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Bolt-joint structural health monitoring by the method of electromechanical impedance

机译:机电阻抗法监测螺栓接头结构健康

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Purpose - The purpose of this paper is to present the problems of the electromechanical impedance (EMI), especially its applications for structural health monitoring of aircraft bolt-joints and innovative approach of EMI prediction at loosening of bolt-joints. Design/methodology/approach - This experimental study includes the results of a full-scale test of the Mi-8 helicopter tail beam, particularly, its bolt-joints of a beam with other parts of the structure. One of the connecting frames of the tail beam was equipped with piezoelectric transducers (PZT) glued on the surface of the frame near the bolts. The bolts' loosening was investigated by using the EMI technology. Findings - It was demonstrated that loosening of the bolt-joint produces a significant and statistically stable change of the EMI metric. Presumably, both the small shift of resonance frequencies and the EMI magnitude and resistance change are caused mainly by damping variation at the bolt-joint loosening. In this analytical study, the 2D model of a constrained PZT is proposed. In contrast with the existing model, the modal decomposition analysis is used as a universal mean to express the dynamic properties and dynamic responses of both the transducer and the host structure. This approach, together with the finite element modal analysis, allows simulation of any complex system "PZT-host structure". The model can be easily transformed also to the 3D one. The bolt-joint of the Mi-8 helicopter with the EMI measurement system was simulated by using the developed 2D model. The simulation results satisfactorily correspond to the test. Practical implications - The results of this research can be used for implementation in the structural health monitoring of bolt-joints and other aerospace structural components. Originality/value - The new experimental results on aircraft real bolt-joints were obtained. Especially significant is the original 2D model of the electromechanical impedance, based on the modal decomposition method, which can significantly improve the accuracy and the realistic description of the dynamic interaction between PZT and structure, as well as the dynamic response to the appearance of structural damage.
机译:目的-本文的目的是提出机电阻抗(EMI)的问题,尤其是其在飞机螺栓接头结构健康监测中的应用以及在螺栓接头松动时EMI预测的创新方法。设计/方法/方法-此实验研究包括对Mi-8直升机尾梁进行全面测试的结果,尤其是其横梁与结构其他部分的螺栓连接。尾梁的连接框架之一配备有压电传感器(PZT),该传感器粘贴在框架表面靠近螺栓的位置。通过使用EMI技术研究了螺栓的松动情况。发现-证明螺栓接头的松动会产生EMI度量的显着且统计上稳定的变化。据推测,共振频率的微小变化以及EMI大小和电阻变化都主要由螺栓接头松动时的阻尼变化引起。在此分析研究中,提出了约束PZT的二维模型。与现有模型相反,模态分解分析被用作表达换能器和主体结构的动态特性和动态响应的通用手段。这种方法与有限元模态分析一起,可以模拟任何复杂的系统“ PZT-主机结构”。该模型也可以轻松转换为3D模型。使用开发的2D模型模拟了带有EMI测量系统的Mi-8直升机的螺栓连接。仿真结果令人满意地对应于测试。实际意义-这项研究的结果可用于螺栓接头和其他航空航天结构部件的结构健康监测中。原创性/价值-获得了有关飞机实际螺栓接头的新实验结果。尤其重要的是基于模态分解方法的原始机电阻抗二维模型,它可以显着提高PZT与结构之间的动态相互作用以及对结构损坏外观的动态响应的准确性和逼真的描述。 。

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