| Literature DB >> 29324716 |
Hongda Chen1, Jihui Wang2,3, Aiqing Ni4, Anxin Ding5, Xia Han6, Ziheng Sun7.
Abstract
In order to improve the efficiency of intumescent class="Disease">flame retardants (IFRs), a novel macromolecular charring agent namedEntities:
Keywords: flame retardancy mechanism; intumescent flame retardant; mechanical properties; polypropylene; thermal properties
Year: 2018 PMID: 29324716 PMCID: PMC5793609 DOI: 10.3390/ma11010111
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Figure 1The synthesis route of TAT and PETAT (poly(ethanediamine-1,3,5-triazine-p-4-amino-2,2,6,6-tetramethylpiperidine)).
Formulations for flame retardancy PP (Polypropylene) composites.
| Samples | PP (wt %) | APP (wt %) | PETAT (wt %) | PER (wt %) |
|---|---|---|---|---|
| PP1 | 100 | 0 | 0 | 0 |
| PP2 | 75 | 25 | 0 | 0 |
| PP3 | 75 | 18.7 | 6.3 | 0 |
| PP4 | 75 | 16.6 | 8.4 | 0 |
| PP5 | 75 | 12.5 | 12.5 | 0 |
| PP6 | 75 | 0 | 25 | 0 |
| PP7 | 75 | 18.7 | 0 | 6.3 |
Figure 2FTIR spectra of TAT and PETAT.
Figure 31H NMR spectra of (a) DTAT (2,4-dichloro-1,3,5-triazine-p-4-amino-2,2,6,6-tetramethylpiperidine) and (b) PETAT.
Figure 4Tensile and flexural strength of PP and its composites.
Figure 5(a) TGA and (b) DTG (thermogravimetric-derivative thermogravimetric) curves of APP (Ammonium polyphosphate), PETAT, IFR (intumescent flame retardants), and IFR calculation under N2.
TGA and DTG data of APP, PETAT, IFR, and IFR calculation under N2.
| Samples | ||||
|---|---|---|---|---|
| APP | 316.3 | 603.5 | 591.6 | 32.5 |
| PETAT | 331.6 | 463.4 | 375.3 | 33.9 |
| 307.2 | 662.7 | 389.8 | 48.2 | |
| IFR Calculation | 321.9 | 592.4 | 590.1 | 32.9 |
IFR is composed by APP and PETAT, (APP/PETAT, weight ratio is 2:1). . Ti and T50% are the temperature at 5 wt % and 50 wt % mass loss, respectively. Tmax is the maximum mass loss rate temperature. Char residue at 700 °C.
Figure 6TGA (a) and DTG (b) curves of PP and PP composites under N2.
TGA and DTG data of PP and PP composites under N2.
| Samples | |||||
|---|---|---|---|---|---|
| PP1 | 390.0 | 427.6 | 430 | 29.5 | 0.9 |
| PP2 | 394.2 | 457.9 | 459.9 | 21.9 | 13.0 |
| PP4 | 328.8 | 501.1 | 437.3 | 4.9 | 23.0 |
| PP6 | 329.8 | 444.0 | 451.2 | 21.0 | 6.3 |
| PP7 | 317.6 | 459.1 | 462.8 | 25.8 | 11.8 |
Ti and T50% are the temperature at 5 wt % and 50 wt % mass loss, respectively. Tmax is the maximum mass loss rate temperature. Rmax is the maximum decomposition rate. Char residue at 700 °C.
Figure 73D TG-FTIR spectra pyrolysis products for PETAT/APP (weight ratio is 2:1) and corresponding FTIR spectra at different temperature.
Before and after soaking LOI (limiting oxygen index) and UL-94 vertical test of PP and pp composites.
| Samples | LOI (%) | UL-94 Rating | Dropping | After Soaking LOI (%) |
|---|---|---|---|---|
| PP1 | 16.4 | No rating | Yes | 16.4 |
| PP2 | 21.2 | No rating | Yes | 19.1 |
| PP3 | 28.1 | No rating | Yes | 25.6 |
| PP4 | 30.3 | V-0 | No | 27.8 |
| PP5 | 28.4 | V-1 | No | 26.6 |
| PP6 | 17.8 | No rating | Yes | 16.9 |
| PP7 | 24.7 | V-1 | No | 19.4 |
Figure 8Photos of char residues after LOI test for PP and PP composites.
Figure 9Heat release rate (a) and total heat release (b) curves of PP and PP composites.
Characteristic parameters of the CCT (cone calorimetric test) for PP and PP composites.
| Samples | TTI (s) | TPHRR (s) | PHRR (kW/m2) | THR (MJ/m2) | FPI (s·m2/kW) | Residue (wt %) |
|---|---|---|---|---|---|---|
| PP1 | 41 | 174 | 840.3 | 115.7 | 0.0488 | 1.4 |
| PP4 | 28 | 250 | 227.9 | 62.0 | 0.1229 | 43.5 |
| PP6 | 30 | 164 | 684.0 | 106.7 | 0.0439 | 5.8 |
| PP7 | 32 | 218 | 354.7 | 82.0 | 0.0902 | 29.8 |
Figure 10Photos, SEM (scanning electron microscopy) images and chemical compositions of residue char for PP4 and PP7.
Figure 11FTIR spectra of PP4 and PP7 residue char.
Figure 12Flame retardant mechanism of PETAT/APP IFR system in PP matrix.