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Damage evaluation and strain monitoring of composite plates using metal-coated FBG sensors under quasi-static indentation

机译:准静态压痕下金属涂层FBG传感器对复合板的损伤评估和应变监测

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摘要

Metal-coated optical fiber sensors (MCOFSs) have a memory effect due to the elasto-plastic characteristics of the metal coating. Our study is first implementation of a new concept for damage evaluation of composite plates using the memory effect of MCOFSs. Quasi-static indentation (QSI) tests for a carbon fiber reinforced plastic (CFRP) composite plate were performed using metal-coated fiber Bragg grating (FBG) sensors. For validation of the QSI tests, a finite element analysis (FEA) based on the continuum damage mechanics (CDM) considering a damage model was performed using a commercial software, ABAQUS/Explicit. The structural responses and damage propagation of the composite plate under QSI were investigated. The results obtained by the experiments and the FEA agreed well. It was found that the metal-coated FBG sensor well monitored the strains of the plate under QSI in real-time. Moreover, the induced permanent residual strains of the surface bonded metal-coated FBG sensors increased with an increase of two parameters (i.e., the central displacement of indentor and the total energy). Based on the damage propagation of the plate and the correlation among three parameters including the residual strains, three damage levels of composite plates were classified. It was verified that the damage level of the composite plate can be simply evaluated by assessing the induced residual strains by metal-coated FBG sensors.
机译:金属涂层的光纤传感器(MCOFS)由于金属涂层的弹塑性特性而具有记忆效应。我们的研究是首次使用MCOFS的记忆效应对复合板的损伤进行评估的新概念的实施。使用金属涂层的光纤布拉格光栅(FBG)传感器对碳纤维增强塑料(CFRP)复合板进行了准静态压痕(QSI)测试。为了验证QSI测试,使用了商用软件ABAQUS / Explicit,基于考虑损伤模型的连续损伤力学(CDM)进行了有限元分析(FEA)。研究了QSI下复合板的结构响应和损伤扩展。实验和有限元分析获得的结果一致。结果发现,金属涂层的FBG传感器可以很好地实时监控QSI下的板应变。此外,表面结合的金属涂覆的FBG传感器的感应永久残余应变随着两个参数(即,压头的中心位移和总能量)的增加而增加。根据板的损伤传播和残余应变这三个参数之间的相关性,对复合板的三种损伤等级进行了分类。已经证实,通过评估金属涂层的FBG传感器引起的残余应变,可以简单地评估复合板的损伤程度。

著录项

  • 来源
    《Composites 》 |2014年第11期| 36-45| 共10页
  • 作者单位

    Launch Complex Team (LCT), KSLV-Ⅱ R&D Executive Office, Korea Aerospace Research Institute (KARI), 169-84 Gwahak-ro, Yuseong-gu, Daejeon 305-806, Republic of Korea;

    Ship Performance Research Department Ⅱ, Hyundai Marine Research Institute, Hyundai Heavy Industries, 1000 Bangeojinsunhwan-doro, Dong-gu, Ulsan 682-792, Republic of Korea;

    Schoot of Mechanical, Aerospace and Systems Engineering, KAIST, 291 Daehak-ro, Yuseong-gu, Daejeon 305-701, Republic of Korea;

    The William E. Boeing Department of Aeronautics and Astronautics, University of Washington, USA;

    Center for Safety Measurement, Korea Research Institute of Standards and Science, 1 Doryong-dong, Yuseong-gu, Daejeon 305-340, Republic of Korea;

    Agency for Defense Development, Daejeon, Republic of Korea;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    A. Plates; B. Impact behavior; C. Finite element analysis (FEA); D. Mechanical testing; E. Memory effects;

    机译:A.盘子;B.冲击行为;C.有限元分析(FEA);D.机械测试;E.记忆效应;

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