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Procedure to Use PZT Sensors in Vibration and Load Measurements

DOI: 10.1155/2013/173605

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Abstract:

In situ correlation procedure is developed for electromechanically coupled PZT sensors to output the structural responses in standard engineering format, namely, displacement, strain, acceleration, and so forth. In order to implement this idea, we have used the standard sensing devices such as laser displacement sensor, strain gauge, and accelerometer. Aluminum beams and composite plate are employed in the experiments as specimens. The experimental results have shown that the structural reactions at critical locations can be monitored by a dynamically correlated PZT patch sensor, besides measuring the intensity of load in terms of acceleration. Furthermore, the influence of damage on sensor correlation has been evaluated. It is seen that the presence of damage has significantly modified the interpreted engineering parameters from the PZT patch and if they are appropriately correlated with respect to healthy structure, then the occurrence of damage related information will be ascertained. The developed sensor correlation concept therefore may be useful in load monitoring, health monitoring, and structural control applications. 1. Introduction Piezoelectric materials are a class of smart materials, which can be used as sensors and actuators to build adaptive and health monitoring aerospace structures. Introduction of these multifunctional materials into composites offers a great potential for stiffness tailoring, static shape correction, health monitoring, and vibration control applications [1–6]. Future unmanned aerospace vehicles demand high performance structural systems with self-thinking and adaptive capabilities, where piezoelectric composite materials may be considered as a solution to build adaptive structural concepts [7–9]. A structural system can be made diagnosable, when it is able to communicate its response with respect to various disturbances. In this regard, PZT material in thin film form provides the distributed sensing opportunity for the structural system to read its spatial information. However the data read from the sensors must be interpreted or examined with a proven health monitoring algorithm or procedure for knowing the vital information such as occurrence of damage, intensity of damage, location of damage, and loading intensity. The sensory information may be static or dynamic (vibration) in real time; therefore the electromechanically coupled (PZT) sensor is found suitable for a frequency dependent response monitoring application. Structural health monitoring concepts, involving piezoelectric sensors, have got considerable

