| Literature DB >> 34071578 |
Elena Ángela Carrión1,2, Belén Ferrer2, Juan Francisco Monge3, Pedro Ignacio Saez1, Juan Carlos Pomares2, Antonio González2.
Abstract
Accidents due to falls from height are one of the main causes of death in workplaces. Fall arrest systems (FAS) are designed to arrest the fall safely without injuring the accident victim. Their main mission is to restrain the body so as to prevent it from hitting the ground, generating forces and accelerations in the arrest process that are not harmful. A lack of empirical evidence and scant technical information provided by manufacturers regarding minimum clearance distance (MCD) below anchorage makes it necessary to study the safety distances required in the use of Energy Absorber Lanyards (EAL). This paper aims to determine the MCD below anchorage to arrest a fall using an EAL without hitting the ground. The real deformation of EAL when stopping a fall is studied. Ten EAL models distributed internationally by six manufacturers were chosen. Dynamic behavior tests were performed on the samples. Using image processing the total elongation of the equipment (elastic plus plastic) is obtained. The main conclusions are that maximum plastic elongation could be reduced by 29%. The method described in EN 355: 2002 underestimates elongation by up to 70% for some equipment 20% of EAL's exceed the maximum arrest force (Fm) allowed in EN 355. The MCD data provided by manufacturers is not reliable. The data provided by manufacturers are incomplete. It is recommended that quality control for EAL's be strengthened to ensure that products launched onto the market meet the requirement of EN355. The findings of this study recommended increasing MCD distance longer than that calculated according to EN355, at less than 1 m.Entities:
Keywords: clearance distance; dynamic performance test; elastic and plastic deformation; energy absorber lanyard; fall arrest systems; high-speed camera
Year: 2021 PMID: 34071578 PMCID: PMC8198569 DOI: 10.3390/ijerph18115823
Source DB: PubMed Journal: Int J Environ Res Public Health ISSN: 1660-4601 Impact factor: 3.390
Figure 1Temporary work at height with FAS with EAL.
Figure 2FAS with EAL near the ground level.
Figure 3Relevant distances in FAS.
International standards requirements.
| Standard | Test Mass | Free Fall | ||
|---|---|---|---|---|
| ISO 10333-2:2000 TYPE1 | 100 | 1.8 | 1.2 | 4 |
| NSI/ASSE Z359.13-2013 | 128 1 | 1.83 | 1.2 | 8 |
| ANSI/ASSE Z359.13-2013 | 128 1 | 3.66 | 1.5 | 8 |
| ISO 10333-2:2000 TYPE 2 | 100 | 4 | 1.75 | 6 |
| AS/NZS 1891.1 2007 | 100 | 4 | 1.75 | 6 |
| Z259.11.17 | manufacturer | manufacturer | 0.7~0.95 ( | 8 |
| EN 355:2002 | 100 | 4 | 1.75 | 6 |
1 Conversion factor 1.1 is being used comparing rigid test weight to the human body (140 kg); 2 Maximum elongation that manufacturer declares.
Samples technical specifications according to the manufacturer’s instruction manual.
| Code | Type | Manufacturer | Connectors | ||||
|---|---|---|---|---|---|---|---|
| I | Rope + EA | A | No | 2 | 5 | 1.75 | 1.5 |
| II | Rope + EA | B | Yes | 2 | 4.75 + | 1.75 | - |
| III | Rope + EA | C | No | 1 | 4.4 | - | - |
| IV | Rope + EA | D | Yes | 1.1 | 4.2 | - | - |
| V | Adjustable rope + EA | D | Yes | 2 | 6.2 | 1.2 | 2 |
| VI | Adjustable rope + EA | D | Yes | 2 | 6.2 | 1.2 | 2 |
| VII | Webbing + EA | B | Yes | 1.5 | 4.25 + | 1.75 | - |
| VIII | Elastic webbing | F | No | 1.7 | 6.5 | - | - |
| IX | Elastic webbing + EA | D | Yes | 2 | 6.2 | 1.2 | 2 |
| X | Wire + EA | D | No | 2 | 3 1 | - | - |
1 The manufacturer of this equipment contemplates a use as a fall arrest device limited by the installation system to factor 1 falls (FF = 1). However, it has been tested under the same conditions as the rest of the devices. 2 w is the distance between harness attachment and the user’s feet.
Figure 4Test bench and mass.
Figure 5Dynamic behavior testing procedure.
Figure 6Frame corresponding to the maximum stretch moment for experiment VIII. Some auxiliary lines in the ground help to locate the point to measure the distance from it to the bottom of the ballast.
Figure 7Samples after dynamic behavior testing.
