| Literature DB >> 30634159 |
Emily Bliven1, Alexandra Rouhier1, Stanley Tsai1, Rémy Willinger2, Nicolas Bourdet2, Caroline Deck2, Steven M Madey1, Michael Bottlang3.
Abstract
BACKGROUND: A novel bicycle helmet concept has been developed to mitigate rotational head acceleration, which is a predominant mechanism of traumatic brain injury (TBI). This WAVECEL concept employs a collapsible cellular structure that is recessed within the helmet to provide a rotational suspension. This cellular concept differs from other bicycle helmet technologies for mitigation of rotational head acceleration, such as the commercially available Multi-Directional Impact Protection System (MIPS) technology which employs a slip liner to permit sliding between the helmet and the head during impact. This study quantified the efficacy of both, the WAVECEL cellular concept, and a MIPS helmet, in direct comparison to a traditional bicycle helmet made of rigid expanded polystyrene (EPS).Entities:
Keywords: Bicycle helmet; Brain injury; Concussion; Impact mitigation; Impact testing; Rotational acceleration
Mesh:
Year: 2019 PMID: 30634159 PMCID: PMC6743977 DOI: 10.1016/j.aap.2018.12.017
Source DB: PubMed Journal: Accid Anal Prev ISSN: 0001-4575
Fig. 1.Three helmet types with identical outer shell and liner thickness were tested: A) Standard EPS helmets (CONTROL); B) helmets with a MIPS slip liner for mitigation of rotational acceleration (SLIP); and C) helmets with a cellular structure for mitigation of linear and rotational acceleration (CELL). Sectioned EPS areas along transverse cut (A-A) and sagittal cut (B-B) are outlined in white for illustration. Impact locations corresponding to the 30°, 45°, and 60° anvils are denoted by red dots on sagittal cross-sections. (For interpretation of the references to colour in this figure legend, the reader is referred to the web version of this article).
Fig. 2.A) Helmet Impact Testing (HIT) facility for vertical drop of a Hybrid III head and neck assembly onto a 0° - 60° adjustable anvil to simulate oblique impacts. B) Drop assembly with linear and rotational headform accelerometers to capture headform kinematics in terms of linear acceleration (a) and rotational acceleration (α).
Fig. 3.Vertical drop tests of a frontal, mid-sagittal helmet location onto A) a 30° anvil, B) a 45° anvil, and C) a 60° anvil. Anvil angles of 30°, 45°, and 60° correspond to impact angles between the head trajectory and impact surface of 60°, 45°, and 30°, respectively.
Summary of results from all impact tests in terms of the average outcomes and standard deviations (STDEV). P-values denote the significance of differences compared to the CONTROL group. “- “ denotes a non-applicable, empty cell.
| Outcome | Result | Helmet | 30° anvil, slow | 45° anvil, slow | 60° anvil, slow | 45° anvil, fast | ||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
| CONTROL | 4.80 | 0.02 | - | 4.81 | 0.01 | - | 4.78 | 0.02 | - | 6.20 | 0.02 | - | |
| [m/s] | SLIP | 4.82 | 0.01 | 0.673 | 4.79 | 0.03 | 0.61 | 4.80 | 0.01 | 0.246 | 6.15 | 0.04 | 0.113 | |
|
| CELL | 4.79 | 0.0 | 0.559 | 4.83 | 0.02 | 0.551 | 4.78 | 0.02 | 0.811 | 6.17 | 0.04 | 0.259 | |
|
|
| CONTROL | 163.8 | 1.4 | - | 164.2 | 1.8 | - | 162.6 | 1.1 | - | 272.9 | 1.5 | - |
| [J] | SLIP | 164.6 | 1.0 | 0.673 | 163.0 | 1.8 | 0.612 | 163.6 | 0.9 | 0.246 | 269.0 | 3.7 | 0.113 | |
| CELL | 162.8 | 1.3 | 0.558 | 165.3 | 1.0 | 0.553 | 162.0 | 1.1 | 0.813 | 269.9 | 3.6 | 0.259 | ||
|
| CONTROL | 87 | 1.1 | - | 65 | 0.7 | - | 45 | 2.3 | - | 81 | 7.7 | - | |
|
| SLIP | 83 | 4.3 | 0.117 | 65 | 2.1 | 0.83 | 44 | 1.0 | 0.997 | 86 | 7.8 | 0.564 | |
| [g] | CELL | 64 | 1.0 | < 0.001 | 53 | 2.7 | < 0.001 | 38 | 1.4 | 0.001 | 80 | 4.2 | 0.808 | |
|
|
| CONTROL | 6821 | 219 | - | 6237 | 255 | - | 2743 | 176 | - | 7243 | 574 | - |
|
|
| SLIP | 5385 | 445 | < 0.001 | 3481 | 359 | < 0.001 | 2023 | 229 | 0.001 | 5683 | 777 | 0.014 |
| [rad/s2] | CELL | 3262 | 63 | < 0.001 | 1702 | 98 | < 0.001 | 1802 | 98 | < 0.001 | 1962 | 644 | < 0.001 | |
|
| CONTROL | 26 | 0.3 | - | 26 | 0.5 | - | 12 | 1.2 | - | 31 | 2.5 | - | |
|
| SLIP | 22 | 0.7 | < 0.001 | 16 | 1.1 | < 0.001 | 4 | 2.2 | < 0.001 | 24 | 1.8 | 0.001 | |
| [rad/s] | CELL | 13 | 0.5 | < 0.001 | 7 | 1.0 | < 0.001 | 3 | 1.9 | < 0.001 | 5 | 3.5 | < 0.001 | |
|
|
| CONTROL | 43 | 1 | - | 44 | 2 | - | 6.4 | 1.6 | - | 59.2 | 8 | - |
|
| BrIC | SLIP | 29 | 2 | < 0.001 | 14 | 2 | < 0.001 | 0.6 | 0.8 | < 0.001 | 34.2 | 6 | 0.001 |
|
| [%] | CELL | 8 | 1 | < 0.001 | 1.2 | 1 | < 0.001 | 0.2 | 0.3 | < 0.001 | 1.2 | 2 | < 0.001 |
Fig. 4.Results for impacts onto the three anvil angles at 4.8 m/s (slow), and for the 45° anvil angle at 6.2 m/s (fast): A) resultant linear headform acceleration,B) headform rotational acceleration, and C) rotational velocity. D) Probability of AIS 2 injury, calculated from peak rotational velocity based on BrIC. (Takhounts et al., 2013) Asterisks denote significant differences (p < 0.05) compared to the CONTROL group.