non-destructive assessment of outer shell degradation for ... · final report by: r. bryan ormond,...
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© 2017 Fire Protection Research Foundation
1 Batterymarch Park, Quincy, MA 02169-7417, USA Email: [email protected] | Web: nfpa.org/foundation
Non-Destructive Assessment of Outer Shell Degradation for Firefighter Turnouts FINAL REPORT BY:
R. Bryan Ormond, Ph.D., William J. Gabler, Ph.D. Textile Protection and Comfort Center North Carolina State University Raleigh, NC October 2017
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FOREWORD Current retirement criteria for firefighter protective clothing including outer shell materials
establishes a maximum service life in NFPA 1851, Standard on Selection, Care, and Maintenance
of Protective Ensembles for Structural Fire Fighting and Proximity Fire Fighting. However, this
maximum service life does not compensate for amount of usage and exposure time, i.e., a major
city fire department versus a rural fire department fire volume. A non-destructive method is
needed to evaluate the outer shell integrity to determine when a garment is no longer protecting
the wearer at peak efficiency.
The goal of this project was to determine whether Fourier Transform Infrared Spectroscopy (FTIR)
can be used as a non-destructive measurement technique to monitor the degradation of outer
shell fabrics of firefighter turnouts. This summary describes the 1) Outer shell materials evaluated
2) Methods used to expose the samples and to test them, and 3) Results from the material-level
testing.
The Fire Protection Research Foundation expresses gratitude to the report authors R. Bryan
Ormond, and William J. Gabler with Textile Protection and Comfort Center at North Carolina State
University located in Raleigh, NC. The Research Foundation appreciates the guidance provided
by the Project Technical Panelists, and all others that contributed to this research effort. Thanks
are expressed to the National Fire Protection Association (NFPA) for providing the project funding
through the NFPA Research Fund.
The content, opinions and conclusions contained in this report are solely those of the authors and
do not necessarily represent the views of the Fire Protection Research Foundation, NFPA,
Technical Panel or Sponsors. The Foundation makes no guaranty or warranty as to the accuracy
or completeness of any information published herein.
About the Fire Protection Research Foundation
The Fire Protection Research Foundation plans,
manages, and communicates research on a broad
range of fire safety issues in collaboration with
scientists and laboratories around the world. The Foundation is an affiliate of NFPA.
About the National Fire Protection Association (NFPA)
Founded in 1896, NFPA is a global, nonprofit organization devoted to
eliminating death, injury, property and economic loss due to fire, electrical and
related hazards. The association delivers information and knowledge through
more than 300 consensus codes and standards, research, training, education,
outreach and advocacy; and by partnering with others who share an interest in
furthering the NFPA mission.
All NFPA codes and standards can be viewed online for free.
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NFPA's membership totals more than 65,000 individuals around the world.
Keywords: turnout, outer shell, degradation, FTIR, trapezoidal tear strength, non-destructive measurement, meta-aramid, para-aramid, polybenzimidazole
Report number: FRPF-2017-13
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PROJECT TECHNICAL PANEL
Jeffrey Stull, International Personnel Protection
Stephen King, Chair Structural and Proximity Fire Fighting Protective
Clothing and Equipment TC
William Haskell, National Institute for Occupational Safety & Health
Dave Trebisacci, NFPA
Steven Townsend, City of Carrollton Fire Rescue
Tim Tomlinson, Addison Fire Department
PROJECT SPONSORS
National Fire Protection Association
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EXECUTIVE SUMMARY
The goal of this project was to determine whether Fourier Transform Infrared Spectroscopy (FTIR)
could be used as a non-destructive measurement technique to monitor the degradation of outer
shell fabrics of firefighter turnouts. In this study, commonly fielded turnout outer shell materials
comprised of para-aramid, meta-aramid, and polybenzimidazole were subjected to ultra-violet
(UV) exposures, standardized laundering cycles, and repeated radiant heat exposures followed
by chemical surface analysis via FTIR and tear strength measurements.
For the UV exposures, the materials were exposed for 2.5, 5, 7.5, and 10 continuous days of UV
light in an Atlas Ci3000+ Weather-Ometer. The laundered samples were subjected to the NFPA
1971 (8.1.2) laundering procedure for 10, 26, and 50 cycles. For the radiant heat exposures, the
samples were exposed to a blackbody radiant heat source with a heat flux of 0.2 cal/cm2/s for 10,
25, and 50 exposures.
Following the exposures, the material surfaces were analyzed through non-destructive FTIR
measurements to determine if any noticeable changes had occurred in the chemical structures of
the materials. The exposed samples were then subjected to the trapezoidal tear strength test to
physically measure any degradation that may have occurred.
