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Wyszukujesz frazę "composite aircraft structures" wg kryterium: Temat


Wyświetlanie 1-5 z 5
Tytuł:
IR thermography in NDE of carbon-glass laminate
Autorzy:
Pawluczy-Majka, J.
Powiązania:
https://bibliotekanauki.pl/articles/242394.pdf
Data publikacji:
2014
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
IR Thermography
NDE
Nordam Repair Division
non-destructive testing
composite aircraft structures
fracture
delamination
Opis:
The article presents a comparison of the effects of using active IR Thermography technique for the tests of composite aircraft structures. The most important question arising together with an increased use of composites in aviation industry is to work out a method, which would allow identification of the technological defects, and damages appeared in the process of the aircraft use. Non-destructive testing which has been used so far to identify defects in the aircraft structure made from metallic materials has a quite limited application in case of composite structures. With the growing use of composites in the aviation industry, a necessity appears to work out a method allowing early identification of technological defects and damages appeared in the process of the aircraft operation. It could be the active thermography techniques used for the thin walled elements tests, such as wing and fuselage skin, with the focus on fractures and delamination. Light composite aircraft have been built for a many of years, however, the annual flight hours of these aircraft are incomparably lower than those of the aircraft used in air transport. In group of light aircraft, the less important elements were made of composites regarding the strength of the whole construction. When the newest aircraft were introduced, with most important construction elements such as the fuselage, wings, horizontal and vertical tails, doors and the interior made of composite materials, it was expected that the increased amount of the annual flight hours (more than 3000 hours) and the expected airliner lifetime (about 30 000 hours) would soon cause degradation of the mechanical properties of the composites following from the progress of ageing of the composite structures. The obtained research results bring closer the problem of selection of the well-fitted non-destructive testing method depending on the kind of the diagnosed construction
Źródło:
Journal of KONES; 2014, 21, 4; 405-410
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Enhancement of Damage Detectability in Aircraft Structures Using the Fusion of NDT Results
Autorzy:
Zapłotny, M.
Katunin, A.
Dragan, K.
Powiązania:
https://bibliotekanauki.pl/articles/97990.pdf
Data publikacji:
2017
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:
aircraft composite structures
ultrasonic testing
information fusion
non-destructive testing
Opis:
Following the damage tolerance philosophy in aircraft design and operation, one of the most significant stages of maintenance is non-destructive testing of structures. It is, therefore, essential to use testing methods sensitive to particular damage types occurring in aircraft structures during operation. In this paper, the authors present a study on selection and comparison of methods of information fusion applied to testing the results of inspection of composite structures used in aircraft elements, obtained using various ultrasonic methods. The presented approach of fusion of ultrasonic scans allows for enhancement of damage detection and identification due to the presence of different parts of information about detected damage obtained from different initial information sources in a single resulting set. Such an approach can be helpful at the decision-making stage during inspection of aircraft elements and structures. Besides the methodology, the GUI-based software for performing fusion of various types of ultrasonic data is presented.
Źródło:
Fatigue of Aircraft Structures; 2017, 9; 55-74
2081-7738
2300-7591
Pojawia się w:
Fatigue of Aircraft Structures
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Lightning Strike Protection of Aircraft Composite Structures: Analysis and Comparative Study
Autorzy:
Katunin, A.
Powiązania:
https://bibliotekanauki.pl/articles/97865.pdf
Data publikacji:
2016
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:
lightning strike protection
conductive composite
aircraft structures
Opis:
Lightning strikes are a serious problem during operation of aircraft due to the increasing applicability of polymeric composites in aircraft structures and the weak electrical conducting properties of such structures. In composite structures, lightning strikes may cause extended damage sites which require to be appropriately maintained and repaired leading to increased operational costs. In order to overcome this problem various lightning strike protection solutions have been developed. Some of them are based on the immersion of metallic elements and particles while others use novel solutions such as intrinsically conductive polymers or other types of highly conductive particles including carbon nanotubes and graphene. The concept of fully organic electrically conductive composites based on intrinsically conductive polymers is currently being developed at the Silesian University of Technology. The results obtained in numerous tests, including concerning electrical conductivity and the capability to carry on high-magnitude electrical charges as well as certain operating properties need to be compared with existing solutions in lightning strike protection of aircraft. The following study presents the properties of the material developed for lightning strike protection and a comparative study with other solutions.
