Conventional cylindrical composite pressure vessels are designed with
continuous fiber hoop wraps to counter the primary stresses developed
in the shell. In certain applications it would be advantageous to be a
ble to assemble a composite pressure vessel around internal components
; however, this forces a discontinuity in the reinforcing fibers in th
e hoop direction. Previous efforts have shown that multi-shell pressur
e vessels can be assembled and that functional performance can be real
ized. The basic concept was to bond together four half-shells with the
seams of the inner and outer pair rotated 90 degrees. Unfortunately,
closed form analysis could not account for localized stress concentrat
ions that severely limited the ultimate Internal pressure. Further, li
near finite element analysis was unable to accurately predict shell st
resses and generated exaggerated deflections, but, was useful in under
standing the general mode of deformation. Based on deformed shapes, fr
om linear finite element analysis, a first generation modified multi-s
hell pressure vessel with tapered inner shells was developed and teste
d, with improved results. This research investigates the design consid
erations involved in the development of an optimized bonded, multi-she
ll composite pressure vessel, the determination of critical design par
ameters, the modeling of stresses in the composite shell, and hydrobur
st testing of prototype pressure vessels. A non-linear finite element
analysis was developed and tapered shell thicknesses were evaluated in
an effort to generate optimal pressure vessel performance and to mini
mize stress concentrations in the joint regions. Optimized test vessel
s based on the finite element analysis, utilizing dual thickness taper
ed shells, were hydroburst tested to pressures beyond 14.5 MPa without
composite failure. The correlation between experiment and finite elem
ent analysis indicates that the optimized, dual thickness tapered, bon
ded multi-shell pressure vessel is an efficient design capable of clos
ely matching internal pressures of continuously reinforced pressure ve
ssels, up to the level where shell-to-shell bond failure occurs.