UV light caused significant changes in trapezoidal tear test for all samples at all levels. Only the
highest number of launderings (50) resulted in changes, for all three fabrics. This could be the
result of changes in friction and yarn structure, not necessarily fiber degradation; however, FTIR
signal intensity was found to be influenced by laundering. Only the polybenzimidazole (PBI)
material was affected by radiant exposure, though the change was small and inconsistent.
Interestingly, transmitted heat flux was not affected by the repeated radiant exposures.
For the para-aramid and meta-aramid materials, several FTIR peaks were found to have some
level of linear correlation with the changes in tear strength. The peak at 1730 cm-1, which is
generally characteristic of a carboxylic acid functional group (a known degradation product for
aramid fibers), produced a correlation value (R2) of 0.95285. Further statistical analysis should be
conducted in the future to determine if any of the data follow correlations other than linear trends.
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NC State University
Textile Protection and Comfort Center
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Table of Contents List of Figures ............................................................................................................................................... 1
List of Tables ................................................................................................................................................ 2
Summary ....................................................................................................................................................... 3
Background ................................................................................................................................................... 3
Outer Shell Materials .................................................................................................................................... 3
Methods ........................................................................................................................................................ 4
Trapezoidal Tear Results .............................................................................................................................. 7
Transmitted Heat Flux Results .................................................................................................................... 13
FTIR Results ............................................................................................................................................... 13
Discussion and Conclusions ....................................................................................................................... 18
Recommendations ....................................................................................................................................... 18
References ................................................................................................................................................... 18
Appendix: FTIR Results ............................................................................................................................. 20
List of Figures
Figure 1. Photograph of NCSU’s Stored Energy Tester; Fabric specimen is being exposed to the
radiant source on the left. .............................................................................................................................. 5
Figure 2. Photograph of the fabric samples loaded into the Atlas Ci3000+ Weather-Ometer ........ 5
Figure 3. Photo of a trapezoidal tear test being performed .............................................................. 6
Figure 4. Photograph of the NCSU FTIR test instrument ................................................................ 7
Figure 5. Trapezoidal Tear Results from the UV Exposures for the Fabric B and Fabric C ........... 9
Figure 6. Trapezoidal Tear Results from the UV Exposures for the Fabric A ................................ 9
Figure 7. Trapezoidal Tear Results from Radiant Exposures for Fabric B and Fabric C .............. 10
Figure 8. Trapezoidal Tear Results from Radiant Exposures for the Fabric A .............................. 10
Figure 9. Trapezoidal Tear Results from the Laundering for Fabric B and Fabric C .................... 11
Figure 10. Trapezoidal Tear Results from the Laundering for Fabric A ....................................... 11
Figure 11. Trapezoidal Tear Results from UV Exposures Followed by one cycle of Laundering
(Wash/Dry) for Fabric B and Fabric C ....................................................................................................... 12
Figure 12. Trapezoidal Tear Results from UV Exposures Followed by one cycle of Laundering
(Wash/Dry) for Fabric A ............................................................................................................................. 12
Figure 13. Average Total Transmitted Heat Flux passing through the fabric samples during the
first and fiftieth radiant heat exposure ........................................................................................................ 13
Figure 14. Control spectra of the three test fabrics ........................................................................ 15
Figure 15. Fabric A after Radiant exposure ................................................................................... 20
Figure 16. Fabric A after UV Exposures ....................................................................................... 21
Figure 17. Fabric A after Laundering ............................................................................................ 22
Figure 18. Fabric C after Radiant Heat .......................................................................................... 23
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Figure 19. Fabric C after UV Exposures........................................................................................ 24
Figure 20. Fabric C after Laundering ............................................................................................ 25
Figure 21. Fabric B after Radiant Heat .......................................................................................... 26
Figure 22. Fabric B after UV Exposures........................................................................................ 27
Figure 23. Fabric B after Laundering ............................................................................................ 28
Figure 24. Fabric A after combined UV and Laundering .............................................................. 29
Figure 25. Fabric C after Combine UV and Laundering ............................................................... 30
Figure 26. Fabric B after Combined UV and Laundering ............................................................. 31
List of Tables
Table 1. Details of the Test Materials .............................................................................................. 4
Table 2. Steel-Dwass Results for UV Exposure .............................................................................. 8
Table 3. Steel-Dwass Results for Radiant Exposure ........................................................................ 8
Table 4. Steel-Dwass Results for Laundering .................................................................................. 8
Table 5. Molecular structures of the polymers .............................................................................. 14
Table 6. Assigned Bands for Meta-Aramid and Para-Aramid ....................................................... 14
Table 7. Linear Coefficients of Determination between FTIR intensity and Tear Strength .......... 16
Table 8. Test results comparing the UV and UV-Wash FTIR intensities ...................................... 17
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Summary
The goal of this project is to determine whether Fourier Transform Infrared Spectroscopy (FTIR) can be
used as a non-destructive measurement technique to monitor the degradation of outer shell fabrics of
firefighter turnouts. This summary describes the 1) Outer shell materials evaluated, 2) Methods used to
expose the samples and to test them, and 3) Results from the material-level testing.
