| Literature DB >> 34424387 |
Paul Borbas1, Rafael Loucas2, Marios Loucas2, Maximilian Vetter2, Simon Hofstede3, Lukas Ernstbrunner2, Karl Wieser2.
Abstract
INTRODUCTION: Coronal plane fractures of the distal humerus are relatively rare and can be challenging to treat due to their complexity and intra-articular nature. There is no gold standard for surgical management of these complex fractures. The purpose of this study was to compare the biomechanical stability and strength of two different internal fixation techniques for complex coronal plane fractures of the capitellum with posterior comminution.Entities:
Keywords: Antiglide plate; Biomechanics; Capitellum; Complex coronal plane fracture; Distal humerus; Locking plate
Mesh:
Year: 2021 PMID: 34424387 PMCID: PMC9522805 DOI: 10.1007/s00402-021-04126-1
Source DB: PubMed Journal: Arch Orthop Trauma Surg ISSN: 0936-8051 Impact factor: 2.928
Fig. 13D printed-patient-specific osteotomy guides. A Humerus-specific 3D cutting guide B Placement of the cutting guide on the surface of the distal humerus
Fig. 2Illustration of fracture fixation of simple coronal shear fractures of the capitellum (Dubberley 2B) with two different fixation methods: 2A) Anteroposterior x-ray (left), lateral 3D CT scan (middle) and anteroposterior view (right) of two anteroposterior HCSs with additional anterior antiglide plate (group HCS + antiGP). 2B) Anteroposterior x-ray (left), lateral 3D CT scan (middle) and posteroanterior view (right) of posterolateral distal humerus locking plate (group PLP)
Fig. 3Experimental set-up with loading of the capitellum in 20 degrees elbow flexion of a group HCS + antiGP specimen
Fig. 4Anterior view of a group PLP specimen after cyclic loading and load to failure testing with the capitellum fragment’s proximal displacement
Displacement and stiffness during cyclic loading as well as ultimate load to failure comparing the two groups
| Variable* | HCS + antiGP group | PLP group | |
|---|---|---|---|
| Displacement 90 cycles, mm | 0.4 ± 0.1 | 0.5 ± 0.2 | 0.180 |
| Displacement 180 cycles, mm | 0.4 ± 0.2 | 0.6 ± 0.2 | 0.105 |
| Displacement 360 cycles, mm | 0.5 ± 0.2 | 0.7 ± 0.2 | 0.200 |
| Displacement 900 cycles, mm | 0.6 ± 0.3 | 0.8 ± 0.2 | 0.324 |
| Displacement 2000 cycles, mm | 0.7 ± 0.3 | 0.8 ± 0.3 | 0.291 |
| Stiffness 90 cycles, N/mm | 447 ± 124 | 517 ± 142 | 0.345 |
| Stiffness 180 cycles, N/mm | 457 ± 139 | 537 ± 118 | 0.266 |
| Stiffness 360 cycles, N/mm | 471 ± 148 | 551 ± 139 | 0.324 |
| Stiffness 900 cycles, N/mm | 476 ± 155 | 568 ± 142 | 0.270 |
| Stiffness 2000 cycles, N/mm | 464 ± 160 | 581 ± 140 | 0.168 |
| Mean total stiffness, N/mm | 463 ± 142 | 551 ± 132 | 0.355 |
| Ultimate load to failure⨎, N | 649 ± 351 | 887 ± 187 | 0.140 |
HCS headless compression screw, antiGP antiglide plate, PLP posterolateral locking plate
aData are presented as mean ± standard deviation
†The two groups were compared with the one-way analysis of variance (ANOVA; parametric data) and Kruskal-Wallis one-way analysis of variance (non-parametric data)
⨎Ultimate load to failure was defined as fragment displacement >3mm