Optical Fiber Sensors for Aircraft Structural Health Monitoring

被引：164

作者：

Garcia, Iker ^{[1
]}

Zubia, Joseba ^{[1
]}

Durana, Gaizka ^{[1
]}

Aldabaldetreku, Gotzon ^{[1
]}

Asuncion Illarramendi, Maria ^{[2
]}

Villatoro, Joel ^{[1
,3
]}

机构：

[1] Univ Basque Country UPV EHU, ETSI Bilbao, Dept Commun Engn, Bilbao 48013, Spain

[2] Univ Basque Country UPV EHU, ETSI Bilbao, Dept Appl Phys, Bilbao 48013, Spain

[3] IKERBASQUE Basque Fdn Sci, E-48011 Bilbao, Spain

来源：

SENSORS | 2015年 / 15卷 / 07期

关键词：

structural health monitoring; optical fiber sensors; fiber Bragg grating; long period grating; turbine condition monitoring; LONG-PERIOD GRATINGS; BRAGG-GRATINGS; STRAIN-MEASUREMENT; IMPACT DETECTION; TIP CLEARANCE; FBG SENSORS; TEMPERATURE; GAUGE; SENSITIVITY; TECHNOLOGY;

D O I：

10.3390/s150715494

中图分类号：

O65 [分析化学];

学科分类号：

070302 ; 081704 ;

摘要：

Aircraft structures require periodic and scheduled inspection and maintenance operations due to their special operating conditions and the principles of design employed to develop them. Therefore, structural health monitoring has a great potential to reduce the costs related to these operations. Optical fiber sensors applied to the monitoring of aircraft structures provide some advantages over traditional sensors. Several practical applications for structures and engines we have been working on are reported in this article. Fiber Bragg gratings have been analyzed in detail, because they have proved to constitute the most promising technology in this field, and two different alternatives for strain measurements are also described. With regard to engine condition evaluation, we present some results obtained with a reflected intensity-modulated optical fiber sensor for tip clearance and tip timing measurements in a turbine assembled in a wind tunnel.

引用

页码：15494 / 15519

页数：26

共 71 条

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