| Literature DB >> 30723687 |
Brett D Crist1, Ferris M Pfeiffer1,2, Michael S Khazzam3, Rebecca A Kueny4, Gregory J Della Rocca1, William L Carson2.
Abstract
BACKGROUND: Pelvic ring-comminuted transforaminal sacral fracture injuries are rotationally and vertically unstable and have a high rate of failure.Entities:
Keywords: bone–implant failure; external fixator; fracture stabilisation; pelvic ring injury; pelvic screws; transforaminal sacral fracture
Year: 2018 PMID: 30723687 PMCID: PMC6350021 DOI: 10.1016/j.jot.2018.06.005
Source DB: PubMed Journal: J Orthop Translat ISSN: 2214-031X Impact factor: 5.191
Figure 1A). Pelvic specimen mounted in an Instron biaxial test cell, with LED blocks in place. a, screw 2 LED block; b, screw 1 LED block; c, single-leg stance supports for the right ilium; d, anterior inferior iliac pelvic external fixator; rami LED blocks at e, the contralateral segment, and f, the ipsilateral segment; comminuted fracture at g, rami, and h, transforaminal sacral; i, sacrum LED block; j, pushrod; k, U-joint and attachment; l, S1 endplate; and m, right ilium LED block. (B). Definitions axes, directions of motion and applied loads. Applied loads: force and torque were applied to the centre of the S1 endplate, via a pushrod with universal joint and attachment—positive force upward, negative force downward (compression) and positive torque CCW when viewed cranial to caudal. Global axes: Rz is transverse plane rotation, with positive direction CCW when viewed cranial to caudal. Ry is flexion-extension rotation, with positive direction CCW when viewed left to right. Rx is lateral bending rotation, with positive direction CCW when viewed anterior to posterior. Screw axes: Positive z direction is cranial, positive y is towards screw tip, and positive x is posterior. CCW = counterclockwise; LED = light-emitting diode.
Figure 2Example of screw 1 and 2's Δy (push-out, pull-in) component of motion relative to ipsilateral ilium during torsional cyclic loading. CCW = counterclockwise.
Figure 3Screw 1 components of rotation (Rx lateral bend, Ry about screw axis, Rz transverse plane) during five cycles of axial compressive loading: from −10 to −50 N, then to −100, −150, −200, −250. (A) Screw rotation relative to the ipsilateral ilium. Rx—slight irreversible progression of increasing displacement per cycle. Ry—significant irreversible progression of increasing displacement per cycle. Rz—very little displacement per cycle. (B) Screw rotation relative to the sacrum. No signs of increasing displacement per cycle relative to the sacrum of any of the components of motion.
Flexibility of sacrum relative to ipsilateral ilium.
| Flexibility coefficient | To torsional loading (1–4 Nm Rz+) (−1 to −4 Nm Rz-) | ||||
|---|---|---|---|---|---|
| WX (with external fixator) | WOX (without external fixator) | ||||
| Rz+ (deg/Nm) | Rz– (deg/Nm) | Rz+ (deg/Nm) | Rz– (deg/Nm) | ||
| Construct | SI | 0.26 ± 0.07a | 0.25 ± 0.06 | 0.42 ± 0.13a | 0.44 ± 0.10 |
| TS | 0.20 ± 0.03b | 0.24 ± 0.04 | 0.38 ± 0.01a,b | 0.44 ± 0.05 | |
| TA | 0.21 ± 0.04c | 0.26 ± 0.04 | 0.34 ± 0.01a,b,c | 0.36 ± 0.03 | |
| All | 0.22 ± 0.05d | 0.25 ± 0.04e | 0.38 ± 0.07d | 0.41 ± 0.07e | |
WOX = without anterior external fixation; WX = with anterior fixation.
a, b, cWOX is significantly more flexible than WX, pooled Rz+ with Rz- data (p < 0.0075, n = 6)
d, eWOX is significantly more flexible than WX, pooled SI, TS, TA (p < 0.00014, n = 9)
z: Only TS WOX approached being more flexible than SI WX (p = 0.08), all others p > 0.13
Rx: WOX flexibility was not different than WX of same or other constructs, p > 0.13,
Approaching significance (p = 0.07) for pooled SI, TS, TA.
f Ry: Only TS WOX was more flexible than SI WX (p = 0.006), all others p > 0.1
Rami motion: contralateral segment of ipsilateral rami relative to ipsilateral rami.
