Editorial Feature

Energy Absorption Properties of Two 3D-Printed Lattice Structures

Metallic three-dimensional lattice structures harbor different mechanical properties. This article considers research published in the journal Materials, that analyzes the energy absorption properties of enhanced pyramidal lattice structures of three strut materials prepared by 3D printing, combined with investment casting and direct metal additive manufacturing. 

Study: Compressive and Energy Absorption Properties of Pyramidal Lattice Structures by Various Preparation Methods. Image Credit: Iaremenko Sergii/Shutterstock.com

Cellular materials are vital structural and functional materials owing to their high specific strength, low density, and porous structure, etc. Traditional cellular materials were mostly sponges, foams, and honeycombs, with numerous limitations. However, recently generated three-dimensional lattice structures can combat the limitations of traditional cellular materials.

These materials are used in many engineering fields, for instance, the aerospace, aviation, and automotive industries.

Cellular materials have many important properties, one among them being energy absorption capacity, and this property can be tailored. Numerous methods are employed to tailor the energy absorption capacity.

Metallic lattice structures are manufactured with numerous methods like stamping forming, extrusion combining, wire cutting, expanded sheet folding, and investment casting. However, these techniques require bonding or welding techniques to assemble the struts to form lattice structures.

To address this, new metallic additive manufacturing technologies were developed, but these too have limitations, resulting in only a small part of metals suitable for these technologies. New technology has been developed combining 3D printing with investment casting, addressing the issues of the former methods.

This article, based on research in the journal Materials, compares pyramidal lattice structures in three strut materials developed with two preparation methods. The influence of preparation methods and design parameters on their compression response and energy absorption are analyzed by finite element analysis and compression tests.

Methodology

Preparation of Lattice Structure Samples

The study analyzes two technologies—direct 3D printing and 3D printing combined with investment casting. Both these techniques were used to prepare the lattice structure samples.

In direct 3D printing, a BLT-A300 printer and selective laser melting (SLM) method were used, while in 3D printing combined with investment casting an as-cast AlSi10Mg alloy and a 7005 aluminum alloy were used.

To analyze the mechanical properties of various aluminum alloys employed, tensile experiments were carried out. Figure 1a shows the geometric dimensions of samples employed for the tensile test, and Figure 1b depicts the stress-strain curves of related alloys.

The tensile test of different aluminum alloys, (a) is the geometric dimensions of tensile sample; (b) is the stress-strain curves.

Figure 1. The tensile test of different aluminum alloys, (a) is the geometric dimensions of tensile sample; (b) is the stress-strain curves. Image Credit: Zhang, et al., 2021.

 

Enhanced Pyramidal Lattice Structure

The mechanical properties of the lattice structure are enhanced through node enhancement. Figure 2 shows an enhanced pyramidal (EP) lattice structure and a usual one, and the enhancement is realized slowly by increasing the diameter of struts toward the node.

Characteristics of pyramidal lattice structures in the present study: the left is usual and the right is enhanced.

Figure 2. Characteristics of pyramidal lattice structures in the present study: the left is usual and the right is enhanced. Image Credit: Zhang, et al., 2021.

The lattice structures are grouped into four (Table 1). A1 is selected as an example (Figure 3), and at least three samples are tested for each structure. The arithmetic mean value is considered to be the representative value.

Group de (mm) dm (mm) Strut Material θ(°) H (mm) ρ*
A1 1.70 1.25 AlSi10Mg powder 35 5.00 0.3278
A2 1.70 1.25 as-cast AlSi10Mg 35 5.00 0.3278
A3 1.70 1.25 as-cast 7005 35 5.00 0.3278
B1 1.70 1.25 AlSi10Mg powder 45 6.16 0.3486
B2 1.70 1.25 as-cast AlSi10Mg 45 6.16 0.3486
B3 1.70 1.25 as-cast 7005 45 6.16 0.3486
C1 1.70 1.25 AlSi10Mg powder 55 7.14 0.3938
C2 1.70 1.25 as-cast AlSi10Mg 55 7.14 0.3938
C3 1.70 1.25 as-cast 7005 55 7.14 0.3938
D1 1.40 1.40 AlSi10Mg powder 35 5.00 0.3307
D2 1.50 1.34 AlSi10Mg powder 35 5.00 0.3415
D3 1.60 1.31 AlSi10Mg powder 35 5.00 0.3484
D4 1.70 1.25 AlSi10Mg powder 35 5.00 0.3278
D5 1.80 1.18 AlSi10Mg powder 35 5.00 0.3410

Table 1. Parameters of lattice structures. Source: Zhang, et al., 2021.

