Performance of a Filament Wound Graphite/Thermoplastic Composite Ring-Stiffened Pressure Hull Model

Author:

Lamontia Mark A.,Gruber Mark B.,Smoot Michael A.,Sloan Jay1,Gillespie John W.2

Affiliation:

1. Du Pont Advanced Material Systems, Delaware Technology Park, PO. Box 6108, Newark, DE 19714-6108

2. Center for Composite Materials and, Department of Mechanical Engineering, University of Delaware, Newark, DE 19716

Abstract

The design, analysis, manufacture, and hydrostatic testing results of a 24- inchdiameter ringstiffened pressurehull model are presented. The AS-4 graphite/PEEK cylinder is manufactured using a nonautoclave insitu filament winding and tape laydown process. The cylinder incorporates 5 hoopwound rings and a shell (hoop/axial construction) that are integrally wound during manufacture. Ultrasonic inspection in conjunction with optical microscopy of end rings indicates that high quality is achieved with a void content of less than 1%. Translation of coupon data into the structure is quantified by subcomponent tests that measure insitu properties (A and Bbasis allowables) including shell axial compressive stiffness and strength and interlaminar shear strength. Analysis of the structure indicates that high interlaminar shear stress exists in the ring fillet areas. Subcomponent tests with supporting analysis to design the test method indicated that this failure mode was not critical. Design and analysis efforts focused on midbay and endbay performance. Axial compressive stress concentrations in the endbay were reduced by incorporating local increases in shell thickness and a steel insert ring that provided radial constraint of the shell to reduce the probability of an endbrooming failure mode. Steel hemispherical heads were designed and manufactured to further reduce axial compressive stress concentrations in the endbay. The test model was instrumented with strain gages and acoustic emission sensors and tested at Carderock Division, Naval Surface Warfare Center (CD-NSWC). Increments in pressure were followed by a 5-minute dwell time. Acoustic emission ceased for all pressures except the last two increments at 5250 and 5500 psi. The collapse pressure of 5500 psi was within 3% of our Bbasis prediction. The cylinder weight-to-displacement ratio, W/D, was 0.212 (unitless). Axial compression failure occurred in the cylinder midbay in agreement with our analysis.

Publisher

SAGE Publications

Subject

Condensed Matter Physics,Ceramics and Composites

Reference6 articles.

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