Background
Previous studies have used spectroscopic methods to investigate changes in high performance fibers and
other materials commonly used in firefighter clothing. A study on the combined hydrolytic and
photochemical ageing of a para-aramid/polybenzimidazole (PBI) blend found that humidity and
photochemical ageing caused reductions in breaking strength. FTIR analysis could relate this change to a
rise in [-COOH] bonds, which were modeled by temperature-dependent reaction kinetics.1 A similar
approach was used to monitor photochemical ageing of an e-PTFE/meta-aramid composite, finding that
UV irradiation had a negative impact on meta-aramid strength and membrane permeability. This study
claimed that the [-COOH] bond was the only consistent change in the aramid under FTIR analysis.2 A
combination of ATR-FTIR and confocal microscopy found similar results that UV light was the primary
source of damage to para-aramid/polybenzimidazole and meta-aramid/para-aramid blend fabrics. Visual
analysis observed pitting of the fibers and spectroscopic analysis observed changes in several absorbance
bands. The results were used to recommend service lifetimes and storage guidelines for turnout ensembles.3
Other studies have explored the use of raman spectroscopy and NMR analysis, especially for PBI, which
has not shown significant changes in FTIR spectra as a result of environmental stresses.4 Raman
spectroscopy was used to measure changes in the microstructure and molecular structure of para-aramid
with a focus on changes caused by thermal exposure.5 These studies suggest that thermal, UV, and moisture
effects can cause changes in the physical properties of firefighter turnout ensemble materials and that
spectroscopic methods can be used to investigate these changes. However, none of the approaches thus far
have explored the predictive capability of such an approach for whole-fabric samples with the inclusion of
radiant heat and laundering effects.
Outer Shell Materials
All three of the materials used are commonly available outer shells and were donated by manufacturers for
use in this project. The identification and details for each material are provided in Table 1. Fabric A was a
70% polybenzimidazole/30% para-aramid fabric, Fabric B was a 50% para-aramid/50% meta-aramid blend,
and Fabric C was mostly a meta-aramid fabric (~95%) with some (~5%) para-aramid fibers added for
stability.
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Table 1. Details of the Test Materials
Fabric A:
-70% polybenzimidazole/para-aramid
spun yarns
-30% para-aramid filament
-Weight = 7.0 oz/sq yd
-Color: Gold
Fabric B:
-50% para-aramid
-50% meta-aramid
-Weight = 7.0 oz/sq yd
-Color = Black
Fabric C:
-95% meta-aramid
-5% para-aramid
-Weight = 7.5 oz/sq yd
-Color = Red
Methods
Three exposure stimuli were chosen to represent stressors that would be typical to a firefighter turnout in
the field. These were: radiant heat (lower level), laundering (wash and dry cycle), and sunlight (ultraviolet
radiation). After exposure, the fabric samples were tested using FTIR and the trapezoidal tear method. The
results from each set of exposures were compared to “unexposed” materials, and the results can be seen in
the following sections. All reported values of tear strength and FTIR spectra are the mean of six
measurements for each fabric.
The radiant heat exposures were performed using the Stored Energy Testing platform (Figure 1) without
compression, where the heat is provided by a temperature controlled ceramic blackbody radiant heat source
set to 0.2 cal/cm2/s. The 6”x6” fabric specimen is loaded into the pneumatically driven holder that moves
the fabric in front of the radiant heat source. A heat flux sensor is located behind the fabric specimen and
measures heat flux transmitted through the fabric. The heat flux sensor and its surrounding plate are water
cooled to 35°C to provide more accurate long duration heat flux and to better replicate the isothermal nature
of human skin. For this project, the outer shells were exposed for 60-second intervals at 0.2 cal/cm2/s and
allowed to cool back down to room temperature between each test. Each of the three sample fabrics were
tested using this method for 10, 25, and 50 radiant exposures.
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Figure 1. Photograph of NCSU’s Stored Energy Tester; Fabric specimen is being exposed to the
radiant source on the left.
Laundering was performed using the wash and dry cycles specified in NFPA 1971 8.1.2. This is Machine
Cycle 1, Wash Temperature V, and Drying Procedure Ai of AATCC 135 Dimensional Changes in
Automatic Home Laundering of Woven and Knit Fabrics. For this project “1 Laundering” is defined as both
the wash and dry cycle, which were performed 10, 26, and 50 times.