Arithmetic mean value of three experimental data.

Figure 3. Arithmetic mean value of three experimental data. Image Credit: Zhang, et al., 2021.

Finite Element Analysis

The finite element analysis (FEA) was carried out to simulate the mechanical response of lattice structures in compression. Table 2 shows relevant plastic parameters. 

AlSi10Mg Powder As-Cast AlSi10Mg 7005 Aluminum Alloy
Plastic Strain Stress (MPa) Plastic Strain Stress (MPa) Plastic Strain Stress (MPa)
0 116.94 0 113.91 0 119.03
0.0037 218.19 0.0126 149.27 0.0106 236.02
0.0077 255.68 0.0262 177.05 0.0210 262.08
0.0116 283.78 0.0396 187.70 0.0316 277.13
0.0156 307.31 0.0529 201.83 0.0421 289.14
0.0195 325.19 0.0661 211.70 0.0527 298.12
0.0234 338.82 0.0769 220.06 0.0632 304.61
0.0268 347.14 0.0919 227.16 0.0738 309.03
0.0334 357.75 0.1194 234.41 0.0843 311.99
0.0398 362.30 0.1345 243.31 0.0998 313.59

Table 2. Plastic parameters of three strut materials. Source: Zhang, et al., 2021.

Compression Tests

Uniaxial compression tests were performed in a material testing system. The samples had 5 × 5 × 5 unit cells (Figure 4) to decrease the size effect. The deformation mechanism of samples was recorded by a high-resolution digital camera.

Four group samples, A, B, C, and D, of node-enhanced pyramidal lattice structures.

Figure 4. Four group samples, A, B, C, and D, of node-enhanced pyramidal lattice structures. Image Credit: Zhang, et al., 2021.

Results and Discussion

Compression Behaviors of Samples

Figure 5 provides the deformation mechanisms of samples in Group A, B, and C, where three various included angles and matrix material states were analyzed.

Deformation process of EP lattice structures in Group A, B, and C; (a–c) represent the compression when the included angle is 35°, 45°, and 55°, respectively.

Figure 5. Deformation process of EP lattice structures in Group A, B, and C; (a–c) represent the compression when the included angle is 35°, 45°, and 55°, respectively. Image Credit: Zhang, et al., 2021.

Figure 6 and Figure 7 depict the results of FEA and the corresponding stress-strain curves.

Mises stress distribution diagrams of EP lattice structures in Group A, B, and C.

Figure 6. Mises stress distribution diagrams of EP lattice structures in Group A, B, and C. Image Credit: Zhang, et al., 2021.

Figure 7 shows that in all situations, only as-cast AlSi10Mg alloy displayed smooth stress-strain curves.

The stress-strain curves of samples; (a–c) represent Group A, B, and C respectively.

Figure 7. The stress-strain curves of samples; (a–c) represent Group A, B, and C respectively. Image Credit: Zhang, et al., 2021.

The observations show that the mechanical properties of the strut material can be the decisive factor for the response behavior of related lattice structures, and are verified by the failure mechanisms depicted in Figure 8.

The strut surface morphology of (a) AM AlSi10Mg and (b) as-cast 7005 Al alloy lattice structures; (c,d) are the morphology of fracture surface of AM AlSi10Mg and as-cast 7005 Al alloy lattice structures; (e,f) magnified microstructures in the red frames of (c,d).

Figure 8. The strut surface morphology of (a) AM AlSi10Mg and (b) as-cast 7005 Al alloy lattice structures; (c,d) are the morphology of fracture surface of AM AlSi10Mg and as-cast 7005 Al alloy lattice structures; (e,f) magnified microstructures in the red frames of (c,d). Image Credit: Zhang, et al., 2021.

Figure 9a illustrates the compression deformation mechanism of usual and enhanced lattice structures while Figure 9b depicts the corresponding Mises stress distribution diagrams.

Deformation process of usual lattice structure D1 and EP sample D4 (a) and corresponded Mises stress distribution (b).

Figure 9. Deformation process of usual lattice structure D1 and EP sample D4 (a) and corresponded Mises stress distribution (b). Image Credit: Zhang, et al., 2021.

Figure 10 shows that the improved structures largely decreased stress concentration in comparison to the usual pyramidal lattice structure.

Mises stress distribution diagrams of a unit cell with different end diameters.

Figure 10. Mises stress distribution diagrams of a unit cell with different end diameters. Image Credit: Zhang, et al., 2021.

The compressive stress-strain curves of samples at end diameters of struts are depicted in Figure 11.

Effect of end diameter on the compressive stress-strain behavior of samples.

