| Literature DB >> 32370263 |
Francisco J Alonso-Montemayor1, Quim Tarrés2, Helena Oliver-Ortega2, F Xavier Espinach3, Rosa Idalia Narro-Céspedes1, Adali O Castañeda-Facio1, Marc Delgado-Aguilar1.
Abstract
Automotive and industrial design companies have profusely used commodity materials like glass fiber-reinforced polypropylene. These materials show advantageous ratios between cost and mechanical properties, but poor environmental yields. Natural fibers have been tested as replacements of glass fibers, obtaining noticeable tensile strengths, but being unable to reach the strength of glass fiber-reinforced composites. In this paper, polyamide 6 is proposed as a matrix for cellulosic fiber-based composites. A variety of fibers were tensile tested, in order to evaluate the creation of a strong interphase. The results show that, with a bleached hardwood fiber-reinforced polyamide 6 composite, it is possible to obtain tensile strengths higher than glass-fiber-reinforced polyolefin. The obtained composites show the existence of a strong interphase, allowing us to take advantage of the strengthening capabilities of such cellulosic reinforcements. These materials show advantageous mechanical properties, while being recyclable and partially renewable.Entities:
Keywords: biocomposites; cellulose; mechanical properties; micromechanics
Year: 2020 PMID: 32370263 PMCID: PMC7284898 DOI: 10.3390/polym12051041
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.329
Figure 1Workflow of the present study.
Figure 2Tensile strength of neat polyamide 6 (PA6) and PA6-composites containing 20 wt % of stone groundwood pulp (SGW), untreated hemp filaments (UHF), bleached kraft hardwood fibers (BKHF), bleached hemp fibers (BHF) and bleached flax fibers (BFF).
Figure 3Proposed mechanism of bleached fibers anchoring onto PA6 surface.
Figure 4Stress-strain curves of neat PA6 and the BHF-reinforced composites.
Tensile characteristics of the BHF-reinforced PA6 composites.
| BHF | Vf
| ||||
|---|---|---|---|---|---|
| 0 | 0 | 69.70 ± 0.86 | 69.70 | 11.38 ± 0.13 | 3.37 ± 0.21 |
| 10 | 0.077 | 78.25 ± 0.94 | 67.65 | 7.21 ± 0.12 | 4.33 ± 0.09 |
| 20 | 0.158 | 88.77 ± 0.46 | 64.87 | 5.77 ± 0.37 | 5.36 ± 0.11 |
| 30 | 0.244 | 98.42 ± 1.27 | 59.29 | 4.45 ± 0.26 | 6.69 ± 0.23 |
Figure 5Scanning electron microscopy (SEM) images of the fracture surfaces of the 20 wt % BHF-reinforced PA6 composites. (a) voids in the structure of the composite PA6-Hemp fibers; (b) interface between fibers and matrix.
Morphology of BHF prior to be incorporated to PA6 and after being incorporated at different reinforcement contents.
| BHF | Vf
| |||||
|---|---|---|---|---|---|---|
| 0 | 0 | 311.56 | 748.32 | 1336.1 | 22.3 | 59.91 |
| 10 | 0.077 | 196.76 | 332.52 | 563.5 | 21.7 | 25.97 |
| 20 | 0.158 | 193.07 | 323.57 | 534.2 | 21.4 | 24.96 |
| 30 | 0.244 | 188.79 | 304.57 | 498.2 | 19.2 | 25.95 |
l: arithmetic average length; l: average length weighted in length; l: average length double weighted.
Figure 6Length distribution of the original BHF and the BHF incorporated to PA6 at different content.
Data used to solve Kelly and Tyson modified equation by using Bowyer and Bader methodology.
| Reinforcement weight content (%) | 10 | 20 | 30 |
| Reinforcement Volume fraction | 0.077 | 0.158 | 0.244 |
| Fiber modulus (GPa) | 30.45 | 30.45 | 30.45 |
| Elongation at break (%) | 7.21 | 5.77 | 4.45 |
| Strain level 1 analyzed (%) | 2.38 | 1.90 | 1.48 |
| Strain level 2 analyzed (%) | 4.76 | 3.81 | 2.97 |
| Composite stress at strain level 1 (MPa) | 54.15 | 50.20 | 49.60 |
| Composite stress at strain level 2 (MPa) | 78.28 | 83.30 | 83.50 |
| Matrix stress at break (MPa) | 68.90 | 69.30 | 69.30 |
| Matrix stress at strain level 1 (MPa) | 46.46 | 38.11 | 30.60 |
| Matrix stress at strain level 2 (MPa) | 67.40 | 66.38 | 55.99 |
Micromechanics tensile strength properties of PA6-based composites.
| Reinforcement weight content (%) | 10 | 20 | 30 |
| Orientation factor χ1 | 0.30 | 0.30 | 0.28 |
| Interfacial shear strength τ (MPa) | 33.0 | 38.2 | 40.0 |
| Critical length (μm) | 354 | 309 | 283 |
| Intrinsic tensile strength | 1051 | 1101 | 1178 |
Figure 7Percentage contributions of the phases of the composite to its tensile strength. Z is the matrix contribution to the tensile strength of composite, X’ is the subcritical fibers contribution and Y’ the supercritical fibers contribution.