한국소음진동공학회논문집 (Transactions of the Korean Society for Noise and Vibration Engineering)

  • 제16권12호
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  • Pages.1252-1261
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  • 2006
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  • 1598-2785(pISSN)
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  • 2287-5476(eISSN)
한국소음진동공학회 (The Korean Society for Noise and Vibration Engineering)
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항공기용 하니콤 트림판넬의 다채널 능동제어

Multichannel Active Control of Honeycomb Trim Panels for Aircrafts

  • 홍진숙 (부산대학교 기계공학부)
  • 발행 : 2006.12.20
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초록

This paper summarizes theoretical work on the multichannel decentralized feedback control of sound radiation from aircraft trim panels using piezoceramic actuators. The aircraft trim panels are generally honeycomb structures designed to meet the design requirement of low weight and high stiffness. They are resiliently-mounted to the fuselage for the passive reduction of noise transmission. It is motivated by the localization of reduction in vibration of single channel active trim panels. 12-channel decentralized feedback control systems are investigated in terms of the reduction of noise and vibration for three configurations of sensor actuator pairs. Local coupling of the closely-spaced sensor and actuator pairs was modeled using single degree of freedom systems. The multichannel control system is characterized using the state-space model. For the stability point of view, the relative stability or robustness is evaluated by comparing the real part of eigenvalues of the system matrix for the three configurations. The control performance is also evaluated and compared for the three configurations. It is found that the multichannel system can lead to the globalization of the reduction in vibration and radiated noise. It does not appear to yield a significant improvement in the vibration because of decreased gain margin. However, the reduction in the radiated noise is remarkably improved due to the variation of the vibration pattern with the actuation configurations.

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참고문헌

  1. Mixson, J. S. and Wilby, J. F., 1995, Interior Noise, Aeroacoustics of Flight Vehicles, Theory and Practice, edited by H. H. Hubbard, NASA Langley Research Center
  2. Mixon, J. S. and Powell, C. A., 'Review of Recent Research on Interior Noise of Propeller Aircraft', AIAA/NASA 9th Aeroacoustics Conference (Williamsburg, VA)
  3. Gardonio, P., 2002, 'Review of Active Technique for Aerospace Vibro-acoustic Control' , Journal of Aircraft, Vol.39, No.2. pp.206-214 https://doi.org/10.2514/2.2934
  4. Gardonio, P. and Elliott, S. J., 1999, 'Active Control of Structure-borne and Airborne Sound Transmission through Double Panel', Journal of Aircraft, Vol.36, No.6, pp.1023-1032 https://doi.org/10.2514/2.2544
  5. Maury, C., Gardonio, P. and Elliott, C. P. S., 2002, 'Model for Active Control of Flow-induced Noise Transmitted through Double Partitions', AIAA Journal, Vol.40, No.6, pp.1113-1121 https://doi.org/10.2514/2.1760
  6. Sulc, J., Hofr, J. and Benda, L., 1982, 'Exterior Noise on the Fuselage of Light Propeller Driven Aircraft in Flight', Journal of Sound and Vibration, Vol.84, No.1, pp.105-120 https://doi.org/10.1016/0022-460X(82)90435-7
  7. Bhat, W. V., 1999, 'Flight Test Measurement of Exterior Turbulent Boundary Layer Pressure Fluctuations on Boeing Model 737 Airplane', Journal of Sound and Vibration, Vol.14, No.4, pp.439-457 https://doi.org/10.1016/0022-460X(71)90574-8
  8. Mixson, J. S., Barton, C. K. Vaicatis, R. 1978, 'Investigation of Interior Noise In a Twin-engine Light Aircraft', Journal of Aircraft, Vol.15, No.4, pp. 227-233 https://doi.org/10.2514/3.58346
  9. Pope, L. D., Wilby, E. G. and Wilby, J. F., 1987, 'Propeller Aircraft Interior Noise Model, Part II : Theoretical Model', Journal of Sound and Vibration, Vol.118, No.3, pp.449-467 https://doi.org/10.1016/0022-460X(87)90364-6
  10. Pope, L. D., Willis, C. M. and Mayer, W., 1987, 'Propeller Aircraft Interior Noise Model, Part II: Scale-model and Flight-test Comparison', Journal of Sound and Vibration, Vol.118, No.3, pp. 469-493 https://doi.org/10.1016/0022-460X(87)90365-8
  11. Unruh, J. F., 1988, 'Structure-borne Noise Control for Propeller Aircraft', Journal of Aircraft, Vol.17, No.2, pp.752-757
  12. Unruh, J. F., 1989, 'Installation Effects on Propeller Wake/vortex-induced Structure-borne Noise Transmissions', Journal of Aircraft, Vol.27, No.5, pp.444-448
  13. Vaicatis, R. 1980, 'Noise Transmissions Into a Light Aircraft', Journal of Aircraft, Vol. 17, No.2, pp.81-86 https://doi.org/10.2514/3.57877
  14. Barton, C. K. and Mixson, J. S., 1981, 'Noise Transmission and Control for a Light Twin-engine Aircraft', Journal of Aircraft, Vol. 18, No.7, pp. 570-575 https://doi.org/10.2514/3.57528
  15. Nelson, P. A. and Elliott, S. J., 1992, 'Active Control of Sound', Academic Press, New York
  16. Fuller, C. R., Elliott, S. J., Nelson, .P. A., 1996, 'Active Control of Vibration', Academic Press, London
  17. Nilsson, E., Nilsson, A. C, 2002, 'Prediction and Measurement of Some Dynamic Properties of Sandwich Structures with Honeycomb and Foam Cores', Journal of Sound and Vibration, Vol. 251, No.3, pp.409-430 https://doi.org/10.1006/jsvi.2001.4007
  18. Saito, T., Parbery, R. D., Okuno, S. and Kawano, S., 1997, 'Parameter Identification for Aluminum Honeycomb Sandwich Panels Based on Orthotropic Timoshenko Beam Theory', Journal of Sound and Vibration, Vol. 208, No.2, pp.271-287 https://doi.org/10.1006/jsvi.1997.1189
  19. Hong, C. 2005, 'Active Control of Resilienly-mounted Flexible Structures', PhD Thesis, ISVR, University of Southampton
  20. Hong, C., 2007 'Local Feedback Control of Light Honeycomb Panels', J. Acoust. Soc. Am. Vol. 121, No.1, pp.1-12 https://doi.org/10.1121/1.2401650
  21. Hong, C., 'Local Coupling between Actuator and Sensor Pairs in Light Honeycomb Structures' , J. of Sound and Vibration, to be published
  22. Stothers, I. 2004, 'Personal Communications'
  23. Reddy, J. N., 1996, 'Mechanics of Laminated Composite Plates' , CRC Press Inc
  24. Warburton, G. B. 1951, 'The Vibration of Rectangular Plates', Proceeding of Institute of Mechanical Engineering, Vol.168, No.2, pp.371-384
  25. Leissa, A. W., 1969. 'Theory of Plates' , NASA
  26. Fahy, F., Walker, J., 2004, 'Advanced Applications in Acoustics' Noise and Vibration, Spon Press