TY - GEN
T1 - Flexible and Transparent Conductive Meshes with Localized Cracks for Highly Sensitive Straining Sensing in Transparent Components
AU - Liu, Linjie
AU - Wang, Bing
AU - Chen, Xiaoliang
AU - Li, Sheng
AU - Gong, Shougang
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - The transparent components of aircraft cockpit canopies undergo complex strain during flight, making effective strain monitoring crucial. Traditional rigid sensors face installation challenges on complex curved surfaces of cockpit canopies, while commercial strain gauges struggle to combine high transmittance with high sensitivity. This paper aims to develop a flexible, transparent, and highly sensitive strain sensor for real-time monitoring of transparent aircraft cockpit canopies. The sensor utilizes polydimethylsiloxane (PDMS) as a flexible substrate and adopts a mesh-like design to ensure high transparency. By integrating silver conductive meshes with localized spontaneous crack patterns, the sensor achieves ultrahigh sensitivity capable of detecting minute strains as low as 0.001%, which is critical for identifying early-stage structural anomalies. Experimental results demonstrate that the proposed sensor exhibits exceptional sensitivity (with a gauge factor of 1061 within a 1% strain range) while maintaining a visible light transmittance of 81.67%. The sub-millistrain resolution further ensures precise monitoring of subtle deformations under dynamic flight conditions. This sensing strategy has minimal impact on the optical performance of cockpit canopies, providing an effective technical solution for lightweight integrated health monitoring of transparent aerospace components.
AB - The transparent components of aircraft cockpit canopies undergo complex strain during flight, making effective strain monitoring crucial. Traditional rigid sensors face installation challenges on complex curved surfaces of cockpit canopies, while commercial strain gauges struggle to combine high transmittance with high sensitivity. This paper aims to develop a flexible, transparent, and highly sensitive strain sensor for real-time monitoring of transparent aircraft cockpit canopies. The sensor utilizes polydimethylsiloxane (PDMS) as a flexible substrate and adopts a mesh-like design to ensure high transparency. By integrating silver conductive meshes with localized spontaneous crack patterns, the sensor achieves ultrahigh sensitivity capable of detecting minute strains as low as 0.001%, which is critical for identifying early-stage structural anomalies. Experimental results demonstrate that the proposed sensor exhibits exceptional sensitivity (with a gauge factor of 1061 within a 1% strain range) while maintaining a visible light transmittance of 81.67%. The sub-millistrain resolution further ensures precise monitoring of subtle deformations under dynamic flight conditions. This sensing strategy has minimal impact on the optical performance of cockpit canopies, providing an effective technical solution for lightweight integrated health monitoring of transparent aerospace components.
KW - Flexible
KW - Transparent Components
KW - strain sensor
UR - https://www.scopus.com/pages/publications/105018737093
U2 - 10.1109/NEMS67320.2025.11169966
DO - 10.1109/NEMS67320.2025.11169966
M3 - 会议稿件
AN - SCOPUS:105018737093
T3 - 2025 IEEE 20th International Conference on Nano/Micro Engineered and Molecular Systems, NEMS 2025
SP - 396
EP - 399
BT - 2025 IEEE 20th International Conference on Nano/Micro Engineered and Molecular Systems, NEMS 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 20th IEEE International Conference on Nano/Micro Engineered and Molecular Systems, NEMS 2025
Y2 - 11 May 2025 through 14 May 2025
ER -