使用基于侧带强度的非线性超声波技术监测板中的疲劳裂
Bo Hu1, Umar Amjad2, Tribikram Kundu3
1Department of Aerospace and Mechanical Engineering, University of Arizona, Tucson, AZ 85721, USA.
Ultrasonics
|May 1, 2024
概括
一种新的侧带强度指数 (SII) 技术有效地检测到飞机钉接头的早期疲劳裂. 这种先进的方法改进了现有的技术,提高了飞行安全.
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
- 非破坏性测试 不破坏性测试
背景情况:
- 飞机的结构依赖于钉关节,这些关节易受疲劳裂的形成.
- 早期发现这些疲劳裂对于确保飞机安全至关重要.
研究的目的:
- 研究一种新的侧带峰值计数 (SPC) 技术的可行性,用于检测钉接头中的疲劳裂.
- 引入和验证一个新的综合指数,侧带强度指数 (SII),以克服现有方法的局限性.
主要方法:
- 使用压电传感器在带接头的板上产生和检测Lamb波.
- 开发并应用了侧带强度指数 (SII) 技术.
- 将SII技术与现有的SPC-I和SPI技术进行了比较.
主要成果:
- 新开发的SII技术在检测关节周围的初始疲劳裂方面显著改善.
- 对比分析证实了SII技术对SPC-I和SPI的有效性.
结论:
- SII技术提供了一种更高效和有效的方法来检测飞机关节中的关键疲劳裂.
- 这一进步有助于加强航空中的结构健康监测和飞行安全.
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