Advanced sensors and sensing systems for structural health monitoring in aerospace composites
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F70883521%3A28110%2F24%3A63580563" target="_blank" >RIV/70883521:28110/24:63580563 - isvavai.cz</a>
Výsledek na webu
<a href="https://onlinelibrary.wiley.com/doi/10.1002/adem.202401745" target="_blank" >https://onlinelibrary.wiley.com/doi/10.1002/adem.202401745</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1002/adem.202401745" target="_blank" >10.1002/adem.202401745</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Advanced sensors and sensing systems for structural health monitoring in aerospace composites
Popis výsledku v původním jazyce
This review examines the state-of-the-art sensors and sensing technologies employed for structural health monitoring (SHM) in aerospace composites, highlighting the shift from conventional nondestructive evaluation techniques to real-time monitoring systems. The review discusses the challenges associated with composite materials, such as their anisotropic nature and susceptibility to invisible damage, and how these challenges have driven the improvement of SHM techniques. Fiber-optic sensors, including interferometric, distributed, and grating-based sensors, are analyzed for their high sensitivity and multiplexing capabilities, making them suitable for distributed sensing applications. Piezoelectric sensors are evaluated for their effectiveness in both active and passive damage detection methods. At the same time, piezoresistive self-sensing systems are explored for their potential to integrate sensing directly into composite materials. The review also addresses the challenges encountered in implementing SHM systems. It suggests solutions like protective coatings, advanced data processing algorithms, and modular system design to overcome these challenges. In conclusion, this review provides a comprehensive overview of the current SHM technologies for aerospace composites, underscoring the need for sustained research and development to improve sensor technology, expand data processing capabilities, and ensure seamless integration with aircraft systems, thus contributing to the safety and efficiency of aerospace operations. Structural health monitoring: This review covers the latest sensors for structural health monitoring in aerospace composites, highlighting advancements in fiber-optic, piezoelectric, and piezoresistive systems. It also addresses challenges like sensor integration and data processing, concluding with recommendations for further research to enhance aerospace safety and system efficiency.
Název v anglickém jazyce
Advanced sensors and sensing systems for structural health monitoring in aerospace composites
Popis výsledku anglicky
This review examines the state-of-the-art sensors and sensing technologies employed for structural health monitoring (SHM) in aerospace composites, highlighting the shift from conventional nondestructive evaluation techniques to real-time monitoring systems. The review discusses the challenges associated with composite materials, such as their anisotropic nature and susceptibility to invisible damage, and how these challenges have driven the improvement of SHM techniques. Fiber-optic sensors, including interferometric, distributed, and grating-based sensors, are analyzed for their high sensitivity and multiplexing capabilities, making them suitable for distributed sensing applications. Piezoelectric sensors are evaluated for their effectiveness in both active and passive damage detection methods. At the same time, piezoresistive self-sensing systems are explored for their potential to integrate sensing directly into composite materials. The review also addresses the challenges encountered in implementing SHM systems. It suggests solutions like protective coatings, advanced data processing algorithms, and modular system design to overcome these challenges. In conclusion, this review provides a comprehensive overview of the current SHM technologies for aerospace composites, underscoring the need for sustained research and development to improve sensor technology, expand data processing capabilities, and ensure seamless integration with aircraft systems, thus contributing to the safety and efficiency of aerospace operations. Structural health monitoring: This review covers the latest sensors for structural health monitoring in aerospace composites, highlighting advancements in fiber-optic, piezoelectric, and piezoresistive systems. It also addresses challenges like sensor integration and data processing, concluding with recommendations for further research to enhance aerospace safety and system efficiency.
Klasifikace
Druh
J<sub>imp</sub> - Článek v periodiku v databázi Web of Science
CEP obor
—
OECD FORD obor
20505 - Composites (including laminates, reinforced plastics, cermets, combined natural and synthetic fibre fabrics; filled composites)
Návaznosti výsledku
Projekt
—
Návaznosti
S - Specificky vyzkum na vysokych skolach
Ostatní
Rok uplatnění
2024
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název periodika
Advanced Engineering Materials
ISSN
1438-1656
e-ISSN
1527-2648
Svazek periodika
26
Číslo periodika v rámci svazku
22
Stát vydavatele periodika
DE - Spolková republika Německo
Počet stran výsledku
27
Strana od-do
—
Kód UT WoS článku
001325999200001
EID výsledku v databázi Scopus
2-s2.0-85205454549