The influence of textile materials on flame resistance ratings of professional uniforms
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Abstract
This study compares the flame speed of different textile materials employed in professional uniforms. Five different garments of aeronauts’ uniforms were analyzed (totaling 200 specimens submitted to flammability tests). Plain weaves and twill weaves composed by 100% CO; 100% PES; 67% PES/33% CO; 50% PES/50% WO; and 55% PES/45%WO were analyzed in the warp and filling directions. The flame speed of each material was determined, and differences in the flame propagation of the fabrics were identified. The lowest flame speed occurred for the material 50% PES/50% WO plain weave and weft direction (0.742 ± 0.140 m/s). The highest flame speed was 3.698 ± 1.806 cm/s for the material 67%PES/33%CO, plain weave and filling direction. Future experiments for reducing the fabric flammability of the uniforms could be related to more closed fabric constructions; mixtures with synthetic fibers to add functionality; changing the direction of the fabric; and changing the weight and torsion of its constituent yarns.
Keywords
Flammability Textile Uniform Aeronaut Civil aviation Statistical analysis of factors1 Introduction
Flammability is explained by Lewin [1] and Sinclair [2] as the tendency of a material to ignite and burn with a flame creating a fire risk situation. In textile materials, it represents the easiness with which the fabric is capable of being ignited and how effectively it burns, considering that the response to the heat depends mainly on its chemical composition. Thus, they can be classified as thermoplastics, which soften and melt above certain temperatures and non-thermoplastics, which tend to carbonize and embrittle at high temperatures.
In addition, textile combustibility is related to the rate at which the flame is able to propagate. Exothermic reactions are triggered when the ignition temperature of the fabric is reached. The high risk of fire attributed to the fabrics is due to their large area surface and the ease of access to the environmental oxygen [3, 4].
Fan and Lau [5] consider the influence of the textile material on the burning mechanism as one of two components of the fire quadrilateral: the fuel and the oxidizing agent (oxygen). The type of fiber such as its chemical composition and the possible application of flame-retardant finishes play important roles as fuel. The structure of the fabric, represented by its ligament, yarn density, covering factor and weight, is related to the air/oxygen ratio on the fabric surface and its action as oxidizing agent.
One of the factors for the differentiation of fabric flame speed is the fiber material composition. Fabrics made from untreated natural fibers such as cotton, linen, silk, present easy ignition and rapid flame propagation. Fabrics made from synthetic fibers and, however, resist ignition, but the textile material melts [6, 7].
Another flammability indicator is the limiting oxygen index (LOI), which represents the minimum concentration of oxygen, expressed as a percentage, that will support combustion of a polymer. In this way, the lower LOI, the easier the fiber burns and this index can be applied to almost all fibers [8].
The textile fibers are selected based on their characteristics, and the most appropriate ones are employed in the final product. Some examples of these characteristics are: durability, fineness, abrasion resistance, impermeability, etc. [9]. The fibers are transformed into yarns and employed in the manufacture of flat woven, knitted or nonwoven fabrics [10]. Among other factors, the chemical nature of the fibers is related to a very large variation in the flammability of the fabrics, being very flammable in the cellulosic fibers and in the common synthetic fibers [11].
Until the eighteenth century, the main fibers employed in domestic production were those of natural origin, such as wool, cotton, silk, hemp and flax. The first manufactured fiber, called regenerated cellulose fiber (rayon or viscose rayon), was developed at the end of the nineteenth century, but only in the twentieth century began its industrial production. The development of chemical fibers based on petroleum products started in the late 1930s and industrial production launched during World War II [12].
Flat woven fabrics are non-continuous materials with anisotropic mechanical properties. Besides the characteristics of the constituent fibers, the performance of the textile materials depends on the weaving mechanics and geometry [13]. The weaving pattern influences the maximum density through the intersecting relationship of warp and weft yarns as well as weight and thickness [9].
