| Literature DB >> 30045716 |
Ali Jabran1, Chris Peach1,2, Zhenmin Zou1, Lei Ren3.
Abstract
BACKGROUND: Treatment of proximal humerus fractures with locking plates is associated with complications. We aimed to compare the biomechanical effects of removing screws and blade of a fixed angle locking plate and hybrid blade plate, on a two-part fracture model.Entities:
Keywords: Biomechanical testing; Blade plate; Locking plate; Proximal humerus fractures
Mesh:
Year: 2018 PMID: 30045716 PMCID: PMC6060456 DOI: 10.1186/s12891-018-2185-5
Source DB: PubMed Journal: BMC Musculoskelet Disord ISSN: 1471-2474 Impact factor: 2.362
Fig. 1Numbering and zoning of screws and blade holes on PHILOS plate (a) and Fx plate (b) based on their proximity to fracture gap]
Length (mm) and descriptions of the screws and blades for the PHILOS plates and Fx plate configuration groups. Emboldened cells correspond to where combination differs from the control. Types of screws, cancellous, cortical locking and cortical compression, are denoted by CA, CO-L and CO-C, respectively
| Configuration Group | Screw Number | |||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9 | 10 | 11 | 12 | |
| P0 (Control) | 40 | 40 | 45 | 50 | 42 | 42 | None | 50 | 50 | 32 | 30 | 30 |
| P1 (No Zone 1) | 40 | 40 | 45 | 50 | 42 | 42 | None | None | None | 32 | 30 | 30 |
| P2 (No Zone 2) | 40 | 40 | 45 | 50 | None | None | None | 50 | 50 | 32 | 30 | 30 |
| P3 (No Zone 3) | 40 | 40 | None | None | 42 | 42 | None | 50 | 50 | 32 | 30 | 30 |
| P4 (No Zone 4) | None | None | 45 | 50 | 42 | 42 | None | 50 | 50 | 32 | 30 | 30 |
| F0 (Control) | 29, CA | 29, CA | 44, CA | 44, CA | 50 | 45, Blade | 26, CO-L | 32, CO-C | 26, CO-L | N/A | N/A | |
| F1 (No Zone 1) | 29, CA | 29, CA | 44, CA | 44, CA | 50 | None | 26, CO-L | 32, CO-C | 26, CO-L | N/A | N/A | |
| F2 (No Zone 2) | 29, CA | 29, CA | 44, CA | 44, CA | None | 45, Blade | 26, CO-L | 32, CO-C | 26, CO-L | N/A | N/A | |
| F3 (Swap Blade with Screws) | 29, CA | 29, CA | 44, CA | 44, CA | 50 | 44, CA | 44, CA | 26, CO-L | 32, CO-C | 26, CO-L | N/A | N/A |
Fig. 2Specimen preparation: Cubic mould (a) was filled with cement mix and humerus. After the block dried, humerus (b) was marked with positions of plate and cuts
Fig. 3Mechanical testing set-up used to apply varus cantilever displacement (red arrow) and determine bending loads and stiffness. Load was applied to the humeral shaft in a cantilever fashion while humeral head was potted inside the cement block
Fig. 4Mean peak load (F5) for PHILOS and Fx plate configuration groups during elastic loading of 5 mm cantilever displacement in extension, flexion, valgus and varus directions
Fig. 5Mean stiffness (K) for PHILOS and Fx plate configuration groups during elastic loading of 5 mm cantilever displacement in extension, flexion, valgus and varus directions
