| Literature DB >> 32150982 |
Marek Pokorný1, Tomáš Suchý2,3, Adéla Kotzianová1, Jan Klemeš1, František Denk2, Monika Šupová2, Zbyněk Sucharda2, Radek Sedláček3, Lukáš Horný3, Vlastimil Králík3, Vladimír Velebný1, Zdeněk Čejka4.
Abstract
A composite nanofibrous layer containing collagen and hydroxyapatite was deposited on selected surface areas of titanium acetabular cups. The layer was deposited on the irregular surface of these 3D objects using a specially developed electrospinning system designed to ensure the stability of the spinning process and to produce a layer approximately 100 micrometers thick with an adequate thickness uniformity. It was verified that the layer had the intended nanostructured morphology throughout its entire thickness and that the prepared layer sufficiently adhered to the smooth surface of the model titanium implants even after all the post-deposition sterilization and stabilization treatments were performed. The resulting layers had an average thickness of (110 ± 30) micrometers and an average fiber diameter of (170 ± 49) nanometers. They were produced using a relatively simple and cost-effective technology and yet they were verifiably biocompatible and structurally stable. Collagen- and hydroxyapatite-based composite nanostructured surface modifications represent promising surface treatment options for metal implants.Entities:
Keywords: collagen composite; electrospinning; hydroxyapatite; nanofibers; titanium implant
Mesh:
Year: 2020 PMID: 32150982 PMCID: PMC7179214 DOI: 10.3390/molecules25051173
Source DB: PubMed Journal: Molecules ISSN: 1420-3049 Impact factor: 4.411
Figure 1Diagram of the experimental deposition method (A). Dimensions of model acetabular cups and levels, at which the thickness of the deposited layer was measured (B). An image of four implants attached to the shaft of the rotary collector (rotary electrode).
Figure 2Results of numerical simulations of the distribution of electrostatic field intensities for a symmetrical arrangement (A) and for spinning jets at the left end of their path (B).
Figure 3Diagram of the method used to measure adhesion of the composite layer to the model implant surface (A). Representative images of test samples before and after COL/HAp layer deposition (B).
Thicknesses of the deposited layers measured at three different levels along the height of the coated implants; average values for each sample after layer deposition and after lyophilization. The data is also shown in a graph included in Figure 4.
| After Deposition | After Deposition | After Lyophilization | |||||
|---|---|---|---|---|---|---|---|
| Implant No. | Scan axis | Layer thickness (µm) | Standard deviation (µm) | Layer thickness (µm) | Standard deviation (µm) | Layer thickness (µm) | Standard deviation (µm) |
| 1 | 3 | 98.9 | 5.2 | 117.1 | 16.8 | 141.9 | 35.0 |
| 13 | 105.6 | 4.4 | |||||
| 23 | 132.5 | 7.8 | |||||
| 2 | 3 | 77.7 | 6.3 | 67.0 | 9.0 | 68.1 | 21.8 |
| 13 | 59.1 | 3.9 | |||||
| 23 | 66.7 | 6.4 | |||||
| 3 | 3 | 139.6 | 7.3 | 115.5 | 19.4 | 139.7 | 110.5 |
| 13 | 122.2 | 6.1 | |||||
| 23 | 95.2 | 5.6 | |||||
| 4 | 3 | 150.6 | 7.3 | 113.0 | 31.6 | 174.4 | 129.7 |
| 13 | 129.2 | 5.0 | |||||
| 23 | 79.5 | 7.5 | |||||
Figure 4Layer thicknesses of the samples measured after their deposition at three different levels (A). Average layer thicknesses of individual samples after their deposition and subsequent lyophilization (B). The data used in these graphs are recorded in Table 1.
Figure 5The distribution of fiber diameters after the deposition of the layer and after its cross-linking and lyophilization (A); corresponding SEM images of layer surfaces (B,C) and layer cross-sections (D,E).
Figure 6A Raman spectrum of the prepared composite material, including spectra of its individual components (COL, HAp).
Figure 7Box-plot of maximum bond stress required for separation of COL/HAp layer from differently treated titanium surfaces. * denotes statistically significant differences (Fisher’s LSD test, 0.05).