Design of Embedded FBG Sensor System for Ultralight Aircraft Wing Monitoring

被引：0
|
作者：
Dvorak, Milan [1 ]
Ruzicka, Milan [1 ]
Kabrt, Miroslav [2 ]
机构：
[1] Czech Tech Univ, Fac Mech Engn, Prague 16607 4, Czech Republic
[2] Vanessa Air Spol Sro, Litomysl 57001, Czech Republic
来源：
STRUCTURAL HEALTH MONITORING 2015: SYSTEM RELIABILITY FOR VERIFICATION AND IMPLEMENTATION, VOLS. 1 AND 2 | 2015年
关键词：
D O I：
暂无
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
This paper presents an experimental investigation of sensor system for monitoring of ultralight aircraft wing. Fiber Bragg Grating (FBG) sensors were chosen as a suitable strain sensors for integration into the composite structural parts. At first, influence of embedded optical fibers on an adhesive joint performance was evaluated, using the single-lap bonded joint specimens. In the next step, FBG sensors were integrated into the load bearing parts of cantilever wing beam and tested during the ground static strength test of the complete wing.
引用
收藏
页码：1665 / 1672
页数：8
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