Zhang Naizhong, Turk Suzana, Davis Claire, Chiu Wing K, Boilard Tommy, Bernier Martin
Department of Mechanical and Aerospace Engineering, Monash University, Wellington Rd, Melbourne, VIC 3800, Australia.
Defence Science and Technology Group, 506 Lorimer Street, Fishermans Bend, Melbourne, VIC 3207, Australia.
Sensors (Basel). 2022 Nov 15;22(22):8812. doi: 10.3390/s22228812.
Strain sensing technology using fibre Bragg grating (FBG) sensors is an attractive capability for aerospace structural health monitoring (SHM) and assessment because they offer resistance to harsh environments, low maintenance, and potential for high density and high strain sensing. The development of FBG inscription techniques through the fibre polymer coating using infrared (IR) lasers has overcome the mechanical weaknesses introduced by removal of the fibre coating, which is typically required for conventional UV laser inscription of FBGs. Type I and Type II femtosecond gratings are fabricated using through-coating inscription techniques, but the higher laser energy used for Type II gratings damages the glass fibre core, impacting mechanical performance. This paper investigates the fatigue performance of Type I and Type II through-coating FBG sensors with different fibre geometries and photosensitisation approaches to evaluate their overall reliability and durability, with a view to assess their performance for potential use in civil and defence SHM applications. The fatigue performance of FBG sensors was assessed under high-strain and high-frequency mechanical loading conditions by using a custom-designed electro-dynamically actuated loading assembly. In addition, pre- and post-fatigue microscopic analyses and high-resolution reflection spectrum characterisation were conducted to investigate the failure regions of the fibres and the effect of fatigue loading on reflection spectrum features. As expected, Type I gratings had a significantly higher fatigue life compared to Type II gratings. However, Type II gratings performed significantly better than conventional UV laser-inscribed FBGs and electrical foil strain gauges. Type II gratings withstand higher temperatures, and are therefore more suitable for application in harsh environments.
使用光纤布拉格光栅(FBG)传感器的应变传感技术对于航空航天结构健康监测(SHM)和评估具有吸引力,因为它们能够抵抗恶劣环境、维护成本低,并且具有高密度和高应变传感的潜力。通过使用红外(IR)激光对光纤聚合物涂层进行FBG刻写技术的发展,克服了去除光纤涂层所带来的机械弱点,而去除光纤涂层通常是传统紫外激光刻写FBG所必需的。I型和II型飞秒光栅是使用穿透涂层刻写技术制造的,但用于II型光栅的较高激光能量会损坏玻璃光纤芯,影响机械性能。本文研究了具有不同光纤几何形状和光敏化方法的I型和II型穿透涂层FBG传感器的疲劳性能,以评估它们的整体可靠性和耐久性,旨在评估它们在民用和国防SHM应用中的潜在性能。通过使用定制设计的电动驱动加载组件,在高应变和高频机械加载条件下评估FBG传感器的疲劳性能。此外,进行了疲劳前后的微观分析和高分辨率反射光谱表征,以研究光纤的失效区域以及疲劳加载对反射光谱特征的影响。正如预期的那样,I型光栅的疲劳寿命明显高于II型光栅。然而,II型光栅的性能明显优于传统紫外激光刻写的FBG和箔式应变片。II型光栅能够承受更高的温度,因此更适合在恶劣环境中应用。