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Damage Detection of Textile Composite Structures Using the Piezoelectric Impedance Method

机译:压电阻抗法检测织物复合结构的损伤

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Structural health monitoring of aerospace structures is becoming vital aslightweight composite materials are increasingly used in aero-structures. Compositeshave various types of failure modes, which make it even more important to identifydamage compared to isotropic materials. Therefore, on-site health monitoring is one ofthe most preferred methodologies for detecting internal crack or damage at its initialstage to enhance operating safety and reduce repair cost. Recently, piezoelectrictransducers are on high demand for on-site health monitoring because of its highbandwidth sensitivity. They simultaneously perform as actuators and sensors andembedded on the structure. The electrical impedance or admittance changes accordingto modification in mass, stiffness or damping properties of the host body. In this study,plain-weave textile composites are utilized to demonstrate capability of piezoelectrictransducer. The elastic properties of composite are determined using the ConcentricCylinder Assemblage micromechanics model. Finite element modeling is done inANSYS APDL to observe electrical admittance variation around natural frequency.Delamination and intra-ply damage cases are studied. Delamination is separation ofadjacent plies and damage is reduction of stiffness in the whole structure. Modalfrequency of the structure decreased with delamination and damage level incrementwithin the body. Pre-preg manufacturing method is carried out to fabricate compositepanel from which samples are cut for testing according to ASTM standards.Piezoelectric test provided voltage drop across the resistor that denoted the couplingeffect of the patch with the host structure. Electrical admittance plot expressedresponse to body deformation actuated by the piezoelectric transducer. Results fromfinite element modeling and experimentation assert that piezoelectric impedancetechnique is efficient in detecting damage or delamination within the compositestructure.
机译:随着航空航天结构的结构健康监测越来越重要 轻质复合材料越来越多地用于航空结构。复合材料 具有各种类型的故障模式,这使得识别故障变得更加重要 与各向同性材料相比,损伤更大。因此,现场健康监测是其中之一 最初检测内部裂缝或损坏的最优选方法 阶段,以提高操作安全性并降低维修成本。最近,压电 换能器对现场健康监测的需求很高,因为它具有很高的可靠性。 带宽敏感度。它们同时充当执行器和传感器,并且 嵌入在结构上。电阻抗或导纳根据 改变主体的质量,刚度或阻尼特性。在这项研究中, 平纹纺织复合材料被用来证明压电的能力 传感器。复合材料的弹性特性使用同心度来确定 气缸总成微力学模型。有限元建模在 ANSYS APDL观察电导率在固有频率附近的变化。 研究了分层和层内损坏的情况。分层就是分离 相邻层的破坏是整个结构刚度的降低。模态 结构的频率随着分层和损伤程度的增加而降低 在体内。进行预浸料的制造方法来制造复合材料 根据ASTM标准从中切出样品进行测试的面板。 压电测试提供了电阻两端的压降,表示耦合 修补程序与宿主结构的作用。表示的电导率图 响应由压电换能器驱动的身体变形。由于。。。导致的结果 有限元建模和实验表明,压电阻抗 技术可有效检测复合材料内的损坏或分层 结构体。

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