Study of Piezoelectric Vibration Damping Based on the SSDI Technology for Aircraft Panels

Li Zhang; Kai Xiang Li; Xia Sheng Sun

doi:10.4028/www.scientific.net/AMM.422.105

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 422Study of Piezoelectric Vibration Damping Based on...

Study of Piezoelectric Vibration Damping Based on the SSDI Technology for Aircraft Panels

Abstract:

In this paper, the typical aircraft panel is excited by the noise induced in traveling wave tube, the vibratory phenomenon of the typical aircraft panel is researched in detail. The piezoelectric vibration of the aircraft panels is damped by Synchronized Switch Damping on Inductor technology (SSDI technology). The acceleration parameters of the structure are controlled and the effect of structural damping is achieved.

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Periodical:

Applied Mechanics and Materials (Volume 422)

Pages:

105-112

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.422.105

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Online since:

September 2013

Authors:

Li Zhang*, Kai Xiang Li, Xia Sheng Sun

Keywords:

Aircraft Panels, Piezoelectric Vibration Damping, SSDI Technology

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* - Corresponding Author

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