Biomedical Engineering Reference
In-Depth Information
Fig. 8.4 a Normal joint, b pincer joint, c dysplastic joint, d cam type joint [ 13 , 15 , 23 ]; (Image
courtesy of Salman Chegini, ARTORG, University of Bern) (With kind permission from Wiley:
Journal of Orthopaedic Research, Penetration depthmethod—novel real-time strategy for evaluating
femoroacetabular impingement, Vol. 28, 2010, pp. 880-886, Arbabi E, Chegini S, Boulic R, Tannast
M, Ferguson S J, Thalmann D, Figs. 3 and 6)
8.3.2 Hip Models
The morphology of the human hip can be described by various selected anatomical
and radiographical parameters [ 27 ]. For simplicity and comparability, only two
important parameters were chosen to quantify acetabular and femoral pathomor-
phologies: the lateral center-edge (CE) angle of Wiberg [ 28 ], and the
α
angle of Nöt-
zli [ 29 ], respectively. The hip models were prepared by Salman Chegini at ARTORG,
University of Bern, by using CAD software. 1 These models included acetabular and
femoral bone, articular cartilage, the labrum and the chondrolabral transition zone. In
order to create a wide range of hip geometries, a consecutive series of
and CE angles
were chosen for evaluation, covering normal and pathological joint morphologies.
The CE angle values ranged from 0 to 40
α
angles ranged from 40 to 80 . Incre-
mentsof10 were selected for both parameters, resulting in a total of 25 different
joints for evaluation, e.g. normal (CE
20 =
40 ), cam (CE
20 =
80 ),
=
=
40 =
40 ), combined FAI (CE
40 =
80 ), dysplas-
pincer (CE
=
=
0 =
40 ), or combined dysplastic and impinging morphologies
tic (CE
=
0 =
80 ) (Fig. 8.4 )[ 23 ].
(CE
=
8.3.3 Simulation
The hipmodels were simulated during standing-to-sittingmovement. Known average
in-vivo load and motion data for standing-to-sitting were used for evaluation [ 30 ].
The total motion for standing-to-sitting was divided into 30 equal and consecutive
sub-motions. All of the penetrating vertices were found, and both curvilinear and
radial penetration depths as well as the von Mises stresses were calculated in each
sub-motion.
1
Solidworks 2005, Solidworks Corp., Boston, MA, USA.
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