Accession Number : ADD017709
Title : High-Damping Rib-Stiffened Composite Hollow Cylinder Core Configuration.
Descriptive Note : Patent, Filed 3 May 94, patented 5 Sep 95,
Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON DC
Personal Author(s) : Crane, Roger M
Report Date : 05 Sep 1995
Pagination or Media Count : 13
Abstract : A multiple-layered, translated rib-stiffened, composite hollow cylinder and method for fabrication thereof utilizing filament winding technique known in the art Selective utilization of high strain-to-failure viscoelastic matrix material, without resort to secondary processing, results in improved damping characteristics in terms of dissipation of mechanical and acoustic-energy as well as improved structural characteristics in terms of damage tolerance.
Descriptors : *STIFFENED CYLINDERS, *CONFIGURATIONS, *PATENTS, DAMAGE, PROCESSING, SECONDARY, DAMPING, DISSIPATION, CYLINDRICAL BODIES, TOLERANCE, UTILIZATION, WINDING
Subject Categories : Machinery and Tools
Distribution Statement : APPROVED FOR PUBLIC RELEASE