In addition, most fabrics are flammable within certain limits. However, this does not mean that the clothes inflame during normal wearing. On the other hand, the number of fatal accidents involving fire in clothing is greater than cases involving furniture [14].
Uniform is emblematic, since it legitimizes and indicates the status of wearer, but also suppresses individuality. It is seen as a barrier, which ensures that each member of the organization will act according to their function and be perceived as important parts of their professional identity [15, 16]. In military sector, besides the status, it plays an important role in the process of transforming the inexperienced and untrained recruit into a member of the military force [17].
Professional uniforms are not required for all functions. It is a company’s choice in order to represent its brand considering the symbolic value of the uniform. The development of professional uniform garments generally takes into account the aesthetic characteristics and cost. For functions requiring uniform such personal protective equipments (PPE), the specifications for the textile material are regulated. In this context, the collections developed for uniforms of aeronauts (workers on board the aircrafts) do not consider their acting also as flight safety agents, which eventually could be subjected to the combat of fires on board [8].
The objective of this study was the analysis of the flammability (flame speed) of textile materials employed in the manufacturing of professional uniforms of aeronauts (flight crew) of Brazilian airlines.
2 Materials and methods
2.1 Specimens
During the period from February 2016 to March 2017, uniforms of aeronauts were acquired by donations. The companies did not allow the disclosure of brand’s name. In this way, they were named as companies “A” and “B.” A preliminary analysis of these samples (P1 to P8) indicated the following structures and materials: Airline company “A”—(P1) 100% polyester (PES) twill fabric female shirt; (P2) 100% PES plain fabric female shirt; and (P3) 67% PES/33% cotton (CO) twill fabric male shirt; Airline company “B”—(P4 and P5) 67% PES/33% CO plain fabric male shirts; (P6) 55% PES/45% wool (WO) male coat; (P7) 50% PES/50% WO male trousers; and (P8) 55% PES/45% WO male coat.
For preliminary analysis, professional fabrics (T1—100% CO, and T2—67% PES/33% CO) were purchased on the market for preliminary destructive testing, preserving professional uniforms material, until the improvement of the methods.
Information on the material of the fibers was collected from the label tags. In addition, FTIR (Fourier-transform infrared spectroscopy) tests were carried out to confirm such information.
Uniforms of Airline company “A”: a P1—100% PES twill fabric female pleats shirt; b P2—100% PES plain fabric female plaid shirt; c P3—67% PES/33% CO twill fabric male maintenance service shirt. Scale 10 cm
Uniforms of Airline company “B”: a, b P4 and P5—67% PES/33% CO plain fabric male shirts; c P6—55% PES/45% WO male coat; d P7—50% PES/50% WO male trousers; e P8—55% PES/45% WO male coat
2.2 Fiber material: label tags and FTIR
A visual analysis of the uniforms and fabrics was performed, and the fabric structure (plain or twill) was verified. In addition, the information of the textile composition was obtained from the product label tag, since such information is obligatory for textile apparels made in Brazil (ABNT NBR NM IS 3758:2013) [18].
In order to confirm the textile materials stated on the label tags, a sample of at least 5 grams of the fabric of each uniform (P1 to P5) and of the fabrics (T1 and T2) was analyzed by spectroscopy in the medium infrared region (700 to 4000 cm−1) in FTIR equipment Thermo Avatar 370 with ATR (Nicolet, USA) and Omnic software, version 4.1 in comparison with standards stored in the equipment library [19].
2.3 Weaving pattern
The determination of the weaving pattern (plain, twill or satin), that is, the interweaving of warp and filling (or weft) yarns of the fabrics (T1 and T2) and the fabrics of parts of the uniforms (P1 to P8), followed the protocol established by standard ABNT 12996: 1993—Textile material—Determination of basic weaves—Method of test [20]. A pick glass, 10 × visualization was employed. Subsidiarily, the Portuguese Standard NP 4114:1991—Textile: Construction. Methods of analysis [21] and ISO 7211-1: 1984—Textiles—Woven fabrics—Construction—Methods of analysis-Part 1: Methods for the presentation of a weave diagram and plans for drafting, denting and lifting [22] were also applied.
