Event Abstract Back to Event Effect of impact assembly on the Interface deformation and fretting corrosion of modular hip tapers: an in vitro study Anna Panagiotidou1, 2*, Timothy Cobb1*, Jayantilal Meswania1*, Alister Hart1, 3*, Fares Haddad2, John Skinner1, 3* and Gordon Blunn1* 1 UCL, Institute of Orthopaedics and Musculoskeletal Science, United Kingdom 2 University College Hospital, United Kingdom 3 Royal National Orthopaedic Hospital, United Kingdom Introduction: Early failure of large head diameter metal-on-metal hip replacements (LH-MoM-HR) has been attributed to wear and corrosion of modular head-neck tapers[1]. Previous studies have also shown that taper surface finish and contact area affect the amount of mechanically assisted corrosion (MAC) at this interface[2]. The industry standard is to manufacture the neck taper with parallel horizontal ridges. The degree of deformation is likely to influence the way that the taper behaves the greater the impaction, the greater the deformation and, in theory, the greater the strength of the surface interlock. As a result, micromotion and fretting are minimised, reducing the potential for MAC and production of wear debris. This study aims to investigate the effect of varying impact assembly load on the amount of fretting corrosion at the head-neck taper junction. Materials and Methods: All samples were made to a single specification. Manufactured neck components, representing short tapers with high surface roughness (average Rz=16.58µm, Ra=4.14µm) or long tapers with low surface roughness (average Rz=3.82µm, Ra=0.81µm), were assembled under controlled conditions with 2kN, 4kN or 8kN of impaction force. All heads were CoCrMo alloy and had a smooth finish similar to the industry standard. Heads had neck offset to induce a high bending moment at the taper interface. Half of the neck tapers used were CoCrMo and the other half were Ti-6Al-4V alloy. For each material, the neck tapers were either a smooth or rough finish. Light microscopy and scanning electron microscopy (SEM) of the component surfaces allowed assessment of surface deformation pre and post in-vitro simulation, while measurement of fretting current allowed evaluation of mechanically assisted corrosion at the taper interface during cyclic loading (5 million cycles). Assessment of corrosion was carried out by high power light microscopy, scanning electron microscopy and optical microscopy. Results: Fretting and amplitude current during the cyclic loading test showed that both smooth-long and rough-short necks, assembled using 8kN of force were significantly reduced compared with either 2kN or 4kN assembly loads. Similarly for both Ti-6Al-4V surface finishes and the CoCrMo rough-short taper, the least fretting current was observed in samples with the greatest force of impaction (p = <0.001) (Fig. 1). Simulator testing over 5 million cycles demonstrated a reduction in fretting corrosion for samples impacted with 4kN and 8kN of force. However, in the case of those impacted at 8kN the fretting current seen after the first one million cycles was considerably lower than those samples impacted at 4kN. For 4kN, there was a significant (p=?) drop in maximum fretting current and amplitude between 1 million and 2 million cycles (p = <0.001), but no such change between 2 million and 3 million cycles. The downward reduction in fretting current continued at 4 and 5 million cycles (Fig.1). At 8kN impaction force, there was no statistically significant difference in current between 1 million and 2 million cycles, and very little change up to 5 million cycles. High-powered light microscopy demonstrated evidence of deformation of the surface of the tapers, which increased with assembly load and was more pronounced on Ti-6Al-4V neck tapers (Fig. 2). Upon inspection using SEM, showed evidence of MAC which was greater in the 4kN assemblies compared with 8kN assemblies and for both impaction loads corrosion occurred in areas associated with large bending moment. Discussion: 1. The impaction force used to assemble modular heads of hip implants should be more than 4kN. 2. When a light impaction force of only 2kN is used, the quality of fixation and resistance to fretting corrosion is inferior. 3. With an impaction force of 4 - 8kN, there is a progressive improvement in fixation and resistance to MAC corrosion over 5 million cycles. 4. With an impaction force of 8kN the resistance to fretting corrosion was immediately effective for Ti-6Al-4V rough-short neck tapers coupled with CoCrMo heads. The clinical implication of this study is that surgeons should apply a greater impact assembly force than is used at present and this is particularly important for titanium stems and for short tapers.
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