Wszystkie pola: Sałaciński, M. - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Diagnosis and Repair Technology of Damaged Elements of Casa Aircraft
Autorzy:: Salacinski, M.
Synaszko, P.
Olszak, R.
Powiązania:: https://bibliotekanauki.pl/articles/97837.pdf
Data publikacji:: 2010
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Opis:: Recently Polish Air Force has been equipped with new types of aircraft. New aircraft have many elements made of composites. Composites enable increasing performance but also pose new challenges. One of these challenges is the necessity of repairing after damage. This paper presents the results of the non-destructive inspection (MIA, conductivity, optical measurement ) of the C-295 plane after damage. Some parts made of composites and metal were damaged. In this paper, the authors propose a technology of repairing damaged parts.
Źródło:: Fatigue of Aircraft Structures; 2010, 2; 98-105
2081-7738
2300-7591
Pojawia się w:: Fatigue of Aircraft Structures
Dostawca treści:: Biblioteka Nauki

Artykuł

Skocz do pozycji: 2.

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

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