2.4 Yarn density (thread count)
The yarn density (thread count) indicates how many warp or filling yarns are aligned per centimeter in the fabric. The test was carried out according to the standard NBR ABNT 10588:2015—Woven—Determination of density yarn [23]. This is a necessary information for calculating cover factor. A pick glass, 10 × visualization was employed. Subsidiarily, the Portuguese Standard NP EM 1049-2:1995—Textiles—Woven fabrics—Construction—Methods of analysis—Part 2: Determination of density of threads per unit length [23] and ISO 7211-2: 1984—Textiles—Woven fabrics—Construction—Methods of analysis—Part 2: Determination of number of threads per unit length [24] were also applied.
2.5 Thickness
The thickness measurement was performed according to the ABNT NBR 13371: 2005—Textiles materials—Determination of thickness [25]. The measurements in each sample were carried out in ten different points without damaging it. The portable analog thickness gauge (model 7321, Mitutoyo, Japan), 0.01 mm precision and 18 Pa pre-established clamp pressure, was employed.
2.6 Weight
2.7 Linear density and crimp
This test was performed according ISO 7211/5:1984 (Textiles—Woven fabrics—Construction—Methods of analysis—Part 5: Determination of linear density of yarn removed from fabric) [28] together the Crimp Test ISO 7211/3:1984 (Textiles—Woven fabrics—Construction—Methods of analysis—Part 3: Determination of crimp of yarn in fabric) [29] employing the Crimp Tester Maillemetre. From each sample fabric, 11 warp and 11 filling threads were extracted. After conducting the pretension test and determining the load, each thread was weighed and the value of its linear density was determined in Tex (grams per 1000 m).
2.8 Thread twist
The tests were carried out according to ISO 7211/4:1984—Textiles—Woven fabrics—Construction—Methods of analysis—Part 4: Determination of twist in yarn removed from fabric [30]. For open-end 70-cm-length threads, twistronic device was employed (Mesdan, Italy). The thread is placed in the jaws of the equipment, causing its distortion and twisting, and the value is displayed on the electronic panel. For samples smaller than 70 cm, twist tester from James H. Heal & Co., Ltd., was employed.
2.9 Yarn diameter calculation by Peirce geometric model
Fiber | ΡF |
---|---|
Cotton | 1.52 |
Polyester | 1.38 |
Wool | 1.32 |
Process | \(\emptyset\) |
---|---|
Ring spinning | 0.60 |
Open end | 0.55 |
Combed yarn | 0.60 |
Spinned wool | 0.55 |
Continuous filament | 0.65 |
d = yarn diameter (mm); T = linear density (Tex); ρf = fiber density (g/cm3); \(\emptyset\) = yarn packing factor.
\(\rho\) = average of fiber densities; pi = weight fraction of umpteenth component; pft = fiber density (g/cm3); n = number of the mixture components.
2.10 Cover factor
C = cover factor; W = warp threads per inch; F = filling threads per inch; dw = warp yarn diameter (in inches); df = filling yarn diameter (in inches).
2.11 Flame speed
The flame speed test was performed from the adaptation of the American standard CFR 1610 (Standard for the flammability of clothing textiles) [34]. The flame size was adjusted at 16 mm and was applied on the surface of the fabric, near the bottom edge for 3 s using propane gas and without forced exhaustion.
Flammability test cabin built for the flame speed experiments
The construction of a flammability test cabin was because of the specificity of the small samples, the prioritization in the measurement of flame speed and the quantity of assayed samples, totaling 200 tests. The measurement system of this flammability cabin was statistically pre-validated according to the cited standards (data not shown).
