| Literature DB >> 29321813 |
Ronny Grunert1,2,3, Stefan Schleifenbaum1,2, Robert Möbius2,4, Michael Kopper5, Christian Rotsch3, Welf-Guntram Drossel3, Niels Hammer6, Torsten Prietzel7,2.
Abstract
BACKGROUND: The modularity in total hip arthroplasty (THA) allows orthopaedic surgeons for an exact reconstruction of hip biomechanical parameters especially in revision and tumor arthroplasty. Modular structured femoral stems using taper junctions showed increased implant breakage in the recent past. PRESENTATION OF THE HYPOTHESIS: We hypothesize that a novel modular stem-neck-interface leads to less implant breakage compared to conventional femoral stems. TESTING OF THE HYPOTHESIS: For this purpose, a novel modular femoral stem for THA was to design and manufacture. Therefore, three different variants of interface mechanisms were developed that enable a simple connection between the stem and the neck modules and allow for intra-operatively adjustment. Three prototypes A, B and C were manufactured and subsequently dynamic fatigue (ISO 7206-6) and body donor tested. IMPLICATION OF THE HYPOTHESIS: Modularity in THA is mainly applied in THA as well as in revision and tumor arthroplasty. Modular implants are barely used because of the high risk of breakage. Another risks in this context are taper fretting, corrosion and disconnection. With the novel design, it should be possible to detach the stem and neck module intra-operatively to adapt the anatomical situation. The novel coupling mechanism of the rotating interface seems to be the most suitable for a secure stem-neck connection and is characterized by good intraoperative handling.Entities:
Keywords: Modular femoral stem; Neck-stem interface; THA; Taper junction
Year: 2018 PMID: 29321813 PMCID: PMC5759261 DOI: 10.1186/s13037-017-0148-7
Source DB: PubMed Journal: Patient Saf Surg ISSN: 1754-9493
Fig. 1Concept variants for novel interface: a sliding conical dovetail interface, b rotating interface, c sliding double-lapped dovetail interface
Fig. 2Prototypes for each variant: a conical dovetail, b rotating interface, c double-lapped dovetail
Fig. 3Experimental setup for dynamic fatigue limit testing according to the ISO 7206–6 standard
Fig. 4Failure pattern after fatigue testing: a breakage, b no damage, c breakage