| Literature DB >> 34069151 |
Weimiao Lu1, Jiewang Ye1, Lianghai Zhu1, Zhenfu Jin1, Yuji Matsumoto2.
Abstract
Intumescent flame retardants (IFR) have been widely used to improve flame retardancy of rigid polyurethane (RPU) foams and the most commonly used char forming agent is pentaerythritol (PER). Lignosulfonate (LS) is a natural macromolecule with substantial aromatic structures and abundant hydroxyl groups, and carbon content higher than PER. The flame retardancy and its mechanism of LS as char forming agent instead of PER in IFR formulation were investigated by scanning electron microscopy, thermogravimetric analysis, limiting oxygen index testing and cone calorimeter test. The results showed LS as a char forming agent did not increase the density of RPU/LS foams. LOI value and char residue of RPU/LS foam were higher than RPU/PER and the mass loss of RPU/LS foam decreased 18%, suggesting enhanced thermal stability. CCT results showed LS as a char forming agent in IFR formulation effectively enhanced the flame retardancy of RPU foams with respect to PER. The flame retardancy mechanism showed RPU/LS foam presented a continuous and relatively compact char layer, acting as the effect of the flame retardant and heat insulation between gaseous and condensed phases. The efficiency of different LS ratio in IFR formulation as char forming agent was different, and the best flame retardancy and thermal stability was obtained at RPU/LS1.Entities:
Keywords: char forming agent; flame retardancy mechanism; intumescent flame retardant; lignosulfonate
Year: 2021 PMID: 34069151 PMCID: PMC8155981 DOI: 10.3390/polym13101585
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.329
The formulation of IFR for RPU foams.
| Sample | APP (g) | MEL (g) | PER (g) | LS (g) | Density (kg/m3) |
|---|---|---|---|---|---|
| RPU/PER | 10.2 | 3.4 | 3.4 | - | 58.0 |
| RPU/PER/LS | 10.2 | 3.4 | 1.7 | 1.7 | 57.6 |
| RPU/LS | 10.2 | 3.4 | - | 3.4 | 57.5 |
The ratio of LS as a char forming agent in IFR formulations for RPU foams.
| Sample | APP (g) | MEL (g) | LS (g) | APP:MEL:LS Ratio | Density (kg/m3) |
|---|---|---|---|---|---|
| RPU/LS0.5 | 10.2 | 3.4 | 1.7 | 3:1:0.5 | 57.3 |
| RPU/LS1 | 10.2 | 3.4 | 3.4 | 3:1:1 | 57.5 |
| RPU/LS1.5 | 10.2 | 3.4 | 5.1 | 3:1:1.5 | 57.6 |
| RPU/LS2 | 10.2 | 3.4 | 6.8 | 3:1:2 | 57.8 |
| RPU/LS3 | 10.2 | 3.4 | 10.2 | 3:1:3 | 58.0 |
| RPU/LS4 | 10.2 | 3.4 | 13.6 | 3:1:4 | 58.2 |
Figure 1The effect of LS as a char forming agent on LOI.
Figure 2HRR curves of RPU/PER, RPU/PER/LS, and RPU/LS foams.
Effect of LS as a char forming agent on heat transfer between the gaseous and condensed phases.
| Sample | HRR | pHRR | tpHRR | THR | FGRI |
|---|---|---|---|---|---|
| RPU/PER | 46.1 | 215.1 | 104 | 28.4 | 2.1 |
| RPU/PER/LS | 45.7 | 202.2 | 110 | 27.8 | 1.8 |
| RPU/LS | 45.0 | 191.4 | 110 | 27.4 | 1.7 |
HRR: heat release rate; pHRR: peak of heat release rate; tpHRR: time to peak heat release rate; THR: total heat release; FGRI: fire growth rate index.