Figure 11. Effect of end diameter on the compressive stress-strain behavior of samples. Image Credit: Zhang, et al., 2021.

Energy Absorption

Table 3 shows the representation of mechanical properties derived from experimental and simulated results.

Sample σP (MPa)
Exp./Sim.
E* (MPa)
Exp./Sim.
WVmax (mJ.mm-3)
Exp./Sim.
Pmax (%)
Exp./Sim.
A1 21.93/19.43 601.46/591.11 10.13/8.54 42.45/43.95
A2 9.55/10.89 185.49/197.56 5.60/5.07 24.46/28.21
A3 11.02/13.67 169.27/192.00 4.58/5.27 22.26/23.79
B1 33.05/31.94 1205.86/1432.18 15.04/14.42 42.98/45.16
B2 20.18/18.03 346.52/426.81 8.69/10.99 28.18/37.41
B3 23.07/22.99 931.93/940.00 9.59/8.79 40.23/38.23
C1 55.38/54.11 2662.91/2842.14 26.64/30.38 47.03/37.44
C2 37.00/34.53 925.26/1066.32 18.77/16.70 31.49/34.12
C3 47.12/44.33 1836.72/1670.97 20.38/23.35 43.24/51.75
D1 18.37/15.77 406.09/451.22 8.72/7.12 41.78/45.15
D2 20.06/16.27 535.66/604.17 8.81/6.98 40.23/42.90
D3 22.16/19.05 550.17/567.75 9.43/8.77 37.95/46.04
D4 21.93/22.43 601.46/591.11 10.13/8.54 42.45/43.95
D5 22.20/24.09 591.26/701.64 9.35/8.74 40.97/36.28

Table 3. Representing mechanical properties of samples. Source: Zhang, et al., 2021.

Figure 12 illustrates the absorbed energy per unit volume against the strain of all samples. The results indicate that different strut materials and different inclination angles lead to various energy absorption behaviors.

Absorbed energy per unit volume of EP lattice structure samples; (a–d) represents Group A–D, respectively.

Figure 12. Absorbed energy per unit volume of EP lattice structure samples; (a–d) represents Group A–D, respectively. Image Credit: Zhang, et al., 2021.

To compare the energy absorption behavior among the three strut materials, the energy absorption diagrams were established (Figure 13a–d).

Energy absorption diagrams of samples with different strut materials and inclination angles; (a–c) represent the results of AM AlSi10Mg, as–cast AlSi10Mg, and 7005 Al alloy, respectively; (d) is the summary of the above results.

Figure 13. Energy absorption diagrams of samples with different strut materials and inclination angles; (a–c) represent the results of AM AlSi10Mg, as–cast AlSi10Mg, and 7005 Al alloy, respectively; (d) is the summary of the above results. Image Credit: Zhang, et al., 2021.

Prediction of Mechanical Parameters

Calculation of σP and E

The relationship between the compressive strength and relative density of foams proposed by Gibson and Ashby was applicable for lattice structures, but those did not involve the change of inclination angle of multi-layer lattice structures. Hence, another model is proposed by including the effect of inclination angle on the compressive strength of lattice structures.

Validation of Theoretical Results

Figure 14 provides the experimental and calculated results. The results show that all the fitted trajectories of mechanical parameters are straight lines, being consistent with the theoretical predictions. K and R, the constants in Table 4, showcase certain discrepancies when the strut material changes.

Theoretical results of mechanical properties against inclination angle; (a–c) are the theoretical relationship of angle with respect to compressive strength, equivalent modulus, and energy absorption, respectively.

Figure 14. Theoretical results of mechanical properties against inclination angle; (a–c) are the theoretical relationship of angle with respect to compressive strength, equivalent modulus, and energy absorption, respectively. Image Credit: Zhang, et al., 2021.

Table 4. Mathematical expressions of fitted trajectories. Source: Zhang, et al., 2021.

Conclusion

The enhanced lattice structures in three strut materials were created by two preparation methods. The influence of preparing methods, strut materials, and geometric parameters on compression behavior and energy absorption was analyzed by finite element analysis and compression experiments.

It was seen that the method of 3D printing combined with investment casting removes stress fluctuations, but the compressive strength decreases. The inclination angle increase of enhanced pyramidal lattice structures channels the gap in the load-bearing capacity and enhances energy absorption. The theoretical equations and finite element analysis carried out were persistent with the experimental results.

Journal Reference:

Zhang, H., Wang, X., Shi, Z., Xue, J., Han, F. (2021) Compressive and Energy Absorption Properties of Pyramidal Lattice Structures by Various Preparation Methods. Materials. Available at: https://www.mdpi.com/1996-1944/14/21/6484/htm.

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