New sensor technologies in aircraft structural health monitoring

被引:0
|
作者
Shang Bo-lin [1 ]
Song Bi-feng [1 ]
Chang Fei [1 ]
机构
[1] NW Polytech Univ, Coll Aeronaut, Xian 710072, Peoples R China
关键词
aircraft; structural health monitoring; sensors;
D O I
暂无
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
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.
引用
收藏
页码:701 / 704
页数:4
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