Effect of thermal residual stress on FBG sensors embedded in composite T-stiffened panels

被引:1
作者
Zhou Yujing [1 ]
Liu Gang [1 ]
Li Xueqin [1 ]
Yi Xiaosu [1 ]
机构
[1] Beijing Inst Aeronaut Mat, Sci & Technol Adv Composites Lab, Beijing 10095, Peoples R China
来源
MECHANICAL ENGINEERING AND MATERIALS, PTS 1-3 | 2012年 / 152-154卷
关键词
FBG sensors; T- stiffened panel; Residual strain; Low-velocity impact;
D O I
10.4028/www.scientific.net/AMM.152-154.1550
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The reflection spectrum from the Fiber Bragg Grating (FBG) sensors embedded in the composite was disturbed because of the thermal residual stress. In this study, two types of the FBG sensors, uncoated and UV-cured resin coated FBG sensors, were embedded in the triangle area of the T-stiffened composite panels. The strains during the curing process were measured by these two kinds of FBG sensors. Through the comparison of the results, it was found that the effect of thermal residual stress on the reflection spectrum could be attenuated when the FBG sensor was coated with UV-cured resin. Furthermore, the strain responses during the low-velocity impact test were observed by both two FBG sensors. The maximum-strain measured by the coated FBG sensors was more accurately than that measured by the uncoated one.
引用
收藏
页码:1550 / 1554
页数:5
相关论文
共 7 条
  • [1] Embedded fibre Bragg grating sensors in advanced composite materials
    Kuang, KSC
    Kenny, R
    Whelan, MP
    Cantwell, WJ
    Chalker, PR
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2001, 61 (10) : 1379 - 1387
  • [2] Okabe Y., 2001, COMPOS SCI TECHNOL, V61, p[1379, 1382]
  • [3] Structural health monitoring of marine composite structural joints using embedded fiber Bragg grating strain sensors
    Silva-Munoz, Rodrigo A.
    Lopez-Anido, Roberto A.
    [J]. COMPOSITE STRUCTURES, 2009, 89 (02) : 224 - 234
  • [4] Taked A.S., 2002, COMPOS PART A-APPL S, V33, p[971, 980]
  • [5] Structural health monitoring of composite wing structure during durability test
    Takeda, S.
    Aoki, Y.
    Ishikawa, T.
    Takeda, N.
    Kikukawa, H.
    [J]. COMPOSITE STRUCTURES, 2007, 79 (01) : 133 - 139
  • [6] Delamination monitoring of laminated composites subjected to low-velocity impact using small-diameter FBG sensors
    Takeda, S
    Minakuchi, S
    Okabe, Y
    Takeda, N
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2005, 36 (07) : 903 - 908
  • [7] Wu Z.J., 2004, ACTA MAT COMPOSITES, V21, p[1, 3]