Fiber Optic Sensors for Structural Health Monitoring of Air Platforms

被引：235

作者：

Guo, Honglei ^{[2
]}

Xiao, Gaozhi ^{[1
]}

Mrad, Nezih ^{[3
]}

Yao, Jianping ^{[2
]}

机构：

[1] Natl Res Council Canada, Inst Microstruct Sci, Ottawa, ON K1A 0R6, Canada

[2] Univ Ottawa, Microwave Photon Res Lab, Sch Informat Technol & Engn, Ottawa, ON K1N 6N5, Canada

[3] Natl Def Hdq, Air Vehicles Res Sect, Def R&D Canada, Dept Natl Def, Ottawa, ON K1A 0K2, Canada

来源：

SENSORS | 2011年 / 11卷 / 04期

关键词：

aircraft; damage detection; fiber Bragg grating; fiber optic acoustic sensor; load monitoring; structural health monitoring; BRAGG GRATING SENSORS; UNDERWATER ACOUSTIC SENSOR; DAMAGE DETECTION; FATIGUE-CRACK; WAVE; INTERROGATION; AIRCRAFT; STRAIN; SYSTEM; LASER;

D O I：

10.3390/s110403687

中图分类号：

O65 [分析化学];

学科分类号：

070302 ; 081704 ;

摘要：

Aircraft operators are faced with increasing requirements to extend the service life of air platforms beyond their designed life cycles, resulting in heavy maintenance and inspection burdens as well as economic pressure. Structural health monitoring (SHM) based on advanced sensor technology is potentially a cost-effective approach to meet operational requirements, and to reduce maintenance costs. Fiber optic sensor technology is being developed to provide existing and future aircrafts with SHM capability due to its unique superior characteristics. This review paper covers the aerospace SHM requirements and an overview of the fiber optic sensor technologies. In particular, fiber Bragg grating (FBG) sensor technology is evaluated as the most promising tool for load monitoring and damage detection, the two critical SHM aspects of air platforms. At last, recommendations on the implementation and integration of FBG sensors into an SHM system are provided.

引用

页码：3687 / 3705

页数：19

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