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Investigation of additive manufactured micro-lattice structures for defence applications Cover

Investigation of additive manufactured micro-lattice structures for defence applications

Open Access
|Nov 2023

Figures & Tables

Fig. 1.

Micro-lattice structure design: (a) honeycomb and (b) gyroid
Micro-lattice structure design: (a) honeycomb and (b) gyroid

Fig. 2.

(a) Laser powder bed fusion process for printing of micro-lattice specimens: EOS M290; (b) micro-lattice specimens honeycomb and gyroid; (c) w-EDM machine; (d) Micro Vickers hardness machine; (e) surface roughness measurement device
(a) Laser powder bed fusion process for printing of micro-lattice specimens: EOS M290; (b) micro-lattice specimens honeycomb and gyroid; (c) w-EDM machine; (d) Micro Vickers hardness machine; (e) surface roughness measurement device

Fig. 3.

Coupon preparation for morphological tests
Coupon preparation for morphological tests

Fig. 4.

LPBF A286 powder: (a) EDS analysis, (b) elemental distribution and (c, d) SEM images of A286 powder
LPBF A286 powder: (a) EDS analysis, (b) elemental distribution and (c, d) SEM images of A286 powder

Fig. 5.

OM and SEM images for (a-d) RHA (e-h) MHA (i-l) HNS
OM and SEM images for (a-d) RHA (e-h) MHA (i-l) HNS

Fig. 6.

OM and SEM images for honeycomb lattice structures: (a–d) as printed; (e–h) stress relieved; (i–l) heat treated
OM and SEM images for honeycomb lattice structures: (a–d) as printed; (e–h) stress relieved; (i–l) heat treated

Fig. 7.

OM and SEM images for gyroid lattice structures: (–d) as printed. (e–h) stress relieved, (i–l) heat treated
OM and SEM images for gyroid lattice structures: (–d) as printed. (e–h) stress relieved, (i–l) heat treated

Fig. 8.

Micro-lattice A286 test specimens placed in salt spray test chamber
Micro-lattice A286 test specimens placed in salt spray test chamber

Fig. 9.

X-ray diffraction plot (a) RHA, MHA, HNS; (b) honeycomb and gyroid micro-lattice structures
X-ray diffraction plot (a) RHA, MHA, HNS; (b) honeycomb and gyroid micro-lattice structures

Response variables, surface roughness, and micro-Vickers hardness for the honeycomb micro-lattice structure

Non-stress relived (as printed)
Surface roughness (Ra)Micro-Vickers Hardness (HV)
S.No.LatticeDesignNon-stress relievedAverage (Ra)MaxMinAverageMaxMin
1HoneycombDesign 12A11.2911.6410.54219HV1225213
2HoneycombDesign 23A9.9411.849.36220HV1227215
3HoneycombDesign 34A11.1811.189.87230HV1242218
4HoneycombDesign 45A8.9112.68.54213HV1218207
5HoneycombDesign 56A11.6912.349.03194HV1201190
Stress relieved
S.No.LatticeDesignStress relievedAverage (Ra)MaxMinAverageMaxMin
1HoneycombDesign 12B14.5824.269.23233HV1239228
2HoneycombDesign 23B14.7917.1210.48214HV1220209
3HoneycombDesign 34B13.7615.9112.11193HV1197190
4HoneycombDesign 45B12.2613.6611.43222HV1226218
5HoneycombDesign 56B20.2424.2317.19220HV1226216
Heat treated (Final specimens)
S. No.LatticeDesignHeat treatedAverage (Ra)MaxMinAverageMaxMin
1HoneycombDesign 12C,2D,2E11.5915.29.12460HV1475451
2HoneycombDesign 23C,3D.3E7.777.947.65418HV1425412
3HoneycombDesign 34C,4D,4E7.678.466.63423HV1426420
4HoneycombDesign 45C,5D,5E8.828.878.77460HV1470451
5HoneycombDesign 56C.6D,6E11.9212.8110.41455HV1461450

Response variables, surface roughness, and micro-Vickers hardness for the gyroid micro-lattice structure

Non-stress relived (as printed)
Surface roughness (Ra)Micro-Vickers hardness (HV)
S. No.LatticeDesignNon-Stress RelievedAverage (Ra)MaxMinAverageMaxMin
1GyroidDesign 11A10.512.868.11215HV1220211
Stress relieved
S. No.LatticeDesignStress relievedAverage (Ra)MaxMinAverageMaxMin
1GyroidDesign 11B11.8513.4610.83226HV1229222
Heat treated (final specimens)
S. No.LatticeDesignHeat treatedAverage (Ra)MaxMinAverageMaxMin
1GyroidDesign 11C,1D,1E3.563.743.37418HV1425411

Particle size distribution – sieve analysis

Particle size (μm)Sieve number% by mass
<45−32578.28
>45+32517.28
>53+2703.78
>63+2300.65

Corrosion rate for RHA, MHA, HNS, honeycomb, and gyroid micro-lattice structures

CaseSpecimenInitial weight (g)Final weight (g)Total weight loss (g)Corrosion rate (mm/ year)
Existing materialsRHA12.409312.40290.00642.847817577
MHA11.883711.87950.00421.868880285
HNS13.611813.60660.00522.313851781
Honeycomb lattice5D (ideal)77.693377.38030.3131.218227858
structure6D (non-ideal)80.630780.31280.31791.237299156
Gyroid1D40.043639.90270.14091.671511872