The UV exposures were performed using the Atlas Ci3000+ Weather-Ometer shown in Figure 2. This
device has a solar lamp located in the center, and the fabric specimens are loaded in a circle facing inward
towards the light. The instrument also regulates the temperature and humidity of the environment to more
closely resemble outside weather. For this project, the instrument was set to represent a summer’s day in
Phoenix, Arizona (highest UV setting), with UV radiation of 350 MJ/m2, temperature of 39°C, and relative
humidity of 32%. The outer shells were exposed to 2.5, 5, 7.5, and 10 continuous days of sun and tested
after each interval.
Figure 2. Photograph of the fabric samples loaded into the Atlas Ci3000+ Weather-Ometer
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Unexposed and exposed samples were scanned using an FTIR (non-destructive) instrument followed by
the trapezoidal tear test (destructive) and compared. From the recommendation of the technical panel,
trapezoidal tear is a primary indicator of outer shell failure in a turnout suit. The trapezoidal tear resistance
was performed according to NFPA 1971 (2013) Section 8.12. The fabric sample is held in place by two
grips, a small slit is cut into the side of the fabric (Figure 3), and a pulling force is applied until the fabric
rips. This test is typically run in both the warp and weft directions, but due to limited fabric amounts, the
samples were only torn in the weft direction, which represented the “worst-case scenario.” However, the
three fabrics were relatively balanced and performed similarly in warp and weft directions. For NFPA 1971,
woven fabrics must have a tear strength of not less than 100N. Due to the high strength of these materials,
the highest level grips and load cell were used for the instrument and occasional “slip” still occurred.
Figure 3. Photo of a trapezoidal tear test being performed
FTIR spectroscopy was performed using a bench-size instrument for this project (Figure 4), but handheld
devices exist. FTIR is a technique where a controlled beam of electromagnetic energy in the infrared
spectrum is applied to the fabric sample and the amount of reflectance/absorbance is quantified. This is
performed for all wavenumbers of the infrared spectrum (500-4,000 cm-1) and the presence of “peaks”
represent the abundance of particular bonds within the fabric specimen. Of particular interest for the aramid-
based materials is the peak located at the wavenumber of 1730 cm-1, which represents the formation of a
carboxylic acid (-COOH) bond as a result of chain scission between the benzene rings in the aramids. This
bond is typically the first to break down when exposed to mechanical or energy stimuli.
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Figure 4. Photograph of the NCSU FTIR test instrument
Trapezoidal Tear Results
Fabrics B and C (para- and meta-aramid blends) performed similarly for the trapezoidal tear, and their data
are included on the same graph. The tear strengths for Fabric A were significantly higher due to the
incorporation of the polybenzimidazole fiber, so the results were included on separate graphs. The data
were analyzed first using the Median Test to detect if the median of each level of treatment was significantly
different from the group, then using the Steel-Dwass method to test for differences in the tear strength
resulting from the various levels of treatment for all pairs. The significance values from the test are
summarized in Table 2-Table 4, with a p<0.05 indicating a significant difference. The mean trapezoidal
tear strengths are given in Figure 5-Figure 12.
The UV exposure had the most drastic impact on the turnout material trapezoidal tear strength, where a
significant drop was seen after just 2.5 days (60 hrs) for all the fabrics (Figure 5 and Figure 6). The majority
of the drop in performance can be seen in the first 2.5 days of UV exposure and the performance drop for
each subsequent 2.5 day interval is not as dramatic. The 10 days of UV exposure resulted in an average
drop in trapezoidal tear strength of 68%, 62%, and 81% for the Fabric A, Fabric B, and Fabric C,
respectively. Both Fabric B and Fabric C dropped below the NFPA performance standard of 100N after
just 2.5 days of constant UV exposure. All of the results for the UV exposures on Fabric A were different
from the control, but were not significantly different from each other.
The trapezoidal tear results for laundering and radiant heat applied in these samples in general did not differ
from the unexposed fabric samples or show inconsistent results. After 50 washes, Fabric A showed a
reduction in trapezoidal tear strength of by approximately 46% (Figure 10), while Fabric B reduced by
approximately 29% (Figure 9). Only the Fabric B sample exposed to 10 radiant exposures showed a
significant drop in tear strength as a result of radiant exposure.
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The addition of one laundering after the UV exposures did not appear to influence the trapezoidal tear
strength. Some of the Fabric A samples exhibited “slip” of the grips during testing, which resulted in high
outlier samples and higher variability.
