳定性. 这种方法平衡了Ti合金板的粘合强度和承载能力.
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
- 结构维修 结构维修
背景情况:
- 复合材料补丁对于修复破裂的飞机部件至关重要.
- 修复方法显著影响修复结构的性能.
研究的目的:
- 通过实验评估和比较不同复合材料补丁方法的维修效率和加工稳定性.
- 确定破裂的Ti合金板的最佳维修策略.
主要方法:
- 研究了预固化,prepreg (单向和平面编织) 和 wet-layup 复合材料修复方法.
- 在破裂的Ti合金面板上使用了一面复合材料补丁的关节配置.
- 评估了承载行为,粘合接口微观结构和故障形态.
主要成果:
- 单向的 prepreg 和 wet-layup 方法显示出良好的粘合和负载恢复,这是由于一个类似拼图的接口.
- 湿置补丁表现出多孔性和高承载能力的变化.
- 预固化和平面编织的 prepreg 贴片分别具有较弱的粘合和较低的轴承强度.
结论:
- 单向的 prepreg 补丁显示出更高的维修效率和加工稳定性.
- 这种方法为恢复破裂的金属结构的机械性能提供了最佳的平衡.
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