| Literature DB >> 32260248 |
Huazheng Sai1,2,3, Jing Zhang1,2,3, Zhiqiang Jin1,2,3, Rui Fu1,2,3, Meijuan Wang1,2,3, Yutong Wang1,2,3, Yaxiong Wang1,2,3, Litong Ma1,2,3.
Abstract
Silica aerogels can be strengthened by forming a nanoscale interpenetrating network (IPN) comprising a silica gel skeleton and a cellulose nanofiber network. Previous studies have demonstrated the effectiveness of this method for improving the mechanical properties and drying of aerogels. However, the preparation process is generally tedious and time-consuming. This study aims to streamline the preparation process of these composite aerogels. Silica alcosols were directly diffused into cellulose wet gels with loose, web-like microstructures, and an IPN structure was gradually formed by regulating the gelation rate. Supercritical CO2 drying followed to obtain composite aerogels. The mechanical properties were further enhanced by a simple secondary regulation process that increased the quantity of bacterial cellulose (BC) nanofibers per unit volume of the matrix. This led to the production of aerogels with excellent bendability and a high tensile strength. A maximum breaking stress and tensile modulus of 3.06 MPa and 46.07 MPa, respectively, were achieved. This method can be implemented to produce robust and bendable silica-based composite aerogels (CAs).Entities:
Keywords: bacterial cellulose; bendable; interpenetrating network; mechanical properties; nanocomposites; silica aerogels
Year: 2020 PMID: 32260248 PMCID: PMC7240684 DOI: 10.3390/polym12040807
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.329
Figure 1Schematic of the preparation process for composite aerogels with a nanoscale interpenetrating network (IPN) structure via three different routes.
Physical properties of the dried BC matrix (BM) and composite aerogels (CAs) with varying precursor concentrations.
| Materials | SiO2 in Aerogels [% | Bulk Density [g cm−3] | Pore Volume (cm3 g−1) | D b [nm] | P c [%] | Thermal Conductivity [W m−1 K−1] | |
|---|---|---|---|---|---|---|---|
| BM | 0 | 0.007 | 113 | 0.35 | 11.4 | 99.5 | 0.029 |
| CA-1 | 78 | 0.032 | 440 | 1.59 | 14.7 | 98.4 | 0.031 |
| CA-2 | 88 | 0.060 | 641 | 1.50 | 9.2 | 97.1 | 0.034 |
| CA-3 | 91 | 0.082 | 648 | 1.56 | 9.5 | 96.0 | 0.028 |
| CA-4 | 93 | 0.104 | 667 | 2.16 | 13.7 | 94.9 | 0.030 |
| CA-4/6 | 89 | 0.108 | 661 | 2.08 | 13.2 | 94.7 | 0.031 |
| CA-4/3 | 81 | 0.119 | 647 | 1.96 | 13.3 | 94.1 | 0.033 |
a BET specific surface area determined using nitrogen sorption. b Mean pore diameter determined using nitrogen adsorption branch and Barrett–Joyner–Halenda (BJH). c The porosity includes both mesopores and all void space in CAs.
Figure 2(a) The effect of soaking time in the silica alcosols (SA-1, SA-2, SA-3, and SA-4 respectively) on the weight of the dried BC wet gel sample, and (b) the microstructure of BC matrix.
Figure 3SEM images of (a) CA-1, (b) CA-2, (c) CA-3, (d) CA-4, (e) CA-4/6, and (f) CA-4/3, where the scale bar represents 1 μm.
Figure 4The sol-gel process of silica alcosols in BC matrix before (top) and after (bottom) squeezing some of the silica sols from the matrix respectively. (a) and (d): BC matrix with silica alcosols; (b) and (e): BC-silica composite gels; (c) and (f): composite aerogels. Photographs show the CA-4 (top) and CA-4/3 (bottom) samples.
Figure 5(a) Nitrogen adsorption-desorption isotherms and (b) BJH pore-size distribution of the BM, CA-1, CA-2, CA-3, and CA-4 samples. It is necessary to illustrate that the curves have been shifted along the Y-axis to show these curves clearly.
Figure 6(a,b) Stress-strain curves of three-point bending tests on all the samples; (c) photographs of a three-point bending test on CA-4; (d) stress-strain curves of CA-4 under repeated three-point bending tests; and (e,f) stress-strain curves of tensile tests on all the samples.
Flexural and tensile mechanical properties of the CAs samples.
| Materials | Flexural Properties | Tensile Properties | |||
|---|---|---|---|---|---|
| Max Flex Stress (MPa) | Flexible Modulus (MPa) | Breaking Stress (MPa) | Elongation at Break (%) | Tensile Modulus (MPa) | |
| BM | 0.05 | 3.45 | 1.12 | 20.0 | 2.95 |
| CA-1 | 0.21 | 4.84 | 1.18 | 18.3 | 3.06 |
| CA-2 | 0.39 | 9.65 | 1.09 | 16.1 | 2.91 |
| CA-3 | 0.57 | 10.99 | 0.99 | 12.7 | 5.42 |
| CA-4 | 0.73 | 13.46 | 1.11 | 11.5 | 9.13 |
| CA-4/6 | 1.47 | 48.76 | 1.70 | 9.6 | 12.92 |
| CA-4/3 | 2.88 | 274.49 | 3.06 | 5.4 | 46.07 |
Note: Data were obtained from the calculation method described in the Supplementary Materials.