Mean stiffness (K) and load values (F) for all PHILOS plate configuration groups, along extension, flexion, valgus and varus, with their respective standard deviations (S.D.). K and F5 denote stiffness and peak load values obtained during elastic tests while F15a and F15b are loads at 15 mm before and after eight-minute intermission and F30 is the load at 30 mm during plastic tests
| P0 (SD) | P1 (SD) | P2 (SD) | P3 (SD) | P4 (SD) | |
|---|---|---|---|---|---|
| Extension | |||||
| K (N/mm) | 9.533 (0.286) | 7.956 (0.314) | 6.349 (0.299) | 6.644 (0.365) | 6.819 (0.495) |
| F5 (N) | 47.749 (1.510) | 39.191 (1.580) | 31.295 (1.425) | 32.597 (1.842) | 33.501 (2.415) |
| Flexion | |||||
| K (N/mm) | 9.997 (0.298) | 8.284 (0.257) | 6.887 (0.391) | 7.045 (0.357) | 7.377 (0.331) |
| F5 (N) | 49.981 (1.569) | 40.475 (1.336) | 33.846 (1.876) | 34.601 (1.850) | 36.152 (1.196) |
| Valgus | |||||
| K (N/mm) | 6.091 (0.181) | 4.671 (0.2150) | 5.439 (0.386) | 5.623 (0.189) | 5.804 (0.140) |
| F5 (N) | 29.746 (0.815) | 23.041 (1.065) | 26.907 (1.769) | 27.765 (0.852) | 28.659 (0.537) |
| Varus | |||||
| K (N/mm) | 6.609 (0.256) | 4.726 (0.259) | 5.867 (0.417) | 6.059 (0.443) | 6.268 (0.317) |
| F5 (N) | 32.561 (1.075) | 23.601 (1.183) | 28.826 (2.041) | 29.862 (2.205) | 30.951 (1.436) |
| F15a (N) | 75.590 (3.049) | 46.636 (1.843) | 53.759 (1.513) | 62.235 (1.941) | 65.012 (2.632) |
| F15b (N) | 71.558 (3.303) | 42.376 (2.141) | 50.199 (2.118) | 58.432 (1.878) | 62.693 (3.592) |
| F30 (N) | 115.531 (6.336) | 70.077 (3.446) | 81.238 (3.127) | 95.103 (2.901) | 103.216 (5.422) |
Mean stiffness (K) and load values (F) for all Fx plate configuration groups, along extension, flexion, valgus and varus, with their respective standard deviations (S.D.). K and F5 denote stiffness and peak load values obtained during elastic tests while F15a and F15b are loads at 15 mm before and after eight-minute intermission and F30 is the load at 30 mm during plastic tests
| F0 (SD) | F1 (SD) | F2 (SD) | F3 (SD) | |
|---|---|---|---|---|
| Extension | ||||
| K (N/mm) | 8.770 (0.156) | 7.734 (0.445) | 8.122 (0.220) | 10.915 (0.362) |
| F5 (N) | 43.979 (0.596) | 38.394 (2.151) | 40.357 (0.927) | 54.071 (1.651) |
| Flexion | ||||
| K (N/mm) | 9.541 (0.221) | 8.248 (0.454) | 8.990 (0.424) | 11.127 (0.385) |
| F5 (N) | 47.711 (0.775) | 40.160 (2.033) | 44.479 (1.321) | 55.095 (1.922) |
| Valgus | ||||
| K (N/mm) | 6.900 (0.200) | 6.332 (0.339) | 6.623 (0.170) | 8.245 (0.324) |
| F5 (N) | 35.131 (0.617) | 31.096 (0.855) | 33.260 (0.919) | 40.946 (1.600) |
| Varus | ||||
| K (N/mm) | 7.590 (0.196) | 5.619 (0.180) | 7.094 (0.280) | 8.663 (0.391) |
| F5 (N) | 37.792 (0.990) | 28.151 (0.946) | 35.001 (1.277) | 43.059 (1.833) |
| F15a (N) | 84.470 (1.547) | 81.472 (2.665) | 73.545 (1.303) | 90.735 (2.439) |
| F15b (N) | 79.304 (2.507) | 78.650 (2.327) | 70.296 (1.547) | 87.577 (2.294) |
| F30 (N) | 134.391 (3.574) | 128.636 (2.339) | 123.032 (6.161) | 141.294 (3.487) |
Fig. 6Mean peak loads (F) for PHILOS and Fx plate configuration groups during plastic loading at 15 mm displacement before (F15a) and after (F15b) eight-minute intermission and at 30 mm displacement (F30)