For the fabric samples removed from the aeronauts’ uniforms (P1 to P8), 20 specimens were prepared in the dimensions of 55 by 155 mm. Each sample was fixed to the frame and placed in the cabin with the inclination of 45°. The flame size, adjusted at 16 mm, was applied to the fabric surface, close to the lower edge for 3 s, employing propane gas and without forced exhaustion. The flame traversed the length of the fabric by 135 mm to the marked limit with the pendulum support line which, upon breaking, triggers the sensor and closes the time count on timer. As pretests, the same assay described was performed with fabric samples T1 and T2.
2.12 Experimental design
Experimental design
2.13 Data analysis
With data collected, a one-way analysis of variance (ANOVA) was performed. To verify the ANOVA assumptions [38], the Anderson–Darling tests were performed to verify the normality of the residual distribution and the Bartlett, Levene and Bonett tests to verify the homogeneity of the variances and the comparison of averages by the multiple comparisons test with the best, proposed by Hsu at the 5% probability level. When necessary, the Kruskal–Wallis nonparametric test was performed.
These data were analyzed statistically using Minitab software (Minitab Inc., version 18—2017), available by Institutional Software Download System of the Information Technology Superintendence of USP.
3 Results and discussion
The FTIR analysis confirmed the information present in the label tags of all uniforms (data not shown).
Results of tests on fabrics from aeronauts’ uniforms and purchased ones, expressed in material (CO—cotton, PES—polyester and WO—wool), weave (plain and twill), number of threads (by cm), weight (g/m2), yarn density (Tex), twist (torsions/m), yarn diameter (calculated by Peirce model), cover factor and flame speed. The values of direct measurements values are indicated in terms of average (in bold), standard deviation and, in parentheses, the coefficient of variation
– | Company/Sample | Material2 | Weave | Number of threads/cm | Thickness (mm) | Weight (g/m2) | Yarn density (tex) | Twist (torsions/m) | Yarn Diameter3 (mm) | Cover factor | Flame speed (cm/s) | ||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
– | – | – | – | Filling | Warp | – | – | Filling | Warp | Filling | Warp | Twist direction | Filling | Warp | – | Filling | Warp |
T1 | Fabric | 100% CO | Twill 3 × 1 | 16 | 23 | 0.504 ± 0.008 (1.67%) | 235.04 ± 0.67 (0.29%) | 59.62 ± 2.68 (4.48%) | 35.30 ± 1.82 (5.16%) | 502.20 ± 34.93 (6.95%) | 705.40 ± 13.38 (1.90%) | Z | 0.289 | 0.222 | 0.74 | 0.979 ± 0.09 (10.50%) | 1.028 ± 0.088 (11.68%) |
T2 | Fabric | 67% PES/33% CO | Plain | 28 | 46 | 0.198 ± 0.004 (2.13%) | 104.20 ± 1.28 (1.23%) | 12.67 ± 0.75 (5.90%) | 37.27 ± 1.89 (5.07%) | 1069.50 ± 56.90 (5.32%) | 989.75 ± 75.74 (7.15%) | S | 0.132 | 0.226 | 1.00 | 2.878 ± 0.138 (4.82%) | 2.920 ± 0.241 (8.25%) |
