| Literature DB >> 18817544 |
Maria E Zeman1, Nicolas Sauwen, Luc Labey, Michiel Mulier, Georges Van der Perre, Siegfried V N Jaecques.
Abstract
BACKGROUND: Sufficient primary stability is a prerequisite for the clinical success of cementless implants. Therefore, it is important to have an estimation of the primary stability that can be achieved with new stem designs in a pre-clinical trial. Fast assessment of the primary stability is also useful in the preoperative planning of total hip replacements, and to an even larger extent in intraoperatively custom-made prosthesis systems, which result in a wide variety of stem geometries.Entities:
Year: 2008 PMID: 18817544 PMCID: PMC2570665 DOI: 10.1186/1749-799X-3-44
Source DB: PubMed Journal: J Orthop Surg Res ISSN: 1749-799X Impact factor: 2.359
Figure 1One element of the prosthesis surface supported by bone.
Figure 2Loading on a hip prosthesis. (a) single force on the head (b) equivalent combination of force and moment on the stem. If is considered as a vector with three components (Rx, Ry, Rz), would cause torque around the three axes and is represented by double-arrow-headed vector components (Mx, My, Mz). In this study, only Mz was considered.
Resistance against axial rotation for the five stem designs, calculated with the analytical model.
| 3.40E+05 | 4.66E+05 | 7.81E+05 | 9.87E+05 | 1.25E+06 |
Figure 3Upper and anteroposterior view of the five stem geometries. From left to right: RotaMIN, RotaLOW, RotaMED, RotaHIGH and RotaMAX.
Figure 4Rotation angle as a function of the applied torsional load. Calculated for the finite element models of the five stem geometries implanted in a trabecular bone mantle.
Rotation angles*, obtained with FEM and with the analytical model.
| 4 | 5,03E-03 | 5,88E-03 | 1,71E-03 | 2,82E-03 | 1,23E-03 | |
| 10 | 1,39E-02 | 1,77E-02 | 7,11E-03 | 6,45E-03 | 4,47E-03 | |
| 20 | 2,93E-02 | 3,26E-02 | 1,38E-02 | 1,20E-02 | 8,76E-03 | |
| 4 | 1,18E-05 | 8,58E-06 | 5,12E-06 | 4,05E-06 | 3,20E-06 | |
| 10 | 2,94E-05 | 2,15E-05 | 1,28E-05 | 1,01E-05 | 8,00E-06 | |
| 20 | 5,88E-05 | 4,29E-05 | 2,56E-05 | 2,03E-05 | 1,60E-05 | |
*Angles expressed in radians, for all five stems, under torsional loads of 4 Nm, 10 Nm and 20 Nm.