| Literature DB >> 30135388 |
Yan Song1,2, Xu Zong3, Nan Wang4, Ning Yan5, Xueying Shan6, Jinchun Li7,8.
Abstract
Lignin can be a candidate as a charring agent applied in halogen-free flame retardant polymers, and incorporation of silicon and nitrogen elements in lignin can benefit to enhancing its thermal stability and charring ability. In the present work, wheat straw alkali lignin (Lig) was modified to incorporate silicon and nitrogen elements by γ-divinyl-3-aminopropyltriethoxysilane, and the modified lignin (CLig) was combined with ammonium polyphosphate (APP) as intumescent flame retardant to be applied in poly(Lactic acid) (PLA). The flame retardancy, combustion behavior and thermal stability of PLA composites were studied by the limited oxygen index (LOI), vertical burning testing (UL-94), cone calorimetry testing (CCT) and thermogravimetric analysis (TGA), respectively. The results showed a significant synergistic effect between CLig and APP in flame retarded PLA (PLA/APP/CLig) occured, and the PLA/APP/CLig had better flame retardancy. CCT data analysis revealed that CLig and APP largely reduced the peak heat release rate (PHRR) and total heat release rate (THR) of PLA, indicating their effectiveness in decreasing the combustion of PLA. TGA results exhibited that APP and CLig improved the thermal stability of PLA at high temperature. The analysis of morphology and structure of residual char indicated that a continuous, compact and intumescent char layer on the material surface formed during firing, and had higher graphitization degree. Mechanical properties data showed that PLA/APP/CLig had higher tensile strength as well as elongation at break.Entities:
Keywords: combustion behavior; poly(lactic acid); silicon and nitrogen elements; thermal stability; wheat straw soda lignin
Year: 2018 PMID: 30135388 PMCID: PMC6164032 DOI: 10.3390/ma11091505
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Scheme 1Schematic of the reaction between B201 and lignin.
Composition of the samples and the testing results of neat PLA and PLA composites’ LOI and UL-94 vertical burning.
| Sample | Component (wt%) | LOI (%) | UL-94 | |||||
|---|---|---|---|---|---|---|---|---|
| PLA | APP | CLig | Lignin | Ranking | Ignition of the Cotton | t1/t2 (s) | ||
| PLA-1 | 100 | - | - | - | 21 | NR | Yes | >30 |
| PLA-2 | 77 | 23 | - | - | 29 | V-2 | Yes | 11/0 |
| PLA-3 | 77 | - | 23 | - | 22 | NR | Yes | >30 |
| PLA-4 | 77 | 15.33 | 7.67 | - | 27 | V-1 | No | 9/2 |
| PLA-5 | 77 | 17.25 | 5.75 | - | 29 | V0 | No | 1/0 |
| PLA-6 | 77 | 18.40 | 4.60 | - | 30.5 | V0 | No | 0/1 |
| PLA-7 | 77 | 19.17 | 3.83 | - | 27.5 | V2 | Yes | 12/0 |
| PLA-8 | 77 | 18.40 | - | 4.60 | 25 | V0 | No | 2/3 |
Figure 1FTIR spectra of Lig (a) and CLig (b).
Element contents of Lig and CLig obtained by XRF.
| Elements | O/% | Si/% | S/% | Fe/% | Ca/% | Cu/% | |
|---|---|---|---|---|---|---|---|
| Samples | |||||||
| Lig | 91.63 | 2.58 | 4.19 | 1.28 | 0.18 | 0.14 | |
| CLig | 79.85 | 14.33 | 4.07 | 1.33 | 0.22 | 0.20 | |
Figure 2TG curves (a) and DTG curves (b) of Lig and CLig under air atmosphere.
Related thermal degradation parameters of Lig and CLig under air atmosphere.
| Samples | T5% (°C) | T50% (°C) | Tmax (%) | Residual (%) 800 °C | |
|---|---|---|---|---|---|
| Tmax1 | Tmax2 | ||||
| Lig | 214 | 409 | 271 | 417 | 0 |
| CLig | 220 | 435 | 261 | 452 | 5 |
Figure 3Effect of CLig content on flame retardancy of PLA/IFR composites with a total loading of 23 wt%.
Figure 4(a) HRR curves; (b) THR curves; (c) MLR curves of PLA and PLA composites.
Cone calorimeter testing data of PLA and PLA composites.
| Sample | TTI (s) | PHRR (kW/m2) | Av-HRR (kW/m2) | TTPH (s) | THR (MJ/m2) | Residual Mass (%) |
|---|---|---|---|---|---|---|
| PLA-1 | 64 | 428.4 | 184.6 | 185 | 69.2 | 0 |
| PLA-6 | 48 | 205.3 | 68.7 | 65 | 34.3 | 40.6 |
| PLA-8 | 58 | 299.4 | 96.7 | 110 | 51.3 | 19.5 |
Figure 5TG curves of PLA, APP/Clig, PLA/IFR composites and PLA-6(Calculation) under N2.
Thermal degradation parameters data of PLA and PLA composites under N2.
| Samples | T5% (°C) | Tmax (°C) | Residue (%) | |||||
|---|---|---|---|---|---|---|---|---|
| 600 °C | 700 °C | 800 °C | ||||||
| Exp. | Cal. | Exp. | Cal. | Exp. | Cal. | |||
| APP | 302 | 593 | 33.2 | - | 20.4 | - | 16.3 | - |
| CLig | 199 | 356 | 41.5 | - | 39.3 | - | 38.6 | - |
| APP/CLig(4:1) | 259 | 593 | 40.7 | 34.7 | 26.9 | 24.1 | 22.6 | 20.7 |
| PLA-1 | 327 | 366 | 0.5 | - | 0.5 | - | 0.5 | - |
| PLA-6 | 320 | 375 | 15.2 | 10.0 | 14.6 | 6.6 | 13.7 | 5.6 |
| PLA-8 | 323 | 365 | 13.6 | - | 13.0 | - | 12.1 | - |
Figure 6SEM micrographs of residues of PLA-8 (a ×100, b ×500, c ×1000) and PLA-6 (d ×100, e ×500, f ×1000) after cone calorimeter testing.
Figure 7Raman spectroscopy analysis curves of char residue for PLA composites: (a) PLA-6 and (b) PLA-8.
Mechanical properties of PLA and PLA/IFR composites.
| Sample | Tensile Strength (MPa) | Elongation at Break (%) |
|---|---|---|
| PLA1 | 61.1 ± 3.1 | 5.8 ± 0.2 |
| PLA6 | 41.2 ± 2.1 | 6.6 ± 0.3 |
| PLA8 | 29.5 ± 1.5 | 5.2 ± 0.2 |