| Literature DB >> 31671837 |
Liancong Wang1,2, Benjamin Tawiah3, Yongqian Shi4, Suncheng Cai5, Xiaohui Rao6, Chuan Liu7, Ye Yang8, Fuqiang Yang9, Bin Yu10, Yuntao Liang11, Libi Fu12.
Abstract
The exteEntities:
Keywords: Polyurethane foam; coal combustion; expandable graphite; intumescent flame-retardant; phosphorus
Year: 2019 PMID: 31671837 PMCID: PMC6918278 DOI: 10.3390/polym11111776
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.329
Figure 1(a) Chemical structure of PAPI; (b) Schematic diagram for fabrication of flame-retardant RPUF composites.
Formulations of RPUF and its composites.
| Sample No. | RPUF-1 | RPUF-2 | RPUF-3 | RPUF-4 | RPUF-5 | RPUF-6 | RPUF-7 |
|---|---|---|---|---|---|---|---|
| LY4110 (g) | 100.00 | 77.47 | 77.47 | 77.47 | 77.47 | 77.47 | 77.47 |
| CEPPG (g) | 0.00 | 22.53 | 22.53 | 22.53 | 22.53 | 22.53 | 22.53 |
| A33 (g) | 1.00 | 1.00 | 1.00 | 1.00 | 1.00 | 1.00 | 1.00 |
| LC (g) | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 |
| Water (g) | 2.00 | 2.00 | 2.00 | 2.00 | 2.00 | 2.00 | 2.00 |
| Si–Oil (g) | 2.00 | 2.00 | 2.00 | 2.00 | 2.00 | 2.00 | 2.00 |
| TEOA (g) | 3.00 | 3.00 | 3.00 | 3.00 | 3.00 | 3.00 | 3.00 |
| PM-200 (g) | 151.66 | 149.12 | 149.12 | 149.12 | 149.12 | 149.12 | 149.12 |
| EG (g) | 0.00 | 13.50 | 18.00 | 20.25 | 9.00 | 6.75 | 0.00 |
| MP (g) | 0.00 | 13.50 | 9.00 | 6.75 | 18.00 | 20.25 | 0.00 |
| Fly ash (g) | 0.00 | 7.50 | 7.50 | 7.50 | 7.50 | 7.50 | 0.00 |
| NCO index | 1.10 | 1.10 | 1.10 | 1.10 | 1.10 | 1.10 | 1.10 |
| P wt % | 0.00 | 1.46% | 1.25% | 1.14% | 1.68% | 1.78% | 0.82% |
Figure 2(a–d) TG and (e,f) DTG curves of RPUF and its composites under air condition.
The related thermal data of RPUF and its composites under air condition.
| Sample No. | T−5 (°C) | T−50 (°C) | Tmax (°C) | Residue (wt %) | |
|---|---|---|---|---|---|
| Step 1 | Step 2 | ||||
| RPUF-1 | 249.9 | 384.5 | 297.8 | 585.8 | 1.99 |
| RPUF-2 | 232.2 | 502.9 | 296.7 | 559.3 | 10.34 |
| RPUF-3 | 246.9 | 513.2 | 302.7 | 560.5 | 11.68 |
| RPUF-4 | 252.1 | 519.0 | 305.7 | 566.7 | 11.96 |
| RPUF-5 | 241.2 | 496.8 | 301.6 | 565.5 | 9.97 |
| RPUF-6 | 246.8 | 497.4 | 301.2 | 576.5 | 10.51 |
| RPUF-7 | 253.1 | 484.8 | 309.3 | 584.4 | 2.40 |
Notes: T−5 means the temperature at 5% weight loss; T−50 denotes the temperature at 50% weight loss; Tmax is the temperature at the maximum weight loss rate.
Figure 3Digital photographs of char residues for RPUF and its composites after vertical burning tests.
Figure 4(a) Weight loss and (b) magnified weight loss curves of RPUF and its composites during combustion.
Figure 5(a,c) HRR and (b,d) THR curves of RPUF and its composites.
The cone calorimeter data of RPUF and its composites at a heat flux of 35 kW m−2.
| Sample No. | TTI | PHRR | THR | PSPR | TSR | PCO PR | PCO2 PR | CO TY | CO2 TY |
|---|---|---|---|---|---|---|---|---|---|
| RPUF-1 | 4 | 339 | 25.4 | 0.285 | 5306 | 0.0053 | 0.168 | 0.38 | 8.76 |
| RPUF-2 | 5 | 183 | 22.3 | 0.275 | 4389 | 0.0069 | 0.079 | 0.51 | 8.46 |
| RPUF-3 | 4 | 221 | 24.2 | 0.354 | 6217 | 0.0076 | 0.095 | 1.02 | 9.14 |
| RPUF-4 | 5 | 235 | 24.6 | 0.348 | 5656 | 0.0075 | 0.100 | 1.10 | 9.80 |
| RPUF-5 | 4 | 195 | 24.1 | 0.268 | 4401 | 0.0058 | 0.082 | 0.54 | 9.29 |
| RPUF-6 | 5 | 160 | 16.3 | 0.268 | 3585 | 0.0054 | 0.072 | 0.31 | 6.66 |
| RPUF-7 | 6 | 289 | 23.3 | 0.410 | 5570 | 0.0103 | 0.127 | 0.73 | 8.68 |
Notes: TTI—Time to ignition; PHRR—Peak of heat release rate (HRR); THR—Total heat release; PSPR—Peak of smoke production rate (SPR); PCO PR—Peak of CO production rate; PCO2 PR—Peak of CO2 production rate; CO TY—Total CO yield; CO2 TY—Total CO2 yield.
Figure 6(a,c) SPR and (b,d) TSR curves of RPUF and its composites.
Figure 7(a) CO PR, (b) CO TY, (c) CO2 PR and (d) CO2 TY curves of RPUF and its composites.
Figure 8Digital photos of char residues of (a) RPUF-1, (b,b′) RPUF-2, (c,c′) RPUF-3, (d,d′) RPUF-4, (e,e′) RPUF-5, (f,f′) RPUF-6, and (g,g′) RPUF-7 after cone calorimeter test.
Figure 9SEM images of external char residues of (a,a′) RPUF-1, (b) RPUF-2, (c) RPUF-3, (d) RPUF-4, (e) RPUF-5, (f) RPUF-6, and (g) RPUF-7 after cone calorimeter test.
Figure 10SEM images of internal char residues of (a) RPUF-1, (b,b′) RPUF-2, (c) RPUF-3, (d) RPUF-4, (e) RPUF-5, (f,f′) RPUF-6, and (g) RPUF-7 after cone calorimeter test.
Figure 11Raman spectra of internal char residues for (a) RPUF-1, (b) RPUF-2, (c) RPUF-3, (d) RPUF-4, (e) RPUF-5, (f) RPUF-6, and (g) RPUF-7 after cone calorimeter test.
Figure 12(a) XPS spectra and (b) N/P ratio and O/P ratio curves of the char residues for RPUF-4 and RPUF-6.
Figure 13RTIR spectra of (a) RPUF-1, (b) RPUF-4 and (c) RPUF-6.
Figure 14Schematic illustration for the proposed flame-retardant mechanism of RPUF-6.
Figure 15Retarding experiment of coal combustion.