T31 | Fabric | 100% PES | Twill 2 × 1 | 28 | 46 | 0.382 ± 0.004 (1.10%) | 160.94 ± 1.78 (1.10%) | 16.96 ± 0.24 (1.41%) | 18.16 ± 0.24 (1.34%) | – | – | – | 0.155 | 0.161 | 0.85 | – | – |
P1 | A—Fem. shirt | 100% PES | Twill 2 × 2 | 27 | 29 | 0.260 ± 0.007(2.84%) | 109.52 ± 0.75 (0.69%) | 16.82 ± 0.29 (1.70%) | 18.16 ± 0.24 (1.34%) | – | 891.25 ± 25.33 (2.84%) | – | 0.155 | 0.163 | 0.69 | 2.65 ± 0.2651 (10.00%) | 1.64 ± 0.285 (17.33%) |
P2 | A—Fem. shirt | 100% PES | Plain | 34 | 40 | 0.210 ± 0.007 (3.44%) | 95.09 ± 2.93 (3.08%) | 13.67 ± 0.54 (3.96%) | 9.27 ± 0.43 (4.60%) | – | – | – | 0.139 | 0.115 | 0.72 | 2.891 ± 0.514 (12.06%) | 3.827 ± 0.462 (17.79%) |
P3 | A—Male shirt | 67%PES/33% CO | Twill 2 × 1 | 24 | 39 | 0.390 ± 0.012 (3.06%) | 195.51 ± 1.03 (0.53%) | 30.85 ± 1.50 (4.85%) | 25.43 ± 1.35 (5.31%) | – | – | – | 0.206 | 0.187 | 0.86 | 1.340 ± 0.116 (8.69%) | 1.410 ± 0.070 (5.03%) |
P4 | B—Male shirt | 67% PES/33%CO | Plain | 26 | 35 | 0.220 ± 0.005 (2.16%) | 105.89 ± 1.33 (1.25%) | 15.77 ± 1.08 (6.82%) | 14.76 ± 1.29 (8.74%) | 986.00 ± 62.19 (6.30%) | 857.25 ± 72.19 (8.42%) | Z | 0.147 | 0.142 | 0.69 | 3.022 ± 0.263 (8.72%) | 3.513 ± 0.418 (11.91%) |
P | B—Male shirt | 67% PES/33%CO | Plain | 26 | 35 | 0.230 ± 0.007 (2.90%) | 108.72 ± 2.39 (2.20%) | 15.88 ± 1.27 (8.01%) | 15.19 ± 1.33 (8.73%) | 991.00 ± 45.75 (4.61%) | 910.00 ± 79.90 (8.77%) | Z | 0.148 | 0.144 | 0.70 | 3.698 ± 1.806 (48.83%) | 3.130 ± 0.493 (15.92%) |
P6 | B—Male coat | 55%PES/ 45%WO | Plain | 22 | 22 | 0.360 ± 0.011 (2.93%) | 179.96 ± 1.27 (0.70%) | 36.72 ± 3.43 (9.35%) | 35.88 ± 2.31 (6.43%) | 549.00 ± 47.48 (8.65%) | 556.00 ± 34.78 (6.25%) | S | 0.240 | 0.237 | 0.77 | 0.972 ± 0.114 (11.78%) | 0.979 ± 0.130 (10.52%) |
P7 | B—Male trousers | 50%PES/ 50% WO | Plain | 20 | 22 | 0.450 ± 0.020 (4.509%) | 225.12 ± 5.02 (2.23%) | 36.61 ± 1.48 (4.19%) | 35.31 ± 2.25 (6.36%) | 598.00 ± 45.34 (7.57%) | 562.00 ± 58.55 (10.49%) | S | 0.219 | 0.218 | 0.71 | 0.742 ± 0.140 (18.92%) | 0.934 ± 0.080 (8.64%) |
P8 | B—Male coat | 55%PES/45% WO | Plain | 22 | 22 | 0.350 ± 0.007 (1.90%) | 168.04 ± 1.98 (1.18%) | 36.03 ± 3.38 (9.38%) | 35.68 ± 1.99 (5.58%) | 507.50 ± 40.91 (8.06%) | 548.00 ± 40.50 (7.40%) | S | 0.228 | 0.227 | 0.75 | 0.994 ± 0.121 (12.19%) | 1.030 ± 0.10 (10.29%) |
Taking in account a general analysis, for the evaluated fabrics in the flammability test, the lowest value was 0.742 ± 0.140 cm/s. This result was obtained from ten tested fabric samples of P7 piece (male trousers—Airline company “B”) in the direction of the filling. The fabric composition is a blend of 50% wool and 50% polyester, 225.12 ± 5.02 g/m2 weight and 36.61 ± 1.48 Tex linear yarn density.
