| Literature DB >> 35744071 |
Lien-Chen Wu1,2,3, Yueh-Ying Hsieh1,2, Fon-Yih Tsuang4, Yueh-Feng Chiang5, Chang-Jung Chiang1,2.
Abstract
Background andEntities:
Keywords: fatigue life; gipping capacity; over-tightening; pedicle screw; torque on set screw
Mesh:
Year: 2022 PMID: 35744071 PMCID: PMC9228452 DOI: 10.3390/medicina58060808
Source DB: PubMed Journal: Medicina (Kaunas) ISSN: 1010-660X Impact factor: 2.948
Specifications of implants assessed in this study.
| Pedicle Screw | A (Matrix) * | B (OCTOPODA) ** |
|---|---|---|
| Rod material | Ti alloy | Ti alloy |
| Screw diameter (mm) | 4.0 | 4.0 |
| Screw length (mm) | 30 | 30 |
| Screw material | Ti alloy | Ti alloy |
| Set screw material | Ti alloy | Ti alloy |
| Tightening torque (Nm) | 9 (lower) | 11 (lower) |
* MATRIX, DePuy Synthes, Oberdorf, Switzerland. ** OCTOPODA, Bricon GmbH, Wurmlingen, Germany.
Figure 1(a) MATRIX Spine System; plane contact surface between set screw and rod. (b) OCTOPODA Spine System; line contact surface between set screw and rod.
Figure 2(a) Setup of axial gripping capacity (AGC) testing. (b) Setup of dynamic mechanical testing.
Figure 3Sample testing curve for axial slip testing showing five test runs for a group.
Comparison of axial gripping capacity (AGC) between test groups.
| Group | Mean | SD * | |
|---|---|---|---|
| A (9 Nm) | 1940.23 | 102.10 | 0.123 |
| A (10 Nm) | 2019.65 | 98.81 | - |
| A (11 Nm) | 2067.30 | 105.66 | 0.241 |
| B (11 Nm) | 1651.23 | 88.05 | 0.031 |
| B (12 Nm) | 1775.70 | 94.78 | - |
| B (13 Nm) | 1818.97 | 69.25 | 0.216 |
* SD standard deviation. ** Bold values indicate statistical significance with a p value < 0.05.
Results of the dynamic compression bending test.
| Sample No. Group A | Torque Value of Set Screw (Nm) | Range of Axial Force (N) | Cycles to Failure |
|---|---|---|---|
| 1 | 10 | 22~220 | 53,548 |
| 2 | 10 | 20~200 | 2,177,963 |
| 3 | 10 | 20~200 | 1,757,238 |
| 4 | 10 | 19~190 | Run-out |
| 5 | 10 | 19~190 | Run-out |
| 6 | 9 | 19~190 | Run-out |
| 7 | 9 | 19~190 | Run-out |
| 8 | 11 | 19~190 | Run-out |
| 9 | 11 | 19~190 | Run-out |
| 10 | 11 | 20~200 | 1,831,177 |
| 11 | 11 | 20~200 | 1,593,474 |
Results of the dynamic compression bending test for two test groups.
| Group | * Fatigue Strength (N) | Maximum Axial Force (N) | Failure Patten If Did Not Run-Out |
|---|---|---|---|
| A (9 Nm) | 190 | 22~220 | Screw fracture |
| A (10 Nm) | |||
| A (11 Nm) | |||
| B (11 Nm) | 190 | 22~220 | Rod fracture |
| B (12 Nm) | |||
| B (13 Nm) | 170 | 19~190 |
* Run-out: run out at 5 million cycles as recommended by ASTM F1717.
Figure 4Failure patterns from the dynamic compression bending test in (a) Group A and (b) Group B.
Figure 5The contact surface between the set screw and Ti6Al4V rod in Groups A and B after tightening the tulip head of the pedicle screw.