|
|
Research Progress of Structural Health Monitoring Technology for Aircraft |
TIAN Tong1, LI Jianle1, DENG Deshuang1, ZENG Xu1, LIN Kuixu1, DONG Shanshan1, YANG Lei1, XU Hao2, YANG Zhengyan3, WU Zhanjun2 |
1. College of Mechanics and Aerospace Engineering, Dalian University of Technology, Dalian 116024, China;
2. College of Materials Science and Engineering, Dalian University of Technology, Dalian 116024, China;
3. Jiangnan University, Wuxi 214122, China |
|
|
Abstract Structural health monitoring (SHM) technology is poised to play a pivotal role in the design, service, and maintenance of aircraft, enhancing structural efficiency and ensuring the safety and reliability of aircraft structures. This article begins by outlining the fundamental concepts and applicability of SHM, emphasizing its significance in the aerospace industry. Subsequently, it delves into the research landscape of SHM technology in typical aircraft structures, focusing on advanced techniques such as impact monitoring, ultrasonic guided wave damage detection, and strain monitoring using fiber optic sensors. The review encompasses an overview of international and domestic research progress, technological capabilities, and typical applications. Lastly, it highlights the challenging issues facing structural health monitoring in aircraft structures and provides insights into its promising future applications in the aerospace field.
|
|
|
|
|
[1] |
WU Zhanjun, DONG Shanshan, LI Jianle, ZHU Mingrui, ZHANG Shicheng, LIU Haitao, SUN Liang, LI Hanke, DONG Zimai, XU Hao. Quantitative Identification Method of Composite Material Delamination Damage Based on Distributed Optical Fiber Sensing and U-Net Network[J]. Aeronautical Manufacturing Technology, 2024, 67(13): 20-27. |
|
|
|
|