Applicability of a Material Constitutive Model Based on a Transversely Isotropic Behaviour for the Prediction of the Mechanical Performance of Multi Jet Fusion Printed Polyamide 12 Parts
Abstract
:1. Introduction
- In all the studies where the printing mode for manufacturing the samples/parts was specified, the Balanced Print Mode was consistently employed. This printing mode offers an optimal balance between printing speed and the final properties (mechanical properties, dimensional accuracy, appearance, surface quality, and more) of the printed parts [13,15,16,21].
- To evaluate the tensile properties of MJF-printed PA12, two different standards are applicable: ISO 527, as referenced in [7,9,13,15,18,19,20], and ASTM D638, as referenced in [5,8,12,16,17,21,24]. It should be noted that the tensile properties of MJF-printed PA12 listed in the catalogues published by the developer of MJF technology (HP Inc.) [14] were determined in reference to ASTM D638. Similarly, the procedures specified in both ISO 178 (see [8,13]) and ASTM D790 (see [16]) are suitable for assessing the flexural properties of MJF-printed PA12.
- The layered structure derived from the MJF printing technology and the method used to generate those layers suggest a mechanical behaviour of the MJF-printed PA12 that is analogous to that of a transversely isotropic material. Transversely isotropic materials exhibit an isotropic behaviour within the plane of isotropy, with mechanical properties that differ from those in a direction perpendicular to that plane. In general, higher values for strength and stiffness were observed in the growing direction compared to the printing plane, along with lower values for elongation at break [5,7,8,13,15,18,19,22,23]. This observation is consistent with the data provided by HP Inc. [14] regarding the mechanical properties of MJF-printed PA12.
- Overall, the mechanical properties of MJF-printed PA12 reported in the various studies that were analysed tend, to varying degrees, to have lower values than those published by HP Inc. [14].
2. Materials and Methods
2.1. Constitutive Model for Transversely Isotropic Materials
2.2. Samples/Parts Fabrication
2.2.1. Manufacture of Tensile and Shear Samples
2.2.2. Manufacture of Handles for Mechanical Testing
2.3. Mechanical Testing
2.3.1. Uniaxial Tensile Tests
2.3.2. Shear Tests
2.4. Mechanical Tests on Printed Handles
3. Results and Discussion
3.1. Uniaxial Tensile Tests
3.2. Shear Tests
3.3. Transversely Isotropic Behaviour of the MJF-Printed PA12
3.4. Structural Behaviour of Handles
4. Conclusions
- MJF-printed PA12 showed superior tensile properties along the vertical growing direction compared to the horizontal printing plane. Specifically, the tensile strength and elastic modulus values were approximately 16% higher along the vertical direction. The Poisson’s ratio values were relatively consistent on both the plane of isotropy of the material and the planes perpendicular to it. The notable variability in the results for the elongation at break complicated any definitive conclusions on the influence of the build orientation on that same parameter.
- The anisotropy of the shear properties of the MJF-printed PA12 was significantly lower compared to its tensile properties. Shear modulus values were nearly identical on both the plane of isotropy of the material and the vertical planes. Moreover, slightly higher shear strength values (+6.7%) were observed on the vertical planes.
- The elastic moduli values used in the numerical model and obtained from uniaxial tensile tests on the printed samples were found to be significantly higher than those from uniaxial tensile tests on samples taken from the printed handles.
- The progressive reduction in material stiffness as the stress/strain increases was not considered in the material constitutive model employed in the numerical simulation to describe the mechanical behaviour of the MJF-printed PA12, leading to an overestimation of the stiffness of the printed material.
