Accession Number : ADA305469
Title : Hybridized Polymer Matrix Composites.
Descriptive Note : Final rept.,
Corporate Author : AVCO SPECIALTY MATERIALS DIV LOWELL MA
Personal Author(s) : Henshaw, Jim
PDF Url : ADA305469
Report Date : 04 APR 1983
Pagination or Media Count : 70
Abstract : Methods of improving the fire resistance of graphite epoxy composite laminates were investigated with the objective of reducing the volume of loose graphite fibers disseminated into the airstream as the result of a high intensity aircraft fuel fire. Improvements were sought by modifying the standard graphite epoxy systems without significantly negating their structural effectiveness. The modifications consisted primarily of an addition of a third constituent material such as glass fibers, glass flakes, carbon black in a glassy resin. These additions were designed to encourage coalescense of the graphite fibers and thereby reduce their aerodynamic float characteristics. A total of 38 fire tests were conducted on thin (1.0 mm) and thick (6.0 mm) hybrid panels. jg p2
Descriptors : *POLYMERS, *COMPOSITE MATERIALS, *MATRIX MATERIALS, *HYBRID SYSTEMS, STRUCTURAL PROPERTIES, PANELS, CARBON FIBERS, FLOATS, FUELS, GLASS FIBERS, EPOXY LAMINATES, AERODYNAMIC CHARACTERISTICS, EPOXY COMPOUNDS, AIRCRAFT FIRES, CARBON BLACK, GRAPHITE EPOXY COMPOSITES, FIRE RESISTANCE.
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE