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Frontiers of Mechanical Engineering

ISSN 2095-0233

ISSN 2095-0241(Online)

CN 11-5984/TH

邮发代号 80-975

2019 Impact Factor: 2.448

Frontiers of Mechanical Engineering  2023, Vol. 18 Issue (2): 29   https://doi.org/10.1007/s11465-022-0745-8
  本期目录
Development of lunar regolith-based composite for in-situ 3D printing via high-pressure extrusion system
Hua ZHAO1, Jihong ZHU1,2(), Shangqin YUAN1,3(), Shaoying LI1, Weihong ZHANG1
1. State IJR Center of Aerospace Design and Additive Manufacturing, School of Mechanical Engineering, Northwestern Polytechnical University, Xi’an 710072, China
2. Key Laboratory of Metal High Performance Additive Manufacturing and Innovative Design, MIIT China, Northwestern Polytechnical University, Xi’an 710072, China
3. Unmanned System Research Institute, Northwestern Polytechnical University, Xi’an 710072, China
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Abstract

To fully utilize the in-situ resources on the moon to facilitate the establishment of a lunar habitat is significant to realize the long-term residence of mankind on the moon and the deep space exploration in the future. Thus, intensive research works have been conducted to develop types of 3D printing approach to adapt to the extreme environment and utilize the lunar regolith for in-situ construction. However, the in-situ 3D printing using raw lunar regolith consumes extremely high energy and time. In this work, we proposed a cost-effective melting extrusion system for lunar regolith-based composite printing, and engineering thermoplastic powders are employed as a bonding agent for lunar regolith composite. The high-performance nylon and lunar regolith are uniformly pre-mixed in powder form with different weight fractions. The high-pressure extrusion system is helpful to enhance the interface affinity of polymer binders with lunar regolith as well as maximize the loading ratio of in-situ resources of lunar regolith. Mechanical properties such as tensile strength, elastic modulus, and Poisson’s ratio of the printed specimens were evaluated systematically. Especially, the impact performance was emphasized to improve the resistance of the meteorite impact on the moon. The maximum tensile strength and impact toughness reach 36.2 MPa and 5.15 kJ/m2, respectively. High-pressure melt extrusion for lunar regolith composite can increase the effective loading fraction up to 80 wt.% and relatively easily adapt to extreme conditions for in-situ manufacturing.

Key wordsin-situ resource utilization    melt extrusion molding    lunar regolith-based composites    mechanical properties    additive manufacturing
收稿日期: 2022-06-08      出版日期: 2023-06-30
Corresponding Author(s): Jihong ZHU,Shangqin YUAN   
 引用本文:   
. [J]. Frontiers of Mechanical Engineering, 2023, 18(2): 29.
Hua ZHAO, Jihong ZHU, Shangqin YUAN, Shaoying LI, Weihong ZHANG. Development of lunar regolith-based composite for in-situ 3D printing via high-pressure extrusion system. Front. Mech. Eng., 2023, 18(2): 29.
 链接本文:  
https://academic.hep.com.cn/fme/CN/10.1007/s11465-022-0745-8
https://academic.hep.com.cn/fme/CN/Y2023/V18/I2/29
SampleWeight fraction/wt.%
SiO2TiO2Al2O3FeOMgOCaONa2OK2OOthers
Apollo 1448.101.7017.4010.409.4010.700.700.551.05
CE-542.205.0010.8022.506.4811.000.260.191.57
Basalt-1#54.481.3914.898.666.317.162.710.394.01
Basalt-2#45.904.8712.178.719.587.823.251.815.89
Basalt-3#50.020.9215.787.606.128.962.850.327.43
Tab.1  
Fig.1  
Fig.2  
Fig.3  
ParametersValues
Nozzle diameter1.0 mm
Layer height0.8 mm
Piston diameter18 mm
Printing temperature225, 230, 235 °C
Bed temperature70 °C
Printing speed7, 8, 9 mm/s
Extrusion speed0.02 mm/s
Number of contours2
Infill percentage100%
Infill patternRectilinear 45°/?45°
Tab.2  
Fig.4  
ParametersValues
Nozzle diameter1.0 mm
Layer height0.8 mm
Piston diameter18 mm
Printing temperature230 °C
Bed temperature70 °C
Printing speed7 mm/s
Extrusion speed0.02 mm/s
Number of contours2
Infill percentage100%
Infill pattern45°/?45°, 0°/90°
Tab.3  
Fig.5  
MaterialOnset melting temperature/°COffset melting temperature/°CMelting peak/°CEnthalpy of melting/(J·g?1)Onset recrystallization temperature/°COffset recrystallization temperature/°CRecrystallization peak/°CEnthalpy of recrystallization/(J·g?1)Glass window width/°C
PA12-Basalt40wt.%181.6190.8187.958.03152.1140.8147.2?31.1029.5
PA12-Basalt50wt.%181.6190.5187.944.54152.6141.3147.9?26.5829.0
PA12-Basalt60wt.%181.5190.3187.736.03153.1142.3148.7?21.8128.4
Tab.4  
Fig.6  
MaterialOnset decomposition temperature/°COffset decomposition temperature/°CDecomposition peak/°CMass loss/%
PA12-Basalt40wt.%375.5518.6439.849.1
PA12-Basalt50wt.%372.3513.2442.744.2
PA12-Basalt60wt.%371.3504.4440.525.5
Tab.5  
Fig.7  
Fig.8  
No.Weight fraction/wt.%Printing temperature/°CPrinting speed/(mm·s?1)σb/MPaE/MPa
140225736.1621674.18
250225723.0551634.31
360225719.5002443.41
440230722.5801382.84
550230721.7171702.24
660230720.5561602.23
740235725.4441531.78
850235723.0411763.04
960235720.0101803.54
1040225832.3921467.06
1150225821.3881682.22
1260225818.8181827.58
1340230821.5101322.97
1450230819.4281662.41
1560230817.1401594.13
1640235824.7521334.63
1750235821.2851455.93
1860235817.3891748.09
1940225930.6931152.13
2050225918.2151515.21
2160225915.5811443.74
2240230920.8981328.17
2350230918.5011460.74
2460230915.4241574.20
2540235922.9591271.04
2650235918.3191343.28
2760235919.4691763.33
Tab.6  
Fig.9  
Fig.10  
Fig.11  
Fig.12  
Fig.13  
Fig.14  
Fig.15  
ParameterValue
Basalt weight fraction80 wt.%
Layer height4 mm
Nozzle diameter5 mm
Raster gap4 mm
Printing temperature235 °C
Bed temperature70 °C
Extrusion screw rotation speed8?10 r/min
Feeding screw rotation speed12.5?15 r/min
Robot motion speed8?9 mm/s
Infill percentage100%
Tab.7  
Abbreviations
AMAdditive manufacturing
DSCDifferential scanning calorimetry
ISRUIn-situ resource utilization
MAMMotor-assisted microsyringe
SEMScanning electron microscope
TGAThermogravimetric analysis
Variables
akImpact toughness
AkImpact energy
EYoung’s modulus
TmMelting peak temperature
TrRecrystallization peak temperature
σbTensile strength
  
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