| Literature DB >> 35566871 |
Raíssa Carvalho Martins1,2, Simone Pereira da Silva Ribeiro1, Michelle Jakeline Cunha Rezende1, Regina Sandra Veiga Nascimento1, Marco Antonio Chaer Nascimento1, Marcos Batistella2, José-Marie Lopez-Cuesta2.
Abstract
The influence of processing intumescent bio-based poly(lactic acid) (PLA) composites by injection and fused filament fabrication (FFF) was evaluated. A raw (ANa) and two acidic-activated (AH2 and AH5) montmorillonites were added to the intumescent formulation, composed by lignin and ammonium polyphosphate, in order to evaluate the influence of the strength and the nature (Brønsted or Lewis) of their acidic sites on the fire behavior of the composites. The thermal stability and the volatile thermal degradation products of the composites were assessed. The injected and 3D-printed composites were submitted to cone calorimeter (CC), limit oxygen index (LOI), and UL-94 flammability tests. A similar tendency was observed for the injected and 3D-printed samples. The high density of strong Lewis sites in AH2 showed to be detrimental to the fire-retarding properties. For the CC test, the addition of the intumescent composite reduced the peak of heat released (pHRR) in approximately 49% when compared to neat PLA, while the composites containing ANa and AH5 presented a reduction of at least 54%. However, the addition of AH2 caused a pHRR reduction of around 47%, close to the one of the composite without clay (49%). In the LOI tests, the composites containing ANa and AH5 achieved the best results: 39% and 35%, respectively, for the injected samples, and 35 and 38% for the 3D-printed samples. For the composite containing AH2 the LOI values were 34% and 32% for injected and 3D-printed samples, respectively. Overall, the best performance in the flammability tests was achieved by the composites containing clays with only weak and moderate strength acidic sites (ANa and AH5).Entities:
Keywords: 3-D printing; PLA; additive manufacturing; flame/fire retardancy; intumescent biocomposite; lignin; montmorillonite acidity
Year: 2022 PMID: 35566871 PMCID: PMC9105856 DOI: 10.3390/polym14091702
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.967
Concentration of Brønsted (Bpy) and Lewis (Lpy) acidic sites, measured by FTIR-Pyr [29].
| Sample | Concentration of Acidic Sites | |||||
|---|---|---|---|---|---|---|
| 150 °C | 250 °C | 350 °C | ||||
| Bpy | Lpy | Bpy | Lpy | Bpy | Lpy | |
| ANa | 50 | 50 | 31 | 69 | - | - |
| AH2 | 52 | 48 | 51 | 49 | 25 | 75 |
| AH5 | 48 | 52 | 55 | 45 | - | - |
Equations used to construct the TGA theoretical curves for each composite.
| Composite | |
|---|---|
| PLA/APP/Lig | |
| PLA/APP/Lig/ANa | |
| PLA/APP/Lig/AH2 | |
| PLA/APP/Lig/AH5 |
Mtheo (T): theoretical mass loss as function of the temperature, T. M (T): experimental mass loss as function of the temperature, T. IF: intumescent formulation, composed by the sum of the ratios of APP and Lig used for each composite, as presented in Section 2.3.1.
Figure 1(a) Mass loss curves and (b) DTG curves for PLA and the composites.
Data for TGA and DTG curves for PLA and the composites produced.
| Sample | Tonset | TDTG peak | Experimental | Theoretical |
|---|---|---|---|---|
| PLA | 324 | 366 | 0 | - |
| PLA/APP/Lig | 318 | 358 | 7.4 | 5.3 |
| PLA/APP/Lig/ANa | 324 | 366 | 12.2 | 6.4 |
| PLA/APP/Lig/AH2 | 323 | 360 | 8.6 | 6.4 |
| PLA/APP/Lig/AH5 | 325 | 357 | 9.5 | 6.4 |
Figure 2Theoretical and experimental mass loss curves for the composites.
Figure 3Gas phase TGA-FTIR spectra of PLA and the composites at (a) 330 °C; (b) 360 °C; (c) 500 °C; (d) 860 °C under air atmosphere.
Assignments for the absorption bands for TGA-FTIR spectra of PLA and the composites.
| Absorption Bands | Assignments | References |
|---|---|---|
| 2359, 2321 and 668 | CO2 | [ |
| 2173 and 2107 | CO | [ |
| 1793 | C=O stretching vibration of lactic acid | [ |
| 1440–1220 | C-O-H bending vibration in alcohols coupled to H-C-H bending vibration | [ |
| 1374 | CH3 bending | [ |
| 1300–1000 | C-O stretching vibrations in alcohols and esters | [ |
| 1033, 1000 and 1060 | C-O bond of methanol | [ |
Cone calorimeter results obtained for PLA and the composites submitted to injection molding and FFF.
