| Literature DB >> 32455967 |
Guido R Sigron1,2, Nathalie Rüedi1,2, Frédérique Chammartin3, Simon Meyer1,2, Bilal Msallem1,2, Christoph Kunz1, Florian M Thieringer1,2.
Abstract
The aim of this study was to compare the efficacy of the intraoperative bending of titanium mesh with the efficacy of pre-contoured "hybrid" patient-specific titanium mesh for the surgical repair of isolated orbital floor fractures. In-house 3D-printed anatomical models were used as bending guides. The main outcome measures were preoperative and postoperative orbital volume and surgery time. We performed a retrospective cohort study including 22 patients who had undergone surgery between May 2016 and November 2018. The first twelve patients underwent conventional reconstruction with intraoperative free-hand bending of an orbital floor mesh plate. The subsequent ten patients received pre-contoured plates based on 3D-printed orbital models that were produced by mirroring the non-fractured orbit of the patient using a medical imaging software. We compared the preoperative and postoperative absolute volume difference (unfractured orbit, fractured orbit), the fracture area, the fracture collapse, and the effective surgery time between the two groups. In comparison to the intraoperative bending of titanium mesh, the application of preformed plates based on a 3D-printed orbital model resulted in a non-significant absolute volume difference in the intervention group (p = 0.276) and statistically significant volume difference in the conventional group (p = 0.002). Further, there was a significant reduction of the surgery time (57.3 ± 23.4 min versus 99.8 ± 28.9 min, p = 0.001). The results of this study suggest that the use of 3D-printed orbital models leads to a more accurate reconstruction and a time reduction during surgery.Entities:
Keywords: 3D-printing; blow-out fracture; hybrid patient-specific; orbital fracture; orbital implant; orbital volume
Year: 2020 PMID: 32455967 PMCID: PMC7291031 DOI: 10.3390/jcm9051579
Source DB: PubMed Journal: J Clin Med ISSN: 2077-0383 Impact factor: 4.241
Figure 1Visualization of the study design.
Figure 2Pre-bent plates based on a 3D-printed orbital model: (a) Orbital floor mesh plate MatrixMIDFACE on a polylactic acid (PLA) model printed with a MakerBot Replicator+; (b) Medartis Modus Midface OPS 1.5 plate on a biocompatible clear MED610 model printed with a Stratasys Objet30 Prime.
The descriptive statistics of the study sample.
| Variable | Intervention Group | Conventional Group |
|---|---|---|
|
| 10 (45.45%) | 12 (54.55%) |
|
| 47.5 (20–83) | 51.8 (21–79) |
| Sex | ||
| Male | 4 | 8 |
| Female | 6 | 4 |
| Cause of Injury | ||
| Fall | 5 | 7 |
| Assaults | 2 | 4 |
| Sports Injuries | 2 | 1 |
| Work-Related Injuries | 1 | 0 |
| Days Between Trauma and Surgery | 2.8 ± 2.5 | 4.1 ± 3.1 |
| Surgery Time (Min) | 57.3 ± 23.4 | 99.8 ± 28.9 |
| Length of Stay (Days) | 4.6 ± 3.9 | 3.8 ± 3.0 |
| Fracture Classification | ||
| AO CMF | ||
| 92 m.OiW2(i) | 5 | 10 |
| 92 Oi.mW2(i) | 5 | 2 |
| Kunz et al. | ||
| A1 | 3 | 7 |
| A2 | 6 | 5 |
| A3 | 1 | 0 |
AO CMF: Arbeitsgemeinschaft für Osteosynthesefragen—Craniomaxillofacial Surgery, A1: Isolated defect of the orbital floor, or the medial wall, 1–2 cm2, A2: Defect of the orbital floor in the anterior two-third, or the medial wall, or both, >2 cm2, bony ledge preserved at medial margin of the infraorbital fissure, A3: Defect of the orbital floor in the anterior two-third, or the medial wall, or both, >2 cm2, missing bony ledge medial to the infraorbital fissure.
Preoperative and postoperative measurements.
| Non-Fractured Orbit (mL) | Fractured orbit (mL) | ||
|---|---|---|---|
|
| |||
| Preoperative | 31.6 ± 4.2 | 33.1 ± 4.7 | |
| Postoperative | 31.4 ± 4.3 | 30.1 ± 4.2 | |
| Absolut Volume Difference (mL) | 1.6 ± 1.2 * | ||
| Fracture Area (mm2) | 408.5 ± 137.5 | ||
| Fracture Max. Collapse (mm) | 6.9 ± 2.3 | ||
|
| |||
| Preoperative | 26.1 ± 2.2 | 28.4 ± 4.0 | |
| Postoperative | 26.1 ± 2.2 | 25.7 ± 3.0 | |
| Absolut Volume Difference (mL) | 1.0 ± 0.7 | ||
| Fracture Area (mm2) | 389.4 ± 135.1 | ||
| Fracture Max. Collapse (mm) | 8.6 ± 5.4 |
* Statistically significant p = 0.002.
Figure 3Disior Bonelogic CMF Orbital software (Craniomaxillofacial surgery) software: (a) Rendered craniofacial bone with defined point (green bullet) at the anterior edge of the optic nerve foramen opening; (b) Orbital volume analyses by an iteratively expansion and deformation of a ball-shaped sphere.
Figure 4The volume of non-fractured orbits and reconstructed orbits between the two groups. CT: Computed tomography.
Figure 5Comparison between intervention and conventional group: (a) Surgery time (min); (b) Length of stay (days).
Figure 6Disior Bonelogic CMF Orbital software: (a) Three-dimensional reconstruction of the orbital floor defect in the area of the right orbit (purple); (b) Former defect area (purple) after reconstruction in projection on the titanium mesh.
Figure 7Disior Bonelogic CMF Orbital software: Automatically segmented orbit (right, in red with defect region in purple; and left, intact in blue).