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Frontiers of Mechanical Engineering

ISSN 2095-0233

ISSN 2095-0241(Online)

CN 11-5984/TH

Postal Subscription Code 80-975

2018 Impact Factor: 0.989

Front. Mech. Eng.    2023, Vol. 18 Issue (2) : 21    https://doi.org/10.1007/s11465-022-0737-8
RESEARCH ARTICLE
Build orientation determination of multi-feature mechanical parts in selective laser melting via multi-objective decision making
Hongsheng SHENG3, Jinghua XU1,2,3, Shuyou ZHANG1,2,3(), Jianrong TAN1,2,3, Kang WANG3
1. State Key Laboratory of Fluid Power and Mechatronic Systems, Hangzhou 310027, China
2. Key Laboratory of Advanced Manufacturing Technology of Zhejiang Province, Hangzhou 310027, China
3. Engineering Research Center for Design Engineering and Digital Twin of Zhejiang Province, Zhejiang University, Hangzhou 310027, China
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Abstract

Selective laser melting (SLM) is a unique additive manufacturing (AM) category that can be used to manufacture mechanical parts. It has been widely used in aerospace and automotive using metal or alloy powder. The build orientation is crucial in AM because it affects the as-built part, including its part accuracy, surface roughness, support structure, and build time and cost. A mechanical part is usually composed of multiple surface features. The surface features carry the production and design knowledge, which can be utilized in SLM fabrication. This study proposes a method to determine the build orientation of multi-feature mechanical parts (MFMPs) in SLM. First, the surface features of an MFMP are recognized and grouped for formulating the particular optimization objectives. Second, the estimation models of involved optimization objectives are established, and a set of alternative build orientations (ABOs) is further obtained by many-objective optimization. Lastly, a multi-objective decision making method integrated by the technique for order of preference by similarity to the ideal solution and cosine similarity measure is presented to select an optimal build orientation from those ABOs. The weights of the feature groups and considered objectives are achieved by a fuzzy analytical hierarchy process. Two case studies are reported to validate the proposed method with numerical results, and the effectiveness comparison is presented. Physical manufacturing is conducted to prove the performance of the proposed method. The measured average sampling surface roughness of the most crucial feature of the bracket in the original orientation and the orientations obtained by the weighted sum model and the proposed method are 15.82, 10.84, and 10.62 μm, respectively. The numerical and physical validation results demonstrate that the proposed method is desirable to determine the build orientations of MFMPs with competitive results in SLM.

