| Literature DB >> 27677290 |
Ryan Siskey1, Lauren Ciccarelli2, Melissa K C Lui3, Steven M Kurtz2.
Abstract
BACKGROUND: Most contemporary total disc replacements (TDRs) use conventional orthopaedic bearing couples such as ultrahigh-molecular-weight polyethylene (polyethylene) and cobalt-chromium (CoCr). Cervical total disc replacements incorporating polyetheretherketone (PEEK) bearings (specifically PEEK-on-PEEK bearings) have been previously investigated, but little is known about PEEK-on-ceramic bearings for TDR. QUESTIONS/PURPOSES: (1) What is the tribologic behavior of a PEEK-on-ceramic bearing for cervical TDR under idealized, clean wear test conditions? (2) How does the PEEK-on-ceramic design perform under impingement conditions? (3) How is the PEEK-on-ceramic bearing affected by abrasive wear? (4) Is the particle morphology from PEEK-on-ceramic bearings for TDRs affected by adverse wear scenarios?Entities:
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Year: 2016 PMID: 27677290 PMCID: PMC5052213 DOI: 10.1007/s11999-016-5041-7
Source DB: PubMed Journal: Clin Orthop Relat Res ISSN: 0009-921X Impact factor: 4.176
Fig. 1A–E(A–B) Representative assembly schematics show the wear coupons used for testing. (C–E) Digital images showing the individual implant components: (C) superior PEEK endplate; (D) ceramic core; (E) inferior PEEK endplate.
The table summarizes the wear testing parameters by wear test scenario
| Motions and loading profiles | Wear test parameters | ||
|---|---|---|---|
| Idealized* | Impingement* | Abrasive* | |
| Flexion/extension (degrees) | ± 7.5 | 17–18† | ± 7.5 |
| Lateral bending (degrees)‡ | ± 6 | N/A | ± 6 |
| Axial rotation (degrees)‡ | ± 6§ | ± 6§ | ± 6§ |
| Axial load (N)| | 50–150 | 150 | 50–150 |
* For each test, six samples were evaluated; for impingement testing, the six samples consisted of three small and three large samples; †this includes a 10° extension bias of the fixtures; ‡lateral bending was shifted 90° relative to flexion/extension and shifted 180° relative to axial rotation per Figure 2 found in ISO 18192-1; flexion/extension and axial load were in phase; §the magnitude of axial rotation as specified in ASTM F2423 was used in this test because it was more severe than the ± 4° magnitude specified in ISO 18192-1; |the magnitude of axial load as specified in ISO 18192-1 was used in this test because the peak load is more severe than the 100-N magnitude specified in ASTM F2423.
Fig. 2A–D(A1–A3) Representative superior endplate, core, and inferior endplate after idealized wear testing are shown. (B1–B3) Representative superior endplate, core, and inferior endplate after impingement wear testing for the small size components. (C1–C3) Representative superior endplate, core, and inferior endplate after impingement wear testing for the large size components. The red arrows in images B1–B3 and C3 indicate the region of impingement. (D1–D3) Representative superior endplate, core, and inferior endplate after abrasive wear testing. The yellow arrow in C2 indicates the titanium transfer applied to the core for abrasive testing.
Fig. 3Graph depicts the total mass loss versus number of cycles for each wear mode evaluated. The top graph shows all intervals and the inset (dashed box) shows only the total mass loss versus number of cycles through 2.0 MC. The data presented at each interval mean ± 1 SD of n = 6 devices for ideal and abrasive conditions and n = 3 for each impingement test.
Fig. 4A–DThe representative penetration maps (A1–A2) show the superior and inferior endplates after idealized wear testing. The representative penetration maps (B1–B2) of the superior and inferior endplates after impingement wear testing for the small size components. The representative penetration maps (C1–C2) of the superior and inferior endplates after impingement wear testing for the large size components. The computational artifact present at the retention ring (dark blue ring indicated by the red arrows in B1 and C1) is not representative of actual penetration. The representative penetration maps (D1–D2) show the superior and inferior endplates after abrasive wear testing.
Fig. 5A–CGraph depicts the equivalent circular diameter (ECD) frequency distribution for maximum wear stations from ideal, impingement, and abrasive wear testing. Representative SEM micrographs of particles taken at × 10,000 are shown from the idealized (A), impingement (B), and abrasive (C) wear testing fluid samples.
