| Literature DB >> 35888548 |
Michał Mazurkiewicz1, Janusz Kluczyński1, Katarzyna Jasik1, Bartłomiej Sarzyński1, Ireneusz Szachogłuchowicz1, Jakub Łuszczek1, Janusz Torzewski1, Lucjan Śnieżek1, Krzysztof Grzelak1, Marcin Małek2.
Abstract
The research shows the comparison between two types of polyamide-based (PA) composites and pure, base material. The conducted analysis describes how the additions of carbon fibers and glass microbeads affect the material's properties and its behavior during the bending tests. All samples have been tested in the three main directions available during the FFF process. To extend the scope of the research, additional digital-image-correlation tests and fracture analyses were made. The obtained results indicated a positive influence of the addition of carbon fibers into the material's volume (from 81.39 MPa in the case of pure PA to 243.62 MPa in the case of the PA reinforced by carbon fibers).Entities:
Keywords: additive manufacturing; fused filament fabrication; polyamide-based composites; three-point bending
Year: 2022 PMID: 35888548 PMCID: PMC9316643 DOI: 10.3390/ma15145079
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.748
Properties of used materials [38].
| Property | PA6 Neat Black | PA6 GK10 | PA6 CF15 |
|---|---|---|---|
| Density (g/cm3) | 1.25 | 1.01 | 1.25 |
| Tensile strength (MPa) | 78 | 87 | 170 |
| Extension at max. force (%) | 4.4 | 2.7 | 2 |
| Modulus of elasticity (GPa) | 3.4 | 4.2 | 15 |
Parameters of the FFF process suggested by the filament supplier.
| Material | Filament Diameter (mm) | Nozzle Diameter (mm) | Table Temperature (°C) | Nozzle Temperature (°C) | Infill (%) | Number of Contours |
|---|---|---|---|---|---|---|
| PA6 NB | 1.75 | 0.4 | 80 | 260 | 100 | 5 |
| PA6GK10 | 1.75 | 0.4 | 80 | 260 | 100 | 5 |
| PA6GK15 | 1.75 | 0.4 | 80 | 260 | 100 | 5 |
Figure 1Axes of the test samples and geometric dimensions.
Figure 2(a) MTS Criterion C; (b) Dantec devices used for the DIC process.
Registered bending properties of all tested samples.
| Material | Average of Flexural Strength σfM (MPa) | Standard Deviation | Average of Flexural Strain εfB (%) | Standard Deviation | Young’s Modulus E (Gpa) | Standard Deviation | |
|---|---|---|---|---|---|---|---|
| PA6 NB | X | 66.75 | 4.94 | 4.87 | 1.32 | 2.97 | 0.20 |
| Y | 81.39 | 1.64 | 5.25 | 0.01 | 1.96 | 0.45 | |
| Z | 23.54 | 0.70 | 1.73 | 0.09 | 1.11 | 0.06 | |
| PA6 CF15 | X | 184.18 | 3.44 | 3.26 | 0.18 | 6.12 | 0.22 |
| Y | 243.62 | 10.85 | 2.53 | 0.16 | 11.65 | 1.41 | |
| Z | 8.59 | 3.65 | 1.40 | 0.30 | 0.92 | 0.26 | |
| PA6 GK10 | X | 60.10 | 1.29 | 3.87 | 0.21 | 2.75 | 0.44 |
| Y | 64.05 | 0.55 | 3.95 | 0.11 | 0.42 | 0.34 | |
| Z | 16.76 | 0.44 | 1.56 | 0.14 | 1.09 | 0.14 | |
Figure 3Orientation of fibers inside the tensile samples observed on the cross-section of samples processed according to different orientations, and schematic representation of the expected specimen microstructures [41].
Figure 4Curves of Flexural Stress (σfM) versus Flexural Strain (εf).
Figure 5Strain levels registered via the DIC method.
Figure 6Fracture images of each sample.
Figure 7Microscope image of PA6 CF15X structure.