Źródło:
Fatigue of Aircraft Structures; 2016, 8; 49-54
2081-7738
2300-7591
Pojawia się w:
Fatigue of Aircraft Structures
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
A Brief Review on NDT&E Methods For Structural Aircraft Components
Autorzy:
Wronkowicz-Katunin, A.
Powiązania:
https://bibliotekanauki.pl/articles/97992.pdf
Data publikacji:
2018
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:
NDT&E methods
non-destructive testing
non-destructive evaluation
aircraft structures
composite structures
Opis:
The paper presents a summary of non-destructive testing and evaluation (NDT&E) methods applied in inspections of structural aircraft components. This brief review covers the most commonly applied methods such as visual and penetrant inspections, tap-testing, eddy current inspections, shearography, thermography, acoustic emission testing, radiographic and tomographic inspections, and ultrasonic inspections. The general operating principles of these methods as well as their main advantages, limitations and application areas are described below.
Źródło:
Fatigue of Aircraft Structures; 2018, 10; 73-81
2081-7738
2300-7591
Pojawia się w:
Fatigue of Aircraft Structures
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Przegląd rozwiązań strukturalnych w zakresie ochrony struktur kompozytowych przed uderzeniem pioruna
Review of structural solutions in regard to lightning strike protection of composite structures
Autorzy:
Zdębski, S.
Powiązania:
https://bibliotekanauki.pl/articles/212961.pdf
Data publikacji:
2016
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:
struktury kompozytowe
samolot
piorun
siatka
aluminium
miedź
śmigłowiec
composite structures
aircraft
lightning
net
copper
helicopter
Opis:
Artykuł opisuje konstrukcje kompozytowe stosowane w lotnictwie, które narażone są na wyładowania atmosferyczne. Zaprezentowano skutki wyładowania atmosferycznego w kontakcie z kompozytem węglowym. Przedstawiono sposób ochrony kompozytu z użyciem zalaminowanej siatki odprowadzającej ładunki elektryczne oraz odprowadzającej i odbierającej ciepło. Przybliżono technologię wytwarzania siatki, budowę siatki LSP oraz sposób doboru odpowiedniego wariantu siatki LSP. Użyto siatki miedzianej, która umożliwiła odprowadzenie ładunków do zewnętrznej powierzchni obiektu latającego, nie tylko rozprowadzenia ładunku elektrycznego w bezpośrednim sąsiedztwie miej sca uderzenia pioruna. Zweryfikowano zasadność wyboru siatki miedzianej i sposobu aplikacji za pomocą wyników prób technologicznych wykonania ochrony przeciwpiorunowej na kompozytach. Przedstawiono lyzyko na jakie narażone są samoloty i śmigłowce podczas swoich lotów oraz sposoby minimalizacji szkód powstałych w wyniku wyładowań atmosferycznych.
The article describes aviation composite structures exposed to lightning strike. Results of atmospheric discharge with carbon reinforced composite contact were presented. There was shown a way to protect the composite with use of laminated net discharging the electric current as well as discharging and absorbing heat. Manufacturing technology of the net was brought closer, as well as the structure and selection strategy of the LSP net. A copper mesh has been used, that enabled channelling the current to the outer surface of a flying object, not only distribution of the current in direct proximity of the strike. The copper mesh choice has been verified and the application method, by the results of technological trials.
Źródło:
Prace Instytutu Lotnictwa; 2016, 2 (243); 40-52
0509-6669
2300-5408
Pojawia się w:
Prace Instytutu Lotnictwa
Dostawca treści:
Biblioteka Nauki
Artykuł
    Wyświetlanie 1-5 z 5

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