使用剪切引导波切断频率的CFRP膝关节的结合质量评估
Yao Xu1, Chongcong Tao2, Hongli Ji2
1State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Yudao Street 29, Nanjing 210016, China; School of Mechanical and Aerospace Engineering, Nanyang Technological University, 639798, Singapore.
Ultrasonics
|August 20, 2025
概括
本研究引入了一种新的非破坏性方法,用于评估碳纤维增强聚合物 (CFRP) 键完整性. 该技术使用引导波切断频率,提供一种可靠的方式来检测关键航空航天结构中的键降解.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 非破坏性测试是一种非破坏性测试.
背景情况:
- 确保碳纤维增强聚合物 (CFRP) 结合结构的结构完整性在航空航天应用中至关重要.
- 传统的引导波检查方法与CFRP和复杂的粘接接口的异型性质作斗争,限制了它们在评估粘接质量的有效性.
- 对于可靠的非破坏性评估技术非常需要,这些技术适用于CFRP粘合结构.
研究的目的:
- 开发和验证一种新的非破坏性评估方法,用于评估CFRP结构的键完整性.
- 调查一级剪切引导波切断频率的使用,作为界面键质量的敏感指标.
- 建立一种稳定可靠的参数,用于对异性质材料的结合评估.
主要方法:
- 开发一个有限元模型来模拟粘合CFRP结构中的波传播.
- 在异性质材料中分析一级剪切引导波传播特征.
- 试验验证债券质量与切断频率之间的关系.
主要成果:
- 一级剪切导向波的切断频率被确定为不依赖于异型材料的传播方向,确保参数稳定性.
- 有限元模型成功模拟了波传播,并证明了结合质量和切断频率之间的相关性.
- 实验结果证实,债券质量下降导致截止频率下降.
结论:
- 使用引导波切断频率的拟议方法为评估CFRP结构中的债券完整性提供了一种定量和强大的方法.
- 这种技术解决了检查异性质材料的传统方法的局限性.
- 这些发现为提高航空航天结构的安全性和可靠性提供了有希望的途径.
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