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Active Piezoelectric Dynamic Absorbers on Vibration and Noise Reductions of the Fuselage

Published online by Cambridge University Press:  05 May 2011

Y.-M. Huang  and
H.-C. Tseng
Y.-M. Huang*
Affiliation:
Department of Mechanical Engineering, National Central University, Chung-Li, Taiwan 32001, R.O.C.
H.-C. Tseng*
Affiliation:
Department of Mechanical Engineering, National Central University, Chung-Li, Taiwan 32001, R.O.C.
*
*Professor
**Graduate student
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Abstract

This research focuses on the analysis of vibration and noise control of a fuselage. A closed cylindrical shell is chosen as the theoretical model of the fuselage of an aircraft. The noise resulted from propellers is the main source of excitation to the fuselage vibration. The vibration can further induce interior noise within the fuselage. For attenuating the vibration of the fuselage and its accompanying interior noise, several pairs of piezoelectric sheets are attached to the shell. Each piezoelectric pair connected to an appropriate electric circuit can serve as a dynamic absorber. For a better performance, feedback control algorithms are introduced to form active absorbers. The dynamic responses of the composite cylindrical shell and the corresponding interior sound fields are analytically formulated. Numerical results are presented. The active absorbers are proven to yield good effects on vibration and noise reductions. Some parameter studies are also given in this manuscript.

Keywords

Vibration of cylindrical shellActive dynamic absorbersVibration and noise control
Type
Articles
Information
Journal of Mechanics , Volume 24 , Issue 1 , March 2008 , pp. 69 - 77
Copyright
Copyright © The Society of Theoretical and Applied Mechanics, R.O.C. 2008