Table 2. Steel-Dwass Results for UV Exposure
UV p-values
Level Level Fabric A Fabric B Fabric C
7.5 0 0.0261 0.0261 0.0261
7.5 2.5 0.9998 0.0261 0.0261
7.5 5 0.747 0.3335 0.0261
5 0 0.0405 0.0261 0.0261
5 2.5 0.9684 0.0261 0.0261
2.5 0 0.0411 0.0261 0.0261
Table 3. Steel-Dwass Results for Radiant Exposure
Radiant p-values
Level Level Fabric A Fabric B Fabric C
50 0 0.2539 0.9998 0.8889
50 10 0.9998 0.9783 0.0931
50 25 0.8149 0.9951 0.9951
25 0 0.0931 0.9783 0.4247
25 10 0.6262 1.000 0.0261
10 0 0.2539 0.9437 0.0261
Table 4. Steel-Dwass Results for Laundering
Wash p-values
Level Level Fabric A Fabric B Fabric C
50 0 0.0261 0.0261 0.4247
50 10 0.0261 0.0261 0.7254
50 26 0.0261 0.134 0.8889
26 0 0.9783 0.0261 0.9998
26 10 0.1873 0.0411 1.000
10 0 0.3335 0.9783 0.9783
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Figure 5. Trapezoidal Tear Results from the UV Exposures for the Fabric B and Fabric C
Figure 6. Trapezoidal Tear Results from the UV Exposures for the Fabric A
140.7
91.168.7 61.9 53.7
169.9
68.846.2 37.0 32.0
0.0
50.0
100.0
150.0
200.0
250.0
Unexposed 2.5 Days UV 5 Days UV 7.5 Days UV 10 Days UV
New
ton
sEffect of UV Light - Fabric B and Fabric C
UV Exposure for Continuous Days
959.5
411.5 412.8 374.9309.5
0.0
200.0
400.0
600.0
800.0
1000.0
1200.0
Unexposed 2.5 Days UV 5 Days UV 7.5 Days UV 10 Days UV
New
ton
s
Effect of UV Light - Fabric A
UV Exposure for Continuous Days
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Figure 7. Trapezoidal Tear Results from Radiant Exposures for Fabric B and Fabric C
Figure 8. Trapezoidal Tear Results from Radiant Exposures for the Fabric A
140.7 136.2 138.0 137.8
169.9149.1
162.1 165.1
0.0
50.0
100.0
150.0
200.0
250.0
Unexposed 10 Radiant Exposures 25 Radiant Exposures 50 Radiant Exposures
New
ton
sEffect of Radiant Exposures - Fabric B and Fabric C
Exposures @ 0.2 Cal/cm2/s for 60 seconds
959.5
757.8 703.1769.7
0.0
200.0
400.0
600.0
800.0
1000.0
1200.0
Unexposed 10 Radiant Exposures 25 Radiant Exposures 50 Radiant Exposures
New
ton
s
Effect of Radiant Exposures - Fabric A
Exposures @ 0.2 Cal/cm2/s for 60 seconds
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Figure 9. Trapezoidal Tear Results from the Laundering for Fabric B and Fabric C
Figure 10. Trapezoidal Tear Results from the Laundering for Fabric A
140.7 139.1110.8 100.8
169.9 171.8 168.2 174.4
0.0
50.0
100.0
150.0
200.0
250.0
Unexposed 10 Launderings 26 Launderings 50 Launderings
New
ton
sEffect of Laundering - Fabric B and Fabric C
Wash and Dry Cycles - NFPA 1971
959.5
749.2
910.5
518.5
0.0
200.0
400.0
600.0
800.0
1000.0
1200.0
Unexposed 10 Launderings 26 Launderings 50 Launderings
New
ton
s
Effect of Laundering - Fabric A
Wash and Dry Cycles - NFPA 1971
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Figure 11. Trapezoidal Tear Results from UV Exposures Followed by one cycle of Laundering
(Wash/Dry) for Fabric B and Fabric C
Figure 12. Trapezoidal Tear Results from UV Exposures Followed by one cycle of Laundering
(Wash/Dry) for Fabric A
140.7
90.367.7 61.1
169.9
56.242.7 37.0
0.0
50.0
100.0
150.0
200.0
250.0
Unexposed 2.5 Days UV+ Wash 5 Days UV+ Wash 7.5 Days UV+ Wash
New
ton
sEffect of Laundering and UV Light - Fabric B and Fabric C
UV Exposure then Wash/Dry Cycle
959.5
465.2331.0 298.3
0.0
200.0
400.0
600.0
800.0
1000.0
1200.0
Unexposed 2.5 Days UV+ Wash 5 Days UV+ Wash 7.5 Days UV+ Wash
New
ton
s
Effect of Laundering and UV Light - Fabric A
UV Exposure then Wash/Dry Cycle
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Transmitted Heat Flux Results
Another finding from the project is related to the thermal protective performance of the outer shell samples.
After 50 exposures under the radiant heat protocol, the fabric samples did not show statistically significant
differences in their protective performance (Figure 13). The mean values of the samples that had undergone
repeated radiant heat exposures did have consistently lower mean heat fluxes, implying there may have
been a small improvement in protective performance for these samples.