References

[1]  J. Sirohi and I. Chopra, “Fundamental understanding of piezoelectric strain sensors,” Journal of Intelligent Material Systems and Structures, vol. 11, no. 4, pp. 246–257, 2000.
[2]  K. Umesh and R. Ganguli, “Shape and vibration control of a smart composite plate with matrix cracks,” Smart Materials and Structures, vol. 18, no. 2, Article ID 025002, 2009.
[3]  J. R. White, D. E. Adams, and K. Jata, “Structural health monitoring of a metallic sandwich panel by the method of virtual forces,” Structural Health Monitoring, vol. 8, no. 6, pp. 537–553, 2009.
[4]  Z. Su, X. Wang, L. Cheng, L. Yu, and Z. Chen, “On selection of data fusion schemes for structural damage evaluation,” Structural Health Monitoring, vol. 8, no. 3, pp. 223–241, 2009.
[5]  S. Kumar, N. Roy, and R. Ganguli, “Monitoring low cycle fatigue damage in turbine blade using vibration characteristics,” Mechanical Systems and Signal Processing, vol. 21, no. 1, pp. 480–501, 2007.
[6]  S. Gopalakrishnan, M. Ruzzene, and S. Hanagud, Computational Techniques for Structural Health Monitoring, Springer Series in Reliability Engineering, Springer, Heidelberg, Germany, 1st edition, 2011.
[7]  V. Giurgiutiu, A. Zagrai, and J. J. Bao, “Piezoelectric wafer embedded active sensors for aging aircraft structural health monitoring,” Structural Health Monitoring, vol. 1, no. 1, pp. 41–61, 2002.
[8]  V. Giurgiutiu and A. Zagrai, “Damage detection in thin plates and aerospace structures with the electro-mechanical impedance method,” Structural Health Monitoring, vol. 4, no. 2, pp. 99–118, 2005.
[9]  A. K. Rao, K. Natesan, M. S. Bhat, and R. Ganguli, “Experimental demonstration of H∞ control based active vibration suppression in composite fin-tip of aircraft using optimally placed piezoelectric patch actuators,” Journal of Intelligent Material Systems and Structures, vol. 19, no. 6, pp. 651–669, 2008.
[10]  S. Mohanty, A. Chattopadhyay, and P. Peralta, “Adaptive residual useful life estimation of a structural hotspot,” Journal of Intelligent Material Systems and Structures, vol. 21, no. 3, pp. 321–335, 2010.
[11]  P. M. Prashant and S. N. Jung, “Support vector machine based online composite helicopter rotor blade damage detection system,” Journal of Intelligent Material Systems and Structures, vol. 19, no. 10, pp. 1217–1228, 2008.
[12]  M. J. Sundaresan, A. Ghoshal, W. N. Martin, and M. J. Schulz, “A continuous sensor to measure acoustic waves in plates,” Journal of Intelligent Material Systems and Structures, vol. 12, no. 1, pp. 41–56, 2001.
[13]  C. P. Fritzen, G. Mengelkamp, and A. Guemes, “A CFRP plate with piezo-electric actuators and sensors as self-diagnosing intelligent structure,” in Proceedings of the International Conference on Noise and Vibration Engineering, pp. 185–191, Leuven, Belgium, September 2002.
[14]  A. Deraemaeker and A. Preumont, “Modal filter for vibration based damage detection,” in Proceedings of the 2nd European Workshop on Structural Health Monitoring, Forum am Deutschen Museum, pp. 844–851, Munich, Germany, 2004.
[15]  B. F. Spencer Jr., M. E. Ruiz-Sandoval, and N. Kurata, “Smart sensing technology: Opportunities and challenges,” Structural Control and Health Monitoring, vol. 11, no. 4, pp. 349–368, 2004.
[16]  J. M. Nichols, L. Moniz, M. Seaver, S. T. Trickey, and US Naval Research Laboratory, “Use of holder exponents and fibre optic sensing for detecting damage in an experimental plate structure,” in Proceeding of the 23rd International Modal Analysis Conference (IMAC '05), no. 197, Orlando, Fla, USA, 2005.
[17]  X. Qing, A. Kumar, C. Zhang, I. F. Gonzalez, G. Guo, and F.-K. Chang, “A hybrid piezoelectric/fiber optic diagnostic system for structural health monitoring,” Smart Materials and Structures, vol. 14, no. 3, pp. S98–S103, 2005.
[18]  P. Castellini, D. P. Willemann, and G. M. Revel, “Application of a laser doppler vibrometry for structural diagnostics on composite panels,” in Proceeding of the 23rd International Modal Analysis Conference (IMAC '05), no. 371, Orlando, Fla, USA, 2005.
[19]  B. J. Grisso, L. A. Martin, and D. J. Inman, “A wireless active sensing system for impedance-based structural health monitoring,” in Proceeding of the 23nd International Modal Analysis Conference (IMAC '05), no. 336, Orlando, Fla, USA, 2005.
[20]  J. M. Park, J. W. Kong, D. S. Kim, and D. J. Yoon, “Nondestructive damage detection and interfacial evaluation of single-fibers/epoxy composites using PZT, PVDF and P(VDF-TrFE) copolymer sensors,” Composites Science and Technology, vol. 65, no. 2, pp. 241–256, 2005.
[21]  B. Bonfiglioli, A. Strauss, G. Pascale, and K. Bergmeister, “Basic study of monitoring on fibre reinforced polymers: theoretical and experimental study,” Smart Materials and Structures, vol. 14, no. 3, pp. S12–S23, 2005.
[22]  S. Park, J. J. Lee, C. B. Yun, and D. J. Inman, “A built-in active sensing system-based structural health monitoring technique using statistical pattern recognition,” Journal of Mechanical Science and Technology, vol. 21, no. 6, pp. 896–902, 2007.
[23]  C. White, B. Whittingham, H. C. H. Li, I. Herszberg, and A. P. Mouritz, “Vibration based structural health monitoring of adhesively bonded composite scarf repairs,” in Proceeding of the 5th Australasian Congress on Applied Mechanics (ACAM '07), pp. 198–203, Engineers Australia, Brisbane, Australia, 2007.
[24]  X. Liu and Z. Jiang, “Design of a PZT patch for measuring longitudinal mode impedance in the assessment of truss structure damage,” Smart Materials and Structures, vol. 18, no. 12, Article ID 125017, 2009.
[25]  Y. Yang, H. Liu, V. G. M. Annamdas, and C. K. Soh, “Monitoring damage propagation using PZT impedance transducers,” Smart Materials and Structures, vol. 18, no. 4, Article ID 045003, 2009.
[26]  Q. Lei, Y. Shenfang, W. Qiang, S. Yajie, and Y. Weiwei, “Design and experiment of PZT network-based structural health monitoring scanning system,” Chinese Journal of Aeronautics, vol. 22, no. 5, pp. 505–512, 2009.
[27]  C. N. Sathyanarayana and S. Raja, “Multifunctional structure calibration by single measurement using hybrid approach for response monitoring,” in Proceeding of the of International Conference on Theoretical, Applied, Computational and Experimental Mechanics, paper ICTACEM -2010/316, Indian Institute of Technology, Kharagpur, India, December 2010.
[28]  V. G. M. Annamdas and C. K. Soh, “Application of electromechanical impedance technique for engineering structures: review and future issues,” Journal of Intelligent Material Systems and Structures, vol. 21, no. 1, pp. 41–59, 2010.
[29]  K. Diamanti and C. Soutis, “Structural health monitoring techniques for aircraft composite structures,” Progress in Aerospace Sciences, vol. 46, no. 8, pp. 342–352, 2010.

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