| Literature DB >> 31936489 |
Mateusz Galeja1, Aleksander Hejna2, Paulina Kosmela2, Arkadiusz Kulawik1.
Abstract
Due to the rapid growth of 3D printing popularity, including fused deposition modeling (FDM), as one of the most common technologies, the proper understanding of the process and influence of its parameters on resulting products is crucial for its development. One of the most crucial parameters of FDM printing is the raster angle and mutual arrangement of the following filament layers. Presented research work aims to evaluate different raster angles (45°, 55°, 55'°, 60° and 90°) on the static, as well as rarely investigated, dynamic mechanical properties of 3D printed acrylonitrile butadiene styrene (ABS) materials. Configuration named 55'° was based on the optimal winding angle in filament-wound pipes, which provides them exceptional mechanical performance and durability. Also in the case of 3D printed samples, it resulted in the best impact strength, comparing to other raster angles, despite relatively weaker tensile performance. Interestingly, all 3D printed samples showed surprisingly high values of impact strength considering their calculated brittleness, which provides new insights into understanding the mechanical performance of 3D printed structures. Simultaneously, it proves that, despite extensive research works related to FDM technology, there is still a lot of investigation required for a proper understanding of this process.Entities:
Keywords: 3D printing; acrylonitrile butadiene styrene; impact strength; infill angle; mechanical performance
Year: 2020 PMID: 31936489 PMCID: PMC7013835 DOI: 10.3390/ma13020297
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Figure 1Alignment of fibers in filament-wound pipes.
Parameters of the 3D printing process.
| Printing Parameter | Value |
|---|---|
| Nozzle Diameter, mm | 0.4 |
| Layer Height, mm | 0.1 |
| Fill Pattern | Rectilinear |
| Fill Percentage, % | 100 |
| Perimeters Speed, mm/s | 25 |
| External Perimeters Speed, mm/s | 12.5 |
| Infill Speed, mm/s | 40 |
| First Layer Temperature, °C | 240 |
| Other Layers Temperature, °C | 230 |
| Bed Temperature, °C | 80 |
| Number of Layers | 40 |
| Fill Angles, ° | 45, 55, 55’, 60, 90 |
Figure 2Scheme of layers’ deposition during 3D printing of samples (at 20% infill percentage) for following infill angles: (a) 45°, (b) 55°, (c) 55’°, (d) 60° and (e) 90°.
Mechanical properties of 3D printed samples depending on used material and infill angle.
| Material | Infill Angle | Porosity, % | Tensile Strength, MPa | Elongation at Break, % | Young’s Modulus, Mpa | Toughness, J/cm3 | Charpy Impact Strength, J/cm2 | E’ at 25 °C, Mpa | Brittleness, 1010 %·Pa |
|---|---|---|---|---|---|---|---|---|---|
| 1W | 45 | 7.48 ± 0.23 | 37.9 ± 0.2 | 7.4 ± 1.0 | 2486 ± 51 | 196 ± 5 | 2.1 ± 0.2 | 1475.1 | 0.9161 |
| 55 | 7.58 ± 0.04 | 37.6 ± 0.4 | 5.0 ± 0.7 | 2432 ± 37 | 139 ± 21 | 2.3 ± 0.1 | 1587.6 | 1.2646 | |
| 55’ | 10.33 ± 0.18 | 31.9 ± 0.5 | 4.1 ± 1.7 | 2112 ± 19 | 118 ± 19 | 2.3 ± 0.1 | 1392.4 | 1.7517 | |
| 60 | 8.89 ± 0.22 | 32.0 ± 0.7 | 3.9 ± 0.5 | 2196 ± 5 | 106 ± 11 | 1.9 ± 0.1 | 1424.9 | 1.7995 | |
| 90 | 8.70 ± 0.93 | 34.4 ± 0.6 | 3.5 ± 0.6 | 2336 ± 41 | 85 ± 8 | 1.4 ± 0.1 | 1482.6 | 1.9271 | |
| IM | - | 40.1 ± 0.1 | 9.6 ± 0.4 | 2667 ± 42 | 312 ± 41 | 6.3 ± 0.6 | - | - | |
| 2W | 45 | 6.08 ± 0.10 | 41.7 ± 0.4 | 5.8 ± 0.2 | 2348 ± 45 | 181 ± 7 | 2.6 ± 0.2 | 1607.1 | 1.0728 |
| 55 | 7.22 ± 0.29 | 41.2 ± 0.3 | 5.4 ± 0.5 | 2327 ± 53 | 153 ± 7 | 2.7 ± 0.2 | 1609.8 | 1.1504 | |
| 55’ | 9.86 ± 0.98 | 41.2 ± 0.3 | 3.4 ± 0.3 | 2329 ± 64 | 98 ± 14 | 2.8 ± 0.1 | 1657.7 | 1.7743 | |
| 60 | 7.96 ± 0.40 | 39.8 ± 0.5 | 3.5 ± 0.2 | 2329 ± 68 | 91 ± 5 | 2.2 ± 0.2 | 1613.6 | 1.7707 | |
| 90 | 8.33 ± 0.31 | 39.2 ± 0.4 | 3.6 ± 0.4 | 2297 ± 57 | 86 ± 13 | 1.9 ± 0.4 | 1480.6 | 1.8761 | |
| IM | - | 48.9 ± 0.6 | 8.7 ± 0.4 | 2747 ± 105 | 318 ± 16 | 6.3 ± 0.7 | - | - | |
| 1B | 45 | 6.22 ± 0.13 | 37.2 ± 0.5 | 5.7 ± 0.9 | 2353 ± 50 | 149 ± 24 | 2.1 ± 0.2 | 1440.4 | 1.2180 |
| 55 | 6.61 ± 0.34 | 36.9 ± 0.5 | 5.2 ± 0.8 | 2369 ± 37 | 132 ± 14 | 2.3 ± 0.1 | 1444.0 | 1.3317 | |
| 55’ | 9.80 ± 0.18 | 33.9 ± 0.3 | 3.7 ± 0.6 | 2181 ± 43 | 96 ± 12 | 2.4 ± 0.2 | 1338.7 | 2.0189 | |
| 60 | 8.45 ± 0.88 | 35.5 ± 0.5 | 3.7 ± 0.5 | 2346 ± 95 | 91 ± 16 | 1.7 ± 0.1 | 1500.1 | 1.8017 | |
| 90 | 8.11 ± 0.84 | 33.3 ± 0.7 | 3.4 ± 0.2 | 2203 ± 77 | 79 ± 7 | 1.3 ± 0.1 | 1526.9 | 1.9263 | |
| IM | - | 40.9 ± 0.5 | 9.2 ± 1.7 | 2544 ± 143 | 277 ± 31 | 6.1 ± 0.9 | - | - |
Figure 3Fracture areas obtained after tensile tests for (a) 3D printed sample with infill angle of 55’° and (b) injection molded sample.
Figure 4Exemplary stress–strain curve for the 1W45 sample.
Figure 5Relationship between toughness and brittleness for analyzed materials. (a) Comparison with literature data by Brostow et al. (26), (b) Detailed data for 3D printed samples.
Figure 6Relationship between Charpy impact strength and brittleness for analyzed materials and comparison with literature data.