| Literature DB >> 31487914 |
Yabo Xiong1, Yang Zou1, Shaoyong Cai1, Huihui Liu2, Shaoyun Huang1, Houbin Li3.
Abstract
Polymer-based far-infrared radiation (FIR) composite materials are receiving increasing attention due to their significant influence on bioactivity. This study reports the processing of FIR composite films based on a polymer matrix and FIR radiation ceramic powders, as well as the characterization of the FIR composites. Field-emission scanning electron microscopy (SEM) and laser particle size analysis were employed to analyze the characteristic of the ceramic powders. The average size, dispersity, and specific surface area of the ceramic powders were 2602 nm, 0.97961, and 0.76 m2/g, respectively. The results show that the FIR ceramic powders used in the composite films had excellent far-infrared emissive performance. Moreover, by using differential scanning calorimetry (DSC) and thermogravimetric analysis (TG), it was indicated that the thermal performance and mechanical properties of the composite films were significantly influenced (p < 0.05) by the addition of the FIR ceramic powders. Specifically, the elongation at break decreased from 333 mm to 201 mm with the increase in FIR ceramic powders. Meanwhile, the contact angle and light transmittance were also changed by the addition of the FIR ceramic powders. Furthermore, the two different processing methods had great influence on the properties of the composite films. Moreover, the composite blown films with 1.5% FIR ceramic powders showed the highest far-infrared emissivity, which was 0.924.Entities:
Keywords: ceramic powders; composites; far-infrared emissivity; polymer
Year: 2019 PMID: 31487914 PMCID: PMC6780572 DOI: 10.3390/polym11091451
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.329
Figure 1Flow chat of method for making eight different types of composite films.
Figure 2SEM images of the far-infrared radiation (FIR) ceramic powders at different magnifications.
Mechanical properties of the composite films along the x-axis and y-axis.
| Elongation at Break (mm) | Young’s Modulus (MPa) | Tensile Stress (MPa) | Strength at Break (N/Tex) | Energy at Break (J) | |
|---|---|---|---|---|---|
| Mean ± SD | Mean ± SD | Mean ± SD | Mean ± SD | Mean ± SD | |
|
| |||||
| 1 | 331.93abc ± 14.99 | 32.74bcd ± 5.04 | 3.74a ± 0.43 | 56.20a ± 6.51 | 11.31c ± 1.49 |
| 2 | 301.12bc ± 14.58 | 33.01bcd ± 2.22 | 3.41ab ± 0.65 | 51.23ab ± 6.84 | 10.07c ± 1.25 |
| 3 | 264.53cd ± 11.94 | 36.40b ± 5.93 | 2.94ab ± 0.46 | 44.18bc ± 6.91 | 8.18c ± 1.58 |
| 4 | 201.08d ± 8.26 | 42.22a ± 3.73 | 2.44bc ± 0.94 | 36.74c ± 4.20 | 6.74c ± 0.77 |
| 5 | 338.46abc ± 12.29 | 2.52gh ± 0.64 | 1.34de ± 0.27 | 20.10d ± 4.07 | 3.25c ± 0.94 |
| 6 | 325.44bc ± 12.61 | 2.44gh ± 0.98 | 1.27de ± 0.21 | 19.17de ± 4.79 | 2.92c ± 1.02 |
| 7 | 305.33bc ± 10.43 | 1.60h ± 0.61 | 1.07de ± 0.22 | 16.08defg ± 3.34 | 2.22c ±0. 63 |
| 8 | 298.44bc ± 10.99 | 2.09gh ± 0.78 | 1.13de ± 0.31 | 17.09def ± 4.72 | 2.42c ±0. 80 |
|
| |||||
| 1 | 311.12bc ± 15.14 | 30.71cde ± 1.41 | 3.18ab ± 0.61 | 9.85defg ± 1.99 | 47.71a ± 3.17 |
| 2 | 215.44d ± 15.48 | 26.49e ± 2.45 | 1.82cd ± 0.25 | 5.56g ± 0.82 | 27.34b ± 1.32 |
| 3 | 320.34bc ± 12.62 | 29.04de ± 2.34 | 3.15ab ± 0.35 | 9.60defg ± 0.96 | 47.34a ± 4.17 |
| 4 | 323.88bc ± 13.22 | 35.57bc ± 2.54 | 3.78a ± 0.84 | 11.93defg ± 1.99 | 56.77a ± 4.65 |
| 5 | 405.83a ± 10.84 | 9.61f ± 1.61 | 0.89de ± 0.12 | 10.62defg ± 0.98 | 2.21c ± 0.26 |
| 6 | 302.26bc ± 10.76 | 6.69fg ± 0.92 | 0.42e ± 0.08 | 6.25fg ±0.33 | 1.50c ± 0.14 |
| 7 | 331.87abc ± 11.21 | 7.65f ± 0.61 | 0.67e ± 0.06 | 8.65efg ±0.61 | 1.98c ± 0.12 |
| 8 | 373.53ab ± 11.89 | 8.38f ± 0.91 | 0.72e ± 0.07 | 9.25defg ± 0.82 | 2.38c ± 0.22 |
Superscript letters refer to a significant difference among different processed films.
Figure 3SEM images of the composite films 1, 5, 6, and 8 at different magnifications.
Differential scanning calorimetry (DSC) and thermogravimetric (TG) analysis of eight different specimens.
| Composite Films | DSC | TG | |||||
|---|---|---|---|---|---|---|---|
| Glass Transition (°C) | Crystallinity (%) | Onset Temperature (°C) | Inflection Temperature (°C) | End Temperature (°C) | Mass Change (%) | Residual Mass (%) | |
| 1 | 111.43 | 25.68 | 465.5 | 488.8 | 493.1 | 98.77 | 0.9 |
| 2 | 102.96 | 20.32 | 461.0 | 482.7 | 492.8 | 98.59 | 0.91 |
| 3 | 102.85 | 19.73 | 462.5 | 479.3 | 490.2 | 98.68 | 1.11 |
| 4 | 102.45 | 16.79 | 462.1 | 482.3 | 492.1 | 97.91 | 1.37 |
| 5 | 112.31 | 26.09 | 461.9 | 474.7 | 492.0 | 99.13 | 0.37 |
| 6 | 101.99 | 22.85 | 461.5 | 476.0 | 492.4 | 98.8 | 0.79 |
| 7 | 101.57 | 21.01 | 464.3 | 481.6 | 491.6 | 98.4 | 1.34 |
| 8 | 101.56 | 19.13 | 464.0 | 480.8 | 491.9 | 97.98 | 1.24 |
Figure 4Water contact angle of eight composite films.
Far-infrared emissivity, light transmittance, and moisture permeability of the composite films.
| Composite Films | Far-Infrared Emissivity (ε) | Light Transmittance (%) | Moisture Permeability (g/m2·day) |
|---|---|---|---|
| 1 | 0.512 | 14.7 | 0.27 |
| 2 | 0.861 | 13.1 | 0.32 |
| 3 | 0.892 | 12.4 | 0.4 |
| 4 | 0.921 | 10.9 | 0.45 |
| 5 | 0.508 | 71.3 | 1.73 |
| 6 | 0.866 | 67.9 | 2.17 |
| 7 | 0.89 | 67.6 | 3.27 |
| 8 | 0.924 | 57.6 | 3.38 |