Study on New Structural Health Monitoring Sensor of Aircraft

Yu Long Zhang; Wei Fang Zhang; Ai Ai Zhang

doi:10.4028/www.scientific.net/AMM.530-531.62

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 530-531Study on New Structural Health Monitoring Sensor...

Study on New Structural Health Monitoring Sensor of Aircraft

Abstract:

Sensor is the core component of structural health monitoring system, which can collect the data of structural damage. The structural damage state can be gained after further processing. Aircraft serves in rigorous environment, and existing sensors cant meet the demand of its structural damage monitoring for inherent defect. A preparation method of partial poling piezoelectric film sensor was proposed in the paper, which can be used for structural damage monitoring of aircraft in combination with lamb wave.

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Periodical:

Applied Mechanics and Materials (Volumes 530-531)

Pages:

62-65

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.530-531.62

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Online since:

February 2014

Authors:

Yu Long Zhang*, Wei Fang Zhang, Ai Ai Zhang

Keywords:

Lamb Wave, Partial Poling, Piezoelectric Film, Sensor, Structural Health Monitoring (SHM)

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* - Corresponding Author

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