Summary of available wear testing data for cervical disc replacements under idealized (Mode I) conditions
| Reference | Design | Bearing couple | Standard referenced | Relevant test inputs | Wear rate | Particle size |
|---|---|---|---|---|---|---|
| SSED for PMA Number: P060023 (Bryan® Cervical Disc) [ | Bryan® (Medtronic Sofamor Danek, Memphis, TN, USA) | Polycarbonate urethane on titanium | N/A | FE: ± 4.9° | As published: | Greater than 90% of particles were less than 1 µm |
| SSED for PMA Number: P070001 (ProDisc™-C Total Disc Replacement) [ | ProDisc™-C (Synthes Spine, West Chester, PA, USA) | UHMWPE on CoCr | N/A | FE: ± 7.5° | As published: | Average size 0.17–0.35 µm |
| Nectow et al., 2008 [ | ProDisc™-C (Synthes Spine) | UHMWPE on CoCr | ISO 18192-1 | FE: ± 7.5° | As published: | Greater than 90% of particles were less than 1 µm |
| Bushelow et al., 2008 [ | ProDisc™-C (Synthes Spine) | UHMWPE on CoCr | N/A | FE: ± 5° | As published: | Greater than 90% of particles were less than 1 µm; average diameter between 0.22 and 0.37 µm |
| N/A | FE: ± 10° | As published: | ||||
| ISO 18192-1 | FE: ± 7.5° | As published: | ||||
| SSED for PMA Number: P110002 (Mobi-C® Cervical Disc Prosthesis) [ | Mobi-C® (LDR Spine, Austin, TX, USA) | UHMWPE on CoCr | ISO 18192-1 | FE: ± 7.5° | As published: | Average size 0.77 µm |
| SSED for PMA Number: P100003 (SECURE®-C Cervical Artificial Disc) [ | SECURE®-C (Globus Medical, Audubon, PA, USA) | UHMWPE on CoCr | N/A | FE: ± 7.0° | As published: | N/A |
| SSED for PMA Number: P100012 (PCM® Cervical Disc) [ | PCM® (NuVasive, San Diego, CA, USA) | UHMWPE on CoCr | ISO 18192-1 | FE: ± 7.5° | As published: | Average size: 0.43 ± 0.04 µm and 0.53 ± 0.15 µm for two samples, respectively |
| Grupp et al., 2015 [ | activ® C (Aesculap AG, Tuttlingen, Germany) | UHMWPE on CoCr | ISO 18192-1 | FE: ± 7.5° | As published: | 99% of particles were less than 1 µm |
| PEEK on PEEK | As published: | 99% of particles were less than 1 µm | ||||
| CFR-PEEK on CFR-PEEK | As published: | 99% of particles were less than 1 µm | ||||
| PEK on PEK | As published: | 90% of particles were less than 1 µm | ||||
| Brown et al., 2010 [ | NuNec (Pioneer Surgical, Marquette, MI, USA) | PEEK on PEEK | ASTM F2423 | FE: ± 7.5° | As published: | N/A |
| ISO 18192-1 | FE: ± 7.5° | As published: | N/A | |||
| Xin et al., 2013 [ | NuNec (Pioneer Surgical) | PEEK on PEEK | ISO 18192-1 | FE: ± 7.5° | As published: | N/A |
| Design History File Report for the Kineflex|C | Kineflex|C (SpinalMotion, Mountain View, CA) | CoCr on CoCr | ISO 18192-1 | FE: ± 7.5° | As published: | Average size: 0.4–0.55 µm |
| Kurtz et al., 2012 [ | Prestige ST (Medtronic Sofamor Danek) | Stainless steel on stainless steel | ASTM F2423 | FE: ± 9.7° (Phase II) | As published: | Average size: 0.3–0.6 µm |
| SSED for PMA Number: P090029 (Prestige® LP Cervical Disc) [ | Prestige® LP (Medtronic Sofamor Danek) | Titanium carbide on Titanium carbide | ASTM F2423* | FE: ± 7.5° (Phase II) | As published: | Average size less than 0.2 µm |
* Four wear tests were described in the SSED for the Prestige® LP Cervical Disc; the maximum standard wear rate has been reported; ASTM = American Society for Testing and Materials; ISO = International Standards Organization; FE = flexion/extension; LB = lateral bending; AR = axial rotation; AL = axial load; F = frequency; SSED = Summary of Safety and Effectiveness Data; N/A = not available.