Flow rate, apparent, and tap density test results

TestTest methodResults
Flow rateASTM B21318s/50g
Apparent densityASTM B2123.98g/cm3
Tap densityASTM B5274.65g/cm3

Compressive residual stress for RHA, MHA, HNS, honeycomb and gyroid micro-lattice structures

MaterialCompressive residual stress values (MPa)
Existing Materials
RHA306.627
MHA348.454
HNS432.367
Micro-metallic lattice structures
Honeycomb581.907
Gyroid483.679

Corrosion resistance (in %) of micro-metallic lattice structures: honeycomb and gyroid vs_ RHA, MHA, and HNS

Before compression
Comparison of corrosion ratePercentage differenceComparison of corrosion ratePercentage difference
Honeycomb vs. RHA57.23%Gyroid vs. RHA41.31%
Honeycomb vs. MHA34.83%Gyroid vs. MHA10.6%
Honeycomb vs. HNS47.36 %Gyroid vs. HNS27.75%
After compression tests
Honeycomb vs. RHA37.61%Gyroid vs. RHA17.88%
Honeycomb vs. MHA4.92%Gyroid vs. MHA25.16%
Honeycomb vs. HNS23.21%Gyroid vs. HNS1.08%
Micro-metallic lattice structures
Honeycomb vs. gyroid (before compression) 27.11%
Honeycomb vs. gyroid (after compression) 24.03%

Micro-lattice structure design variations

GyroidDesign 1
Dimensions (L × W × H) (mm) 24 × 20 × 30
HoneycombDesign 1Design 2Design 3Design 4Design 5
Dimensions (L × W × H) (mm)24 × 20 × 30
Wall thickness (mm)22222
Detail size (mm)11111
Hole diameter (mm)1.41.210.80.5
Infill thickness (mm)1.41.210.80.5

Corrosion rate for honeycomb and gyroid micro-lattice structures after compression test

CaseSpecimenInitial weight (g)Final weight (g)Total weight loss (g)Corrosion rate (mm/year)
Honeycomb lattice5C (ideal)82.12981.67250.45651.776744463
structure6C (non-ideal)78.425277.96830.45691.778301304
Gyroid1C32.146531.94940.19712.338218523

Compressive residual stress comparison of micro metallic lattice structures honeycomb and gyroid vs_ RHA, MHA, and HNS

Comparison of residual stress values% Increase in residual stressComparison of residual stress values% Increase in residual stress
Honeycomb vs. RHA47.30%Gyroid vs. RHA36.6%
Honeycomb vs. MHA40.12%Gyroid vs. MHA27.96%
Honeycomb vs. HNS25.70%Gyroid vs. HNS10.61%
Micro-metallic lattice structures
Honeycomb vs. Gyroid16.88%

TOPSIS analysis for honeycomb micro-lattice structure for LPBF-generated specimens

Non-stress-relieved condition
Normalized residual matrixWeighted residual matrixDistance to ideal
Coupon no.NRaNVHNWRaWVHNSi+Si-CiRank
2A0.3690.4190.1850.2090.0390.0070.1544
3A0.3250.4210.1630.2100.0170.0290.6332
4A0.3650.4400.1830.2200.0370.0100.2043
5A0.2910.4080.1460.2040.0000.0460.9941
6A0.3820.3710.1910.1860.0470.0010.0025
Stress-relieved condition
Normalized residual matrixWeighted residual matrixDistance to ideal
Coupon no.NRaNVHNWRaWVHNSi+Si-CiRank
2B0.4770.4460.2390.2230.0380.0940.7133
3B0.4840.4090.2420.2050.0420.0900.6824
4B0.4500.3690.2250.1850.0260.1060.8032
5B0.4010.4250.2010.2120.0000.1310.9991
6B0.6620.4210.3310.2100.1310.0010.0055
Heat-treated condition
Normalized residual matrixWeighted residual matrixDistance to ideal
Coupon no.NRaNVHNWRaWVHNSi+Si-CiRank
2C,2D,2E0.3790.8800.1900.4400.0640.0070.0994
3C,3D.3E0.2540.8000.1270.4000.0030.0680.9542
4C,4D,4E0.2510.8090.1250.4050.0010.0700.9821
5C,5D,5E0.2890.8800.1440.4400.0190.0520.7363
6C.6D,6E0.3900.8710.1950.4350.0700.0010.0185

Physical properties of A286 steel

Property Value
Ultimate tensile strength620 MPa
Yield strength275 MPa
Elongation at break40%
Modulus of elasticity201 GPa
Poisson’s ratio0.3
Shear modulus77 GPa
Reduction of area20%
Chemical composition (% weight factor) of A286 steel
ElementCMnSiPSNiCrMoVAlTiCuFe
Weight (%)0.0340.1260.2360.0120.00625.6215.401.3310.1960.2092.0540.014Bal.
DOI: https://doi.org/10.2478/msp-2023-0023 | Journal eISSN: 2083-134X | Journal ISSN: 2083-1331
Language: English
Page range: 383 - 400
Submitted on: Aug 4, 2023
Accepted on: Sep 13, 2023
Published on: Nov 29, 2023
Published by: Wroclaw University of Science and Technology
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2023 Ameer Malik Shaik, Bobbili Veera Siva Reddy, C. Chandrasekhara Sastry, J. Krishnaiah, B. Ramakrishna, published by Wroclaw University of Science and Technology
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.