Accession Number : AD0288856

Title :   FUSELAGE-BONDED ALUMINUM SANDWICH-EDGE MEMBER SEALING SYSTEM AND STRUCTURAL EVALUATION

Corporate Author : GENERAL DYNAMICS/FORT WORTH TEX

Personal Author(s) : SWAIN,J.W.

Report Date : 14 DEC 1960

Pagination or Media Count : 1

Abstract : Identi iers: B-58. Fuel tightness of bonded aluminum sandwich panels with various gla reinforced plastic edge member configurations was determined under cyclic loading conditions and varying temperatures. SMR-7 silicone rubber bonded to Conolon 506 laminate using Dow Corning A-4094 primer,ALUMINUM FOIL BONDED WITH Narmco 406 adhesive on top of Conolon 506 laminate, and Narmco 406 outer layer on Conolon 533 laminate are considered satisfactory edge member configurations. (Auhor)

Descriptors :   *AIRPLANE PANELS, *ALUMINUM, *SANDWICH PANELS, ADHESIVES, AIRCRAFT, BONDING, COMPOSITE MATERIALS, FUELS, GLASS TEXTILES, JET ENGINE FUELS, LAMINATES, RUBBER, SILICONES

Distribution Statement : APPROVED FOR PUBLIC RELEASE