Test results and F′a.
| Test | |||||
|---|---|---|---|---|---|
| I | 1770 | 2690 | 7156 | 4493 | 4439 |
| II | 2030 | 3180 | 4237 | 3823 | 4121 |
| III | 989 | 1152 | 4169 | 3951 | 4347 |
| IV | 880 | 1263 | 5177 | 4504 | 5155 |
| V | 1960 | 3130 | 4326 | 3795 | 4099 |
| VI | 2010 | 3250 | 4220 | 3863 | 4001 |
| VII | 1520 | 2390 | 4127 | 3820 | 4185 |
| VIII | 1660 | 2470 | 4622 | 4172 | 4768 |
| IX | 1430 | 1770 | 5995 | 5075 | 5372 |
| X | 2070 | 2910 | 4911 | 4342 | 5579 |
Kruskal–Wallis.
| Statistic | ||
|---|---|---|
| Kruskal–Wallis | 4.3636 | 0.03671 |
Results (8 samples) of the Wilcoxon test for F.
| Hypothesized Median | Alternative Hypothesis | Statistic | Value Null | Value Null | |
|---|---|---|---|---|---|
| 6 | <6 | 0 | 0.0039 | Reject | Reject |
| 5 | <5 | 2 | 0.0117 | Reject | Accept |
| 4.5 | <4.5 | 16 | 0.4219 | Accept | Accept |
F′–F Exp.
| Test | I | II | III | IV | V | VI | VII | VIII | IX | X |
|---|---|---|---|---|---|---|---|---|---|---|
| 4.493 | 3.823 | 3.951 | 4.504 | 3.795 | 3.863 | 3.820 | 4.172 | 5.075 | 4.342 | |
|
| 4.439 | 4.121 | 4.347 | 5.155 | 4.099 | 4.001 | 4.185 | 4.768 | 5.372 | 5.579 |
| −0.054 | 0.298 | 0.396 | 0.651 | 0.304 | 0.138 | 0.365 | 0.596 | 0.297 | 1.237 |
Figure 8Normal Q–Q plot for F′ Exp.
Figure 9Freefall vs. maximum arrest force (F) and average deployment force.
Elongations.
| Test | ||||||
|---|---|---|---|---|---|---|
| I | 705 | 920 | 235 | 1155 | 1750 | −20.35 |
| II | 105 | 1150 | 345 | 1495 | 1750 | −23.08 |
| III | 2033 | 563 | 45 | 607 | 1750 | −7.25 |
| IV | 2282 | 383 | 85 | 468 | 1750 | −18.16 |
| V | 315 | 1170 | 185 | 1355 | 1750 | −13.65 |
| VI | 185 | 1240 | 195 | 1435 | 1750 | −13.59 |
| VII | 1065 | 870 | 175 | 1045 | 1750 | −16.75 |
| VIII | 1025 | 810 | 135 | 945 | 1750 | −14.29 |
| IX | 1090 | 340 | 770 | 1110 | 1750 | −69.37 |
| X | 610 | 840 | 110 | 950 | 1750 | −11.58 |
Figure 10Elongation vs. free fall distance.
Figure 11Fa Exp, free fall distance and elongation.
Minimum clearance distance (mm).
| Test | MCD | MCDMAN | MCDEN355 | Difference MCDMAN−MCD | Difference MCDEN355−MCD |
|---|---|---|---|---|---|
| I | 5513 | 5000 | 5460 | −513 | −53 |
| II | 6113 | 4750 + | 6210 | 97 | |
| III | 4184 | 4400 | 3541 | 216 | −643 |
| IV | 3936 | 4200 | 3143 | 264 | −793 |
| V | 5903 | 6200 | 6090 | 297 | 187 |
| VI | 6033 | 6200 | 6260 | 167 | 227 |
| VII | 5153 | 4250 + | 4910 | −243 | |
| VIII | 5193 | 6500 | 5130 | 1307 | −63 |
| IX | 5128 | 6200 | 4200 | 1072 | −928 |
| X | 5608 | 6000 | 5980 | 392 | 372 |
Experimental elongation vs. EN 355 requirement.
| Test |
|
| EN 355 | % | % |
|---|---|---|---|---|---|
| I | 920 | 1155 | 1750 | 90 | 52 |
| II | 1150 | 1495 | 1750 | 52 | 17 |
| III | 563 | 607 | 1750 | 211 | 188 |
| IV | 383 | 468 | 1750 | 357 | 274 |
| V | 1170 | 1355 | 1750 | 50 | 29 |
| VI | 1240 | 1435 | 1750 | 41 | 22 |
| VII | 870 | 1045 | 1750 | 101 | 67 |
| VIII | 810 | 945 | 1750 | 116 | 85 |
| IX | 340 | 1110 | 1750 | 415 | 58 |
| X | 840 | 950 | 1750 | 108 | 84 |