Keywords selective laser melting (SLM)      build orientation determination      multi-feature mechanical part (MFMP)      fuzzy analytical hierarchy process      multi-objective decision making (MODM)     
Corresponding Author(s): Shuyou ZHANG   
Just Accepted Date: 23 September 2022   Issue Date: 12 May 2023
 Cite this article:   
Hongsheng SHENG,Jinghua XU,Shuyou ZHANG, et al. Build orientation determination of multi-feature mechanical parts in selective laser melting via multi-objective decision making[J]. Front. Mech. Eng., 2023, 18(2): 21.
 URL:  
https://academic.hep.com.cn/fme/EN/10.1007/s11465-022-0737-8
https://academic.hep.com.cn/fme/EN/Y2023/V18/I2/21
Fig.1  Schematic of the proposed method. ABO: alternative build orientation, CSM: cosine similarity measure, FAHP: fuzzy analytical hierarchy process, FG: feature group, MADR: machining accuracy design requirement, MFMP: multi-feature mechanical part, MOO: many-objective optimization, OBO: optimal build orientation, SLM: selective laser melting, TOPSIS: technique for order of preference by similarity to ideal solution.
Fig.2  Illustration of the (a) features and (b) feature groups of a multi-feature mechanical part.
Fig.3  Illustration of the volumetric error in additive manufacturing (AM).
Fig.4  Illustration of support volume estimation: (a) manifold mesh model, (b) grids and ray origins, (c) required rays intersected with the overhang facets, and (d) support segments.
Fig.5  Illustration of the model slicing and the laser scanning path: (a) model slicing and (b) laser scanning path.
Linguistic variables TFN Scale of TFN
Equal importance 1 (1, 1, 1)
Little importance 1~ (1, 1, 3)
Intermediate value between 1 ~ and 3~ 2~ (1, 2, 4)
Moderate importance 3~ (1, 3, 5)
Intermediate value between 3 ~ and 5~ 4~ (2, 4, 6)
Essential importance 5~ (3, 5, 7)
Intermediate value between 5 ~ and 7~ 6~ (4, 6, 8)
Extreme importance 7~ (5, 7, 9)
Intermediate value between 7 ~ and 9~ 8~ (6, 8, 10)
Absolute importance 9~ (7, 9, 11)
Tab.1  TFNs for linguistic variables [51]
MFMP Length/mm Width/mm Height/mm Volume/mm3 Area/mm2
Connecting rod 53.58 26.92 25.99 10236.77 5360.21
Bracket 63.00 46.78 60.13 17644.09 9573.85
Tab.2  Geometric information of the two MFMPs
Parameter Value
lt 0.03 mm
Tr 20 s
vs 1250 mm/s
H dp 0.07 mm
H ds 1 mm
Hpp 3 mm
Mdensity 4.43 g/cm3
Mporosity 99.5%
Rwaste 0.1
Sdensity 0.3
Pmaterial 300 USD/kg
Penergy 0.18 USD/(kW·h)
Econsumption 162.13 kW·h/kg
Rindirect 53.35 USD/h
Aplatform 62500 mm2
Tab.3  SLM process parameters used for the objective estimation models
Fig.6  Manifold mesh models of the two multi-feature mechanical parts: (a) connecting rod and (b) bracket.
Fig.7  Features and feature groups of the connecting rod: (a) features and (b) feature groups.
Fig.8  Features and feature groups of the bracket: (a) features and (b) feature groups.
Fig.9  Pareto front of the four objectives for the connecting rod: (a) Vwve, R awasr, and Vs, (b) V wve, Rawasr, and Tb, (c) V wve, Vs, and T b, and (d) R awasr, V s, and T b.
Fig.10  Pareto front of the four objectives for the bracket: (a) Vwve, R awasr, and Vs, (b) V wve, Rawasr, and Cbuild, (c) Vwve, Vs, and C build, and (d) R awasr, V s, and C build.
Orientation Vwve /mm3 R awasr /μm Vs /mm3 Tb /s IV
Original 8.1129 10.8011 6041.0644 23547.7393 0.00970
OBO 7.8981 10.5099 2836.6676 35423.6799 0.01137
Tab.4  Comparison of the original orientation and OBO for the connecting rod
Orientation Vwve /mm3 R awasr /μm Vs /mm3 Cbuild /USD IV
Original 9.6181 10.9872 39258.6953 82.1573 0.00414
OBO 9.2628 10.5730 1292.4769 64.5985 0.01297
Tab.5  Comparison of the original orientation and OBO for the bracket
Fig.11  Optimal build orientations for the connecting rod and bracket: (a) connecting rod and (b) bracket.
MFMP Orientation Support volume/mm3 Difference/%
Proposed method Netfabb
Connecting rod Original 6041.10 5828.10 3.650
OBO 2836.70 2787.60 1.760
Bracket Original 39258.70 37961.10 3.420
OBO 1292.50 1236.40 4.540
Tab.6  Comparison of support volume estimation
MFMP Orientation Build time/s Difference/%
Proposed method Netfabb
Connecting rod Original 23548 24016 −1.95
OBO 35424 35678 −0.71
Bracket Original 50905 53597 −5.02
OBO 45705 45809 −0.23
Tab.7  Comparison of build time estimation
Method Vwve /mm3 R awasr /μm Vs /mm3 Tb /s IV
WSM 8.2895 10.7758 4654.8951 24039.8217 0.01050
Proposed method 7.8981 10.5099 2836.6676 35423.6799 0.01137
