| Literature DB >> 35054714 |
Yajun Chen1,2,3, Xingde Wu1,2,3, Mengqi Li1,2,3, Lijun Qian1,2,3, Hongfu Zhou1.
Abstract
The addition of intumescent flame retardant to PLA can greatly improve the flame retardancy of the material and inhibit the dripping, but the major drawback is the adverse impact of the mechanical properties of the material. In this study, we found that the flame retardant and mechanical properties of the materials can be improved simultaneously by constructing a cross-linked structure. Firstly, a cross-linking flame-retardant PLA structure was designed by adding 0.9 wt% DCP and 0.3 wt% TAIC. After that, different characterization methods including torque, melt flow rate, molecular weight and gel content were used to clarify the formation of crosslinking structures. Results showed that the torque of 0.9DCP/0.3TAIC/FRPLA increased by 307% and the melt flow rate decreased by 77.8%. The gel content of 0.9DCP/0.3TAIC/FRPLA was 30.8%, indicating the formation of cross-linked structures. Then, the mechanical properties and flame retardant performance were studied. Results showed that, compared with FRPLA, the tensile strength, elongation at break and impact strength of 0.9DCP/0.3TAIC/FRPLA increased by 34.8%, 82.6% and 42.9%, respectively. The flame retardancy test results showed that 0.9DCP/0.3TAIC/FRPLA had a very high LOI (the limiting oxygen index) value of 39.2% and passed the UL94 V-0 level without dripping. Finally, the crosslinking reaction mechanism, flame retardant mechanism and the reasons for the improvement of mechanical properties were studied and described.Entities:
Keywords: crosslinked structures; crystallization behavior; flame retardant property; mechanical property; poly(lactic acid)
Year: 2022 PMID: 35054714 PMCID: PMC8782028 DOI: 10.3390/polym14020308
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.329
Formulations of PLA composites.
| Number | Sample | PLA (g) | Triazine | APP | DCP | TAIC | TAIC | |||
|---|---|---|---|---|---|---|---|---|---|---|
| (g) | (wt%) | (g) | (g) | (g) | (wt%) | (g) | (wt%) | |||
| 1 | PLA | 200 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
| 2 | FRPLA | 160 | 8 | 4 | 32 | 0 | 0 | 0 | 0 | 0 |
| 3 | 0.9DCP/FRPLA | 160 | 8 | 4 | 32 | 0 | 0 | 0.9 | 0 | 0 |
| 4 | 0.3TAIC/FRPLA | 160 | 8 | 4 | 32 | 0.48 | 0.48 | 0 | 0.48 | 0.3 |
| 5 | 0.9DCP/0.3TAIC/FRPLA | 160 | 8 | 4 | 32 | 0.48 | 0.48 | 0.9 | 0.48 | 0.3 |
Figure 1The flow chart of the processing process.
Figure 2Characterization of crosslinked structures: (a) Torque curve; (b) gel content; (c) molecular weight; (d) MFR.
Figure 3SEM photos of the impact fracture surface: (a) PLA; (b) FRPLA; (c) 0.9DCP/FRPLA; (d) 0.3TAIC/FRPLA; (e) 0.9DCP/0.3TAIC/FRPLA.
Figure 4The mechanical properties of pure PLA and PLA composites.
Figure 5The flame retardant properties of PLA and PLA composites: (A) LOI and UL 94 vertical burning test; (B) digital image of composite UL94 sample (a: FRPLA, b: 0.9DCP/FRPLA, c: 0.3TAIC/FRPLA, d: 0.9DCP/0.3TAIC/FRPLA); (C) HRR curves; (D) THR curves; (E) TSR curves; (F) mass loss curve.
Combustion parameters of pure PLA and PLA composites during cone calorimeter test.
| Sample | TTI | pk-HRR | av-HRR | THR | av-MLR | Final Mass | TSR |
|---|---|---|---|---|---|---|---|
| PLA | 39 | 494 | 249 | 87 | 0.111 | 0.2 | 30 |
| FRPLA | 28 | 119 | 43 | 42 | 0.034 | 22.6 | 563 |
| 0.9DCP/FRPLA | 26 | 111 | 64 | 37 | 0.040 | 44.9 | 241 |
| 0.3TAIC/FRPLA | 27 | 97 | 57 | 38 | 0.033 | 45.2 | 244 |
| 0.9DCP/0.3TAIC/FRPLA | 30 | 108 | 57 | 38 | 0.036 | 44.8 | 140 |
Figure 6Residual char digital photos and SEM photos (400×) of the residual char after cone calorimeter test: (a1–a3) FRPLA; (b1–b3) 0.9DCP/FRPLA; (c1–c3) 0.3TAIC/FRPLA; (d1–d3) 0.9DCP/0.3TAIC/FRPLA.
Figure 7The curves of thermal performance: (a) TG curves; (b) DTG curves; (c) the crystallization curves of the heating process; (d) the crystallization curves of the cooling process.
The data of TG and DTG for PLA and PLA composites under N2 atmosphere.
| Samples | N2 | ||
|---|---|---|---|
| Residual at 600 °C (wt%) | |||
| PLA | 353 | 380 | 2.1 |
| FRPLA | 337 | 374 | 14.2 |
| 0.9DCP/FRPLA | 336 | 373 | 15.8 |
| 0.3TAIC/FRPLA | 337 | 374 | 16.1 |
| 0.9DCP/0.3TAIC/FRPLA | 337 | 374 | 15.7 |
The DSC data of PLA and flame-retardant PLA composites.
| Samples | ||||||
|---|---|---|---|---|---|---|
| PLA | 60.3 | 159.4 | 33.1 | 31.1 | 2.1 | 119.2 |
| FRPLA | 60.6 | 159.1 | 26.1 | 23.4 | 3.6 | 114.9 |
| 0.9DCP/FRPLA | 60.6 | 159.8 | 21.5 | 16.5 | 6.6 | 104.6 |
| 0.3TAIC/FRPLA | 60.3 | 163.3 | 24.9 | 21.3 | 4.9 | 106.9 |
| 0.9DCP/0.3TAIC/FRPLA | 59.6 | 153.3 | 23.6 | 6.7 | 22.6 | 116.6 |
Figure 8The formation of cross-linked structure in flame-retardant PLA composite under the action of DCP and TAIC.