TY - JOUR
T1 - Real-time fatigue crack prediction using self-sensing buckypaper and gated recurrent unit
AU - Hwang, Hyeonho
AU - Song, Jinwoo
AU - Kim, Heung Soo
AU - Chattopadhyay, Aditi
N1 - Funding Information:
This research was supported by the MOTIE (Ministry of Trade, Industry, and Energy) in Korea, under the Fostering Global Talents for Innovative Growth Program (P0017307) supervised by the Korea Institute for Advancement of Technology (KIAT).
Publisher Copyright:
© 2023, The Korean Society of Mechanical Engineers and Springer-Verlag GmbH Germany, part of Springer Nature.
PY - 2023/3
Y1 - 2023/3
N2 - Aircraft is regarded as a collection of modern technologies from throughout all industries. However, it is inevitable to develop defects during its service life. In general, the aircraft has a periodic maintenance period, and is inspected according to a well-established process, for example non-destructive testing. However, the maintenance requires massive time and cost. If an unexpected defect occurs due to external environments before the maintenance cycle returns, it is impossible to prevent subsequent damage. This study proposes a novel real-time fatigue crack prediction method using self-sensing carbon nanotube buckypaper and deep learning algorithm. Carbon nanotube buckypaper was fabricated by the wet method. The physics-informed gated recurrent unit was used to predict real time crack growth. The physics-informed deep learning model accurately predicted the fatigue crack length. The results showed that the proposed method is promising in detecting the real-time fatigue crack growth of aircraft structure.
AB - Aircraft is regarded as a collection of modern technologies from throughout all industries. However, it is inevitable to develop defects during its service life. In general, the aircraft has a periodic maintenance period, and is inspected according to a well-established process, for example non-destructive testing. However, the maintenance requires massive time and cost. If an unexpected defect occurs due to external environments before the maintenance cycle returns, it is impossible to prevent subsequent damage. This study proposes a novel real-time fatigue crack prediction method using self-sensing carbon nanotube buckypaper and deep learning algorithm. Carbon nanotube buckypaper was fabricated by the wet method. The physics-informed gated recurrent unit was used to predict real time crack growth. The physics-informed deep learning model accurately predicted the fatigue crack length. The results showed that the proposed method is promising in detecting the real-time fatigue crack growth of aircraft structure.
KW - Buckypaper
KW - Carbon nanotube
KW - Fatigue crack
KW - Gated recurrent unit
KW - Strain sensing
KW - Structural health monitoring
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U2 - 10.1007/s12206-023-0226-y
DO - 10.1007/s12206-023-0226-y
M3 - Article
AN - SCOPUS:85148906407
SN - 1738-494X
VL - 37
SP - 1401
EP - 1409
JO - Journal of Mechanical Science and Technology
JF - Journal of Mechanical Science and Technology
IS - 3
ER -