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A modal approach to identify fatigue damage in threaded connections of large scale tubular structures in a resonant bending test rig

机译:鉴定谐振弯曲试验台中大规模管状结构螺纹连接疲劳损伤的模态方法

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The current work aims at using a modal approach to detect fatigue damage of threaded connections in large scale tubular structures. A full scale resonant bending fatigue test rig has been developed to test at first a plain pipe with notches. Two kinds of vibration testing are used for fatigue crack detection. Forced vibration tests (input-output) are performed before and after the fatigue test, in which input signals from forced excitation as well as output signals from accelerometers and dynamic strain gauges are both recorded. Whereas, the ambient vibration test (output only) follows the fatigue experiment. The modal parameters of the structure can be determined from the acquired data using subspace identification algorithms, i.e. the Reference-based Combined Deterministic-Stochastic Subspace Identification one for the forced vibration tests and the Reference-based Stochastic Subspace Identification one for the ambient vibration test. An observed change in the extracted modal parameters implies the degradation of the bending stiffness when a fatigue crack initiates. The modal approach demonstrates to be a viable and reliable way to detect fatigue cracks in large scale tubular structures. This potentiality makes vibration based testing a complement to conventional approaches like e.g. global deflection control;;moreover, it is rather simple to implement and can be used for longterm monitoring.
机译:目前的工作旨在使用模态方法来检测大规模管状结构中螺纹连接的疲劳损坏。已经开发出全规模共振弯曲疲劳试验台以首先用凹口的普通管测试。两种振动测试用于疲劳裂纹检测。在疲劳试验之前和之后执行强制振动测试(输入输出),其中来自强制激励的输入信号以及来自加速度计的输出信号和动态应变计均被记录。鉴于环境振动测试(仅输出)遵循疲劳实验。可以使用子空间识别算法从所获取的数据确定结构的模态参数,即基于参考的组合确定性 - 随机子空间识别,用于强制振动测试和用于环境振动测试的基于参考的随机子空间识别。当疲劳裂纹引发时,提取的模态参数的观察改变意味着弯曲刚度的劣化。模态方法表明是一种可行且可靠的方法来检测大规模管状结构中的疲劳裂缝。这种潜力使基于振动的测试对常规方法的补充如例如。全局偏转控制;;实现,实现并可用于Longterm Monitory。

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