| Sample | TTI | pHRR | THR | Mresidue |
|---|---|---|---|---|
| PLA | 36 ± 3 | 498 ± 6 | 95 ± 1 | 0 |
| PLA/APP/Lig | 31 ± 2 | 259 ± 11 | 57 ± 9 | 25 ± 6 |
| PLA/APP/Lig/ANa | 34 ± 4 | 229 ± 6 | 58 ± 1 | 31 ± 2 |
| PLA/APP/Lig/AH2 | 27 ± 6 | 259 ± 20 | 60 ± 7 | 25 ± 4 |
| PLA/APP/Lig/AH5 | 34 ± 2 | 213 ± 18 | 56 ± 8 | 30 ± 3 |
| PLA/APP/Lig 3D | 31 ± 8 | 251 ± 14 | 50 ± 2 | 38 ± 1 |
| PLA/APP/Lig/ANa 3D | 28 ± 3 | 225 ± 13 | 54 ± 3 | 36 ± 4 |
| PLA/APP/Lig/AH2 3D | 31 ± 7 | 268 ± 16 | 55 ± 6 | 21 ± 5 |
| PLA/APP/Lig/AH5 3D | 21 ± 0 | 226 ± 14 | 45 ± 5 | 33 ± 6 |
Figure 4Heat release rate (HRR) curves for PLA and the composites submitted to injection molding.
Figure 5Heat release rate (HRR) curves for the composites submitted to additive manufacturing.
Assignment of the bands for the FTIR spectra of the composites char residues.
| Bands | Assignment | References |
|---|---|---|
| 886 | asymmetric vibration of the P-O bond in a P-O-P chain | [ |
| 997 | symmetrical axial deformation of PO2 and PO3 in complex carbon phosphates | [ |
| 1128–1167 | stretching mode of P-O-C bonds in phosphate-carbon complexes | [ |
| 1401 | CH2 bending absorption | [ |
| 1635 | C=C stretching vibrations | [ |
Figure 6FTIR spectra of the composites char residues.
Melt flow rate for the neat PLA and the composites.
| Sample | MFR |
|---|---|
| PLA | 6 |
| PLA/APP/Lig | 15 |
| PLA/APP/Lig/ANa | 18 |
| PLA/APP/Lig/AH2 | 20 |
| PLA/APP/Lig/AH5 | 23 |
Figure 7Comparison between LOI values for injected (inj) and 3D-printed (3D) samples.
Figure 8SEM images of the inner surface of PLA and the composites at (a) 500× and (b) 50× magnification.
Figure 9Stress X strain curves for (a) PLA; and comparison between injected and 3D-printed samples for (b) PLA/AP/Lig; (c) PLA/AP/Lig/ANa; (d) PLA/AP/Lig/AH2; (e) PLA/AP/Lig/AH5 for five specimens.
Tensile test results for the injected and 3D-printed samples for five specimens per sample.
| Sample | Yield Strength | Yield Strain | Strength at Break | Elongation at Break | Modulus |
|---|---|---|---|---|---|
| (MPa) | (%) | (MPa) | (%) | (MPa) | |
| PLA | 77.1 ± 0.3 | 3.82 ± 0.02 | 72 ± 2 | 4.4 ± 0.2 | 3871 ± 311 |
| PLA/APP/Lig | 44.1 ± 1.4 | 2.66 ± 0.05 | 37 ± 1 | 8.7 ± 0.4 | 4271 ± 282 |
| PLA/APP/Lig/Ana | 44.9 ± 0.5 | 2.57 ± 0.05 | 40 ± 1 | 6.1 ± 1.0 | 4224 ± 205 |
| PLA/APP/Lig/AH2 | 44.7 ± 0.9 | 2.59 ± 0.07 | 40 ± 1 | 5.8 ± 1.2 | 4596 ± 328 |
| PLA/APP/Lig/AH5 | 46.0 ± 0.4 | 2.62 ± 0.04 | 42 ± 1 | 5.8 ± 0.7 | 4637 ± 273 |
| PLA/APP/Lig 3D | 41.3 ± 1.3 | 2.70 ± 0.03 | 35 ± 1 | 13.2 ± 2.8 | 3741 ± 170 |
| PLA/APP/Lig/ANa 3D | 39.8 ± 0.7 | 2.62 ± 0.04 | 35 ± 2 | 8.2 ± 2.6 | 3662 ± 133 |
| PLA/APP/Lig/AH2 3D | 39.1 ± 0.4 | 2.57 ± 0.05 | 35 ± 1 | 6.1 ± 0.8 | 3520 ± 178 |
| PLA/APP/Lig/AH5 3D | 39.0 ± 0.7 | 2.63 ± 0.04 | 34 ± 1 | 8.7 ± 1.9 | 3697 ± 53 |
Figure 10Comparison between injected and 3D-printed samples for (a) tensile strength and (b) Young’s modulus.