At the other extreme, the highest value was 3.698 ± 1.806 cm/s. This result was obtained from ten tested fabric samples of P5 (male shirt—Airline company “B”) in the direction of the filling. The composition is a blend of 67% polyester and 33% cotton, 108.72 ± 2.39 g/m2 weight and 15.88 ± 1.27 Tex linear yarn density.
3.1 Statistical analysis of the variables
In order to evaluate the contribution of the factor studied, the analysis of variance (ANOVA) initially performed, which tests the hypothesis that the averages of two or more populations are equal. The hypothesis test for the comparison between the average flame speeds (response variable) in relation to the explanatory variables (material, weave, thread direction, weight, thickness, linear density and yarn diameter) was ANOVA one way for the verification of each variable influence in the result. However, it was not possible to validate the ANOVA one way with all the factors (explanatory variables) since the residues did not meet the assumptions of normal distribution and variance equality (data not shown).
In this way, it was opted to analyze the relationship of three explanatory variables (“direction,” “material” and “weave”) with the response variable “flame speed,” by grouping the results from the physical tests performed on the fabrics with specific affinities, i.e., similar technical specifications.
The results were grouped by type of weave pattern (plain and twill) and direction (filling and warp) and verified the hypothesis of equality of averages of the response variable flame speed with respect to the material explanatory variable (100% CO, 100% PES, 67% PES/33% CO, 55% PES/45% WO, 50% PES/50% WO).
Analysis of the influence of the fabric material (explanatory variable) on the flame speed (response variable) considering weave pattern (twill and plain) and direction (filling and warp)
Analysis of variance | |||||
---|---|---|---|---|---|
Source | DFa | Adj. SSb | Adj. MSc | F value | p value |
Twill weave, filling direction—G1 | |||||
Material | 2 | 16.6807 | 8.34033 | 271.74 | 0.000 |
Error | 27 | 0.8287 | 0.03069 | ||
Total | 29 | 17.5093 | |||
Twill weave, warp direction—G2 | |||||
Material | 2 | 2.8391 | 1.41957 | 44.04 | 0.000 |
Error | 27 | 0.8703 | 0.03224 | ||
Total | 29 | 3.7095 | |||
Plain weave, filling direction—G3 | |||||
Material | 2 | 61.498 | 30.7492 | 311.79 | 0.000 |
Error | 47 | 4.635 | 0.0986 | ||
Total | 49 | 66.134 | |||
Plain weave, warp direction—G4 | |||||
Material | 2 | 65.776 | 32.880 | 321.12 | 0.000 |
Error | 47 | 4.814 | 0.1024 | ||
Total | 49 | 70.590 |
Interval plot of flame speed vs. material: G1 (twill weave, filling direction), G2 (twill weave, warp direction), G3 (plain weave, filling direction) and G4 (plain weave, warp direction), all of them with 95% confidence interval
In order to validate the ANOVA analysis, it is necessary to check the distribution and homogeneity of the residues. Anderson–Darling normality tests were performed for the residues and returned the following values for groups G1 (p = 0.115) and G2 (p = 0.054). Then, with p values greater than α, the hypothesis of the normal distribution of the residues is accepted. For the values of G3 (p < 0.005) and G4 (p < 0.005), p value was lower than α and the hypothesis of normal distribution of residues was rejected. Additionally, Levene test was applied to confirm the homogeneity of the residue variance and returned the p values for G1 (p = 0.059), G2 (p = 0.003), G3 (p = 0.000) and G4 (p = 0.000).
It was verified that G1 indicates there is sufficient evidence that the variances are equal. In this way, the analysis of variance was validated and the alternative hypothesis was accepted at a significance level α = 0.05 considering that there is difference in the flame speed between the tested materials.
