BACKSIDE NONCONFORMITY AND LOCKING RESTRAINTS AFFECT LINER SHELL LOAD-TRANSFER MECHANISMS AND RELATIVE MOTION IN MODULAR ACETABULAR COMPONENTS FOR TOTAL HIP-REPLACEMENT
Sm. Kurtz et al., BACKSIDE NONCONFORMITY AND LOCKING RESTRAINTS AFFECT LINER SHELL LOAD-TRANSFER MECHANISMS AND RELATIVE MOTION IN MODULAR ACETABULAR COMPONENTS FOR TOTAL HIP-REPLACEMENT, Journal of biomechanics, 31(5), 1998, pp. 431-437
Nonconformity between the polyethylene liner and the metal shell may e
xist in modular acetabular components by design, due to manufacturing
tolerances, or from locking mechanisms that attach the polyethylene li
ner to the metal shell. Relative motion at the liner/shell interface h
as been associated with backside wear, which may contribute to osteoly
sis which has been clinically observed near screw holes. The purpose o
f this study was to investigate the effect of nonconformity and lockin
g restraints on the liner/shell relative motion and load transfer mech
anisms in a commercially available, metal-backed acetabular component
with a polar fenestration. The finite element method was used to explo
re the hypothesis that backside nonconformity and locking restraints p
lay important roles in long-term surface damage mechanisms that are un
ique to modular components, such as backside wear and liner extrusion
through screw holes. The three-body quasi-static contact problem was s
olved using a commercially available explicit finite element code, whi
ch modeled contact between the femoral head, polyethylene liner, and t
he metal shell. Four sets of liner boundary conditions were investigat
ed: no restraints, rim restraints, equatorial restraints,and both rim
and equatorial restraints. The finite element model with a conforming
shell predicted between 8.5 and 12.8 mu m of incremental extrusion of
the polyethylene through the polar fenestration, consistent with in vi
tro experiments of the same design under identical loading conditions.
Furthermore, idealized rim and/or equatorial liner restraints were fo
und to share up to 71% of the load across the liner/shell interface. C
onsequently, the results of this study demonstrate that backside nonco
nformity and locking restraints substantially influence backside relat
ive motion as well as load transfer at the liner/shell interface. (C)
1998 Elsevier Science Ltd. All rights reserved.