Tab.8  Comparison of the OBOs obtained by different methods for the connecting rod
Method Vwve /mm3 R awasr /μm Vs /mm3 Cbuild /USD IV
WSM 6.6203 10.584 28077.8537 74.5537 0.00743
Proposed method 9.2628 10.573 1292.4769 64.5985 0.01470
Tab.9  Comparison of the OBOs obtained by different methods for the bracket
Fig.12  Virtual manufacturing with build time coloration in different orientations for the connecting rod: (a) original orientation; optimal build orientation obtained by (b) the weighted sum model and (c) the proposed method.
Fig.13  Surface roughness visualizations in different orientations for the connecting rod: (a) original orientation; optimal build orientation obtained by (b) the weighted sum model and (c) the proposed method.
Fig.14  Supports in different orientations for the connecting rod: (a) original orientation; optimal build orientation obtained by (b) the weighted sum model and (c) the proposed method.
Fig.15  Type of laser scanning pattern of the connecting rod in different part heights and orientations: (a) 35% and (b) 70% part height in original orientation; (c) 35% and (d) 70% part height in the optimal build orientation obtained by the weighted sum model; and (e) 35% and (f) 70% part height in the optimal build orientation obtained by the proposed method.
Fig.16  Virtual manufacturing with build time coloration in different orientations for the bracket: (a) original orientation; optimal build orientation obtained by (b) the weighted sum model and (c) the proposed method.
Fig.17  Surface roughness visualizations in different orientations for the bracket: (a) original orientation; optimal build orientation obtained by (b) the weighted sum model and (c) the proposed method.
Fig.18  Supports in different orientations for the bracket: (a) original orientation; optimal build orientation obtained by (b) the weighted sum model and (c) the proposed method.
Fig.19  Type of laser scanning pattern of the bracket in different heights and orientations: (a) 35% and (b) 70% part height in original orientation; (c) 35% and (d) 70% part height in the optimal build orientation obtained by the weighted sum model; and (e) 35% and (f) 70% part height in the optimal build orientation obtained by the proposed method.
Fig.20  Selective laser melting fabrications for the bracket in different orientations: (a) selective laser melting machine; (b) laser scanning process, (c) fabricated bracket with lattice support in original orientation; fabricated bracket after stripping lattice support in (d) original orientation, (e) the optimal build orientation obtained by the weighted sum model, and (f) the optimal build orientation obtained by the proposed method.
Fig.21  Surface roughness measurement system using a noncontact optical profiler.
Fig.22  Measured surface topographies of the sampling regions for the selective laser melting fabricated brackets in different orientations: (a) first and (b) second regions in original orientation; optimal build orientation obtained by (c) the weighted sum model and (d) the proposed method.
Abbreviations
ABO Alternative build orientation
AM Additive manufacturing
CSM Cosine similarity measure
FAHP Fuzzy analytical hierarchy process
FDM Fused deposition modeling
FG Feature group
GA Genetic algorithm
MADR Machining accuracy design requirement
MFMP Multi-feature mechanical part
MODM Multi-objective decision making
MOO Many-objective optimization
NSGA-II Non-dominated sorting genetic algorithm II
OBO Optimal build orientation
SLA Stereolithography
SLM Selective laser melting
SLS Selective laser sintering
STL Standard tessellation language
TFN Triangular fuzzy number
TOPSIS Technique for order of preference by similarity to ideal solution
WSM Weighted sum model
Variables
A~ Triangular fuzzy number
A+ Positive ideal solution
A Negative ideal solution
A g Area of the grid generated in the projection of the bounding box on the platform
Aif Area of the ith facet
Aplatform Area of the fabrication platform
Blength Length of the part’s bounding box along the x-axis
Bwidth Width of the part’s bounding box along the y-axis
Cbuild Build cost of an SLM part
Cenergy Energy cost for building an SLM part
Ci Relative closeness to the ideal solution of the ith alternative
Ci Normalized relative closeness to the ideal solution of the ith alternative
C i nd ir ec t Indirect build cost of an SLM part
