Development of an integrated sacrificial sensor for damage detection and monitoring in composite materials and adhesively bonded joints

被引:6
作者
Olafsson, G. [1 ]
Tighe, R. C. [2 ]
Boyd, S. W. [1 ]
Dulieu-Barton, J. M. [3 ]
机构
[1] Univ Southampton, Sch Engn, Southampton SO16 7QF, Hants, England
[2] Univ Waikato, Sch Engn, Hamilton, New Zealand
[3] Univ Bristol, Bristol Composites Inst, Sch Civil Aerosp & Mech Engn, Bristol, Avon, England
来源
STRUCTURAL HEALTH MONITORING-AN INTERNATIONAL JOURNAL | 2021年 / 20卷 / 06期
基金
英国工程与自然科学研究理事会;
关键词
Non-destructive evaluation; structural health monitoring; integrated sensor; adhesively bonded joints; DEFECTS; LOAD;
D O I
10.1177/1475921721989041
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Quality assurance of adhesively bonded joints is of vital importance if their benefits are to be exploited across a wide range of industrial applications. A novel lightweight, low-cost, non-invasive embedded sacrificial sensor is proposed, capable of detecting damage within an adhesively bonded joint, which could also be used in a laminated composite structure. The sensor operation uses changes in electrical resistance, increasing as the sensing material area diminishes with damage progression. Initial tests prove the sensor concept by showing that the electrical resistance of the sensor increases proportionally with material removal, mimicking the sensor operation. Thermography is used to verify the current flow through the sensor and that any localised heating caused by the sensor is minimal. Short beam interlaminar shear strength (ILSS) tests show that embedding sensors in a composite laminates did not cause a reduction in material interfacial structural performance. Finally, the in situ performance of the sensor is demonstrated in quasi-static tensile tests to failure of adhesively bonded single lap joints (SLJs) with sensors embedded in the bond line. Prior to crack initiation, an electrical response occurs that correlates with increasing applied load, suggesting scope for secondary uses of the sensor for load monitoring and cycle counting. Crack initiation is accompanied by a rapid increase in electrical resistance, providing an indication of failure ahead of crack propagation and an opportunity for timely repair. As the crack damage propagated, the electrical response of the sensor increased proportionally. The effect of the sensor on the overall structural performance was assessed by comparing the failure load of joints with and without the embedded sensor with no measurable difference in ultimate strength. The research presented in the article serves as an important first step in developing a simple yet promising new technology for structural health monitoring with numerous potential applications.
引用
收藏
页码:3406 / 3423
页数:18
相关论文
共 24 条
  • [1] A Review on SHM Techniques and Current Challenges for Characteristic Investigation of Damage in Composite Material Components of Aviation Industry
    Abbas, Saqlain
    Li, Fucai
    Qiu, Jianxi
    [J]. MATERIALS PERFORMANCE AND CHARACTERIZATION, 2018, 7 (01) : 224 - 258
  • [2] Adams R.D., 1974, J STRAIN ANAL, V9, P185, DOI [DOI 10.1243/03093247V093185, 10.1243/03093247V093185]
  • [3] A REVIEW OF DEFECT TYPES AND NONDESTRUCTIVE TESTING TECHNIQUES FOR COMPOSITES AND BONDED JOINTS
    ADAMS, RD
    CAWLEY, P
    [J]. NDT INTERNATIONAL, 1988, 21 (04): : 208 - 222
  • [4] Nondestructive testing of adhesively-bonded joints
    Adams, RD
    Drinkwater, BW
    [J]. NDT & E INTERNATIONAL, 1997, 30 (02) : 93 - 98
  • [5] [Anonymous], 2005, ENG MECH COMPOSITE M
  • [6] Optimisation of steel-composite connections for structural marine applications
    Boyd, S. W.
    Blake, J. I. R.
    Shenoi, R. A.
    Mawella, J.
    [J]. COMPOSITES PART B-ENGINEERING, 2008, 39 (05) : 891 - 906
  • [7] THE SIGNIFICANCE OF DAMAGE AND DEFECTS AND THEIR DETECTION IN COMPOSITE-MATERIALS - A REVIEW
    CANTWELL, WJ
    MORTON, J
    [J]. JOURNAL OF STRAIN ANALYSIS FOR ENGINEERING DESIGN, 1992, 27 (01) : 29 - 42
  • [8] Evaluating the localised through-thickness load transfer and damage initiation in a composite joint using digital image correlation
    Crammond, G.
    Boyd, S. W.
    Dulieu-Barton, J. M.
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2014, 61 : 224 - 234
  • [9] Structural health monitoring techniques for aircraft composite structures
    Diamanti, K.
    Soutis, C.
    [J]. PROGRESS IN AEROSPACE SCIENCES, 2010, 46 (08) : 342 - 352
  • [10] Sensing of Damage Mechanisms in Fiber-Reinforced Composites under Cyclic Loading using Carbon Nanotubes
    Gao, Limin
    Thostenson, Erik T.
    Zhang, Zuoguang
    Chou, Tsu-Wei
    [J]. ADVANCED FUNCTIONAL MATERIALS, 2009, 19 (01) : 123 - 130