Figure 13. Average Total Transmitted Heat Flux passing through the fabric samples during the
first and fiftieth radiant heat exposure
FTIR Results
The averaged FTIR spectra for all the test scenarios are displayed in the Appendix (Figure 15-Figure 26).
The intensity of the peaks are related to their abundance in the chemical structure of the fibers. Figure 14
shows the spectra of the controls. Table 5 shows the molecular structures of the polymers and Table 6
identifies several peaks of interest for each polymer based on the cited literature.
135
140
145
150
155
160
165
170
175
180
Average Total Transmitted Heat Flux (kJ/m2)
1st Exposure 50th Exposure
Fabric B
Para-Aramid BlendFabric A
PBI/Para-Aramid Blend
Fabric C
Meta-Aramid Blend
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Table 5. Molecular structures of the polymers
Fiber type Molecular structure
Para-Aramid1
Meta-Aramid
Polybenzimidazole1
Table 6. Assigned Bands for Meta-Aramid and Para-Aramid
Wavenumber (cm-1) Band assignments6,7
3300 N—H stretchin in secondary amide
1730 -COOH formed from degredation
1645 C=O stretching on amide
1600 C=C stretching in aromatic ring
1540 N—H bending and C—N stretching of the C—N—H group
1305 C—N aromatic stretching
1240 C—N stretching, N—H in plane bending, and C—C stretching
Unidentified wavenumbers that show changes in this study: 2915, 2845, 2358, 1405, 1043
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Figure 14. Control spectra of the three test fabrics
The purpose of the FTIR analysis was to test the hypothesis that changes in peak intensities could be
correlated with changes in tear strength caused by the environmental treatments. An initial analysis of the
relation between FTIR intensities and tear strength was performed using linear regression analysis for each
wavenumber. The 108 combinations of fiber, treatment, and wavenumber analyzed and sorted by the
coefficient of determination value, R2 (an ideal or perfect correlation would produce an R2 value of 1.0000).
Thirteen (12%) of the 108 combinations resulted in R2>0.8 (Table 7), though the values dropped off quickly,
with 75% of the combinations showing an R2 of less than 0.3. These were all for wavenumbers from the
meta-aramid and para-aramid samples exposed to UV. All of these fits had positive slopes with the
exception of the 1730cm-1 wavenumber, which had a negative regression line between peak intensity and
tear strength. This supports previous findings that this wavenumber represents the formation of a
degradation product of the aramid polymer.
None of the Fabric A samples showed high correlation (R2) values with a wavenumber. The highest was
R2=0.5 for the 1240cm-1 of the laundered samples. It should be noted that Fabric A did contain 30% para-
aramid fibers blended with the polybenzimidazole fibers. A previous study on the FTIR spectrum of a para-
aramid/PBI yarn blend found that para-aramid dominated the FTIR spectra and few characteristic peaks
were attributable to the PBI polymers.6 The 1240cm-1 band should be shared by all three polymers and was
found to be a highly influencing wavenumber. Interestingly, several of the unidentified bands, notably 2358,
were found to be significant.
0
0.01
0.02
0.03
0.04
0.05
5001000150020002500300035004000
Abso
rban
ce
Wavenumber (cm -1)
Control Samples (Unwashed and Unexposed to UV or Radiant Heat)
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Table 7. Linear Coefficients of Determination between FTIR intensity and Tear Strength
Fabric Treatment Wavenumber
(cm-1) R2
Fabric C - meta-aramid UV 1240 0.82490
Fabric C - meta-aramid UV 1730 0.86564
Fabric B - para-aramid UV 1540 0.88038
Fabric C - meta-aramid UV 1305 0.88055
Fabric B - para-aramid UV 1305 0.88850
Fabric C - meta-aramid UV 1540 0.88940
Fabric B - para-aramid UV 2915 0.90892
Fabric B - para-aramid UV 1645 0.91738
Fabric B - para-aramid UV 1240 0.91787
Fabric B - para-aramid UV 2845 0.92388
Fabric B - para-aramid UV 1600 0.92873
Fabric B - para-aramid UV 1730 0.95285
Fabric B - para-aramid UV 2358 0.95321
The influence of combined factors and treatments was examined next. FTIR is a surface measurement and
it is possible that a treatment may not cause a linear change in FTIR signal. Changes to the molecular
structure that are located deeper inside the fiber or fabric structure may not be detected and an
environmental treatment could exhibit a “saturated” surface signal. Additionally, interference or
counteracting effects could result from surface soiling or the combination of treatments such as radiation
and laundering.