| Displacement at 5th cycle of max compression to 150 N | |||||||
|---|---|---|---|---|---|---|---|
| Construct: | x (mm) AP shear | y (mm) Open/close | z (mm) CrCa shear | Rx (deg) Lat. bend | Ry (deg) Flex/Ext | Rz (deg) Tran Plane | |
| WX | SI | −2.5 ± 0.6 | −0.7 ± 0.7 | −2.7 ± 0.5 | −1.0 ± 0.1 | 1.0 ± 0.3b | 1.0 ± 0.2 |
| TS | −2.3 ± 1.6 | −0.4 ± 0.8 | −3.0 ± 1.2 | −0.6 ± 0.5 | 0.9 ± 0.8 | 0.7 ± 0.2 | |
| TA | −5.7 ± 1.9a | −0.3 ± 1.4 | −4.0 ± 0.9 | −0.6 ± 1.3 | 2.5 ± 0.6b,c,d | 1.4 ± 0.5 | |
| WOX | SI | 0.3 ± 8.3 | 0.6 ± 1.1 | −7.1 ± 5.0 | −1.3 ± 0.5 | 3.1 ± 1.5 | 0.9 ± 0.8 |
| TS | −2.6 ± 2.0 | −0.1 ± 1.0 | −3.4 ± 0.4 | −0.8 ± 1.0 | 1.1 ± 0.4d | 1.0 ± 0.8 | |
| TA | −1.5 ± 0.7a | 0.2 ± 0.9 | −2.8 ± 0.5 | −0.8 ± 0.7 | 0.9 ± 0.5c | 0.8 ± 0.4 | |
WOX = without anterior external fixation; WX, with anterior fixation.
x: aTA WX greater magnitude than TA WOX (p = 0.046), all others p > 0.076.
y: No significant difference between any constructs (p > 0.25)
z: No significant difference between any constructs (p > 0.12)
Rx: No significant difference between any constructs (p > 0.18)
Ry: b,c,dTA WX greater magnitude than other three (p < 0.036), all others p > 0.064.
Rz: No significant difference between any constructs (p > 0.13.)
x: a,b(p < 0.017), all others p > 0.06.
y: c,d,eAll WX less opening–closing than WOX (p < 0.006)
z: f,g(p < 0.014), all other p > 0.19.
Rx: h,i(p < 0.040), all other p > 0.15.
Ry: No significant difference between any constructs (p > 0.36)
Rz: j,k,l(p < 0.030), all other p > 0.21.
Sacrum motion: sacrum relative to ipsilateral ilium.
| Displacement at 5th cycle of max compression to 150 N | |||||||
|---|---|---|---|---|---|---|---|
| Construct: | x (mm) PA | y (mm) Lateral left | z (mm) CaCr | Rx (deg) Lat. bend | Ry (deg) Flex/Ext | Rz (deg) Tran Plane | |
| WX | SI | 0.48 ± 0.05 | 0.11 ± 0.11 | −1.06 ± 0.19a | −0.71 ± 0.15 | 1.36 ± 0.17c,d | −0.22 ± 0.37 |
| TS | 0.53 ± 0.23 | 0.08 ± 0.14 | −1.36 ± 0.41 | −0.68 ± 0.27 | 1.79 ± 0.65e | −0.13 ± 0.26 | |
| TA | 1.20 ± 0.71 | 0.09 ± 0.16 | −2.31 ± 0.49a | −0.46 ± 0.21 | 3.70 ± 0.95c,e,f | −0.05 ± 0.17 | |
| WOX | SI | 1.26 ± 0.96 | −0.11 ± 0.48 | −2.11 ± 0.89 | −0.57 ± 0.30 | 4.29 ± 2.51 | −0.57 ± 1.07 |
| TS | 0.51 ± 0.17 | 0.18 ± 0.14 | −1.93 ± 0.62 | −0.98 ± 0.42 | 2.23 ± 0.34d | −0.09 ± 0.35 | |
| TA | 0.73 ± 0.30 | 0.32 ± 0.48 | −1.67 ± 0.74 | −1.00 ± 0.75 | 1.68 ± 0.48f | −0.22 ± 0.11 | |
WOX = without anterior external fixation; WX, with anterior fixation.
x: No significant difference between any constructs (p > 0.22)
y: No significant difference between any constructs (p > 0.33)
z: a(p < 0.034), all others p > 0.06
Rx: No significant difference between any constructs (p > 0.15)
Ry: c,d,e,f(p < 0.052), all others p > 0.10.
Rz: No significant difference between any constructs (p > 0.22)
x: a(p < 0.018), all others p > 0.06.
y: b(p = 0.055), all others p > 0.10.
z: No significant difference between any constructs (p > 0.11)
Rx: c,d(p < 0.011), all others p > 0.08.
Ry: No significant difference between any constructs (p > 0.17)
Rz: eWX had lower ROM than any WOX, at or approach significance (0.043 < p < 0.10)
Axial force F at failure.
| Construct | Initial failure force F (N) | Maximum failure force F (N) | ||
|---|---|---|---|---|
| WX | WOX | WX | WOX | |
| SI n=3 | −393 ± 69 | −249 ± 141 | −827 ± 34a | −438 ± 207 |
| TS n=3 | −486 ± 171 | −513 ± 157 | −718 ± 74 | −664 ± 54a |
| TA n=2 | −416 ± 226 | −425 ± 43 | −528 ± 269 | −689 ± 59 |
WOX = without anterior external fixation; WX, with anterior fixation.
Initial: p > 0.10
Max: a(p = 0.017), all others p > 0.080