Application of C/epoxy prepregs for increasing the construction stiffness

• Autorzy: Klement J. , Kunz K.
• Konferencja: Proceedings of the Third Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(III; 23-25.11.1998; Warszawa, Polska)
• Języki publikacji: EN

Abstrakty

EN

This paper provides a study of the bimaterial consisting of the metal AICu4Mg Alclad sheet and the UD C/epoxy prepreg composite reinforcement. The resulting properties are compared and evaluated with the help of ILSS short beam test. The influences of various technological factors, such as surface preparation, co-cure pressure and the application of the film adhesive KFL 120 and the cold two components adhesive PL 20 are studied, as well the artificial ageing at the hot/wet conditions.

Słowa kluczowe

EN

composites; composite structures; composite materials; aircraft structures

PL

kompozyty; materiały kompozytowe; struktura kompozytów; budowa samolotu

• Wydawca: Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology
• Czasopismo: Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics
• Rocznik: 1999
• Tom: nr 9
• Strony: 47--50
• Opis fizyczny: Bibliogr. 4 poz., tab., wykr.

Twórcy

autor

Klement J.

autor

Kunz K.

• Technical University of Brno, Czech Republic