The most likely combined effect was decided to be laundering and UV exposure, so a separate set of
samples were subjected to the UV exposure regime with the addition of a laundering immediately after each
UV exposure. The FTIR readings taken before and after each laundering were compared using the Kruskal-
Wallis test, a nonparametric test with a null hypothesis that the mean ranks of data from the two groups are
the same (i.e. whether the readings before and after laundering come from indistinguishable distributions).
The 108 combinations of data (12 wavenumbers for 3 fibers at 4 levels of UV exposure) were tested, and
28 (26%) of the results indicated a significant difference (p<0.05 for the 2-sample normal approximation),
meaning the laundering caused a significant change in the FTIR readings. The values are presented in Table
8, sorted by wavenumber. A positive Z value indicates that the laundering caused an increase in FTIR peak
intensity and a negative Z value indicates a decrease. The most significant finding is that the laundering
was shown to decreases the 1730 cm-1 signal for all treatment levels of Fabric C and some levels of Fabric
B and the 1540cm-1 signal was increased. This means that laundering counteracted the trends seen in the
linear fits in the previous section. 2845cm-1 and 2358cm-1 were also affected.
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Table 8. Test results comparing the UV and UV-Wash FTIR intensities
Wavenumber Fabric Intensity Z Prob>|Z|
1043 B 5 2.32186 0.0202
1043 B 2.5 2.00160 0.0453
1405 A 7.5 2.16173 0.0306
1540 A 7.5 2.64211 0.0082
1540 C 2.5 2.32186 0.0202
1540 C 5 2.32186 0.0202
1540 B 2.5 2.00160 0.0453
1645 A 7.5 2.48199 0.0131
1645 A 5 2.16173 0.0306
1730 C 2.5 -2.80224 0.0051
1730 C 5 -2.80224 0.0051
1730 B 7.5 -2.80224 0.0051
1730 C 7.5 -2.80224 0.0051
1730 B 5 -2.64211 0.0082
1730 A 5 -2.16173 0.0306
2358 B 2.5 -2.80224 0.0051
2358 C 7.5 -2.80224 0.0051
2358 C 5 2.64211 0.0082
2358 A 5 -2.64211 0.0082
2358 C 2.5 2.16552 0.0303
2358 A 2.5 -2.16173 0.0306
2845 C 2.5 2.64211 0.0082
2845 A 7.5 2.32186 0.0202
2845 C 5 2.16173 0.0306
2915 C 7.5 -2.16173 0.0306
2915 C 2.5 2.0016 0.0453
3300 A 7.5 2.16173 0.0306
Three of the wavenumbers, 1200, 1305, and 1600, were not found to be impacted by laundering and could
potentially be more reliable wavenumbers to monitor.
The future step in evaluating the relation between FTIR intensity and tear strength will be to form a multiple
regression fit model that incorporates several wavenumbers to see if a combination of the signals gathered
can provide better predictive capability than the single wavenumber data above.
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Discussion and Conclusions
This work is unique in that it considers the possibility of correlating FTIR surface measurements of whole
fabric samples with changes in physical properties of aramid fibers caused by environmental exposure.
Fabrics used in commercially available firefighter turnout shells were conditioned to UV light, laundering,
and radiant heat exposure. UV light caused significant changes in trapezoidal tear test for all samples at all
levels. Only the highest number of launderings (50) resulted in changes, for all three fabrics. This could be
the result of changes in friction and yarn structure, not necessarily fiber degradation; however, FTIR signal
intensity was found to be influenced by laundering. Only Fabric A was affected by radiant exposure, though
the change was small and inconsistent. Interestingly, transmitted heat flux was not affected by the repeated
radiant exposures.
Several FTIR peaks were found to change linearly with changes in trapezoidal tear strength; however, none
of the signals were applicable for Fabric A and the changes were only as a result of UV exposure in the
other fibers/fabrics. Further, several of these wavenumber correlations were found to be counteracted by
laundering, meaning that samples would have to be tested before laundering, or the effect would have to be
corrected for in an applied field method. While some effects on outer shell material strength can be
ascertained on some materials using FTIR, at the current time a significant amount of further work would
be needed to develop a procedure that may provide means of non-destructively assessing shell strength.
Recommendations
This work opens the possibility for additional phases of study to further evaluate non-destructive
measurements of turnout gear materials. Building directly off this research, the next step would be to apply
more sophisticated data correlation models to assess the correlation between the measured tear strength and
the FTIR spectra. Instead of taking only a single peak in the spectrum to assess correlations, it should be
possible to assess multiple peaks simultaneously with the appropriate models.
Several additional questions could be addressed such as:
What is the variability of the FTIR test?
Do surface characteristics of the fabrics affect response?
Do the treatment methods affect those characteristics?
What is the influence of soiling and laundering on analysis of worn samples?
