| Literature DB >> 30979247 |
Desire Abellán1, José Nart2, Andrés Pascual3, Robert E Cohen4, Javier D Sanz-Moliner5.
Abstract
The aim of this study was to evaluate and compare the mechanical properties of five suture materials on three knot configurations when subjected to different physical conditions. Five 5-0 (silk, polyamide 6/66, polyglycolic acid, glycolide-e-caprolactone copolymer, polytetrafluoroethylene) suture materials were used. Ten samples per group of each material were used. Three knot configurations were compared A.2=1=1 (forward⁻forward⁻reverse), B.2=1=1 (forward⁻reverse⁻forward), C.1=2=1 (forward⁻forward⁻reverse). Mechanical properties (failure load, elongation, knot slippage/breakage) were measured using a universal testing machine. Samples were immersed in three different pH concentrations (4,7,9) at room temperature for 7 and 14 days. For the thermal cycle process, sutures were immersed in two water tanks at different temperatures (5 and 55 °C). Elongation and failure load were directly dependent on the suture material. Polyglycolic acid followed by glycolide-e-caprolactone copolymer showed the most knot failure load, while polytetrafluoroethylene showed the lowest (P < 0.001). Physical conditions had no effect on knot failure load (P = 0.494). Statistically significant differences were observed between knot configurations (P = 0.008). Additionally, individual assessment of suture material showed statistically significant results for combinations of particular knot configurations. Physical conditions, such as pH concentration and thermal cycle process, have no influence on suture mechanical properties. However, knot failure load depends on the suture material and knot configuration used. Consequently, specific suturing protocols might be recommended to obtain higher results of knot security.Entities:
Keywords: failure load; knot configuration; knot slippage; physical conditions; suture materials
Year: 2016 PMID: 30979247 PMCID: PMC6432448 DOI: 10.3390/polym8040147
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.329
Five suture materials were used in order to assess their properties.
| Suture material | Codification | Composition | Structure | Degradation |
|---|---|---|---|---|
| Silk 1 | SILK | Natural | Multifilament | Non absorbable |
| Polyamide 2 | PV | Synthetic | Monofilament | Non absorbable |
| Polyglycolic acid 3 | AP7 | Synthetic | Multifilament | Absorbable |
| Glycolide-e-caprolactone copolymer 4 | GC7 | Synthetic | Monofilament | Absorbable |
| Polytetrafluoroethylene 5 | PTFE | Synthetic | Monofilament | Non absorbable |
1 Silk. Triangular, 3/8 circle premium DS16 5/0 Ancladén® (Barcelona, Spain). Product code: 5650; 2 Polyamide 6/66. PV monofil triangular, 3/8 circle premium DS16 5/0 Ancladén® (Barcelona, Spain). Product code: 7625; 3 Polyglycolic acid. AP7 rapid triangular, 3/8 circle premium DS16 5/0 Ancladén® (Barcelona, Spain). Product code: 2604; 4 glycolide-e-caprolactone copolymer. GC7 monofil triangular, 3/8 circle Premium DS16 5/0 Ancladén® (Barcelona, Spain). Product code: 4623; 5 Polytetrafluoroethylene. PTFE 3/8 circle premium 4/0 Osteogenics® (Lubbock, Texas) Product code: CS 0618.
Figure 1Sample preparation. (a) Suture material before tying; (b) Tying of suture material around a 26 mm metal cylinder; (c) Different suture materials after tying; (d) Sample of suture material prepared for testing mechanical and chemical conditions.
Figure 2Mechanical and physical tests. (a) Hydraulic grip of the Universal Testing Machine; (b) 5 and 55 °C water tanks of the Universal Thermal Cycling Testing Machine; (c) Metal boxes which contained the sample for the thermal cycle process.
Figure 3Tables for variables elongation and load failure (a) Elongation of suture materials at the three knot configurations; (b) Load failure of the suture materials to the different knot configurations.
Figure 4Comparison of suture material failure load in three knot configurations.
Analysis of interaction of variables.
| Variables | Interactions | |
|---|---|---|
| A: material | AB | <0.001 * |
| B: knot | CF | 0.404 |
| C: group | DA | <0.001 * |
| D: knot breakage | DB | <0.001 * |
| E: elongation | AE | <0.001 * |
| F: failure load | FB | 0.008 * |
| F: failure load | FA | <0.001 * |
* Statistically significant.
Figure 5Knot configurations failure load according to the suture material used.
Descriptive analysis of sutures failure load at the three knot configurations.
| Material | Knot configuration | Analysis of failure load (N) | ||
|---|---|---|---|---|
| Mean | Variance | Standard deviation | ||
| SILK | A | 6.298 | 8.477 | 2.911 |
| SILK | B | 7.242 | 7.941 | 2.818 |
| SILK | C | 5.494 | 8.534 | 2.921 |
| PV | A | 5.738 | 6.435 | 2.536 |
| PV | B | 7.301 | 18.288 | 4.276 |
| PV | C | 8.665 | 22.652 | 4.759 |
| AP7 | A | 11.218 | 15.528 | 3.94 |
| AP7 | B | 10.276 | 19.614 | 4.428 |
| AP7 | C | 7.557 | 13.912 | 3.729 |
| GC7 | A | 12.342 | 48.637 | 6.974 |
| GC7 | B | 7.252 | 24.767 | 4.976 |
| GC7 | C | 7.668 | 31.942 | 5.651 |
| PTFE | A | 6.593 | 2.593 | 1.61 |
| PTFE | B | 5.521 | 3.55 | 1.884 |
| PTFE | C | 5.41 | 6.414 | 2.532 |
Figure 6(a) Failure load of knots according to each suture material. (b) Frequency of knot breakage in relation to suture material and knot configuration used.