New sensor technologies in aircraft structural health monitoring

Bo Lin Shang, Bi Feng Song, Fei Chang

科研成果: 书/报告/会议事项章节会议稿件同行评审

11 引用 (Scopus)

摘要

The traditional nondestructive testing (NDT) method contributes greatly to aircraft structural safety and reliability. However, it also significantly increases operating expense, or leads to the decrease of the aircraft's runtime because of the disassemble and reassemble of structural components. Aircraft structural health monitoring (SHM) is a new in-situ, online structure detection method which was developed on the basis of the traditional NDT method. It can increase the reliability, safety and runtime of aircrafts while reduce the structure's operating and maintenance costs. This paper describes this new technology and introduces the principles and applications of some new sensor technologies in aircraft structural health monitoring, the candidate SHM sensor technologies including optical fiber sensors, piezoelectric sensors, MEMS sensors, wireless sensing systems etc. The paper will finish with a perspective for further research in this field.

源语言英语
主期刊名Proceedings of 2008 International Conference on Condition Monitoring and Diagnosis, CMD 2008
出版商IEEE Computer Society
701-704
页数4
ISBN(印刷版)9781424416219
DOI
出版状态已出版 - 2008
活动2008 International Conference on Condition Monitoring and Diagnosis, CMD 2008 - Beijing, 中国
期限: 21 4月 200824 4月 2008

出版系列

姓名Proceedings of 2008 International Conference on Condition Monitoring and Diagnosis, CMD 2008

会议

会议2008 International Conference on Condition Monitoring and Diagnosis, CMD 2008
国家/地区中国
Beijing
时期21/04/0824/04/08

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