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References

1.Jones, J. D. and Fuller, C. R., “Reduction of Interior Sound Fields in Flexible Cylinders by Active Vibration Control,” Proceedings of the 6th IMAC Conference, Florida, U.S.A. (1983).Google Scholar
2.Fuller, C. R. and Jones, J. D., “Experiments on Reduction of Propeller Induced Interior Noise by Active Control of Cylinder Vibration,” Journal of Sound and Vibration, 112, pp. 389–395 (1987).CrossRefGoogle Scholar
3.Thomas, D. R., Nelson, P. A. and Elliott, S. J., “Active Control of the Transmission of Sound through a Thin Cylindrical Shell, Part I: The Minimization of Vibration Energy,” Journal of Sound and Vibration, 167, pp. 91–111(1993).CrossRefGoogle Scholar
4.Thomas, D. R., Nelson, P. A. and Elliott, S. J., “Active Control of the Transmission of Sound through a Thin Cylindrical Shell, Part II: The Minimization of Acoustic Potential Energy,” Journal of Sound and Vibration, 167, pp. 112–128(1993).Google Scholar
5.Mandic, D. S. and Jones, J. D., “Adaptive Active Control of Enclosed Sound Fields in Elastic Cylinders via Vibrational Inputs,” AIAA, pp. 89–1075 (1989).CrossRefGoogle Scholar
6.Simpson, M. A., Luong, T. M., Fuller, C. R. and Jones, J. D., “Full-Scale Demonstration Tests of Cabin Noise Reduction Using Active Vibration Control,” Journal of Aircraft, 28, pp. 208–215 (1991).CrossRefGoogle Scholar
7.Bullmore, A. J., Nelson, P. A. and Elliott, S. J., “Theoretical Studies of the Active Control of the Propeller-Induced Cabin Noise,” Journal of Sound and Vibration, 140, pp. 191–271 (1990).CrossRefGoogle Scholar
8.Silcox, R. J., Lester, H. C. and Abler, S. B., “An Evaluation of Active Noise Control in a Cylindrical Shell,” ASME Journal of Vibration, Acoustics, Stress, and Reliability in Design, 111, pp. 337–342 (1989).CrossRefGoogle Scholar
9.Simpson, M. A. and Tran, B. N., “Aircraft Cabin Active Noise Control Performance Sensitivity Tests,” AIAA, pp. 93–4436 (1993).CrossRefGoogle Scholar
10.Fuller, C. R., Maillard, J. P., von Flotow, A. H. and Mercadal, M., “Control of Aircraft Interior Noise Using Globally Mis-tuned Vibration Absorbers,” Proceedings of First Joint CEAS/AIAA Aeroacoustics Conference, Germany (1995).Google Scholar
11.Huang, Y. M. and Fuller, C. R., “The Effects of Dynamic Absorbers on the Forced Vibration of a Cylindrical Shell and Its Coupled Interior Sound Field,” Journal of Sound and Vibration, 200, pp. 401–418 (1997).CrossRefGoogle Scholar
12.Huang, Y. M. and Fuller, C. R., “Vibration and Noise Control of the Fuselage via Dynamic Absorbers,” ASME Journal of Vibration and Acoustics, 120, pp. 496–502 (1998).CrossRefGoogle Scholar
13.Huang, Y. M. and Chen, C. C., “Optimal Design of Dynamic Absorbers on the Vibration and Noise Control of a Fuselage,” Computers and Structures, 76, pp. 691–702 (2000).CrossRefGoogle Scholar
14.Halvorsen, W. G. and Emborg, U., “Interior Noise Control of the SAAB 340 Aircraft,” SAE Paper 891080 (1989).CrossRefGoogle Scholar
15.Dosch, J. J., Inman, D. J. and Garcia, E., “A Self-Sensing Piezoelectric Actuator for Collocated Control,” Journal of Intelligent Material Systems and Structures, 3, pp. 166–185 (1992).CrossRefGoogle Scholar
16.Tzou, H. S., Piezoelectric Shells: Distributed Sensing and Control of Continua, Kluwer Academic Publishers, Dordercht, Netherlands (1993).Google Scholar
17.Anderson, E. H. and Hagood, N. W., “Simultaneous Piezoelectric Sensing/ Actuator: Analysis and Application to Controlled Structures,” Journal of Sound and Vibration, 174, pp. 617–639 (1994).CrossRefGoogle Scholar
18.Wang, B. T., Chen, P. H. and Chen, R. L., “Finite Element Model Verification for the Use of Piezoelectric Sensor in Structural Modal Analysis,” Journal of Mechanics, 22, pp. 107–114 (2006).CrossRefGoogle Scholar
19.Hollkamp, J. J., “Multimodal Passive Vibration Suppression with Piezoelectric Materials and Resonant Shunts,” Journal of Intelligent Material Systems and Structure, 5, pp. 49–57 (1994).CrossRefGoogle Scholar
20.Hagood, N. W. and von Flotow, A., “Damping of Structure Vibration with Piezoelectric Materials and Passive Electrical Networks,” Journal of Sound and Vibration, 146, pp. 243–268(1991).CrossRefGoogle Scholar
21.Wang, K. W., Yu, W. K. and Lai, J. S., “Adaptive-Passive Control of Structural Vibrations via Piezoelectric Materials with Real-Time Adaptive Circuits,” Proceedings of Noise-Con 94, Florida, U.S.A. (1994).CrossRefGoogle Scholar
22.Huang, Y. M. and Yang, C. H., “Using Piezoelectric Dynamic Absorbers on Noise Control of the Fuselage,” Journal of Chinese Society of Mechanical Engineers, 24, pp. 147–155 (2003).Google Scholar
23.Tasi, M. S. and Wang, K. W., “Control of a Ring Structure with Multiple Active-Passive Hybrid Piezoelectrical Networks,” Journal of Smart Materials and Structure, 5, pp. 695–703 (1996).Google Scholar
24.Tasi, M. S. and Wang, K. W., “On the Structure Damping Characteristics of Active Piezoelectric Actuators with Passive Shunt,” Journal of Sound and Vibration, 221, pp. 1–22(1999).Google Scholar
25.Yang, C. H., “Using Electromechanical Dynamic Absorbers on Vibration and Noise Control of the Fuselage,” Master Thesis, National Central University, Taiwan, R.O.C. (1997).Google Scholar
26.Soedel, W., Vibrations of Shells and Plates, Marcel Dekker, Inc., New York, U.S.A. (1981).Google Scholar
27.Fahy, F., Sound and Structural Vibration: Radiation, Transmission and Response, Academic Press, London, Britain (1985).Google Scholar