Effect of LS as a char forming agent on gas transfer between the gaseous and condensed phases.
| Sample | TSR | SEA | EHC | pCO | mCOY | mCO2Y |
|---|---|---|---|---|---|---|
| RPU/PER | 717.4 | 430.2 | 18.1 | 0.14 | 0.55 | 2.05 |
| RPU/PER/LS | 765.9 | 444.3 | 16.7 | 0.18 | 0.49 | 1.95 |
| RPU/LS | 700.4 | 343.8 | 17.0 | 0.03 | 0.68 | 2.03 |
TSR: total smoke release; SEA: specific extinction area; EHC: effective heat combustion; pCO: peak of carbon monoxide; mCOY: mean carbon monoxide yield; mCO2Y: mean carbon dioxide yield.
Effect of LS as a char forming agent on mass loss.
| Sample | CCT Results | TG Results | |||||||
|---|---|---|---|---|---|---|---|---|---|
| PMLR (g/s) | SMLR | tPMLR | Char600 s (g) | Tonset2 | Tmax2
| Tfinal2
| Mass Loss | Char800 °C (wt%) | |
| RPU/PER | 0.48 | 11.1 | 9 | 2.1 | 273 | 311 | 361 | 61.9 | 29.9 |
| RPU/PER/LS | 0.30 | 10.3 | 6 | 2.1 | 274 | 309 | 364 | 63.0 | 29.5 |
| RPU/LS | 0.26 | 9.6 | 35 | 2.6 | 277 | 311 | 356 | 50.7 | 34.3 |
PMLR: peak of mass loss rate; SMLR: specific mass loss rate; tPMLR: time to peak mass loss rate; Char600 s: char residue at 600 s after cone calorimeter test; Tonset2: initial temperature; Tmax2: peak temperature; Tfinal2: stop temperature of second mass loss step; Char800 °C: char residue at 800 °C from TG analysis.
Figure 3TG (a) and DTG (b) curves of RPU/PER, RPU/PER/LS, and RPU/LS foams under nitrogen atmosphere.
Figure 4Digital photos (a,b) and SEM micrograph (c,d) of char residues for RPU/PER and RPU/LS foams.
Figure 5Flame retardant mechanism of PER/APP/MEL (a) and LS/APP/MEL (b) IFR formulation in RPU foam.
Figure 6LOI (a) and THR (b) curves of RPU/LS foams.
Effects of LS ratios as a char forming agent for the flame retardancy of RPU/LS foams.
| Sample | THR | HRR | EHC | PMLR | tPCO2 |
|---|---|---|---|---|---|
| RPU/LS0.5 | 39.3 | 65.9 | 17.4 | 0.35 | 118 |
| RPU/LS1 | 27.4 | 46.0 | 17.0 | 0.26 | 596 |
| RPU/LS1.5 | 32.6 | 54.6 | 16.9 | 0.44 | 563 |
| RPU/LS2 | 32.5 | 54.5 | 19.3 | 0.61 | 205 |
| RPU/LS3 | 28.2 | 47.4 | 18.8 | 0.29 | 366 |
| RPU/LS4 | 39.6 | 66.5 | 18.5 | 0.29 | 565 |
THR: total heat release; HRR: heat release rate; EHC: effective heat combustion; PMLR: peak of mass loss rate; tPCO2: time to peak carbon dioxide.
Figure 7TG (a) and DTG (b) curves of RPU/LS foams under nitrogen atmosphere.
TG data of LS ratios as a char forming agent on the thermal stability of RPU/LS foams.
| Sample | Tmax1 | Mass Loss1 | Tmax2 | Mass Loss2 | Char800
°C |
|---|---|---|---|---|---|
| RPU/LS0.5 | 181 | 2.4 | 302 | 59.3 | 29.6 |
| RPU/LS1 | 174 | 2.4 | 311 | 50.6 | 34.3 |
| RPU/LS1.5 | 169 | 2.5 | 307 | 58.3 | 31.2 |
| RPU/LS2 | 173 | 2.7 | 307 | 59.8 | 32.3 |
| RPU/LS3 | 173 | 2.9 | 304 | 57.5 | 31.4 |
| RPU/LS4 | 183 | 2.4 | 308 | 55.4 | 32.8 |
Tmax1 and Tmax2: maximum degradation temperature in the first degradation step and the second degradation step; Mass loss1 and Mass loss2: the mass loss in the first step and second step; Char800 °C: char residue at 800 °C from TG analysis.