@inproceedings{d0a3bf3167904fb6864823a5a0463884,
title = "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 can't 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.",
keywords = "Lamb wave, Partial poling, Piezoelectric film, Sensor, Structural health monitoring",
author = "Zhang, \{Yu Long\} and Zhang, \{Wei Fang\} and Zhang, \{Ai Ai\}",
year = "2014",
doi = "10.4028/www.scientific.net/AMM.530-531.62",
language = "英语",
isbn = "9783038350392",
series = "Applied Mechanics and Materials",
publisher = "Trans Tech Publications",
pages = "62--65",
booktitle = "Advances in Measurements and Information Technologies",
address = "德国",
note = "2014 International Conference on Sensors Instrument and Information Technology, ICSIIT 2014 ; Conference date: 18-01-2014 Through 19-01-2014",
}