Author Contributions
Funding
Institutional Review Board Statement
Data Availability Statement
Conflicts of Interest
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Reference | Type of Tests/Build Orientations/Standard | Printer | Print Mode |
---|---|---|---|
O’Connor et al. [13] | Tensile/XYZ (X), YZX (Y) and ZYX (Z)/ISO 527 [26] | HP Jet Fusion 4200 | Balanced |
Flexural/XYZ (X), YZX (Y) and ZYX (Z)/ISO 178 [27] | |||
O’Connor and Dowling [16] | Tensile/XYZ (X), YZX (Y) and ZYX (Z)/ASTM D638 [28] | HP Jet Fusion 4200 | Balanced |
Flexural/XYZ (X), YZX (Y) and ZYX (Z)/ASTM D790 [29] | |||
Morales-Planas et al. [17] | Tensile/XY, YZ and ZX/ASTM D638 | HP Jet Fusion 4200 | Balanced |
Palma et al. [5] | Tensile/Vertical and horizontal/ASTM D638 | - | - |
Riedelbauch et al. [15] | Tensile/YXZ and ZXY/ISO 527 | HP Jet Fusion 4200 | Balanced |
Galati et al. [9] | Tensile/XY and Z/ISO 527 | HP Jet Fusion 4200 | - |
Tensile/XY, XY-50°, Z and Z-50°/- | |||
Sillani et al. [18] | Tensile/X, Y and Z/ISO 527 | HP Jet Fusion 4200 | - |
Mehdipour et al. [19] | Tensile/Flatwise, edgewise and upright/ISO 527 | HP Jet Fusion 4200 | Balanced |
Cai et al. [8] | Tensile/X, Y and Z/ASTM D638 | HP Jet Fusion 4200 | Balanced |
Flexural/X, Y and Z/ISO 178 | |||
Rosso et al. [20] | Tensile/Z/ISO 527 | HP Jet Fusion 4200 | Balanced |
Calignano et al. [7] | Tensile/fx, fd, fy, vx, vd, vy, zx, zd and zy/ISO 527 | HP Jet Fusion 4200 | Balanced |
Chen et al. [21] | Tensile/XY_0°, XY_90° and Z/ASTM D638 | HP Jet Fusion 5200 | Balanced |
Shear/XY_0° and Z/ASTM B831 [30] | |||
Chen et al. [22] | Tensile/Vertical and horizontal/- | HP Jet Fusion 5200 | - |
Osswald et al. [23] | Tensile/Vertical and horizontal/- | HP Jet Fusion 4200 | Balanced |
Compression/Vertical and horizontal/- | |||
Torsion/Vertical, horizontal and 45°/- | |||
Torsion + axial/Vertical, horizontal and 45°/- | |||
Abdallah et al. [24] | Tensile/0° and 25°/ASTM D638 | - | - |
Koh et al. [12] | Tensile/X, X45 and Z/ASTM D638 | HP Jet Fusion 5200 | - |
HP Inc. [14] | Tensile/XY, YX and Z/ASTM D638 | HP Jet Fusion 4200 | Balanced |
Powder: | PA12 |
---|---|
Average particle size [µm]: | 60 |
Bulk density of powder [g/cm3]: | 0.425 |
Density of parts [g/cm3]: | 1.01 |
Powder melting point [°C]: | 187 |
Layer thickness [µm]: | 80 |
Mixing ratio of virgin/recycled powder: | 20:80 |
Build volume [mm3]: | 380 × 254 × 380 |
Sample | Width [mm] | Thickness [mm] | Maximum Load [N] | Tensile Strength [MPa] | Elastic Modulus [GPa] | Elongation at Break [%] | Poisson’s Ratio [-] |
---|---|---|---|---|---|---|---|
YX-1-T | 9.95 | 4.08 | 1455 | 35.84 | 1.737 | 3.61 | 0.381 |
YX-2-T | 10.03 | 4.06 | 1221 | 29.98 | 1.709 | 2.20 | 0.369 |
YX-3-T | 9.97 | 4.06 | 1927 | 47.61 | 1.576 | 13.36 | - |
XY-1-T | 9.84 | 4.13 | 985 | 24.20 | 1.401 | 2.07 | 0.381 |
XY-2-T | 9.88 | 4.10 | 1259 | 31.10 | 1.559 | 2.80 | 0.355 |
XY-3-T | 9.90 | 4.14 | 1695 | 41.30 | 1.404 | 9.12 | - |
YX + XY | Mean value | 1424 ± 343.09 | 35.00 ± 8.44 | 1.564 ± 0.144 | 5.53 ± 4.66 | 0.372 ± 0.012 | |
