Verfahrens- und Konstruktionstechnisch optimierte Multiaxialgelege fuer beanspruchungsgerechte rationelle Kunststoffverstaerkung - OPTIMAX Abschlussbericht

Abstract

Multiaxial-layered C-fiber composites suitable for production of aeroplane component parts have been constructed and characterized. Compared with costly prepreg composites, the multi-layered composites exhibited lower compression and shear resistances. This effect could be attributed to lower matrix resin strength, lower fiber-matrix bonding strength and disoriented and ondulated fiber strands in the multi-layered composites. However, improved process conditions may overcome these disadvantages.SIGLEAvailable from TIB Hannover: F03B852 / FIZ - Fachinformationszzentrum Karlsruhe / TIB - Technische InformationsbibliothekBundesministerium fuer Bildung und Forschung, Berlin (Germany)DEGerman