- Tytuł:
- Composite Aerospace Structure Monitoring with use of Integrated Sensors
- Autorzy:
-
Dragan, K.
Dziendzikowski, M.
Kurnyta, A.
Salacinski, M.
Klysz, S.
Leski, A. - Powiązania:
- https://bibliotekanauki.pl/articles/97867.pdf
- Data publikacji:
- 2015
- Wydawca:
- Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
- Tematy:
-
structural health monitoring
PZT sensor network
barely visible impact damages - Opis:
- One major challenge confronting the aerospace industry today is to develop a reliable and universal Structural Health Monitoring (SHM) system allowing for direct aircraft inspections and maintenance costs reduction. SHM based on guided Lamb waves is an approach capable of addressing this issue and satisfying all the associated requirements. This paper presents an approach to monitoring damage growth in composite aerospace structures and early damage detection. The main component of the system is a piezoelectric transducers (PZT) network integrated with composites. This work describes sensors’ integration with the structure. In particular, some issues concerning the mathematical algorithms giving information about damage from the impact damage presence and its growth are discussed.
- Źródło:
-
Fatigue of Aircraft Structures; 2015, 7; 12-17
2081-7738
2300-7591 - Pojawia się w:
- Fatigue of Aircraft Structures
- Dostawca treści:
- Biblioteka Nauki
Artykuł