ZY-1-T | 10.05 | 4.00 | 1550 | 38.50 | 1.879 | 2.85 | 0.355 |
ZY-2-T | 10.10 | 4.03 | 1619 | 39.80 | 1.809 | 3.14 | 0.356 |
ZY-3-T | 10.02 | 4.00 | 1679 | 41.90 | 1.734 | 4.70 | - |
ZX-1-T | 10.00 | 3.90 | 1283 | 32.90 | 1.714 | 2.41 | 0.371 |
ZX-2-T | 10.10 | 4.06 | 1640 | 40.00 | 1.866 | 3.08 | 0.349 |
ZX-3-T | 10.15 | 4.07 | 2056 | 49.80 | 1.872 | 8.96 | - |
ZY + ZX | Mean value | 1638 ± 249.21 | 40.48 ± 5.49 | 1.812 ± 0.073 | 4.19 ± 2.46 | 0.358 ± 0.010 |
Reference | Tensile Strength [MPa] | Elastic Modulus [GPa] | Elongation at Break [%] |
---|---|---|---|
O’Connor et al. [13] O’Connor and Dowling [16] | X = 47 ± 0.9 Y = 48 ± 0.8 Z = 49 ± 0.6 | X = 1.242 ± 0.028 Y = 1.147 ± 0.040 Z = 1.246 ± 0.037 | X = 19 ± 2.8 Y = 27 ± 1.2 Z = 16 ± 1.9 |
Morales-Planas et al. [17] | XY = 47.9 ÷ 51.6 YZ = 45.6 ÷ 52.1 ZX = 50.9 ÷ 57.4 | XY = 3.525 ÷ 4.202 YZ = 3.767 ÷ 4.321 ZX = 4.106 ÷ 4.409 | XY = 2.5 ÷ 4.1 YZ = 2.0 ÷ 2.5 ZX = 2.1 ÷ 4.8 |
Palma et al. [5] | H = 45.15 V = 47.77 | - | H = 23.2 V = 17.4 |
Riedelbauch et al. [15] | YXZ = 46.7 ZXY = 52.3 | YXZ = 1.439 ZXY = 1.580 | YXZ = 13.8 ZXY = 12.5 |
Galati et al. [9] | XY = 36 Z = 39 | - | XY = 25 Z = 18 |
Sillani et al. [18] | X = 45.8 ± 3.5 Y = 47.9 ± 0.9 Z = 53.7 ± 1.1 | X = 1.128 ± 0.068 Y = 1.204 ± 0.084 Z = 1.337 ± 0.098 | X = 11.2 ± 1.8 Y = 13.2 ± 1.5 Z = 11.4 ± 1.3 |
Mehdipour et al. [19] * | Flatwise = 34.39 ± 1.71 Edgewise = 44.07 ± 0.79 Upright = 42.79 ± 0.38 | Flatwise = 1.063 ± 0.025 Edgewise = 1.435 ± 0.024 Upright = 1.495 ± 0.039 | Flatwise = 17.19 ± 1.36 Edgewise = 16.39 ± 0.28 Upright = 11.98 ± 1.38 |
Cai et al. [8] | X = 48.7 ± 0.8 Y = 44.5 ± 0.7 Z = 49.6 ± 1.2 | X = 1.369 ± 0.025 Y = 1.369 ± 0.069 Z = 1.669 ± 0.067 | X = 27.4 ± 2.2 Y = 15.9 ± 1.1 Z = 14.8 ± 0.3 |
Rosso et al. [20] | Z = 45.6 ± 0.4 | Z = 1.53 ± 0.06 | Z = 30.0 ± 4.9 |
Calignano et al. [7] | fx = 35.4 ± 2.6 fd = 34.0 ± 2.6 fy = 35.2 ± 2.0 vx = 38.2 ± 1.9 vd = 30.5 ± 4.6 vy = 35.2 ± 0.6 zx = 38.4 ± 3.3 zd = 39.8 ± 0.7 zy = 36.8 ± 2.5 | fx = 1.223 ± 0.157 fd = 1.170 ± 0.136 fy = 1.286 ± 0.029 vx = 1.326 ± 0.070 vd = 0.974 ± 0.087 vy = 1.337 ± 0.083 zx = 1.205 ± 0.536 zd = 1.499 ± 0.291 zy = 1.513 ± 0.296 | fx = 21.5 ± 7.3 fd = 13.7 ± 1.6 fy = 15.9 ± 3.2 vx = 25.3 ± 4.2 vd = 15.1 ± 8.1 vy = 13.2 ± 2.0 zx = 11.2 ± 8.4 zd = 18.5 ± 1.7 zy = 18.0 ± 1.1 |
Chen et al. [22] | H = 45.8 ± 0.5 V = 45.7 ± 0.7 | H = 1.436 ± 0.043 V = 1.561 ± 0.031 | H = 29.3 ± 3.8 V = 10.7 ± 0.2 |
Osswald et al. [23] | H = 41.24 ± 1.18 V = 48.97 ± 1.01 | - | - |
HP Inc. [14] | XY = 50 Z = 50 | XY = 1.7 Z = 1.9 | XY = 17 Z = 9 |
Current work | YX + XY = 35.00 ± 8.44 ZY + ZX = 40.48 ± 5.49 | YX + XY = 1.564 ± 0.144 ZY + ZX = 1.812 ± 0.073 | YX + XY = 5.53 ± 4.66 ZY + ZX = 4.19 ± 2.46 |
Sample | Width [mm] | Thickness [mm] | [N] | Shear Strength [MPa] | Shear Modulus [GPa] |
---|---|---|---|---|---|
YX-1-S | 12.00 | 10.00 | 2523 | 21.03 | 0.615 |
YX-2-S | 12.00 | 10.00 | 2392 | 19.93 | 0.598 |
YX-3-S | 12.00 | 10.10 | 2198 | 18.14 | 0.507 |
XY-1-S | 12.00 | 10.00 | 2339 | 19.49 | 0.595 |
XY-2-S | 12.00 | 10.00 | 2023 | 16.86 | 0.485 |