The approach for the groups that did not meet the ANOVA assumptions was the nonparametric Kruskal–Wallis test. This was performed to verify the equality of the averages of the flame speeds of the materials returning p values for G2 (p = 2.62019E − 05), G3 (p = 0.000) and G4 (p = 0.000). In this way, the alternative hypothesis was accepted at a significance level α = 0.05 considering that there is difference in the flame speeds between the group of materials.
Flame speed comparison through multiple comparisons test
Explanatory variables groups | ANOVA | Validation p value | Lesser flame speed | ||||
---|---|---|---|---|---|---|---|
Weave | Twill | Direction | Filling | 0.000 | 0.115 | Material | 100%CO |
Twill | Warp | 0.000 | 0.054 | 100%CO | |||
Plain | Filling | 0.000 | > 0.005 | 50%PES/50%WO | |||
Plain | Warp | 0.000 | > 0.005 | 50%PES/50%WO |
In this way, the results of Hsu’s multiple comparisons test confirm the previously statistical analysis.
Summary of statistical analysis for “flame speed” response variable with respect to the three explanatory variables (“direction,” “material” and “weave”)
Group of explanatory variables | ANOVA | Normality validation | Kruskal–Wallis | Response variable | Result (lower flame speed) | ||||||
---|---|---|---|---|---|---|---|---|---|---|---|
p value | |||||||||||
A.D.1 | Bartlett | Levene | Bonett | ||||||||
Material | 100% CO | Weave | Twill | 0.775 | 0.881 | 0.738 | 0.474 | 0.706 | – | Direction | Equal ones |
100% PES | Twill | 0.000 | 0.573 | 0.832 | 0.688 | 0.811 | – | Warp | |||
100% PES | Plain | 0.000 | 0.077 | 0.753 | 0.742 | 0.823 | – | Filling | |||
67% PES/33% CO | Twill | 0.121 | 0.928 | 0.156 | 0.131 | 0.114 | – | Equal ones | |||
67% PES/33% CO | Plain | 0.285 | 0.105 | 0.548 | 0.165 | 0.723 | – | Equal ones | |||
50% WO/50% PES | Plain | 0.888 | 0.909 | 0.757 | 0.747 | 0.782 | – | Equal ones | |||
Weave | Twill | Direction | Filling | 0.000 | 0.115 | 0.004 | 0.059 | 0.041 | – | Material | 100% CO |
Twill | Warp | 0.000 | 0.054 | 0.000 | 0.003 | 0.002 | 0.000 | 100% CO | |||
Plain | Filling | 0.270 | 0.018 | 0.475 | 0.486 | 0.717 | 0.090 | Equal ones | |||
Plain | Warp | 0.001 | 0.625 | 0.990 | 0.561 | 0.990 | – | 67% PES/33% CO |
The explanatory variable “direction” presents two levels: filling and warp. The behavior of the explanatory variable “direction” on the response variable “flame speed” resulted in statistically equal values for filling and warp for the material groups: “100% CO, twill weave”; “67% PES/33% CO, twill weave”; “67% PES/33% CO, plain weave”; and “50% WO/50% PES, plain weave” (Table 6).
For the groups corresponding to polyester material “100% PES, twill weave,” the value for “flame speed” was lower in the warp direction. For the “100% PES, plain weave,” the lowest velocity was observed in the direction of the filling. This result can be explained by the higher linear density of the filling yarn (13.67 ± 0.54 Tex), slightly smaller weight and higher number of yarns for the “100% PES, plain weave.”
The results for the explanatory variable “material” on the response variable “flame speed” resulted in statistically equal values for filling and warp for: “100% CO, twill weave”; “67% PES/33% CO, twill weave”; “67% PES/33% CO, plain weave”; and “50% WO/50% PES, plain weave.”