C m at er ia l Material cost used for the part, support structure, and wasted material
d Ordinate of the highest intersection point D between μS1 and μS2
d( Si) Normalized weight of the ith object
d( Si) Weight of the ith object obtained by the FAHP
Di+ Distance of the ith alternative to the positive ideal solution
Di Distance of the ith alternative to the negative ideal solution
d Build direction vector
DM Decision matrix of an MODM problem
E c on su mp ti on Energy consumption rate
fi(θx,θy) Estimation model function of the ith objective
Fi ith facet
F w sm WSM evaluation value of one solution
gi ith object
Hi, j Height of the jth segment of the ith supported ray
Hdp Hatch distance for filling the part
Hds Hatch distance of the lattice support structure
H p Part’s height
H p p Height between the part and the platform
IV Integrated MODM evaluation value
I Vi Integrated MODM evaluation value of the ith alternative
k Number of convex fuzzy numbers
l Lower bound of a TFN
l e Edge length of the grid
lgij Lower bound of the TFN M gij
l t Layer thickness
l Si Lower bound of the TFN Si
m Most promising value of a TFN
mgij Most promising value of the TFN M gij
m Si Most promising value of the TFN Si
M d en si ty Density of the material
Mgij Extent analysis value of the jth factor to the ith object
Mi CSM value between the ith alternative and the positive ideal solution
Mi Normalized CSM value between the ith alternative and the positive ideal solution
M p or os it y Porosity of the material
Mn× q Fuzzy judgment matrix used in the FAHP
n Number of the objects
nf Number of facets of the manifold mesh model
nfg Number of the feature groups
nfn Number of the facets without supports
nfs Number of the facets with supports
ng Number of the grids
ngx Number of the grids along the x-axis
ngy Number of the grids along the y-axis
no Number of the considered objectives
nr Number of the rays intersected with the overhang facets
nif Unit normal vector of the ith facet
O Vi Value of the ith objective
OVimax Maximum value of the ith objective
OVimin Minimum value of the ith objective
P e ne rg y Energy price
P m at er ia l Material price
q Number of the factors of one object
Qifg Pairwise fuzzy comparison matrix of the feature groups of the ith part
Q o Pairwise fuzzy comparison matrix of the optimization objectives
ri, j Normalized value of the jth objective for the ith alternative
Rbp Build rate of the part
Rbs Build rate of the support
R i nd ir ec t Indirect cost rate
R w as te Material waste rate
R aasr Average surface roughness of an SLM part
R aasr,i Average surface roughness of the ith feature group
Rai f Surface roughness of the ith facet
Rai f s Surface roughness of the ith supported facet
R awasr Weighted average surface roughness of an SLM part
S d en si ty Volume fraction of the lattice support structure
Si Fuzzy synthetic extent concerning the ith object
T b Build time of an SLM part
T r Recoating time of each layer
u Upper bound of a TFN
ugij Upper bound of the TFN M gij
u Si Upper bound of the TFN Si
vi, j Weighted normalized value of the jth objective for the ith alternative
vj+ Positive ideal weighted normalized value of the jth objective among all alternatives
vj Negative ideal weighted normalized value of the jth objective among all alternatives
v s Laser scanning speed
Vig Support volume of the ith grid
V p Part volume
V s Support volume of an SLM part
Vwve Weighted volumetric error of an SLM part
VE Volumetric error of an AM part
VEi f g Volumetric error of the ith feature group
V( S2? S1) Degree of possibility of a TFN S2 greater than a TFN S1
V( S? S1,S2,...,Sk) Degree of possibility for a convex fuzzy number to be greater than k convex fuzzy numbers
wifg Weight of the ith feature group
wio Weight of the ith objective
W Normalized non-fuzzy weight vector
Wifg Weight vector of the feature groups of the ith part
W o Weight vector of the considered objectives
x Real value
xi, j Value of the jth objective for the ith ABO
αi Angle between the build direction and normal vector of the ith facet
θx Rotation angle of the part around x-axis
θy Rotation angle of the part around y-axis
ρ Coefficient to adjust the relative importance of the TOPSIS and CSM
σ Weight for the surface roughness calculation of a supported facet
μA~ (x) Membership function of the TFN A~
μSi (x) Membership function of the TFN Si
  
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