XY-3-S | 12.00 | 10.00 | 2212 | 18.43 | 0.513 |
YX + XY | Mean value | 2281 ± 174.65 | 18.98 ± 1.47 | 0.552 ± 0.057 | |
ZY-1-S | 12.00 | 10.00 | 2505 | 20.88 | 0.644 |
ZY-2-S | 12.00 | 10.00 | 2336 | 19.47 | 0.515 |
ZY-3-S | 12.00 | 10.00 | 2430 | 20.25 | 0.511 |
ZX-1-S | 12.00 | 9.90 | 2389 | 20.11 | 0.593 |
ZX-2-S | 12.00 | 9.95 | 2451 | 20.53 | 0.539 |
ZY + ZX | Mean value | 2422 ± 63.69 | 20.25 ± 0.52 | 0.560 ± 0.057 |
1-H | 2-H | 5-H | |
---|---|---|---|
EX (GPa) | 1.564 | 1.564 | 1.812 |
EY (GPa) | 1.564 | 1.812 | 1.564 |
EZ (GPa) | 1.812 | 1.564 | 1.564 |
PRXY (-) | 0.372 | 0.309 * | 0.309 * |
PRYZ (-) | 0.309 * | 0.309 * | 0.372 |
PRXZ (-) | 0.309 * | 0.372 | 0.309 * |
GXY (GPa) | 0.552 | 0.560 | 0.560 |
GYZ (GPa) | 0.560 | 0.560 | 0.552 |
GXZ (GPa) | 0.560 | 0.552 | 0.560 |
Sample | Width [mm] | Thickness [mm] | Maximum Load [N] | Tensile Strength [MPa] | Elastic Modulus [GPa] | Elongation at Break [%] |
---|---|---|---|---|---|---|
1-H-A | 5.04 | 3.95 | 769 | 38.63 | 1.317 | 7.90 |
2-H-A | 5.03 | 3.97 | 769 | 38.51 | 1.217 | 8.20 |
2-H-B | 4.93 | 3.97 | 824 | 42.10 | 1.436 | 7.40 |
5-H-B | 4.95 | 3.98 | 821 | 41.67 | 1.339 | 9.20 |
Mean value | 796 ± 30.91 | 40.23 ± 1.92 | 1.327 ± 0.090 | 8.18 ± 0.76 | ||
YX + XY (Table 3) | 35.00 ± 8.44 | 1.564 ± 0.144 | 5.53 ± 4.66 | |||
1-H-B | 4.98 | 3.98 | 609 | 30.73 | 1.256 | 4.20 |
5-H-A | 4.98 | 3.98 | 633 | 31.94 | 1.430 | 4.20 |
Mean value | 621 ± 16.97 | 31.34 ± 0.56 | 1.343 ± 0.123 | 4.20 ± 0.00 | ||
ZY + ZX (Table 3) | 40.48 ± 5.49 | 1.812 ± 0.073 | 4.19 ± 2.46 |
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Perez-Barcenilla, S.; Cearsolo, X.; Aramburu, A.; Castano-Alvarez, R.; Castillo, J.R.; Gayoso Lopez, J. Applicability of a Material Constitutive Model Based on a Transversely Isotropic Behaviour for the Prediction of the Mechanical Performance of Multi Jet Fusion Printed Polyamide 12 Parts. Polymers 2024, 16, 56. https://doi.org/10.3390/polym16010056
Perez-Barcenilla S, Cearsolo X, Aramburu A, Castano-Alvarez R, Castillo JR, Gayoso Lopez J. Applicability of a Material Constitutive Model Based on a Transversely Isotropic Behaviour for the Prediction of the Mechanical Performance of Multi Jet Fusion Printed Polyamide 12 Parts. Polymers. 2024; 16(1):56. https://doi.org/10.3390/polym16010056
Chicago/Turabian StylePerez-Barcenilla, Sergio, Xabier Cearsolo, Amaia Aramburu, Ruben Castano-Alvarez, Juan R. Castillo, and Jorge Gayoso Lopez. 2024. "Applicability of a Material Constitutive Model Based on a Transversely Isotropic Behaviour for the Prediction of the Mechanical Performance of Multi Jet Fusion Printed Polyamide 12 Parts" Polymers 16, no. 1: 56. https://doi.org/10.3390/polym16010056
APA StylePerez-Barcenilla, S., Cearsolo, X., Aramburu, A., Castano-Alvarez, R., Castillo, J. R., & Gayoso Lopez, J. (2024). Applicability of a Material Constitutive Model Based on a Transversely Isotropic Behaviour for the Prediction of the Mechanical Performance of Multi Jet Fusion Printed Polyamide 12 Parts. Polymers, 16(1), 56. https://doi.org/10.3390/polym16010056