From nonlinear system identification to structural health monitoring
Conférence invitée
Date
2016Résumé
The process of implementing a damage monitoring strategy for aerospace, civil and mechanical engineering infrastructure is referred to as structural health monitoring (SHM) and implies a sensor network that monitors the behavior of the structure on-line. A SHM process potentially allows for an optimal use of the monitored structure, a minimized downtime, and the avoidance of catastrophic failures. The SHM process classically relies on four sequential steps that are damage detection, localization, classification, and quantification. The key idea underlying this seminary is that structural damages may result in nonlinear dynamical signatures that are not yet used in SHM despite the fact that they can significantly enhance their monitoring. We thus propose to monitor these structural damages by identifying their nonlinear signature on the basis of a cascade of Hammerstein models representation of the structure. This model is here estimated at very low computational cost by means of the Exponential Sine Sweep Method. It will be shown that on the basis of this richer dynamical representation of the structure, SHM algorithms dedicated to damage detection, classification and quantification can be derived. This will be illustrated in the aeronautic and civil engineering contexts and using experimental as well as numerical data.
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Documents liés
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Communication sans acte
RÉBILLAT, Marc;
NICARD, Cyril;
DEVOS, Olivier;
EL MAY, Mohamed; LETELLIER, Frédéric; THOMACHOT, Matthieu; FOURNIER, Marc;
MECHBAL, Nazih (2024-09)
al components, roughening the outer surface, loosening fasteners, hastening cracking, and facilitating the entry of water into electronic fixtures. In 2016, the combined commercial aircraft fleet operated by European ... -
Communication avec acteREBUFA, Jocelyn; JAUSSAUD, Gladys; FOURNIER, Marc; LOGEAIS, M.; BENCHEIKH, N.; CLAEYSSEN, F.;
RÉBILLAT, Marc;
GUSKOV, Mikhail (A. Benjeddou, N. Mechbal and J.F. Deü, 2019)
Required improvements of piezoelectric elements actuation and measurement system efficiency and robustness are introduced as a critical feature for structural health monitoring (SHM) applications. An electronic module (Lamb ... -
Communication avec acteJAUSSAUD, Gladys; REBUFA, Jocelyn; FOURNIER, Marc; LOGEAIS, Matthieu; BENCHEIKH, Nabil;
MECHBAL, Nazih;
RÉBILLAT, Marc (NTD, 2019)
In the context of Condition Based Maintenance (CBM) for aircrafts, Structural Health Monitoring (SHM) is one main field of research. Detection and localization of damages in a structure request reliability of the equipment ... -
Communication avec acte
WIRTH, Ingo;
RÉBILLAT, Marc;
LETELLIER, Frederic; KOHL, Mario; CONEN, Jan; BECKER, Marc-Oliver; RUSCH, Tim (Dept. of Mechanical Engineering & Aeronautics University of Patras, 2023)
This paper presents the research activities in the framework of the European MORPHO H2020 project regarding the integration of sensors in composite parts using printing technologies. Printed sensors reported here are ... -
Communication sans acte
RÉBILLAT, Marc; NICARD, Cyril;
EL MAY, Mohamed; LETELLIER, Frédéric; DUBENT, Sébastien; THOMACHOT, Mathieu; FOURNIER, Marc;
MECHBAL, Nazih (2024)
Corrosion is a major threat in the aeronautic industry, both in terms of safety and cost. Efficient, versatile, and cost affordable solutions for corrosion monitoring are thus needed. Ultrasonic Lamb Waves (LW) appear to be ...