What other non-destructive measurement techniques are feasible for evaluation?
References
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Kevlar®-PBI blend. Polym. Degrad. Stab. 96, 1411–1419 (2011).
2. El Aidani, R., Nguyen-Tri, P., Malajati, Y., Lara, J. & Vu-Khanh, T. Photochemical aging of an e-
PTFE/NOMEX® membrane used in firefighter protective clothing. Polym. Degrad. Stab. 98,
1300–1310 (2013).
3. Davis, R., Chin, J., Lin, C.-C. & Petit, S. Accelerated weathering of polyaramid and
polybenzimidazole firefighter protective clothing fabrics. Polym. Degrad. Stab. 95, 1642–1654
(2010).
4. Guenther, J., Wong, M., Sue, H.-J., Bremner, T. & Blümel, J. High-temperature steam-treatment
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of PBI, PEKK, and a PEKK-PBI Blend: A solid-state NMR and IR spectroscopic study. J. Appl.
Polym. Sci. 128, 4395–4404 (2013).
5. Ahmed, D. et al. Structural Changes Of Kevlar Fibers In The Process Of Heat Treatment Using
Raman Spectroscopy. Int. J. Adv. Sci. Tech. Res. 4, 11–16 (2013).
6. Arrieta, C., David, E., Dolez, P. & Vu-Khanh, T. Thermal aging of a blend of high-performance
fibers. J. Appl. Polym. Sci. 115, 3031–3039 (2010).
7. Villar-Rodil, S., Paredes, J. I., Martínez-Alonso, A. & Tascón, J. M. D. Atomic Force Microscopy
and Infrared Spectroscopy Studies of the Thermal Degradation of Nomex Aramid Fibers.
doi:10.1021/cm001219f
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Appendix: FTIR Results
Figure 15. Fabric A after Radiant exposure
-Unexposed
- After 10 Radiant Exposures
- After 25 Radiant Exposures
- After 50 Radiant Exposures
Fabric A
Radiant Exposures
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Figure 16. Fabric A after UV Exposures
-Unexposed
- After 2.5 Hours UV
- After 5 Hours UV
- After 7.5 Hours UV
Fabric A
UV Exposures
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Figure 17. Fabric A after Laundering
-Not Laundered
- After 10 Launderings
- After 26 Launderings
- After 50 Launderings
Fabric A
Laundering Cycles
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Figure 18. Fabric C after Radiant Heat
-Unexposed
- After 10 Radiant Exposures
- After 25 Radiant Exposures
- After 50 Radiant Exposures
Fabric C
Radiant Exposures
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Figure 19. Fabric C after UV Exposures
-Unexposed
- After 2.5 Hours UV
- After 5 Hours UV
- After 7.5 Hours UV
Fabric C
UV Exposures
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Figure 20. Fabric C after Laundering
-Not Laundered
- After 10 Launderings
- After 26 Launderings
- After 50 Launderings
Fabric C
Laundering Cycles
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Figure 21. Fabric B after Radiant Heat
-Unexposed
- After 10 Radiant Exposures
- After 25 Radiant Exposures
- After 50 Radiant Exposures
Fabric B
Radiant Exposures
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Figure 22. Fabric B after UV Exposures
-Unexposed
- After 2.5 Hours UV
- After 5 Hours UV
- After 7.5 Hours UV
Fabric B
UV Exposures
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Figure 23. Fabric B after Laundering
-Not Laundered
- After 10 Launderings
- After 26 Launderings
- After 50 Launderings
Fabric B
Laundering Cycles
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Figure 24. Fabric A after combined UV and Laundering
-Unexposed, Not Laundered
- 2.5 Hours UV, Before Laundering
- 2.5 Hours UV, After Laundering
- 5 Hours UV, Before Laundering
- 5 Hours UV, After Laundering
- 7.5 Hours UV, Before Laundering
- 7.5 Hours UV, After Laundering
Fabric A
Combined UV and
Laundering
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Figure 25. Fabric C after Combine UV and Laundering
-Unexposed, Not Laundered
- 2.5 Hours UV, Before Laundering
- 2.5 Hours UV, After Laundering
- 5 Hours UV, Before Laundering
- 5 Hours UV, After Laundering
- 7.5 Hours UV, Before Laundering
- 7.5 Hours UV, After Laundering
Fabric C
Combined UV and
Laundering
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Figure 26. Fabric B after Combined UV and Laundering
-Unexposed, Not Laundered
- 2.5 Hours UV, Before Laundering
- 2.5 Hours UV, After Laundering
- 5 Hours UV, Before Laundering
- 5 Hours UV, After Laundering
- 7.5 Hours UV, Before Laundering
- 7.5 Hours UV, After Laundering
Fabric B
Combined UV and
Laundering