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Simultaneous position and displacement sensing using two bre Bragg grating sensors

机译:使用两个 fbre布拉格光栅传感器同时感测位置和位移

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摘要

Over the years, many shape sensing methods have been developed with technologies including optical bre, PZTand fringe projection. Among them, optical bres have gained a lot of attention due to their unobtrusive naturewhen either surface mounted or embedded in the structure. Optical bre Bragg gratings (FBG) are currentlyemployed for structural health monitoring in civil and aerospace systems and their shape sensing capabilitieshave been previously reported. In this paper, we propose a novel bre optic based shape sensor of an isotropiccantilever beam based on the principles of interferometry and FBG sensing. The method described in this paperuses a standard single core single-mode optical bre and the least number of sensors to estimate the shape,making it comparatively an inexpensive sensing method. On displacing the beam with an unknown magnitudeand at an unknown location along the beam, we are able to demonstrate that we can measure the shape of thedisplaced beam and the magnitude and location of the force applied. The analysis involves using a calibrationmethod and an iterative calculation to measure the two unknowns. An analytical model based on the knownbeam theories was used to assess the accuracy of the measurements. The preliminary analysis yielded an accuracyof ±1 mm and ±50 mm for the displacement and location, respectively.
机译:多年来,已经开发了许多形状感应方法,包括光学\ fbre,PZT \ r \ n和条纹投影技术。其中,无论是表面安装还是嵌入结构中,光学纤维都具有引人注目的特性,因此受到了广泛的关注。光纤布拉格光栅(FBG)目前已被用于民用和航空航天系统的结构健康监测,并且其形状感测能力以前也已有报道。在本文中,我们基于干涉法和FBG传感原理,提出了一种新型的基于\光纤的各向同性\ r \ n悬臂梁形状传感器。本文描述的方法\ n使用标准的单芯单模光纤和最少数量的传感器来估计形状,从而使其成为一种比较便宜的传感方法。在以未知的大小\ r \ n以及沿波束的未知位置移动波束时,我们能够证明我们可以测量\ r \ n移位的波束的形状以及所施加力的大小和位置。分析涉及使用校准方法和迭代计算来测量两个未知数。基于已知的光束理论的分析模型用于评估测量的准确性。初步分析得出位移和位置的精度分别为±1 mm和±50 mm。

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  • 会议地点 0277-786X;1996-756X
  • 作者单位

    Aerospace NDT Laboratory, Faculty of Aerospace Engineering, Delft University ofTechnology, Kluyverweg 1, 2629 HS Delft, The Netherlands N.Nazeer@tudelft.nl;

    Aerospace NDT Laboratory, Faculty of Aerospace Engineering, Delft University ofTechnology, Kluyverweg 1, 2629 HS Delft, The Netherlands R.M.Groves@tudelft.nl;

    Structural Integrity Composites, Faculty of Aerospace Engineering, Delft University ofTechnology, Kluyverweg 1, 2629 HS Delft, The Netherlands R.Benedictus@tudelft.nl;

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