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© 2025 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.

Abstract

In the rapidly advancing era of intelligent technology, flexible strain sensors are emerging as a key component in wearable electronics. Laser-induced graphene (LIG) stands out as a promising fabrication method due to its rapid processing, environmental sustainability, low cost, and superior physicochemical properties. However, the stretchability and conformability of LIG are often limited by the substrate material, hindering its application in scenarios requiring high deformation. To address this issue, we propose a high-performance flexible and stretchable strain sensor fabricated by generating graphene on a polyimide (PI) substrate using laser induction and subsequently transferred onto a polydimethylsiloxane (PDMS). The resultant sensor demonstrates an ultra-low detection limit (0.1%), a rapid response time (150 ms), a wide strain range (40%), and retains stable performance after 1000 stretching cycles. Notably, this sensor has been successfully applied to the real-time monitoring of civil aviation test pilots during flight for the first time, enabling the accurate detection of physiological signals such as pulse, hand movements, and blink frequency. This study introduces a unique and innovative solution for the real-time health monitoring of civil aviation test pilots, with significant implications for enhancing flight safety.

Details

Title
Flexible Stretchable Strain Sensor Based on LIG/PDMS for Real-Time Health Monitoring of Test Pilots
Author
Li Shouqing 1 ; Wu Zhanghui 2 ; Fan Hongyun 2 ; Zhong Mian 3   VIAFID ORCID Logo  ; Xing Xiaoqing 3 ; Wang Yongzheng 4 ; Yang Huaxiao 5 ; Liu Qijian 6 ; Zhang, Deyin 2 

 Civil Aviation Administration of China Academy, Civil Aviation Flight University of China, Deyang 618307, China; [email protected] 
 College of Aviation and Electronics and Electrical, Civil Aviation Flight University of China, Deyang 618307, China; [email protected] (Z.W.); [email protected] (H.F.); [email protected] (X.X.); [email protected] (D.Z.) 
 College of Aviation and Electronics and Electrical, Civil Aviation Flight University of China, Deyang 618307, China; [email protected] (Z.W.); [email protected] (H.F.); [email protected] (X.X.); [email protected] (D.Z.), Key Laboratory of Flight Techniques and Flight Safety, Civil Aviation Administration of China, Deyang 618307, China 
 Civil Aviation Flight Test Institute, Civil Aviation Flight University of China, Deyang 618307, China; [email protected] 
 Mianyang Branch, Civil Aviation Flight University of China, Mianyang 621000, China; [email protected] 
 College of Computer Science, Civil Aviation Flight University of China, Deyang 618307, China; [email protected] 
First page
2884
Publication year
2025
Publication date
2025
Publisher
MDPI AG
e-ISSN
14248220
Source type
Scholarly Journal
Language of publication
English
ProQuest document ID
3203247555
Copyright
© 2025 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.