After grouping, the explanatory variable “material” presented three levels: 100% CO; 100% PES; and 67% PES/33% CO. For the “plain weave, filling direction” group, the average flame speed was equal for “100% PES” and “67% PES/33% CO” materials.
In Table 6, the results for the “twill weave, filling direction” and “twill weave, warp direction” groups presented different results for “flame speed” averages for “100% CO,” “100% PES” and “67% PES/33% CO” materials. The material with the lowest “flame speed” value was “100% CO” and then “67% PES/33% CO.” Such behavior can be explained by the mixing of cotton fibers with polyester fibers.
The values obtained in the present study, expressed in “flame speed” response variable by explanatory variables (“direction,” “material” and “weave”), cannot be compared directly with another ones in the literature, since they depend on the employed equipments and methodologies as well as the textile material kind and size of specimens, which may vary widely from study to study.
Limiting oxygen index (LOI) data for natural and man-made fibers [8]
Fiber | LOI | Classification |
---|---|---|
Flax | 17.4 | |
Cotton | 18.4 | LOI < 20.95 |
Polyester | 20.0–21.0 | Flammable |
Silk | 23.0 | 21 < LOI < 28 |
Wool | 25.2 | Slow burning |
Thus, taking in account natural fibers, wool presents the best burning resistance with a LOI of 25%. Its flame-retardant activity can be associated with the protein chemical composition of fibers, in which nitrogen is present. This element is characterized as nonflammable and does not support combustion. In this way, there is slow propagation of the flames, i.e., the burning becomes slow. According to the LOI values (Table 7), only taking into account the flammability issue, fibers like silk and wool, from animal origin, can be employed as suitable textile materials for uniforms. Furthermore, protein fibers exhibit excellent moisture absorption, antistatic behavior, comfort in almost all environmental conditions and aesthetic qualities, desired characteristics for the development of uniforms.
4 Conclusion
The explanatory variable “material” was grouped in five levels: (1) 100% CO; (2) 100% PES; (3) 67% PES/33% CO; (4) 50% PES/50% WO; and (5) 55% PES/45% WO. The test of the material “50% PES/50% WO, plain weave and filling direction” presented the lowest flame speed (0.742 ± 0140 cm/s). At the other extreme, the highest value was 3.698 ± 1.806 cm/s for the material “67%PES/33%CO, plain weave and filling direction.”
These values were obtained for the test of a masculine trousers (the smallest value) and masculine shirt (the highest value), being materials already used in the manufacture of some uniforms, accessible to the development of new collections. Such care, i.e., to consider a material with a lower flame speed, means for professionals trained to fight fire on board, take time to remove a burning garment, maintain their physical integrity and continue to fulfill their duties as security agents on board at the end of the event.
- 1.
More closed fabric constructions, with minimum distance between the threads, increasing the cover factor and decreasing the oxygen that circulates in the interstices of the fabric;
- 2.
Construction of natural fiber fabrics from vegetal or animal origin or mixtures with synthetic fibers to add functionality, such as flame-retardant additives. The tests demonstrated that the flame speed response is not proportional to the different proportion of fibers;
- 3.
Changing the direction of the fabric employed in the preparation of the uniforms, since the flame speed is smaller in the direction of the weft. Thus, variations in the modeling of clothing (e.g., straight or bias cut) could be related to some change in the flammability (flame speed) of the uniform. Still a better studied model (besides the aesthetic question) could help to protect the body of the aeronauts of possible accidents involving flammability;
- 4.
To study changes in the weight and torsion of its constituent yarns, since the composition of the fabrics is dependent on these variables, which contribute to the mass of fuel available for burning.
Notes
Acknowledgements
The authors gratefully acknowledge the funding by São Paulo Research Foundation—FAPESP (“Fundação de Amparo à Pesquisa do Estado de São Paulo”) Grant Number 2016/01331-9.
Compliance with ethical standards
Conflict of interest
The authors declare that they have no conflict of interest.
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