Adhesive properties and adhesive joints strength of graphite/epoxy composites
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60460709%3A41310%2F17%3A74335" target="_blank" >RIV/60460709:41310/17:74335 - isvavai.cz</a>
Výsledek na webu
<a href="http://dx.doi.org/10.1088/1742-6596/842/1/012073" target="_blank" >http://dx.doi.org/10.1088/1742-6596/842/1/012073</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1088/1742-6596/842/1/012073" target="_blank" >10.1088/1742-6596/842/1/012073</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Adhesive properties and adhesive joints strength of graphite/epoxy composites
Popis výsledku v původním jazyce
The article presents the results of experimental research of the adhesive joints strength of graphite/epoxy composites and the results of the surface free energy of the composite surfaces. Two types of graphite/epoxy composites with different thickness were tested which are used to aircraft structure. The single-lap adhesive joints of epoxy composites were considered. Adhesive properties were described by surface free energy. Owens-Wendt method was used to determine surface free energy. The epoxy two-component adhesive was used to preparing the adhesive joints. Zwick/Roell 100 strength device were used to determination the shear strength of adhesive joints of epoxy composites. The strength test results showed that the highest value was obtained for adhesive joints of graphite-epoxy composite of smaller material thickness (0,48 mm). Statistical analysis of the results obtained, the study showed statistically significant differences between the values of the strength of the confidence level of 0,95. Th
Název v anglickém jazyce
Adhesive properties and adhesive joints strength of graphite/epoxy composites
Popis výsledku anglicky
The article presents the results of experimental research of the adhesive joints strength of graphite/epoxy composites and the results of the surface free energy of the composite surfaces. Two types of graphite/epoxy composites with different thickness were tested which are used to aircraft structure. The single-lap adhesive joints of epoxy composites were considered. Adhesive properties were described by surface free energy. Owens-Wendt method was used to determine surface free energy. The epoxy two-component adhesive was used to preparing the adhesive joints. Zwick/Roell 100 strength device were used to determination the shear strength of adhesive joints of epoxy composites. The strength test results showed that the highest value was obtained for adhesive joints of graphite-epoxy composite of smaller material thickness (0,48 mm). Statistical analysis of the results obtained, the study showed statistically significant differences between the values of the strength of the confidence level of 0,95. Th
Klasifikace
Druh
D - Stať ve sborníku
CEP obor
—
OECD FORD obor
20301 - Mechanical engineering
Návaznosti výsledku
Projekt
—
Návaznosti
S - Specificky vyzkum na vysokych skolach
Ostatní
Rok uplatnění
2017
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název statě ve sborníku
12th International Conference on Damage Assessment of Structures, DAMAS 2017
ISBN
—
ISSN
1742-6588
e-ISSN
—
Počet stran výsledku
9
Strana od-do
1-9
Název nakladatele
Institute of Physics Publishing
Místo vydání
Kitakyushu, Japan
Místo konání akce
Kitakyushu
Datum konání akce
2. 6. 2017
Typ akce podle státní příslušnosti
WRD - Celosvětová akce
Kód UT WoS článku
000414147600073