Optical fiber sensing and reconstruction method for morphing wing flexible skin shape

被引:0
|
作者
Qu D. [1 ]
Sun G. [1 ]
Li H. [1 ]
Lou X. [1 ]
Zhu L. [1 ]
机构
[1] Beijing Engineering Research Center of Optoelectronic Information and Instruments, Beijing Information Science and Technology University, Beijing
关键词
Fiber grating; Flexible sensing; Flexible skin; Morphing wing; Reconstruction algorithm;
D O I
10.19650/j.cnki.cjsi.j1702537
中图分类号
学科分类号
摘要
In order to solve the problem of real-time monitoring of flexible skin shape of morphing wing, the fiber sensing and reconstruction method of flexible skin shape is studied. The relationship between the wavelength shift of fiber grating and the bending curvature of the flexible skin, and the interpolation surface reconstruction algorithm based on curvature information are theoretically analyzed. An experiment system for curvature calibration of flexible skin was built. A flexible skin with two layers of silicone rubber embedding organic silica gel and fiber Bragg grating sensors was fabricated. The wavelength shifts of the fiber grating for different samples under different curvatures were experimentally measured. The relationship between the wavelength shift of the fiber grating and the curvature of the flexible skin is analyzed. The interpolation algorithm is used to reconstruct the deformation surface of the flexible skin. The technical feasibility of real time monitoring of morphing wing flexible skin shape with fiber sensing is verified. The study results show that the fiber grating sensing method can be used for real-time shape perception of flexible skin; the measurable curvature range is not less than 25 m-1 and the sensitivity can reach 28.07 pm/m-1. The optical fiber sensing method has a promising application prospect in real-time monitoring of deformed wing shape. © 2018, Science Press. All right reserved.
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页码:144 / 151
页数:7
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共 20 条
  • [1] Platus A.D.L., Negative-stiffness-mechanism vibration isolation systems, Proceedings of SPIE - The International Society for Optical Engineering, 3786, 2, pp. 44-54, (1999)
  • [2] Guo T.B., Bai J.Q., Yang Y.X., Influence analysis of continuous trailing-edge variable camber wing on aerodynamic characteristics of airliner, Journal of Beijing University of Aeronautics and Astronautics, 43, 8, pp. 1559-1566, (2017)
  • [3] Tao T., Chen Q., Feng S., Et al., High-precision real-time 3D shape measurement using a bi-frequency scheme and multi-view system, Applied Optics, 56, 13, (2017)
  • [4] Wang Y., Negahdaripour S., Aykin M.D., Calibration and 3D reconstruction of underwater objects with non-single-view projection model by structured light stereo imaging, Applied Optics, 55, 24, (2016)
  • [5] Yatabe K., Ishikawa K., Oikawa Y., Compensation of fringe distortion for phase-shifting three-dimensional shape measurement by inverse map estimation, Applied Optics, 55, 22, (2016)
  • [6] Daneshpanah M., Javidi B., Three-dimensional imaging with detector arrays on arbitrarily shaped surfaces, Optics Letters, 36, 5, pp. 600-602, (2011)
  • [7] Tao T., Chen Q., Da J., Et al., Real-time 3-D shape measurement with composite phase-shifting fringes and multi-view system, Optics Express, 24, 18, (2016)
  • [8] Song Y.M., Meng F.Y., Lou X.P., Et al., Research on static load identification using FBG orthogonal sensing network, Journal of Electronic Measurement and Instrumentation, 31, 8, pp. 1227-1232, (2017)
  • [9] Blandino J., Duncan R., Nuckels M., Et al., Three-dimensional shape sensing for inflatable booms, AIAA Journal, (2015)
  • [10] Clements G.M., Fiber optic sensor for precision 3-D position measurement, (2005)