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CLC number: V27

On-line Access: 2024-08-27

Received: 2023-10-17

Revision Accepted: 2024-05-08

Crosschecked: 2012-05-29

Cited: 8

Clicked: 6258

Citations:  Bibtex RefMan EndNote GB/T7714

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Journal of Zhejiang University SCIENCE A 2012 Vol.13 No.7 P.538-545

http://doi.org/10.1631/jzus.A1100336


Strain transfer of surface-bonded fiber Bragg grating sensors for airship envelope structural health monitoring


Author(s):  Hai-tao Zhao, Quan-bao Wang, Ye Qiu, Ji-an Chen, Yue-ying Wang, Zhen-min Fan

Affiliation(s):  School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China

Corresponding email(s):   zht@sjtu.edu.cn, qiuye@sju.edu.cn

Key Words:  Airship envelope, Fiber Bragg grating (FBG), Surface-bonded, Strain transfer, Structural health monitoring (SHM)



Abstract: 
This paper deals with an improved bonding approach of surface-bonded fiber Bragg grating (FBG) sensors for airship envelope structural health monitoring (SHM) under the strain transfer theory. A theoretical formula is derived from the proposed model to predict the strain transfer relationship between the airship envelope and fiber core. Then theoretical predictions are validated by numerical analysis using the finite element method (FEM). Finally, on the basis of the theoretical approach and numerical validation, parameters that influence the strain transfer rate from the airship envelope to fiber core and the ratio of effective sensing length are analyzed, and some meaningful conclusions are provided.

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